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Aerospool WT9 Dynamic LSA Club Maintenance Manual

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Table of Contents

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AIRCRAFT MAINTENANCE
MANUAL
Document Number: AS-AMM-10-000
Date of Issue: 10. 10. 2018
Aircraft Models: WT9 Dynamic LSA / Club
WT9 Dynamic LSA / Speed
THE AIRPLANE HAS TO BE MAINTAINED IN COMPLIANCE WITH INFORMATION AND
LIMITATIONS CONTAINED HEREIN.

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Summary of Contents for Aerospool WT9 Dynamic LSA Club

  • Page 1 AIRCRAFT MAINTENANCE MANUAL Document Number: AS-AMM-10-000 Date of Issue: 10. 10. 2018 Aircraft Models: WT9 Dynamic LSA / Club WT9 Dynamic LSA / Speed THE AIRPLANE HAS TO BE MAINTAINED IN COMPLIANCE WITH INFORMATION AND LIMITATIONS CONTAINED HEREIN.
  • Page 2 This page is left blank intentionally...

  • Page 3: Table Of Contents

    INTRODUCTION 01 INTRODUCTION CONTENTS Section Description Page 01-00 GENERAL ................. 3 01-10 AIRCRAFT CLASSIFICATION ......... 5 01-20 MANUFACTURERS ............7 AIRCRAFT MANUFACTURER ..........7 ENGINE MANUFACTURER ............7 PROPELLER MANUFACTURER ..........7 EVRA PerformanceLine 175/xxx/805.5 ......7 SR 2000D, SR 3000/3, SR 2000DN, SR 3000/3N, SR 3000/2, SR 3000/2N ............
  • Page 4 INTRODUCTION 01-60 REVISIONS ..............49 MANUAL REVISIONS ............. 49 Procedure: ..............49 MARKED OF REVISIONS ............49 LOG OF TEMPORARY REVISIONS ........50 LOG OF REVISIONS .............. 52 Chapter 01 CONTENTS Page 01-2 Effectivity: ALL 04. 05. 2021...

  • Page 5: General

    INTRODUCTION 01-00 GENERAL The purpose of this manual is to provide guidance to owners, mechanics, airports, regulatory officials, and aircraft and component manufacturers who may accomplish maintenance, repairs, and alterations on a light sport aircraft. In addition, this practice covers format content maintenance...
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  • Page 7: Aircraft Classification

    INTRODUCTION 01-10 AIRCRAFT CLASSIFICATION The aircraft WT9 Dynamic LSA is a single engine, two seats (arranged side by side), cantilever low wing aircraft with a cruciform tail. The primary structures consist of glass and carbon composite. The aircraft is equipped with tricycle undercarriage (fixed or retractable) with steerable nose wheel.
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  • Page 9: Manufacturers

    INTRODUCTION 01-20 MANUFACTURERS AIRCRAFT MANUFACTURER Aerospool, spol. s r. o. Letisková 10 971 03 Prievidza Slovak republic E-mail: dynamic@aerospool.sk Web: www.aerospool.sk ENGINE MANUFACTURER BRP-Powertrain GmbH&Co. KG. Rotaxstrasse 1 A-4623 Gunskirchen Austria Web: www.flyrotax.com PROPELLER MANUFACTURER EVRA PerformanceLine 175/xxx/805.5 SARL Production EVRA 4 Avenue de la Forêt d'Halatte...
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  • Page 11: Manual Description

    This Maintenance Manual does not reflect part numbers and cannot be used for ordering replacement parts. For material purchase contact the airplane manufacturer’s local representative or contact airplane manufacturer directly at spareparts@aerospool.sk. ARRANGEMENT OF CHAPTERS Chapters in this manual are arranged and divided in accordance with GAMA No. 2 Specification.

  • Page 12: Numbering Of Pages, Figures And Tables

    INTRODUCTION Numbering of pages, figures and tables Numbering of pages: Example: Page 27 – 11 Page No. Chapter No. Numbering of figures: Example: Fig. 27 – 1 Figure No. Chapter No. Numbering of tables: Example: Tab. 27 – 1 Table No. Chapter No.

  • Page 13: Warnings, Cautions, And Notes

    The manufacturer points out that all maintenance work must be carried out only by qualified personnel to maintain the aircraft. Aerospool company reserves the right at any time to terminate or change specifications, designs, features or versions without obligation to notify.
  • Page 14 INTRODUCTION When performing maintenance, the safety must be always considered. Always use proper personal protective equipment, at least but not limited to: • Wear protective gloves when handling with chemicals and sealants. Do not use protective hand creams as they can contaminate the sealants and surfaces.

  • Page 15: Abbreviations

    INTRODUCTION ABBREVIATIONS ADAHRS Air Data, Attitude and Heading Reference System ADS-B Automatic Dependent Surveillance – broadcast Angle of Attack Aircraft Maintenance Manual As Required Air Traffic Control COMM Communication Cylinder Head Temperature Cable Retractor Winch with Guillotine CS-LSA Certification Specifications for Light Sport Aeroplanes EASA European Aviation Safety Agency EFIS...
  • Page 16 INTRODUCTION Traffic Information System Value Added Tax Visual Flight Rules VHF Omnidirectional range XPDR Transponder Chapter 01-30 MANUAL DESCRIPTION Page 01-14 Effectivity: ALL 14. 05. 2020...

  • Page 17: Manual Improvement Request Form

    INTRODUCTION MANUAL IMPROVEMENT REQUEST FORM Aerospool spol. s r. o. Aerospool reference No.: Letisková 10 MANUAL IMPROVEMENT 973 01 Prievidza REQUEST Date: Slovak republic airworthiness@aerospool.sk www.aerospool.sk Dear owner / operator / maintainer: In the case of suggestions for improvement to the content of the manual, or if errors or omissions were found, please submit the proposed changes by means of MANUAL IMPROVEMENT REQUEST form.

  • Page 18: Safety Of Flight And Service Difficulty Report Form

    INTRODUCTION SAFETY OF FLIGHT AND SERVICE DIFFICULTY REPORT FORM Aerospool reference No.: Aerospool spol. s r. o. Letisková 10 SAFETY OF FLIGHT AND 973 01 Prievidza SERVICE DIFFICULTY REPORT Date: Slovak republic airworthiness@aerospool.sk www.aerospool.sk Dear owner / operator / maintainer: For continued increasing reliability of aircrafts, we would like to ask you for your assistance in the case of safety of flight or service difficulty.

  • Page 19: List Of Chapters

    INTRODUCTION 01-40 LIST OF CHAPTERS INTRODUCTION 01 INTRODUCTION AIRCRAFT 04 AIRWORTHINESS LIMITATIONS 05 PERIODIC INSPECTIONS 06 DIMENSIONS AND AREAS 07 LIFTING AND SHORING 08 LEVELING AND WEIGHING 09 TOWING AND TAXIING 10 PARKING, MOORING 11 PLACARDS AND MARKINGS 12 SERVICING AIRFRAME SYSTEMS 20 STANDARD PRACTICES - AIRFRAME 21 AIR CONDITIONING...
  • Page 20 INTRODUCTION PROPELLER 61 PROPELLER POWER PLANT 71 POWER PLANT - GENERAL 73 ENGINE - FUEL SYSTEMS 74 IGNITION 75 ENGINE COOLING 76 ENGINE CONTROLS 77 ENGINE INDICATING 78 EXHAUST 79 OIL SUPPLEMENTS 95 OPTIONAL EQUIPMENT Chapter 01-40 LIST OF CHAPTERS Page 01-18 Effectivity: ALL 14.

  • Page 21: List Of Effective

    INTRODUCTION 01-50 LIST OF EFFECTIVE PAGES Page No. Date of Issue Effectivity Title 10. 10. 2018 01-1 04. 05. 2021 01-2 04. 05. 2021 01-3 04. 05. 2021 01-4 04. 05. 2021 01-5 04. 05. 2021 01-6 04. 05. 2021 01-7 04.
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  • Page 51: Revisions

    INTRODUCTION 01-60 REVISIONS MANUAL REVISIONS CAUTION MANUAL OWNER RESPONSIBLE KEEPING UP-TO-DATE. Procedure: All Revisions / Temporary revisions of this Manual are made as follows: The aircraft manufacturer will send the Revision / Temporary revision with new manual pages: Free of charge to the Authority and to all foreign aviation authorities on request.

  • Page 52: Log Of Temporary Revisions

    INTRODUCTION LOG OF TEMPORARY REVISIONS Temp. Incorporated Affected Pages Description / Effectivity Date of Issue Rev. No. by / Date Chapter 01-60 REVISIONS Page 01-50 Effectivity: ALL 14. 05. 2020...
  • Page 53 INTRODUCTION Temp. Incorporated Affected Pages Description / Effectivity Date of Issue Rev. No. by / Date REVISIONS Chapter 01-60 14. 05. 2020 Effectivity: ALL Page 01-51...

  • Page 54: Log Of Revisions

    Description / Effectivity Date of Issue by / Date 01-1, 01-3, 01-5, 01-7, 01-13 Added propellers SR 2000D, 27. 08. 2019 Aerospool to 01-16, 01-19 to 01-50, SR 2000DN, SR 3000/3, spol. s r. o. 05-13, 05-17 to 05-30, 05-32, SR 3000/3N.
  • Page 55 Date of Issue by / Date 01-1 to 01-8, 01-19 to 01-48, Supplemented information for 04. 05. 2021 Aerospool 01-52 to 01-54, 05-1 to Rotax 914 engine and its spol. s r. o. 05-38, 06-1 to 06-22, 10-7, systems. Supplemented...
  • Page 56 INTRODUCTION This page is left blank intentional Chapter 01-60 REVISIONS Page 01-54 Effectivity: ALL 04. 05. 2021...
  • Page 57 AIRWORTHINESS LIMITATIONS 04 AIRWORTHINESS LIMITATIONS CONTENTS Chapter Description Page 04-00 AIRWORTHINESS LIMITATIONS ........3 GENERAL .................. 3 Maintenance limitations ............. 3 Replacement limitations ............ 3 Structural limitations ............3 DESCRIPTION ................4 Maintenance limitations ............. 4 Replacement limitations ............ 4 Structural limitations ............
  • Page 58 AIRWORTHINESS LIMITATIONS This page is left blank intentionally Chapter 04 CONTENTS Page 04-2 Effectivity: ALL 14. 05. 2020...

  • Page 59: Airworthiness Limitations

    AIRWORTHINESS LIMITATIONS 04-00 AIRWORTHINESS LIMITATIONS GENERAL The Airworthiness Limitations chapter is approved by European Aviation Safety Agency (EASA) in accordance with the applicable certification procedures and the type certification basis. It specifies the airworthiness limitations required by CS-LSA. This chapter specifies the maximum intervals for replacement and/or maintenance requirements of aircraft components, systems and structures determined by life limits and/or requiring monitoring during scheduled maintenance.

  • Page 60: Description

    AIRWORTHINESS LIMITATIONS DESCRIPTION Maintenance limitations The scheduled maintenance requirements listed below are also included in Chapter 05-20 SCHEDULED MAINTENANCE CHECKS. The following criteria must be adhered to: Emergency Parachute System (EPS): Components of EPS (parachute, rocket, actuator and straps) must be inspected and repacked every 6 year by EPS manufacturer within the service life.
  • Page 61 PERIODIC INSPECTIONS 05 PERIODIC INSPECTIONS CONTENTS Chapter Description Page 05-00 GENERAL ................. 3 1. INTRODUCTION ................3 2. SPECIAL CONDITIONS ..............3 3. DEFINITIONS ................3 05-10 TIME LIMITS ..............7 1. INTRODUCTION ................7 2. INSPECTION INTERVALS ............7 3.
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  • Page 63: General

    PERIODIC INSPECTIONS 05-00 GENERAL INTRODUCTION This chapter includes the aircraft manufacturer's recommended time limits, mainte- nance checks and inspections (both scheduled and unscheduled). Recommended intervals for items inspection are based on normal usage under aver- age environmental conditions. SPECIAL CONDITIONS All inspection intervals for scheduled maintenance checks, replacement and overhaul schedule and special inspections schedule noted in this manual are based on average usage and average environmental conditions.
  • Page 64 PERIODIC INSPECTIONS United States Federal Aviation Administration. FLIGHT TIME / FLIGHT HOURS The time in service from the moment the aircraft leaves the ground until it touches the ground at the end of the flight. FUNCTIONAL INSPECTION It is a quantitative inspection to determine if one or more functions of an item performs within specified limits.
  • Page 65 PERIODIC INSPECTIONS MINOR REPAIR, ALTERATION, OR MAINTENANCE repair, alteration, maintenance which instructions provided for in the maintenance manual(s) supplied to the consumer of the product are consid- ered minor. ON CONDITION The necessary inspections and/or checks to determine that a malfunction or failure will not occur prior to the next scheduled inspection.
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  • Page 67: Time Limits

    PERIODIC INSPECTIONS 05-10 TIME LIMITS The inspections described herein constitute what the aircraft manufacturer considers necessary to ensure the continued airworthiness of WT9 Dynamic LSA aircraft. INTRODUCTION The inspection program is based on the number of flight hours, operating hours of engine and calendar time.

  • Page 68: Inspection Tolerances

    PERIODIC INSPECTIONS INSPECTION TOLERANCES The inspection intervals shall not deviate from the inspection time limits shown in table of inspection tolerances (see Tab. 05-1). The exceeding of scheduled inspection interval shall be used only to finish the flight that started before inspection interval or for a flight with the purpose to reach a place, where the inspection will be carried out.
  • Page 69 PERIODIC INSPECTIONS Fig. 05-1 Description and Application of Inspection Tolerances (example) TIME LIMITS Chapter 05-10 04. 05. 2021 Effectivity: ALL Page 05-9...

  • Page 70: Service Bulletins

    PERIODIC INSPECTIONS SERVICE BULLETINS The aircraft manufacturer issues service information for owners in the form of three classes of service bulletins. The service bulletins determine the time limit until the aircraft must comply with. Mandatory Service Bulletin (“Safety Related”) Mandatory Service Bulletin is issued in such cases: •...

  • Page 71: Replacement Schedule

    PERIODIC INSPECTIONS 05-11 REPLACEMENT SCHEDULE The first replacement must be performed no later than the recommended period. The condition of the item at the end of the first period can be used as a criterion for determining subsequent periods. Items NOT listed in Tab. 05-2 are to be replaced "ON CONDITION". If "ON CONDITIONS" items are worn, inoperative, inaccurate, and intermittent and are not repairable through normal maintenance practices, they must be replaced.
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  • Page 73: Overhaul Schedule

    PERIODIC INSPECTIONS 05-12 OVERHAUL SCHEDULE The first overhaul must be performed no later than the recommended period. The condition of the item at the end of the first period can be used as a criterion for determining subsequent periods. Items NOT listed in Tab. 05-3 are to be overhauled "ON CONDITION". If "ON CONDITIONS" items are worn, inoperative, inaccurate, and intermittent and are not repairable through nor- mal maintenance practices, they must be overhauled or replaced.
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  • Page 75: Scheduled Maintenance Checks

    PERIODIC INSPECTIONS 05-20 SCHEDULED MAINTENANCE CHECKS CAUTION THE RECOMMENDED PERIODS DO NOT CONSTITUTE A GUARANTEE THE ITEM WILL REACH THE PERIOD WITHOUT MALFUNCTION. RESPONSIBILITY OF OWNER The owner is responsible for maintaining the aircraft in an airworthy condition, including compliance with all applicable Airworthiness Directives. The owner must ensure that qualified personnel do the maintenance.

  • Page 76: Inspection Guidelines

    PERIODIC INSPECTIONS INSPECTION GUIDELINES The List of Inspection Requirements is given in Tab. 05-4. Detailed inspection procedures of systems and components in the aircraft will be found in various chapters of this Aircraft Maintenance Manual. INSPECTION OF ITEMS – GENERAL ln the text of individual operations, where the check for condition is required, dominant activities carried out at checking for condition can be mentioned in brackets, e.

  • Page 77: Scheduled Inspection Program

    PERIODIC INSPECTIONS SCHEDULED INSPECTION PROGRAM AC MODEL: ☐ WT9 Dynamic LSA / Club ☐ WT9 Dynamic LSA / Speed SERIAL NUMBER: REGISTRATION NUMBER: LAST INSPECTION DATE: LAST INSPECTION HOURS: TOTAL F.H.: CYCLES: DATE IN: DATE OUT: INSPECTION INTERVAL (inappropriate scrape): First 25 hr.
  • Page 78 PERIODIC INSPECTIONS Interval (flight hours) Engine Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Engine Cowlings and Firewall Remove engine cowlings. Clean and perform visual inspection for cracks, damages, loose or missing fasteners. Inspect the condition of oil inspection door. Visual inspection of engine cowlings fireproofing for condition and attachment (only bottom cowling).
  • Page 79 PERIODIC INSPECTIONS Interval (flight hours) Engine Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special 5.7 Check the electric fuel pump/pumps for conditions and attachment. 5.8 Install the fuel filter covers. Engine Controls Check the throttle controller for condition, attachment, connection to carburettor and function.
  • Page 80 PERIODIC INSPECTIONS Interval (flight hours) Engine Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Induction System Visual inspection of carburettors, drip trays, and control cables for condition, attachment and security. Visual inspection of airbox and airbox-carburettors hoses and drain hoses for condition, attachment and security.
  • Page 81 PERIODIC INSPECTIONS Interval (flight hours) Engine Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special 12. Engine Wiring 12.1 Visual inspection of wires for damage and security. Visual inspection of sensors for condition, attachment and 12.2 security. 13. Lubrication in Engine Compartment 13.1 Lubricate according to lubrication chart (Chapter 12-20).
  • Page 82 PERIODIC INSPECTIONS Interval (flight hours) Propeller Group Initials: 100 hr./ First Annual/ 25 hr. Special Propeller PerformanceLine 175/xxx/805.5 Remove the spinner. Visual inspection of spinner for condition, cracks and damage. Visual inspection of propeller blades, especially on leading edges for condition, nicks, bends, cracks and damage. Visual inspection of propeller hub for condition, cracks, attachment and security.
  • Page 83 PERIODIC INSPECTIONS Interval (flight hours) Propeller Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special 3.7 Install spinner. 150 hr. The points 12. and 13. of section Operational and Functional Note 150 hr. - Check must be performed to complete the propeller inspection. Interval (flight hours) Landing Gear and Brake System Group...
  • Page 84 PERIODIC INSPECTIONS Interval (flight hours) Landing Gear and Brake System Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Visual inspection of fuselage structure at the entry points of landing gear legs for delaminations. Visual inspection of main gear legs for attachment and securing. Inspect for proper nut torque.
  • Page 85 PERIODIC INSPECTIONS Interval (flight hours) Landing Gear and Brake System Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Inspect the damping elements for conditions, wear, cracks, defor- mation, damages and security. Inspect the drag struts for condition, deformations, geometry, plays and security.
  • Page 86 PERIODIC INSPECTIONS Interval (flight hours) Wing Group Initials: 100 hr./ First Annual/ 25 hr. Special Wing Visual inspection wings condition, delaminations, deterioration, distortion, cracks, paint condition and other damages. Visual inspection of stall strips and ACI stall warner for condition and attachment.
  • Page 87 PERIODIC INSPECTIONS Interval (flight hours) Fuselage Group Initials: 100 hr./ First Annual/ 25 hr. Special Visual inspection of fuselage for condition, delaminations, deterio- ration, distortion, cracks, paint condition and other damages. Pay special attention to the bottom of wing central section and walkway areas.
  • Page 88 PERIODIC INSPECTIONS Interval (flight hours) Empennage Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Visual inspection of elevator hinges for condition, wear, play and freedom of movement. 1.4 Lubricate according to lubrication chart (Chapter 12-20). Visual inspection of elevator sealing tapes for conditions attachment.
  • Page 89 PERIODIC INSPECTIONS Interval (flight hours) Control Systems Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Rudder Control System, Nose Wheel Steering Visual inspection of rudder pedals for excessive play, smooth op- eration and security. Inspect the control cables for condition, attachment, wear, and se- curity.
  • Page 90 PERIODIC INSPECTIONS Interval (flight hours) Wing Flap Control System Group (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Model WT9 Dynamic LSA / Speed only: Inspect the flaps position sensor for condition, attachment and security. Lubricate according to lubrication chart (Chapter 12-20). Install the pedestal panel.
  • Page 91 PERIODIC INSPECTIONS Interval (flight hours) Cockpit Group Initials: 100 hr./ First Annual/ 25 hr. Special Visual inspection of safety belts for condition, attachment, wear and locking. Visual inspection of upholstery for condition and wear. Visual inspection of seats for delamination, cracks and damages. Remove the instrument panel cover.
  • Page 92 PERIODIC INSPECTIONS Interval (flight hours) Towing Equipment Initials: 100 hr./ First Annual/ 25 hr. Special Tow release mechanism Visual inspection of tow release for condition, attachment and security. Inspect the tow release control handle and levers for condition, attachment, wear and security. Inspect the tow release control cable and joints for condition, attachment, wear and security.
  • Page 93 PERIODIC INSPECTIONS Interval (flight hours) Operational and Functional Check (Continued) Initials: 100 hr./ First Annual/ 25 hr. Special Check the vertical speed indicators to indicate zero. Check the radio communication capability. Check the landing lights (if installed) and ACL/NAV/POS lights (if installed) operation.
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  • Page 95: Unscheduled Maintenance Checks

    PERIODIC INSPECTIONS 05-50 UNSCHEDULED MAINTENANCE CHECKS GENERAL During operation, the aircraft may be subjected to any incidents that could damage the aircraft and therefore unscheduled maintenance checks are required. The following procedures may be in the details amended or supplemented according to the extent of damage.

  • Page 96: Hard Landing Checks

    PERIODIC INSPECTIONS HARD LANDING CHECKS AC MODEL: ☐ WT9 Dynamic LSA / Club ☐ WT9 Dynamic LSA / Speed SERIAL NUMBER: REGISTRATION NUMBER: LAST INSPECTION DATE: LAST INSPECTION HOURS: TOTAL F.H.: CYCLES: DATE IN: DATE OUT: INSPECTION INTERVAL (inappropriate scrape): UNSCHEDULED Inspection Hard Landing...
  • Page 97 PERIODIC INSPECTIONS Inspection Hard Landing (Continued) Initials: result Main Landing Gear – Model WT9 Dynamic LSA / Club Remove the main wheel fairings and main leg fairings. Visual in- spection for damage. Visual inspection of main legs for damage, deformation and cracks.
  • Page 98 PERIODIC INSPECTIONS Inspection Hard Landing Initials: result Main Landing Gear – Model WT9 Dynamic LSA / Speed Visual inspection of main legs for damage, deformation and cracks. Check damage from damper body and main leg collision. Visual inspection of trailing links for damage, deformation and cracks.
  • Page 99 DIMENSIONS AND AREAS 06 DIMENSIONS AND AREAS CONTENTS Chapter Description Page 06-00 DIMENSIONS AND AREAS ..........3 DESCRIPTION ................3 THREE-VIEW DRAWINGS ............4 General................9 Wing .................. 9 Wing flaps ................9 Ailerons ................9 Vertical tail ................. 9 Horizontal tail ..............
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  • Page 101: Dimensions And Areas

    DIMENSIONS AND AREAS 06-00 DIMENSIONS AND AREAS DESCRIPTION This chapter shows three-view drawing of aircraft, describes dimensions, hatches and covers. In the hatches and covers section the legends to the above figures specify what components are accessible after opened / removed and how hatches / covers are attached.

  • Page 102: Three-View Drawings

    DIMENSIONS AND AREAS THREE-VIEW DRAWINGS Model 2005 Fig. 06-1 WT9 Dynamic LSA / Club (page 1 of 5) Chapter 06-00 DIMENSIONS AND AREAS Page 06-4 Effectivity: ALL 04. 05. 2021...
  • Page 103 DIMENSIONS AND AREAS Model 2005 – winch tow equipment Fig. 06-1 WT9 Dynamic LSA / Club (page 2 of 5) DIMENSIONS AND AREAS Chapter 06-00 04. 05. 2021 Effectivity: ALL Page 06-5...
  • Page 104 DIMENSIONS AND AREAS Model 2011 Fig. 06-1 WT9 Dynamic LSA / Club (page 3 of 5) Chapter 06-00 DIMENSIONS AND AREAS Page 06-6 Effectivity: ALL 04. 05. 2021...
  • Page 105 DIMENSIONS AND AREAS Model 2005 RG Fig. 06-1 WT9 Dynamic LSA / Speed (page 4 of 5) DIMENSIONS AND AREAS Chapter 06-00 04. 05. 2021 Effectivity: ALL Page 06-7...
  • Page 106 DIMENSIONS AND AREAS Model 2011 RG Fig. 06-1 WT9 Dynamic LSA / Speed (page 5 of 5) Chapter 06-00 DIMENSIONS AND AREAS Page 06-8 Effectivity: ALL 04. 05. 2021...

  • Page 107: General

    DIMENSIONS AND AREAS General Wing span (Overall) ........... 8.926 m ....29.28 ft Length (Overall) “Model 2005” ......6.410 m ....21.03 ft Length (Overall) “Model 2011” ......6.460 m ....21.19 ft Height (Maximum) ..........1.850 m ....6.07 ft Propeller diameter: EVRA PerformanceLine 175/xxx/805.5 .....
  • Page 108 DIMENSIONS AND AREAS Retractable landing gear Wheel track (main to main) ........2.240 m ....7.35 ft Wheel base (main to nose) ........1.440 m ....4.72 ft Main wheel tire size ........15x6.00 Nose wheel tire size ........13x5.00 Chapter 06-00 DIMENSIONS AND AREAS Page 06-10 Effectivity: ALL...

  • Page 109: Control Surfaces Deflections And Cable Tension

    DIMENSIONS AND AREAS CONTROL SURFACES DEFLECTIONS AND CABLE TENSION SETTINGS Aileron Aileron up deflection ....... 25° ±2° Aileron down deflection ......15° ±2° Elevator Elevator up deflection ......28° ±2° Elevator down deflection ......18° ±2° Rudder Rudder left deflection ......25° ±2° Rudder right deflection ......

  • Page 110: Hatches And Covers

    DIMENSIONS AND AREAS HATCHES AND COVERS External hatches and covers FG Model 2005 Fig. 06-2 External Hatches and Covers FG (page 1 of 3) Chapter 06-00 DIMENSIONS AND AREAS Page 06-12 Effectivity: ALL 04. 05. 2021...
  • Page 111 DIMENSIONS AND AREAS Model 2011 Fig. 06-2 External Hatches and Covers FG (page 2 of 3) DIMENSIONS AND AREAS Chapter 06-00 04. 05. 2021 Effectivity: ALL Page 06-13...
  • Page 112 DIMENSIONS AND AREAS Propeller spinner (Model 2005) – screwed on Propeller spinner (Model 2011) – screwed on Upper engine cowling (Model 2005) – quick lock fasteners Upper engine cowling (Model 2011) – quick lock fasteners Lower engine cowling (Model 2005) –quick lock fasteners to upper engine cowling and screwed on fuselage Lower engine cowling (Model 2011) –quick lock fasteners to upper engine cowling and screwed on fuselage...

  • Page 113: External Hatches And Covers Rg

    DIMENSIONS AND AREAS External hatches and covers RG Model 2005, Rotax 912 Fig. 06-3 External Hatches and Covers RG (page 1 of 4) DIMENSIONS AND AREAS Chapter 06-00 04. 05. 2021 Effectivity: ALL Page 06-15...
  • Page 114 DIMENSIONS AND AREAS Model 2011, Rotax 912 Fig. 06-3 External Hatches and Covers RG (page 2 of 4) Chapter 06-00 DIMENSIONS AND AREAS Page 06-16 Effectivity: ALL 04. 05. 2021...
  • Page 115 DIMENSIONS AND AREAS Model 2011, Rotax 914 Fig. 06-3 External Hatches and Covers RG (page 3 of 4) DIMENSIONS AND AREAS Chapter 06-00 04. 05. 2021 Effectivity: ALL Page 06-17...
  • Page 116 DIMENSIONS AND AREAS Propeller spinner (Model 2005) – screwed on Propeller spinner (Model 2011) – screwed on Upper engine cowling RG, R912 (Model 2005) – quick lock fasteners Upper engine cowling RG, R912 (Model 2011) – quick lock fasteners Upper engine cowling RG, R914 (Model 2011) – quick lock fasteners Lower engine cowling RG, R912 (Model 2005) –quick lock fasteners to upper engine cowling and screwed on fuselage Lower engine cowling RG, R912 (Model 2011) –quick lock fasteners...

  • Page 117: Internal Hatches And Covers

    DIMENSIONS AND AREAS Internal hatches and covers Fig. 06-4 Internal Hatches and Covers (page 1 of 3) DIMENSIONS AND AREAS Chapter 06-00 04. 05. 2021 Effectivity: ALL Page 06-19...
  • Page 118 DIMENSIONS AND AREAS Fig. 06-4 Internal Hatches and Covers (page 2 of 3) Chapter 06-00 DIMENSIONS AND AREAS Page 06-20 Effectivity: ALL 04. 05. 2021...
  • Page 119 DIMENSIONS AND AREAS Fuel filter cover RH (access to RH fuel filter) – snapped on Fuel filter cover LH (access to LH fuel filter) – snapped on Inner fuel tank rib cover RH (access to RH fuel level sensor) – Velcro tape Inner fuel tank rib cover LH (access to LH fuel level sensor) –...
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  • Page 121 LIFTING AND SHORING 07 LIFTING AND SHORING CONTENTS Chapter Description Page 07-00 GENERAL ................. 3 INTRODUCTION ............... 3 07-10 JACKING ................5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 5 Jacking ................5 07-20 SHORING ................7 DESCRIPTION ................7 MAINTENANCE PRACTICES ........... 7 Shoring ................
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  • Page 123: General

    LIFTING AND SHORING 07-00 GENERAL INTRODUCTION The aircraft is jacked and shored for maintenance, replacement of components, overhaul, and repair etc. When possible, the aircraft should be located on a level surface. The jacking site should be protected from wind (preferably inside a hangar). The aircraft may be jacked with the full fuel tanks.
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  • Page 125: Jacking

    LIFTING AND SHORING 07-10 JACKING DESCRIPTION The aircraft has three jacking points (see Fig. 07-1). They are located under the fuselage and wing central section. The front jack is installed under the jacking point located on the right front lower side of the fuselage (under firewall). The two rear jacks are installed under jacking points, located symmetrically in wing central section (under auxiliary spar).
  • Page 126 LIFTING AND SHORTING Fig. 07-1 Aircraft Jacking Aircraft lowering: CAUTION MAKE SURE THAT THE AREA UNDER THE AIRCRAFT IS CLEAR BEFORE YOU LOWER THE AIRCRAFT OFF JACKS. Remove stand under the tail. Retract the jacks until the wheels are on the ground. Operate the jacks together to keep the aircraft levelled as much as possible.

  • Page 127: Shoring

    LIFTING AND SHORING 07-20 SHORING DESCRIPTION Before carrying out any maintenance in the rear section of aircraft, shore the aircraft to avoid upset (see Fig. 07-2). The aircraft is shored by the front jack installed under the jacking point located on the right front lower side of the fuselage and the stand under the tail.

  • Page 128: Shoring

    LIFTING AND SHORTING Fig. 07-2 Aircraft Shoring Chapter 07-20 SHORING Page 07-8 Effectivity: ALL 14. 05. 2020...
  • Page 129 LEVELING AND WEIGHING 08 LEVELING AND WEIGHING CONTENTS Chapter Description Page 08-00 GENERAL ................. 3 INTRODUCTION ............... 3 08-10 LEVELING ................ 5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 5 Aircraft on jacks ..............5 Aircraft on wheels .............. 6 08-20 WEIGHING ................
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  • Page 131: General

    LEVELING AND WEIGHING 08-00 GENERAL INTRODUCTION This chapter describes how to level and weigh the aircraft. Use the procedures in Chapter 08-10 to level the aircraft. Use the procedures in Chapter 08-20 to weigh the aircraft and to calculate the aircraft CG position. GENERAL Chapter 08-00 14.
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  • Page 133: Leveling

    LEVELING AND WEIGHING 08-10 LEVELING DESCRIPTION Some operations related to maintenance or repairs require the aircraft to be leveled. The aircraft may be leveled with jacks or by changing the tire inflation. To level the aircraft, the cabin sills above main spar and canopy frame are used (Fig. 08-1). Lateral and longitudinal leveling is checked using a spirit level.

  • Page 134: Aircraft On Wheels

    LEVELING AND WEIGHING Aircraft on wheels Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Pads (various thickness) Spirit level 1 pc Persons Tab. 08-2 Recommended tools, materials, persons and documentation Leveling: Open the canopy.
  • Page 135 LEVELING AND WEIGHING Fig. 08-1 Aircraft Leveling LEVELING Chapter 08-10 14. 05. 2020 Effectivity: ALL Page 08-7...
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  • Page 137: Weighing

    LEVELING AND WEIGHING 08-20 WEIGHING DESCRIPTION The aircraft must be operated within the permitted limits of load and center of gravity to obtain the expected flight performance, flight characteristics and flight safety. After more complex modification, more extended repair, repainting, etc., of the aircraft, etc., the weight and center of gravity may be influenced, the new basic empty weight / moment and CG position must be determined by weighing.

  • Page 138: Maintenance Practices

    LEVELING AND WEIGHING MAINTENANCE PRACTICES Aircraft weighing Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Scales 1 pc Spirit level 1 pc Plumb line (or optical level) 1 pc Persons Tab.
  • Page 139 LEVELING AND WEIGHING Aircraft leveling: Level the aircraft on wheels (Chapter 08-10). Weighing: With the aircraft leveled and canopy closed, obtain and record the aircraft data into a photocopy of the Aircraft Weighing Form (Fig. 08-2 or Fig. 08-3). Obtain and record the value “X” by measuring horizontally and parallel to the aircraft center line, from a line stretched between main wheel centers to a plumb line dropped from the Reference Point (RP).
  • Page 140 LEVELING AND WEIGHING Aircraft: Serial Number: Reg. Number: Date: WT9 Dynamic LSA / Club Measured: Calculated: X =………………… m (in) A = X + 1.975 m (77.76 in) Y =………………… m (in) B = A – Y AIRCRAFT EMPTY WEIGHT / MOMENT AND CG AS WEIGHED (Including operating fluids without unusable fuel) Weight Scale reading...
  • Page 141 LEVELING AND WEIGHING Aircraft: Serial Number: Reg. Number: Date: WT9 Dynamic LSA / Speed Measured: Calculated: X =………………… m (in) A = X + 1.975 m (77.76 in) Y =………………… m (in) B = A – Y AIRCRAFT EMPTY WEIGHT / MOMENT AND CG AS WEIGHED (Including operating fluids without unusable fuel) Scale reading - Tare...

  • Page 142: Calculation Method

    LEVELING AND WEIGHING Calculation method Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Calculator 1 pc Persons Tab. 08-4 Recommended tools, materials, persons and documentation Calculation: Record the date the item was installed on (or removed from) to the aircraft in the “Date“...
  • Page 143 LEVELING AND WEIGHING Fig. 08-4 Weighing and Balance Record WEIGHING Chapter 08-20 14. 05. 2020 Effectivity: ALL Page 08-15...
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  • Page 145 TOWING AND TAXIING 09 TOWING AND TAXIING CONTENTS Chapter Description Page 09-00 GENERAL ................. 3 INTRODUCTION ............... 3 09-10 TOWING ................5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 6 Aircraft towing ..............6 09-20 TAXIING ................9 DESCRIPTION ................9 MAINTENANCE PRACTICES ...........
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  • Page 147: Towing And Taxiing

    TOWING AND TAXIING 09-00 GENERAL INTRODUCTION You can move the aircraft on the ground with: • pushing / pulling • tow bar • taxiing When towing or handling the aircraft close to obstacles (buildings, other aircraft) a wing walker should follow the aircraft and inform about a danger of the aircraft collision with the obstacles.
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  • Page 149: Towing

    TOWING AND TAXIING 09-10 TOWING DESCRIPTION The aircraft can be moved for a short distance by means of towing by holding the blade roots. Handle the propeller by holding the blade root – never blade tip. There is also possibility of using tow bar that attaches to the nose landing gear. CAUTION AVOID EXCESSIVE PRESSURE AT THE AIRCRAFT CONTROL SURFACES AND THE WING TIPS.

  • Page 150: Maintenance Practices

    TOWING AND TAXIING MAINTENANCE PRACTICES Aircraft towing Type of maintenance: Line Personnel qualification: Pilot/Owner qualified in accordance with M.A.803 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Tow bar 1 pc Wheel chocks 1 pc Persons Tab. 09-1 Recommended tools, materials, persons and documentation Aircraft towing: Fixed gear: Attach the tow bar to the nose wheel leg (1, Fig.
  • Page 151 TOWING AND TAXIING Fig. 09-1 Tow Bar - Fixed Landing Gear TOWING Chapter 09-10 14. 05. 2020 Effectivity: ALL Page 09-7...
  • Page 152 TOWING AND TAXIING Fig. 09-2 Tow Bar - Retractable Landing Gear Chapter 09-10 TOWING Page 09-8 Effectivity: ALL 14. 05. 2020...

  • Page 153: Taxiing

    TOWING AND TAXIING 09-20 TAXIING DESCRIPTION Taxiing is a way of aircraft moving, using the aircraft power plant thrust. For taxiing procedures refer to Pilot´s Operating Handbook (Chapter 4). WARNING DO NOT TAXI THE AIRCRAFT UNLESS YOU HAVE BEEN TRAINED TO TAXI AND YOU HAVE BEEN AUTHORIZED.
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  • Page 155 PARKING, MOORING, STORAGE AND RETURN TO SERVICE 10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE CONTENTS Chapter Description Page 10-00 GENERAL ................. 3 INTRODUCTION ............... 3 10-10 PARKING / STORAGE ............. 5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 5 Parking ................5 Temporary storage (30 to 90 days) ........
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  • Page 157: General

    PARKING, MOORING, STORAGE AND RETURN TO SERVICE 10-00 GENERAL INTRODUCTION This chapter determines instructions needed for parking and mooring of the aircraft at all expected weather conditions. A procedure for anchoring the aircraft must always be realized if strong wind or long term parking of aircraft is expected. This chapter also contains instructions that should be executed during storage of the aircraft.
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  • Page 159: Parking / Storage

    PARKING, MOORING, STORAGE AND RETURN TO SERVICE 10-10 PARKING / STORAGE DESCRIPTION Parking procedure depends on parking time (or on expected weather conditions). If adverse weather conditions are expected (very strong wind, downpours, sand storm etc.), the aircraft should be parked inside a hangar. When parking inside the hangar, carry out the same operations as during a short-time parking.
  • Page 160 PARKING, MOORING, STORAGE AND RETURN TO SERVICE NOTE In the case of parking under bad weather conditions, moor the aircraft to avoid of its damage (Chapter 10-20). NOTE Under snow or arctic conditions, or when icing or snowing is expected, cover the aircraft with suitable covers. 1 –...
  • Page 161 PARKING, MOORING, STORAGE AND RETURN TO SERVICE Temporary storage (30 to 90 days) Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons Tab. 10-2 Recommended tools, materials, persons and documentation Parking and mooring: Park and moor the aircraft (see 2.A.
  • Page 162 PARKING, MOORING, STORAGE AND RETURN TO SERVICE Long term storage (over 91 days) Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Protective foil Lithium grease NLGI 3 MOL Liton LTA 3EP Persons Tab.

  • Page 163: Mooring

    PARKING, MOORING, STORAGE AND RETURN TO SERVICE 10-20 MOORING GENERAL The aircraft is moored when parked outside (on apron). A correct mooring is highly important if strong wind is expected, or during long-time parking. When a strong wind affects the aircraft (e.g. storm), the aircraft structure could be damaged. When strong wind is expected, park the aircraft inside a hangar.
  • Page 164 PARKING, MOORING, STORAGE AND RETURN TO SERVICE Aircraft mooring: Park the aircraft (Chapter 10-10, 2.A.) Put the chocks (1, Fig. 10-2) in front of and behind main landing gear wheels. Put the control surfaces into neutral position and fix them using an adhesive tape.

  • Page 165: Maintenance Practices

    PARKING, MOORING, STORAGE AND RETURN TO SERVICE 10-30 RETURN TO SERVICE GENERAL Depending on the time the aircraft was inactive, the aircraft must be prepared for the return to service after temporary or long term storage. MAINTENANCE PRACTICES Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance...

  • Page 166: Return To Service After Long Term Storage (Over 91 Days)

    PARKING, MOORING, STORAGE AND RETURN TO SERVICE Pre-flight inspection: Carry out the pre-flight inspection (POH, Chapter 4). Instructions for continued airworthiness: Verify all airworthiness directives complied with. Verify all service letters, bulletins, and instructions complied with. Return to service after long term storage (over 91 days) Parking: Remove all covers and adhesive tapes.
  • Page 167 PLACARDS AND MARKINGS 11 PLACARDS AND MARKINGS CONTENTS Chapter Description Page 11-00 GENERAL ................. 3 INTRODUCTION ............... 3 MAINTENANCE PRACTICES ........... 3 Replacing damaged placards ..........3 11-20 EXTERIOR PLACARDS AND MARKINGS ....... 5 11-30 INTERIOR PLACARDS AND MARKINGS ......9 CONTENTS Chapter 11 04.
  • Page 168 PLACARDS AND MARKINGS This page is left blank intentionally Chapter 11 CONTENTS Page 11-2 Effectivity: ALL 04. 05. 2021...

  • Page 169: Placards And

    PLACARDS AND MARKINGS 11-00 GENERAL INTRODUCTION Placards are used for identification and indication purposes. They show the function, directional movements, position identifications, operating instructions, operating limitations of systems and equipment. Self-adhesive plastic foils are used for all placards except for the metal aircraft manufacturer’s placard.
  • Page 170 PLACARDS AND MARKINGS This page is left blank intentionally Chapter 11-00 GENERAL Page 11-4 Effectivity: ALL 04. 05. 2021...

  • Page 171: Exterior Placards And Markings

    PLACARDS AND MARKINGS 11-20 EXTERIOR PLACARDS AND MARKINGS Exterior placards and markings are listed in the Tab. 11-2. ITEM. PLACARD COLOUR LOCATION FIG. White / Fuselage L / R front 11-1 blue part Black / Fuselage L / R 11-1 orange center part Yellow /...
  • Page 172 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Acc. to Fuselage L / R rear color 11-1 part below rudder design Outer part of the White / main landing gear 11-1 black legs White / Right part of the 11-1 black nose wheel cover Upper engine...
  • Page 173 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Near jack points and drain valves on the fuselage / wing center 11-1 section bottom part; symmetrically next to canopy opening lever Trailing edge of the White / control surfaces and trim 11-1 Near jack points on the White /...
  • Page 174 PLACARDS AND MARKINGS Fig. 11-1 Exterior Placards Location (illustrative figure) Chapter 11-20 EXTERIOR PLACARDS AND MARKINGS Page 11-8 Effectivity: ALL 04. 05. 2021...

  • Page 175: Interior Placards And Markings

    PLACARDS AND MARKINGS 11-30 INTERIOR PLACARDS AND MARKINGS Interior placards and markings are listed in the Tab. 11-3. ITEM. PLACARD COLOUR LOCATION FIG. INSTRUMENT PANEL White / Magnetic compass 11-2 black White / Magnetic compass 11-2 black Instrument panel Black / white center part or left 11-2 part...
  • Page 176 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Instrument panel left part or center part - near airspeed indicator, fixed gear Black / white 11-2 Note: Placard is valid only for knots air speed indicator. Instrument panel left part or center part - near airspeed indicator, Black / white...
  • Page 177 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Black / white Central console 11-2 Black / white Central console 11-2 Black / white Central console 11-2 Black / white Central console 11-2 Black / white Central console 11-2 Central console 11-2 Black / white Pedestal...
  • Page 178 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Instrument panel 17a. Black / white 11-2 center part Instrument panel 17b. Black / white 11-2 center part Instrument panel Black / white left and/or right part 11-2 - near socket 12V Instrument panel Black / white right part –...
  • Page 179 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Instrument panel Black / white right part - near fuel 11-2 switch Instrument panel center part - above intercom switch; Black / white 11-2 Instrument panel right part - bellow the circuit breakers Instrument panel left or center part - above switches;...
  • Page 180 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Instrument panel left part - LH Dynon USB port; Black / white 11-2 Instrument panel center part – above switch Instrument panel right part - RH Dynon USB port; Black / white 11-2 Instrument panel center part –...
  • Page 181 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Instrument panel left part - above the switches; Black / white 11-2 Instrument panel right part - bellow the circuit breakers Instrument panel Black / white right part - bellow 11-2 the circuit breakers Instrument panel L/R part –...
  • Page 182 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Instrument panel Black / white right part - bellow 11-2 the circuit breakers Instrument panel Black / white right part - bellow 11-2 the circuit breakers Instrument panel right part - bellow 11-2 Black / white the circuit breakers;...
  • Page 183 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. Instrument panel Black / white left or center part - 11-2 above switch; Instrument panel Black / white left or center part - 11-2 above switch; Instrument panel left side - above the check lamp;...
  • Page 184 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. BAGGAGE COMPARTMENTS Left side of the baggage 100. Metal 11-3 compartment bulkhead Left side of the baggage 101. Metal 11-3 compartment bulkhead L / R side of the baggage 102. Black / white 11-3 compartment bulkhead...
  • Page 185 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. PEDESTAL PANEL Pedestal - flap 130. Black / white 11-3 control slotted link Pedestal - flap 131. Black / white 11-3 control slotted link Pedestal - flap 132. Black / white 11-3 control slotted link Pedestal - flap 133.
  • Page 186 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. CANOPY FRAME / FUSELAGE Right side of the canopy frame, near 160. Black / white 11-3 the canopy opening lever L / R side of canopy frame, near the 161. Black / white 11-3 ventilation control knob...
  • Page 187 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. ENGINE COMPARTMENT Firewall in the engine compartment - near 180a. Black / white 11-4 the overflow bottle (fixed gear only) Firewall in the engine compartment - near 180b. Black / white 11-4 the overflow bottle (retractable gear only)
  • Page 188 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. TOWING EQUIPMENT Tow release handle, Black / 200. left side of central 11-2 white tunnel near throttle Left side of the cockpit Valid for tow release 201a. Red / white 11-3 version of tow equipment Left side of the cockpit 201b.
  • Page 189 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. RETRACTABLE GEAR Instrument panel right part - bellow the circuit Black / 220. breakers; Instrument 11-2 white panel left side - above the checklights Instrument panel right Black / 221. part - bellow the circuit 11-2 white breakers;...
  • Page 190 PLACARDS AND MARKINGS ITEM. PLACARD COLOUR LOCATION FIG. RETRACTABLE GEAR Black / Instrument panel left 232. 11-2 white side - above switch Instrument panel right Black / 233. part - above the circuit 11-2 white breakers; Instrument panel right Black / 234.
  • Page 191 PLACARDS AND MARKINGS Fig. 11-2.1 Placards on the Instrument Panel DY-337/2009 Fig. 11-2.2 Placards on the Instrument Panel DY-347/2010 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-25...
  • Page 192 PLACARDS AND MARKINGS Fig. 11-2.3 Placards on the Instrument Panel DY-363/2010 LSA Fig. 11-2.4 Placards on the Instrument Panel DY-377/2010 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-26 Effectivity: ALL 04. 05. 2021...
  • Page 193 PLACARDS AND MARKINGS Fig. 11-2.5 Placards on the Instrument Panel DY-387/2010 LSA Fig. 11-2.6 Placards on the Instrument Panel DY-390/2010 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-27...
  • Page 194 PLACARDS AND MARKINGS Fig. 11-2.8 Placards on the Instrument Panel DY-392/2010 LSA Fig. 11-2.9 Placards on the Instrument Panel DY-395/2010 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-28 Effectivity: ALL 04. 05. 2021...
  • Page 195 PLACARDS AND MARKINGS Fig. 11-2.10 Placards on the Instrument Panel DY-400/2011 LSA Fig. 11-2.11 Placards on the Instrument Panel DY-420/2011 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-29...
  • Page 196 PLACARDS AND MARKINGS Fig. 11-2.12 Placards on the Instrument Panel DY-427/2011 LSA Fig. 11-2.13 Placards on the Instrument Panel DY-428/2011 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-30 Effectivity: ALL 04. 05. 2021...
  • Page 197 PLACARDS AND MARKINGS Fig. 11-2.14 Placards on the Instrument Panel DY-429/2012 LSA Fig. 11-2.15 Placards on the Instrument Panel DY-433/2012 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-31...
  • Page 198 PLACARDS AND MARKINGS Fig. 11-2.16 Placards on the Instrument Panel DY-434/2012 LSA Fig. 11-2.17 Placards on the Instrument Panel DY-435/2012 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-32 Effectivity: ALL 04. 05. 2021...
  • Page 199 PLACARDS AND MARKINGS Fig. 11-2.18 Placards on the Instrument Panel DY-436/2012 LSA Fig. 11-2.19 Placards on the Instrument Panel DY-439/2012 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-33...
  • Page 200 PLACARDS AND MARKINGS Fig. 11-2.20 Placards on the Instrument Panel DY-442/2012 LSA Fig. 11-2.21 Placards on the Instrument Panel DY-445/2012 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-34 Effectivity: ALL 04. 05. 2021...
  • Page 201 PLACARDS AND MARKINGS Fig. 11-2.22 Placards on the Instrument Panel DY-448/2012 LSA Fig. 11-2.23 Placards on the Instrument Panel DY-449/2012 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-35...
  • Page 202 PLACARDS AND MARKINGS Fig. 11-2.24 Placards on the Instrument Panel DY-459/2012 LSA Fig. 11-2.25 Placards on the Instrument Panel DY-460/2012 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-36 Effectivity: ALL 04. 05. 2021...
  • Page 203 PLACARDS AND MARKINGS Fig. 11-2.26 Placards on the Instrument Panel DY-461/2012 LSA Fig. 11-2.27 Placards on the Instrument Panel DY-463/2013 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-37...
  • Page 204 PLACARDS AND MARKINGS Fig. 11-2.28 Placards on the Instrument Panel DY-464/2013 LSA Fig. 11-2.29 Placards on the Instrument Panel DY-466/2013 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-38 Effectivity: ALL 04. 05. 2021...
  • Page 205 PLACARDS AND MARKINGS Fig. 11-2.30 Placards on the Instrument Panel DY-468/2013 LSA Fig. 11-2.31 Placards on the Instrument Panel DY-470/2013 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-39...
  • Page 206 PLACARDS AND MARKINGS Fig. 11-2.32 Placards on the Instrument Panel DY-475/2013 LSA Fig. 11-2.33 Placards on the Instrument Panel DY-477/2013 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-40 Effectivity: ALL 04. 05. 2021...
  • Page 207 PLACARDS AND MARKINGS Fig. 11-2.34 Placards on the Instrument Panel DY-480/2013 LSA Fig. 11-2.35 Placards on the Instrument Panel DY-485/2013 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-41...
  • Page 208 PLACARDS AND MARKINGS Fig. 11-2.36 Placards on the Instrument Panel DY-487/2013 LSA Fig. 11-2.37 Placards on the Instrument Panel DY-491/2013 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-42 Effectivity: ALL 04. 05. 2021...
  • Page 209 PLACARDS AND MARKINGS Fig. 11-2.38 Placards on the Instrument Panel DY-493/2014 LSA Fig. 11-2.39 Placards on the Instrument Panel DY-494/2014 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-43...
  • Page 210 PLACARDS AND MARKINGS Fig. 11-2.40 Placards on the Instrument Panel DY-496/2013 LSA Fig. 11-2.41 Placards on the Instrument Panel DY-499/2013 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-44 Effectivity: ALL 04. 05. 2021...
  • Page 211 PLACARDS AND MARKINGS Fig. 11-2.42 Placards on the Instrument Panel DY-500/2014 LSA Fig. 11-2.43 Placards on the Instrument Panel DY-501/2014 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-45...
  • Page 212 PLACARDS AND MARKINGS Fig. 11-2.44 Placards on the Instrument Panel DY-508/2014 LSA Fig. 11-2.45 Placards on the Instrument Panel DY-510/2014 LSA Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-46 Effectivity: ALL 04. 05. 2021...
  • Page 213 PLACARDS AND MARKINGS Fig. 11-2.46 Placards on the Instrument Panel DY-514/2014 LSA INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-47...
  • Page 214 PLACARDS AND MARKINGS Fig. 11-3 Interior Placards Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-48 Effectivity: ALL 04. 05. 2021...
  • Page 215 PLACARDS AND MARKINGS Fig. 11-4 Engine Compartment Placards INTERIOR PLACARDS AND MARKINGS Chapter 11-30 04. 05. 2021 Effectivity: ALL Page 11-49...
  • Page 216 PLACARDS AND MARKINGS This page is left blank intentionally Chapter 11-30 INTERIOR PLACARDS AND MARKINGS Page 11-50 Effectivity: ALL 04. 05. 2021...
  • Page 217 SERVICING 12 SERVICING CONTENTS Chapter Description Page 12-00 GENERAL ................. 3 INTRODUCTION ............... 3 RECOMMENDED MATERIALS ..........3 DISPOSABLE REPLACEMENT PARTS ........5 12-10 REPLENISHING ..............7 DESCRIPTION ................7 MAINTENANCE PRACTICES ........... 9 Fuel system ............... 9 Oil system ................ 13 Engine cooling system ............
  • Page 218 SERVICING 12-30 UNSCHEDULED SERVICING ......... 43 DESCRIPTION ................ 43 MAINTENANCE PRACTICES ..........43 Winter maintenance ............43 Chapter 12 CONTENTS Page 12-2 Effectivity: ALL 04. 05. 2021...

  • Page 219: General

    SERVICING 12-00 GENERAL INTRODUCTION This chapter provides instructions on how to replenish operating fluids. ln addition, this chapter provides instructions for scheduled servicing, unscheduled servicing and recommended materials. RECOMMENDED MATERIALS Tab. 12-1 shows recommended materials, including required specifications, recommended by the aircraft manufacturer or the engine manufacturer. Any products with identical specifications can be used.
  • Page 220 SERVICING MATERIAL DESIGNATION SPECIFICATION NOTE Hydraulic Conventional DOT 4 Brake system fluid hydraulic fluid Classification J1703c Mineral oil based Hydraulic Retractable landing gear Aeroshell Fluid 41 "super clean" fluid hydraulic system hydraulic fluid Tab. 12-1 Recommended Materials (page 2 of 2) Chapter 12-00 GENERAL Page 12-4...

  • Page 221: Disposable Replacement Parts

    (Beringer wheel discs) Nose wheel tire Any source 13x5.00-6 (tubeless) (Beringer wheel discs) Main wheel tire Any source 15x6.00-6 or 14x4.00-6 (Aerospool wheel discs) Nose wheel tire Any source 13x5.00-6 (Aerospool wheel discs) NH1220 Tashima, Japan 12 V / 20 Ah GP 12170 CSB BATTERY CO.,...
  • Page 222 CRG Beringer (Beringer brake Part No. ZEA01 system) Brake pads GOLDfren (Aerospool Part No. 925AD brake system) *Originally delivered end piece is fitted with 500 daN weak links that must be replaced with max. 300 daN weak links. Tab. 12-2 List of Disposable Replacement parts (Page 2 of 2)

  • Page 223: Replenishing

    SERVICING 12-10 REPLENISHING DESCRIPTION This chapter provides replenishing information of all operating fluids of aircraft: • Fuel system • Oil system • Engine cooling system • Brake system • Hydraulic system (retractable landing gear only) For servicing points refer to Fig. 12-1, Fig. 12-2 and Fig. 12-3. 1a –...
  • Page 224 SERVICING Not installed for 100 l fuel tanks Fig. 12-2 Drain Valves 1 – hydraulic fluid reservoir cap Fig. 12-3 Hydraulic Fluid (Retractable Landing Gear Only) Chapter 12-10 REPLENISHING Page 12-8 Effectivity: ALL 04. 05. 2021...
  • Page 225 SERVICING MAINTENANCE PRACTICES Fuel system Integral fuel tanks are located in RH wing / both wings and wing central section in front of main spar. Wing and wing central section tanks are interconnected with hose. Depending on the fuel tanks capacity, the fuel tank cap is located on the top surface of the wing or on the fuselage wing section.
  • Page 226 SERVICING The risk of operation with a contaminated fuel can be reduced by: • Keeping the fuel servicing equipment and filters of such equipment clean • Proper storage of the fuel • Regular drainage (prior to drainage, let the fuel in calm position for a sufficient period of time for impurities and suspended water to settle down) •...
  • Page 227 SERVICING WARNING GROUND THE EXHAUST PIPE OUTLET AND FUEL SERVICE EQUIPMENT PRIOR TO AIRCRAFT REFUELING/DEFUELING! MAKE SURE THAT A SUITABLE FIRE EXTINGUISHER IS AVAILABLE AT ALL TIMES DURING AIRCRAFT REFUELING/DEFUELING! SMOKING MANIPULATING WITH OPEN FIRE DURING REFUELING/DEFUELING AND DRAINING IS PROHIBITED! MASTER SWITCH AND IGNITION MUST BE SWITCHED OFF! NO PERSONS ALLOWED TO BE IN THE COCKPIT! DO NOT USE THE MATERIALS WHICH CAN CAUSE STATIC...
  • Page 228 SERVICING Install the fuel tank cap and make sure that opening arm directs rearward. Make sure that no spilled fuel is on the aircraft; clean if necessary. NOTE If refueling only one fuel tank, fill such fuel quantity that in both tanks will be same amount of fuel. Remove the ground cable from the aircraft.
  • Page 229 SERVICING Oil system The engine Rotax 912 ULS / 914 UL uses a dry sump forced lubrication system with total oil system capacity 3.5 l. A filler cap and dipstick is provided for determining the amount of oil in the system. WARNING ALWAYS ALLOW ENGINE TO COOL DOWN TO AMBIENT TEMPERATURE BEFORE START OF ANY WORK, OTHERWISE...
  • Page 230 SERVICING Oil replenish: Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY New oil Cotton cloth Persons Tab. 12-8 Recommended tools, materials, persons and documentation NOTE For longer flights replenish oil to max.
  • Page 231 SERVICING 1 Oil tank 2 Oil tank cap 3 Dipstick Fig. 12-4 Oil Level Check Oil change: Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 17 1 pc...
  • Page 232 SERVICING WARNING CARELESS DRAINING OF HOT ENGINE OIL MAY CAUSE SCALDS. DISPOSE USED FILTERS RESPECTING ENVIRONMENTAL SAFETY REGULATIONS. CAUTION FAILURE TO FOLLOW INSTRUCTIONS BELOW COULD LEAD TO AIR ENTERING THE OIL SYSTEM AND DEFECTS ON VALVE TRAIN. NOTE Run engine to warm oil before beginning oil change procedure. Do not drain the oil suction line, oil radiator and return line to avoid of air entering the oil system.
  • Page 233 SERVICING WARNING METAL CONTAMINATION FOUND PLUG (FIG. 12-5), CONTACT AIRCRAFT MANUFACTURER! Fig. 12-5 Magnetic Plug (illustrative figure) (m) Fill the oil cooler with new oil. Make sure that the corresponding kind of oil is used (Tab. 12-1). Connect hoses (4; 5, Fig. 12-6) on the oil cooler (2); secure them with safety wire.
  • Page 234 SERVICING On vent hose (8) put on jig making pressure at 0.45 bar. CAUTION PRESSURE SHOULD NEVERRISE OVER 1 BAR. Rotate the propeller while beginning a continual flow of oil from hose (7). Add more oil if necessary. Disconnect jig, connect back hose (7) on oil tank and reinstall spark plugs;...

  • Page 235: Engine Cooling System

    SERVICING Engine cooling system Aircraft has combined water and air cooling system. Coolant capacity is approximately 2.5 l (cooling system + overflow bottle). WARNING ALWAYS ALLOW ENGINE TO COOL DOWN TO AMBIENT TEMPERATURE BEFORE START OF ANY WORK. ENGINE IGNITION MUST BE SWITCHED OFF. NEVER OPEN EXPANSION...
  • Page 236 SERVICING Coolant replenishing: Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY New coolant Persons Tab. 12-11 Recommended tools, materials, persons and documentation NOTE If necessary, replenish with coolant of same specification. Make sure that the corresponding kind of coolant is used (Tab.
  • Page 237 SERVICING Coolant change: Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 10 1 pc 1 pc Syringe 1 pc Suitable container 1 pc New coolant Persons Maintenance Manual (Line Maintenance) for Rotax...

  • Page 238: Tires

    The aircraft uses following tires: Beringeer wheels: • Nose landing gear wheel with tire 13x5.00-6. • Main landing gear wheels with tires 15x6.00-6. Aerospool wheels: • Nose landing gear wheel with tire 13x5.00-6. • Main landing gear wheels with tires 15x6.00-6 or 14x4.00-6. During...

  • Page 239: Brake System

    Aerospool brake system. Open the cap (4, Fig. 12-1) of Beringer brake fluid reservoir or unscrew the screw and remove the cap of Aerospool brake fluid reservoir. Check if brake fluid level is between min. and max. level marks.
  • Page 240 Install the cap (4, Fig. 12-1) on the brake fluid reservoir for Beringer brake system or install the cap and attach by screw for Aerospool brake system. Install the tunnel cover and upholstery cover of the central tunnel or the pilot seat (Chapter 25-10).

  • Page 241: Scheduled Servicing

    SERVICING 12-20 SCHEDULED SERVICING INTRODUCTION This chapter contains the information necessary to perform scheduled service of the aircraft. In this chapter is presented lubrication chart and instructions for cleaning the exterior and interior of the aircraft including the required materials. SPECIAL TOOLS, MATERIALS Recommended tools, materials, persons and documentation: ITEM...

  • Page 242: Lubrication Chart

    SERVICING LUBRICATION CHART Lubricate movable or rotary places on the aircraft in scheduled intervals (Tab. 12-18). Regular lubrication decreases frictional forces in movable joints and protects lubricated places against corrosion. Use recommended lubricants for lubrication (see below). The lubricants shall not be contaminated with water or foreign matters and their storage period or usability shall not be expired.
  • Page 243 SERVICING 100 hr. / Location Lubrication point Annual / Lubricant Special Refer to Maintenance Manual (Line Maintenance) for Rotax Engine Engine Type 912/914 Series, Ref. No. MML-912/914, the latest issue Throttle control cables at the entry to Engine installation bowdens. (Fig.
  • Page 244 SERVICING 100 hr. / Location Lubrication point Annual / Lubricant Special Movable connection points of nose landing Main landing gear gear (retractable landing gear) (Fig. 12-7) All points with grease cap fitting Movable connecting points of elevator control system. Elevator control Sliding bearings on the control stick’s system torsion tube.
  • Page 245 SERVICING Throttle control Fig. 12-7 Lubrication Chart (page 1 of 9) SCHEDULED SERVICING Chapter 12-20 04. 05. 2021 Effectivity: ALL Page 12-29...
  • Page 246 SERVICING Engine installation Fig. 12-7 Lubrication Chart (page 2 of 9) Chapter 12-20 SCHEDULED SERVICING Page 12-30 Effectivity: ALL 04. 05. 2021...
  • Page 247 SERVICING Nose landing gear leg Fig. 12-7 Lubrication Chart (page 3 of 9) SCHEDULED SERVICING Chapter 12-20 04. 05. 2021 Effectivity: ALL Page 12-31...
  • Page 248 SERVICING Fig. 12-7 Lubrication Chart (page 4 of 9) Chapter 12-20 SCHEDULED SERVICING Page 12-32 Effectivity: ALL 04. 05. 2021...
  • Page 249 SERVICING Fig. 12-7 Lubrication Chart (page 5 of 9) SCHEDULED SERVICING Chapter 12-20 04. 05. 2021 Effectivity: ALL Page 12-33...
  • Page 250 SERVICING Elevator control Rudder control (Fixed landing gear) Fig. 12-7 Lubrication Chart (page 6 of 9) Chapter 12-20 SCHEDULED SERVICING Page 12-34 Effectivity: ALL 04. 05. 2021...
  • Page 251 SERVICING Rudder control (Fixed landing gear) Fig. 12-7 Lubrication Chart (page 7 of 9) SCHEDULED SERVICING Chapter 12-20 04. 05. 2021 Effectivity: ALL Page 12-35...
  • Page 252 SERVICING Aileron control Flaps control Fig. 12-7 Lubrication Chart (page 8 of 9) Chapter 12-20 SCHEDULED SERVICING Page 12-36 Effectivity: ALL 04. 05. 2021...
  • Page 253 SERVICING Fig. 12-7 Lubrication Chart (page 9 of 9) SCHEDULED SERVICING Chapter 12-20 04. 05. 2021 Effectivity: ALL Page 12-37...

  • Page 254: Aircraft Cleaning

    SERVICING AIRCRAFT CLEANING Type of maintenance: Line Personnel qualification: Pilot/Owner qualified in accordance with M.A.803 except engine cleaning where minimum authorization independent certifying staff qualified in accordance with Part-66 or higher is required. Recommended tools, materials, persons and documentation: List of special tools and materials for the cleaning of the aircraft is shown in Tab.

  • Page 255: Cabin Cleaning

    SERVICING Use large quantities of water to clean the aircraft. If necessary, add a mild-cleaning agent to the water and remove dust and dirt from painted surfaces with a sponge CAUTION WHEN WASHING THE AIRCRAFT WITH WATER AND CLEANING AGENT, USE SPECIAL CARE TO AVOID WASHING AWAY GREASE FROM ANY LUBRICATED AREA.

  • Page 256: Interior Cleaning

    SERVICING CAUTION NEVER GASOLINE, BENZENE, ALCOHOL, ACETONE, FIRE EXTINGUISHER, ANTI-ICE FLUID, LACQUER THINNER OR GLASS CLEANER TO CLEAN PLEXIGLASS. THESE MATERIALS WILL CORRODE THE PLEXIGLASS. DO NOT RUB THE CANOPY WHILE IT IS DRY. DO NOT USE DIRTY CLOTHS OR SPONGES. THE PLEXIGLASS CANOPY SCRATCHES VERY EASILY WITH EVEN THE SMALLEST PARTICLES OF DUST.

  • Page 257: Engine Cleaning

    SERVICING Engine cleaning CAUTION DO NOT USE EASILY FLAMMABLE LIQUIDS OR CAUSTIC CLEANING AGENT FOR CLEANING THE ENGINE! Repair leaks if required before cleaning. Always clean engine in cold state. Usage of commercially available cold cleaning agent for the engine is recommended - see Maintenance Manual (Line Maintenance) for Rotax Engine Type 912/914 Series (Ref.
  • Page 258 SERVICING This page is left blank intentionally Chapter 12-20 SCHEDULED SERVICING Page 12-42 Effectivity: ALL 04. 05. 2021...
  • Page 259 SERVICING 12-30 UNSCHEDULED SERVICING DESCRIPTION This chapter contains information regarding unscheduled service which includes removal of ice and snow from the aircraft. MAINTENANCE PRACTICES Winter maintenance Ice and snow removal: Contamination aircraft surface snow degrades the aerodynamic characteristics of the aircraft and increases its weight. It is therefore important to get rid of any deposit of ice or snow before flight.
  • Page 260 SERVICING This page is left blank intentionally Chapter 12-30 UNSCHEDULED SERVICING Page 12-44 Effectivity: ALL 04. 05. 2021...
  • Page 261 STANDARD PRACTICES - AIRFRAME 20 STANDARD PRACTICES - AIRFRAME CONTENTS Chapter Description Page 20-00 GENERAL ................. 3 INTRODUCTION ............... 3 20-10 TORQUE DATA ..............5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 5 Fasteners installation ............5 Torque wrenches ............... 6 Torque values ..............
  • Page 262 STANDARD PRACTICES - AIRFRAME This page is left blank intentionally Chapter 20 CONTENTS Page 20-2 Effectivity: ALL 14. 05. 2020...

  • Page 263: General

    STANDARD PRACTICES - AIRFRAME 20-00 GENERAL INTRODUCTION This chapter describes the standard maintenance practices for maintaining items of the airframe and systems that are typical to more than one area or system, in an airworthy condition. Maintenance practices that are unique to a particular system or subject are described in the appropriate chapter in the maintenance manual.
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  • Page 265: Torque Data

    STANDARD PRACTICES - AIRFRAME 20-10 TORQUE DATA DESCRIPTION This chapter deals with general torque used to ensure security of installation and prevent overstressing components. The torque value tables, listed in this chapter, are standard torque values for the nut and bolt combinations shown. Special torque values for specific installations are given in maintenance practices and installation instructions applicable to the various components.

  • Page 266: Torque Wrenches

    STANDARD PRACTICES - AIRFRAME washer or installing a standard washer can result in bolt failure (Fig. 20-1). Fig. 20-1 Washer Installation – Close Tolerance Bolts Torque wrenches Whenever possible, use the torque wrench when tightening of threaded fasteners. Use of a torque wrench: Whenever possible, the nut shall be torqued.
  • Page 267 STANDARD PRACTICES - AIRFRAME Fig. 20-2 Torque Wrench and Adapter Formulas TORQUE DATA Chapter 20-10 14. 05. 2020 Effectivity: ALL Page 20-7...

  • Page 268: Torque Values

    STANDARD PRACTICES - AIRFRAME Torque values The torque values have been calculated on the assumption that no lubrication is used on the bolted joints and that cadmium plating is a standard surface finish. STRENGTH CLASS METRIC THREAD MAXIMAL TORQUE VALUE 1.67 kg.m 0.17...

  • Page 269: Safetying

    STANDARD PRACTICES - AIRFRAME 20-20 SAFETYING DESCRIPTION The use of safety wire, cotter pins, lock washers, self-locking nuts, and Loctite is to prevent relative movement of critical components subject to vibration, torque, tension, etc., which could cause attaching parts to be broken, loosened and or detached.

  • Page 270: Maintenance Practices

    STANDARD PRACTICES - AIRFRAME MAINTENANCE PRACTICES Lockwire Lock wire comes in two types, which are identified by size: • Zinc plated and Tin-plated steel wire. Used for general lock wiring procedures. • Corrosion resistant steel wire. This wire is to be used in areas with high temperature and chemical corrosion.
  • Page 271 STANDARD PRACTICES - AIRFRAME NOTE This does not necessarily apply to the castellated nuts when the slot is close to the top of the nut, the wire will be more secure if it is made to pass along the side of the stud.
  • Page 272 STANDARD PRACTICES - AIRFRAME Fig. 20-3 Lockwire Safetying Chapter 20-20 SAFETYING Page 20-12 Effectivity: ALL 14. 05. 2020...
  • Page 273 STANDARD PRACTICES - AIRFRAME Fig. 20-4 RH Thread Lockwiring Examples SAFETYING Chapter 20-20 14. 05. 2020 Effectivity: ALL Page 20-13...

  • Page 274: Cotter Pins

    STANDARD PRACTICES - AIRFRAME Fig. 20-5 Electrical Connectors Lockwiring Examples Cotter pins Use of cotter pins: Select cotter pins in accordance with atmosphere and service limitations. Use only a new cotter pin of the same type as the one removed. Never reuse cotter pins.
  • Page 275 STANDARD PRACTICES - AIRFRAME lnstall the cotter pins (if it is possible): - from above-downwards - from the front-backwards. Cadmium plated cotter pins should not be used in applications bringing them in contact with fuel, hydraulic fluid or synthetic lubricant. If using a castellated nut and new bolt, screw the castellated nut to operating position and use diameter 1,6 mm drill to drill a hole for the cotter pin.

  • Page 276: Self-Locking Nuts

    STANDARD PRACTICES - AIRFRAME Self-locking nuts Self-locking nuts may be used in some applications. The following guidelines must be followed when using self-locking nuts: Use of self-locking nuts: Self-locking nuts must be installed so at least two threads of bolt, stud or screw are visible.

  • Page 277: Loctite

    STANDARD PRACTICES - AIRFRAME Loctite NOTE Loctite type and suitable cleaner is listed in the relevant chapter in the Materials table. Use of Loctite: Loctite is used on the aircraft when it is impossible to cotter pins/lock wire a fastener or if cotter pins/lock wire is impractical. Use only Loctite of the same type as that which was originally used.
  • Page 278 STANDARD PRACTICES - AIRFRAME This page is left blank intentionally Chapter 20-20 SAFETYING Page 20-18 Effectivity: ALL 14. 05. 2020...
  • Page 279 CONDITIONING 21 AIR CONDITIONING CONTENTS Chapter Description Page 21-00 GENERAL ................. 3 INTRODUCTION ............... 3 TROUBLESHOOTING ............... 3 21-20 DISTRIBUTION ..............5 DESCRIPTION ................5 Cockpit ventilation ............. 5 MAINTENANCE PRACTICES ........... 9 Control box ................ 9 Ventilation control .............. 9 Blowers................
  • Page 280 CONDITIONING This page is left blank intentionally Chapter 21 CONTENTS Page 21-2 Effectivity: ALL 04. 05. 2021...

  • Page 281: General

    CONDITIONING 21-00 GENERAL INTRODUCTION The aircraft is equipped with heating and ventilation system that ensures delivery of cockpit heating and fresh ambient air. The heating and ventilation system consist of cold and warm air passing through a control box on the firewall. Ambient air is received from the induction ram air tunnel on the left side of lower engine cowling.
  • Page 282 CONDITIONING This page is left blank intentionally Chapter 21-00 GENERAL Page 21-4 Effectivity: ALL 04. 05. 2021...

  • Page 283: Distribution

    CONDITIONING 21-20 DISTRIBUTION DESCRIPTION Cockpit ventilation Venting air comes from the ram air tunnel (1, Fig. 21-1) installed on the left side of lower engine cowling and directs through the air hose (2) to the control box (3). Amount of venting air entering the cockpit is controlled by the CABIN VENTILATION controller (4).
  • Page 284 CONDITIONING Fig. 21-1 Cockpit Ventilation (page 1 of 3) Chapter 21-20 DISTRIBUTION Page 21-6 Effectivity: ALL 04. 05. 2021...
  • Page 285 CONDITIONING Fig. 21-1 Cockpit Ventilation (page 2 of 3) DISTRIBUTION Chapter 21-20 04. 05. 2021 Effectivity: ALL Page 21-7...
  • Page 286 CONDITIONING 1 – Ram air tunnel 5 – Ball vents 2 – Air hose NACA intake 3 – Control box VENTILATION knob 4 – Sliding window CABIN VENTILATION controller Fig. 21-1 Cockpit Ventilation (page 3 of 3) Chapter 21-20 DISTRIBUTION Page 21-8 Effectivity: ALL 04.

  • Page 287: Maintenance Practices

    CONDITIONING MAINTENANCE PRACTICES Control box For maintenance practices see Chapter 21-40. Ventilation control Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Special wrench 14 1 pc Screwdriver 5...
  • Page 288 CONDITIONING Ventilation control removal: Make sure that the ignition switch is set to OFF. Remove the engine cowlings (Chapter 71-10). Unscrew cable end fitting (1, Fig. 21-3), remove shrink tube, and unsolder thread rod (2). From the cockpit, remove the inner cable by pulling handle (12). Remove cable tie (13), unstick adhesive tape (14), pull green sleeve (11).
  • Page 289 CONDITIONING Insert the ball and simultaneously slide on the green sleeve (11, Fig. 21-3): • Push the green sleeve (11) just to first indication of minimal resistance. • Check for correct operation by pulling and pushing handle; the ball must engage with ratchet, movement must not be free. Apply two layers of textile adhesive tape (14) and lock it with cable tie (13).
  • Page 290 CONDITIONING 1 – Cable end fitting 12 – Handle 2 – Thread rod 13 – Cable tie 2.6 3 – Bowden end 14 – Textile adhesive tape 4 – Screw shackle 15 – Low nut M10 5 – Low nut M6 16 –...
  • Page 291 CONDITIONING Blowers Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 5 1 pc Wrench 10 1 pc Hex key 5 1 pc Pliers 1 pc Persons Tab.

  • Page 292: Blowers

    CONDITIONING 1 – Blower 4 – Screw M6 x 16 2 – Holder 5 – Washer Ø4.3 x 12 x 1 3 – Bolt M4x50 Self-locking nut M4 Fig. 21-4 Blower Removal / Installation Chapter 21-20 DISTRIBUTION Page 21-14 Effectivity: ALL 04.

  • Page 293: Heating

    CONDITIONING 21-40 HEATING DESCRIPTION Cockpit heating Fixed gear: The preheat air is received from the deflector (1, Fig. 21-5) installed behind the water radiator and directs through the air hose (2) to the heat exchanger (3) on the muffler to be heated. Warm air from the heat exchanger directs through the air hose (4) to the control box (5).
  • Page 294 CONDITIONING Fig. 21-5 Cockpit Heating (page 1 of 2) Chapter 21-40 HEATING Page 21-16 Effectivity: ALL 04. 05. 2021...
  • Page 295 CONDITIONING 1 – Deflector 4 – Air hose 2 – Air hose 5 – Control box 3 – Heat exchanger 6 – Controller Fig. 21-5 Cockpit Heating (page 2 of 2) HEATING Chapter 21-40 04. 05. 2021 Effectivity: ALL Page 21-17...

  • Page 296: Maintenance Practices

    CONDITIONING MAINTENANCE PRACTICES Control box Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 5 1 pc Special wrench 14 1 pc Wrench 10 1 pc Wrench 8 1 pc...

  • Page 297: Control Box

    CONDITIONING Only FG Rotax 912: Remove the heating deflector (26) (see 2.C.(1)). Remove the heat exchanger (25) (Chapter 78-10). Disconnect control cables (8; 14) from control box (1). Remove cable end fitting (19) from cable (14). Remove screw shackle (15), by removing lockwire, unscrew nut (16) and remove washers (17;...
  • Page 298 CONDITIONING Control cable for heating (8), instead of screw shackle, has a bracket (11) installed on firewall with bolt (9), washers (10; 13) and nut (12). Seal the control cables in the firewall around the bowdens with gasket sealant. Check if hoses are firmly secured and sealed and check operation of heating and ventilation flaps (fully open and fully close).
  • Page 299 CONDITIONING Fig. 21-6 Control Box Removal / Installation (page 1 of 2) HEATING Chapter 21-40 04. 05. 2021 Effectivity: ALL Page 21-21...
  • Page 300 CONDITIONING 1 – Control box 16 – Low nut M6 2 – Rectifier warm air 17 – Washer Ø6.4 x 12 x 0.5 3 – Bolt M5 x 18 (3 pc) 18 – Serrated locking washer Ø6.4 4 – Self-locking nut M5 (3 pc) 19 –...

  • Page 301: Heat Exchanger

    CONDITIONING Heat exchanger For removal / installation, see the Chapter 78-10. Heating deflector (only FG) Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 5 1 pc Hex key 5 1 pc...
  • Page 302 CONDITIONING 1 – Heating deflector 6 – Washer Ø6.4 x 18 x 1.6 2 – Air hose Ø55 x 160 Distance spinner 3 – Hose clamp Ø 40 x 60 8 – Washer Ø14.5 x 28 x 4 4 – Allen bolt M6 x 16 For information: 5 –...
  • Page 303 CONDITIONING Heating control Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Special wrench 14 1 pc Screwdriver 5 1 pc Hex key 4 1 pc Hex key 5...
  • Page 304 CONDITIONING Unscrew the nut (13), remove the washers (15; 16), bolt (12) and disconnect control cable (4) with bracket (14) from firewall. Unscrew the nut (10), remove washer (11) and pull out control cable (4) from central console. NOTE For easier removal use special tool (Fig. 21-2) and hex key inserted on control cable end from cockpit side.
  • Page 305 CONDITIONING Carry out test and check: • If all screws connections are tight. • Operation of control flap (fully open and fully close). • That no foreign objects remain in the aircraft or engine compartment. Install the engine cowlings (Chapter 71-10). 1 –...
  • Page 306 CONDITIONING This page is left blank intentionally Chapter 21-40 HEATING Page 21-28 Effectivity: ALL 04. 05. 2021...
  • Page 307 COMMUNICATIONS 23 COMMUNICATIONS CONTENTS Chapter Description Page 23-00 GENERAL ................. 3 INTRODUCTION ............... 3 TROUBLESHOOTING ............... 4 23-10 SPEECH COMMUNICATIONS ......... 5 DESCRIPTION ................5 Garmin GNC 255A NAV / COM ......... 5 Garmin GTR 225A VHF COMM Transceiver ..... 6 Funkwerk ATR833 VHF COMM Transceiver .....
  • Page 308 COMMUNICATIONS MAINTENANCE PRACTISES ..........16 PM3000 Intercom ............16 GMA 240 Intercom ............16 PM1000II Intercom ............16 PM1000 Intercom ............16 PM501 Intercom ............. 16 SPA-4S Intercom ............16 Push-To-Talk Button ............16 Audio Socket ..............19 Chapter 23 CONTENTS Page 23-2 Effectivity: ALL...

  • Page 309: General

    COMMUNICATIONS 23-00 GENERAL INTRODUCTION This chapter describes the system, individual equipment and components that provide communications inside the aircraft, mutually between aircrafts or between aircraft and ground stations. This chapter describes only the on-aircraft data about the system and components. Refer to the appropriate manufacturer's manuals for data about the equipment.

  • Page 310: Troubleshooting

    COMMUNICATIONS TROUBLESHOOTING TROUBLE POSSIBLE CAUSE REMEDY Radiostation does not No power to the Check power connections, power on radiostation breakers, and main avionic switch Faulty electrical wiring or Contact your dealer to connection perform electrical system test No Nav audio * Output disabled or set to a Contact dealer low level...

  • Page 311: Speech Communications

    COMMUNICATIONS 23-10 SPEECH COMMUNICATIONS DESCRIPTION Garmin GNC 255A NAV / COM Garmin GNC 255A NAV / COMM (Fig. 23-1) consists of transmitter / receiver for VHF communication (COM) and receiver for navigation information (NAV). These are combined with operating controls in one unit. The COM section of the GNC 255A NAV / COMM operates in the aviation voice band, from 118.000 to 136.975 MHz, in 25 kHz and 8.33 kHz steps.

  • Page 312: Garmin Gtr 225A Vhf Comm Transceiver

    COMMUNICATIONS Garmin GTR 225A VHF COMM Transceiver The GTR 225 COM Radio series provides a powerful VHF communications transceiver. In addition to the traditional COM features, the GTR 225 series incorporates workload-reducing functions. The GTR 225 series monitors the standby COM frequencies and stores the user’s most-used frequencies. The GTR 225 (10 watt) COM radio operates in the aviation voice band, from 118.000 to 136.975 MHz, in 25 kHz steps (default).

  • Page 313: Funkwerk Atr833 Vhf Comm Transceiver

    COMMUNICATIONS Funkwerk ATR833 VHF COMM Transceiver Funkwerk ATR833 provide VHF communication transceiver with 6W output power in 57 mm format. Frequency range 118,000 to 136,975 MHz. 4 microphone inputs (2x standard, 2x dynamic). Dual-watch technology, simultaneous monitoring of two frequencies. All pilot controls and displays are presented on the Funkwerk ATR833 front panel as indicated in Figure 23-3.

  • Page 314: Antennas

    COMMUNICATIONS Antennas Figure 23-4 shows the antenna locations. VHF COMM antenna AV-17 / CI-122 may be installed above the upper or lower skin of fuselage. VHF COMM antenna SP-2000 is installed inside of fin and is maintenance free. 1 – AV-17 / CI-122 antenna 2 –...

  • Page 315: Maintenance Practises

    COMMUNICATIONS MAINTENANCE PRACTISES Garmin GNC 255A NAV/COMM For removal / installation procedures refer to Chapter 39-10. Garmin GTR 225A VHF COMM Transceiver For removal / installation procedures refer to Chapter 39-10. Funkwerk ATR833 VHF COMM Transceiver For removal / installation procedures refer to Chapter 39-10. Antennas Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher.
  • Page 316 COMMUNICATIONS NOTE Fig. 23-5 shows installation of VHF COMM antenna AV-17 / CI-122 on the upper skin of fuselage. Installation on the lower skin of fuselage is analogic. 1 – VHF COMM antenna 5 – Washer 4.3 x 12 x 1 2 –...

  • Page 317: Audio Integrating

    COMMUNICATIONS 23-50 AUDIO INTEGRATING DESCRIPTION PM3000 Intercom PM3000 is a voice-activated intercom that enables to interconnect up to 4 headsets. It is equipped with setting volume and level of switching the intercom (Fig. 23-6). For transmitting via VHF transceiver it is necessary to press down and hold the button on the control stick.

  • Page 318: Garmin Gma 240 Audio Panel

    COMMUNICATIONS Garmin GMA 240 Audio Panel The Garmin GMA 240 is a headphones only audio control panel. Pushbutton keys control audio selection of COM, NAV, telephone (TEL), and intercom. Two AUX inputs are available for additional avionics or audio devices. LED annunciators indicate when a key function is selected.

  • Page 319: Pm1000Ii Intercom

    COMMUNICATIONS PM1000II Intercom The PM1000II is a 4-place, panel mounted intercom with individual volume and squelch controls for the pilot and copilot. The copilot's squelch control adjusts the trip level of the copilot and passengers (Fig. 23-8). Fig. 23-8 PM1000II Intercom NOTE Refer to the PM1000II 4-Place, Panel Mounted Intercom Operator's and Installation Manual Part Number 11920 (with Crew) and 11922...

  • Page 320: Pm501 Intercom

    COMMUNICATIONS PM501 Intercom The PM501 is a 4-place, panel-mount intercom with individual output amplifiers for the pilot, copilot, and passengers 1 & 2. The VOX (Voice Activated Squelch) circuit prevents mic audio from getting through the intercom until someone speaks and automatically opens the circuit. The volume control adjusts the level for all headsets and functions as a PUSH-ON/ PUSH-OFF power switch (Fig.

  • Page 321: Push-To-Talk Button

    COMMUNICATIONS Push-To-Talk Button Push-to-talk buttons are located on the upper area of both control sticks. Buttons can be plastic or metal design. Pushing of the push-to-talk button will activate radio transmitting. Audio Sockets The audio sockets are used for connecting the headsets to intercom. They are located on the top of central tunnel rear section behind the backrest.
  • Page 322 COMMUNICATIONS MAINTENANCE PRACTISES PM3000 Intercom For removal / installation procedures refer to Chapter 39-10. GMA 240 Intercom For removal / installation procedures refer to Chapter 39-10. PM1000II Intercom For removal / installation procedures refer to Chapter 39-10. PM1000 Intercom For removal / installation procedures refer to Chapter 39-10. PM501 Intercom For removal / installation procedures refer to Chapter 39-10.
  • Page 323 COMMUNICATIONS 1 – Push-To-Talk (PTT) button 3 – Foam handle 2 – Wires 4 – Wooden / plastic handle Fig. 23-12 Push-To-Talk button Removal / Installation PTT button (metal design) removal: Set MASTER SWITCH to OFF position. Using small flat screwdriver, hook edge of cover (6, Fig. 23-13) and pull it from stick handle (3 or 4).
  • Page 324 COMMUNICATIONS 1 – Push-To-Talk (PTT) button 4 – Wooden / plastic handle 2 – Wires 5 – Nut 3 – Foam handle 6 – Cover Fig. 23-13 Push-To-Talk button Removal / Installation Chapter 23-50 AUDIO INTEGRATING Page 23-18 Effectivity: ALL 14.
  • Page 325 COMMUNICATIONS Audio Socket Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Flat screwdriver 1 pc Wrench 13 1 pc Shrink tube 3 pcs Persons Tab.
  • Page 326 COMMUNICATIONS NOTE Headphone sockets have larger diameter than microphone sockets and are located on outer side of socket holder. 1 – Socket holder 5 – Insulating back washer 2 – Headphone socket 6 – Nut 3 – Microphone socket 7 – Screw M4 4 –...
  • Page 327 ELECTRICAL POWER 24 ELECTRICAL POWER CONTENTS Chapter Description Page 24-00 GENERAL ................. 3 INTRODUCTION ............... 3 24-30 DC GENERATION ............7 DESCRIPTION ................7 Generator system .............. 7 Battery ................7 Backup battery SV-BAT-320 ..........7 Backup battery Dynon D100 ..........7 MAINTENANCE PRACTICES ...........
  • Page 328 ELECTRICAL POWER Switches ................. 29 Trim switch on pedestal panel ........29 Chapter 24 CONTENTS Page 24-2 Effectivity: ALL 04. 05. 2021...

  • Page 329: General

    ELECTRICAL POWER 24-00 GENERAL INTRODUCTION The information in this chapter covers DC generation, external power, and electrical load distribution. The aircraft is equipped with a dual-wire type electrical system. The system has two sources of electrical power - generator and 12 V battery. A generator integrated into the engine and connected to a rectifier/voltage regulator supplies power to the electrical system.
  • Page 330 ELECTRICAL POWER *If installed, **RG only Fig. 24-2 Simplified Schematic Diagram Flymap L Chapter 24-00 GENERAL Page 24-4 Effectivity: ALL 04. 05. 2021...
  • Page 331 ELECTRICAL POWER *If installed Fig. 24-3 Simplified Schematic Diagram Trutrak GENERAL Chapter 24-00 04. 05. 2021 Effectivity: ALL Page 24-5...
  • Page 332 ELECTRICAL POWER *If installed, **RG only Fig. 24-4 Simplified Schematic Diagram Dynon D100 / EMS-D120 Chapter 24-00 GENERAL Page 24-6 Effectivity: ALL 04. 05. 2021...

  • Page 333: Dc Generation

    ELECTRICAL POWER 24-30 DC GENERATION DESCRIPTION Generator system The generator system consists of the following components: • Generator / Auxiliary generator • Voltage regulator • Charging fuse • Low voltage warning light • Alternator (if installed) The maintenance free AC generator is integrated into the engine and supplies power to the equipment during normal operation.

  • Page 334: Maintenance Practices

    ELECTRICAL POWER MAINTENANCE PRACTICES Generator Refer to the Maintenance Manual for Engine Type 912/914 Series, Ref. No.: MML-912/914 for maintenance practices information. Voltage regulator Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY...

  • Page 335: Voltage Regulator

    ELECTRICAL POWER 1 – Voltage regulator 5 – Washer Ø6.4 x 12 x 1.6 2 – Bolt M6 x 25 6 – Ground wire 3 – Self-locking nut M6 7 - Connector 4 – Washer Ø6.4 x 18 x 1.6 8 –...

  • Page 336: Battery 17 Ah

    ELECTRICAL POWER Battery 17 Ah / 20 Ah Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Wrench 8 1 pc Persons Tab.
  • Page 337 ELECTRICAL POWER Fig. 24-6 Battery Removal / Installation (page 1 of 2) DC GENERATION Chapter 24-30 04. 05. 2021 Effectivity: ALL Page 24-11...
  • Page 338 ELECTRICAL POWER 1 – Battery 10 – Washer Ø6.4 x 20 x 6 2 – Econet casing 11 – Self-locking nut M5 3 – Cover 12 – Wires (-) 4 – Bolt M5 x 15 13 – Negative terminal 5 – Bolt M5 x 18 14 –...

  • Page 339: Battery 10 Ah

    ELECTRICAL POWER Battery 10 Ah Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Wrench 8 1 pc Persons Tab. 24-3 Recommended tools, materials, persons and documentation Battery removal: Make sure that the IGNITION switches are set to OFF.
  • Page 340 ELECTRICAL POWER Fig. 24-7 Battery Removal / Installation (page 1 of 2) Chapter 24-30 DC GENERATION Page 24-14 Effectivity: ALL 04. 05. 2021...
  • Page 341 ELECTRICAL POWER 1 – Battery 10 – Washer Ø6.4 x 20 x 6 2 – Econet casing 11 – Self-locking nut M5 3 – Cover 12 – Wires (-) 4 – Bolt M6 x 10 13 – Negative terminal 5 – Bolt M5 x 18 14 –...
  • Page 342 ELECTRICAL POWER Connect wires (12) to negative terminal (13) by means of screw (4) and washer (16). Install the engine cowlings (Chapter 71-10). Fig. 24-8 Battery Removal / Installation (page 1 of 2) Chapter 24-30 DC GENERATION Page 24-16 Effectivity: ALL 04.

  • Page 343: Backup Battery Sv-Bat-320

    ELECTRICAL POWER 1 – Battery 10 – Washer Ø6.4 x 20 x 6 2 – Econet casing 11 – Self-locking nut M5 3 – - 12 – Wires (-) 4 – Screw M6 x 10 13 – Negative terminal 5 – Bolt M5 x 18 14 –...
  • Page 344 ELECTRICAL POWER 1 – Left backup battery 6 – Washer Ø4.3 x 12 x 1 2 – Right backup battery For information: 3 – Connector 7 – Left instrument floor 4 – Bolt M4 x 12 8 – Right instrument floor 5 –...

  • Page 345: Backup Battery For Dynon D100

    ELECTRICAL POWER Backup battery for Dynon D100 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Philips screwdriver 1 pc Persons Tab. 24-6 Recommended tools, materials, persons and documentation Backup battery removal: Remove the instrument panel cover (Chapter 39-10).
  • Page 346 ELECTRICAL POWER 1 – Backup battery 2 – Cover 3 – Screws Fig. 24-10 Backup Battery for Dynon D100 Removal / Installation Alternator Refer to the Maintenance Manual for Engine Type 912 Series, Ref. No.: MML-912 for maintenance practices information. Chapter 24-30 DC GENERATION Page 24-20...
  • Page 347 ELECTRICAL POWER Auxiliary generator Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Wrench 8 1 pc Persons Tab. 24-7 Recommended tools, materials, persons and documentation Auxiliary generator removal: Make sure that the IGNITION switches are set to OFF.

  • Page 348: Auxiliary Generator

    ELECTRICAL POWER 1 – Auxiliary generator 4 – Lock washer Ø6.4 2 – Flange 11 – Hex nut M6 3 – Gasket Fig. 24-11 Auxiliary Generator Removal / Installation Chapter 24-30 DC GENERATION Page 24-22 Effectivity: ALL 04. 05. 2021...

  • Page 349: External Power

    ELECTRICAL POWER 24-40 EXTERNAL POWER DESCRIPTION The aircraft may be equipped with the external power source socket, which is located in the left side of the cabin, bellow the instrument panel. External power source is intended for engine starting, maintenance procedures requiring reliable power for an extended period and for battery charging.
  • Page 350 ELECTRICAL POWER 1 – External power socket 5 – Cable 2 – Bolt M5 x 18 For information: 3 – Self-locking nut M5 6 – Bracket 4 – Washer Ø5.3 x 15 x 1.2 Fig. 24-12 External Power Socket Removal / Installation Chapter 24-40 EXTERNAL POWER Page 24-24...

  • Page 351: Dc Electrical Load Distribution

    ELECTRICAL POWER 24-60 DC ELECTRICAL LOAD DISTRIBUTION DESCRIPTION The electrical power from the generator and the battery is supplied via 12 V bus, switches and circuit breakers to the individual electrical equipment. Switches are installed mostly at the lower edge of instrument panel’s left side. Circuit breakers are installed mostly at the lower edge of instrument panel’s right side.
  • Page 352 ELECTRICAL POWER Alternator (if installed) is activated by separate ALTERNATOR switch and is connected through ALTERNATOR circuit breaker to the MASTER SWITCH and then to the battery. RG only: Landing gear controller is connected through the GEAR SIGNAL circuit breaker to the MASTER SWITCH. Gear legs sensors are connected directly to landing gear controller and legs position is indicated by check lamps.
  • Page 353 ELECTRICAL POWER MARKING PROTECTED INSTRUMENT VALUE (A) TRIM Pitch trim motor ENGINE FIRE Engine fire warning STALL Stall warning system AVIONICS Avionics relay FUEL PUMP Fuel pump GNC 255A (COMM), GNC 225A (COMM) COMM ATR 833 GTX-328 XPDR TRT-800H LH D1000 LH Dynon SkyView SV-D1000 RH D1000 RH Dynon SkyView SV-D1000...
  • Page 354 ELECTRICAL POWER MARKING PROTECTED INSTRUMENT VALUE (A) Autopilot sys. (Dynon SV-32 / SV-42) AUTOPILOT Autopilot sys. (TRUTRAK DSB-B, FLYMAP) FLYMAP L1 Flymap L 1 FLYMAP L2 Flymap L 2 FLYMAP L3 Flymap L 3 GPS system EFIS EFIS display D100 Dynon D100 D120 Dynon EMS-D120...

  • Page 355: Maintenance Practices

    ELECTRICAL POWER MAINTENANCE PRACTICES 12 V socket For removal / installation, see the Chapter 39-10. Circuit breakers ETA 106-P10 For removal / installation, see the Chapter 39-10. Switches For removal / installation, see the Chapter 39-10. Trim switch on pedestal panel Type of maintenance: Line Personnel qualification:...
  • Page 356 ELECTRICAL POWER 1 – Trim switch 3 – Pedestal panel 2 – Wires Fig. 24-13 Trim Switches Removal / Installation Chapter 24-60 DC ELECTRICAL LOAD DISTRIBUTION Page 24-30 Effectivity: ALL 04. 05. 2021...
  • Page 357 EQUIPMENT/ FURNISHINGS 25 EQUIPMENT / FURNISHING CONTENTS Chapter Description Page 25-00 GENERAL ................. 3 INTRODUCTION ............... 3 25-10 FLIGHT COMPARTMENT ..........5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 6 Seats ................. 6 Safety harnesses ............... 8 25-50 CARGO COMPARTMENTS ..........11 DESCRIPTION ................
  • Page 358 EQUIPMENT/ FURNISHINGS This page is left blank intentionally Chapter 25 CONTENTS Page 25-2 Effectivity: ALL 14. 05. 2020...

  • Page 359: General

    EQUIPMENT/ FURNISHINGS 25-00 GENERAL INTRODUCTION This chapter describes equipment and furnishing in the flight compartment. Chapter 25-10 includes the pilot and co-pilot seats, safety harnesses and safety belts. Chapter 25-60 gives the data for the Emergency Parachute System (EPS) and Emergency Locator Transmitter (ELT).
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  • Page 361: Flight Compartment

    EQUIPMENT/ FURNISHINGS 25-10 FLIGHT COMPARTMENT DESCRIPTION Pilot and co-pilot's seats are integral part of interior arranged side-by-side and consist of removable laminate seats (2, Fig. 25-1) and backrest, which is bonded with central tunnel and fuselage. Seats are covered with upholstery seats (1). Seats are equipped with 4-point safety harnesses (3).
  • Page 362 EQUIPMENT/ FURNISHINGS MAINTENANCE PRACTICES Seats Described is procedure for removal of left laminated seat. Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 10 1 pc Persons Tab.
  • Page 363 EQUIPMENT/ FURNISHINGS 1 – Upholstery seat 3 – Bolt M5 x 12 2 – Laminated seat Fig. 25-2 Illustrative Seat Removal / Installation FLIGHT COMPARMENT Chapter 25-10 14. 05. 2020 Effectivity: ALL Page 25-7...
  • Page 364 EQUIPMENT/ FURNISHINGS Safety harnesses Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 13 2 pcs Persons Tab. 25-2 Recommended tools, materials, persons and documentation Safety harness removal: Remove the seat upholstery (see par.
  • Page 365 EQUIPMENT/ FURNISHINGS 1 – Bolt M8 x 32 4 – Self-locking nut M8 2 – Shoulder belt bracket 5 – Lap belt bracket ø ø 3 – Washer 6 – Washer 8.4 x 24 x 2 20 x 8 x 4 Fig.
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  • Page 367: Cargo Compartments

    EQUIPMENT/ FURNISHINGS 25-50 CARGO COMPARTMENTS DESCRIPTION The baggage compartment (1) is situated between backrest and baggage bulkhead. Central tunnel passes through the baggage compartment and divides it in two sections. Each baggage compartment has attaching points (2) to which the baggage can be restrained (Fig.
  • Page 368 EQUIPMENT/ FURNISHINGS This page is left blank intentionally Chapter 25-50 CARGO COMPARMENTS Page 25-12 Effectivity: ALL 14. 05. 2020...

  • Page 369: Description

    EQUIPMENT/ FURNISHINGS 25-60 EMERGENCY DESCRIPTION The aircraft is equipped with emergency parachute system (EPS) MAGNUM 601 or 501from the company STRATOS 07 spol. s r. o. Parachute container (1, Fig. 25-5) is located behind instrument panel and is attached to the board. Two main straps (3) are attached to the stiffened areas at firewall and stabilizing strap is attached to the steel cable (5) (bonded in the structure of right fuselage shell).
  • Page 370 EQUIPMENT/ FURNISHINGS The aircraft may be equipped with ELT KANNAD 406 AF COMPACT or Ameri-King AK-451 Series. The KANNAD 406 AF COMPACT is a FAA TSO’d approved, EASA ETSO’d approved, 406 MHz, Automatic Fixed (AF) Emergency Locator Transmitter. The ELT KANNAD 406 AF COMPACT can be activated either automatically when the crash occurs (by a shock sensor) or manually (by a switch on the transmitter itself or on a remote control unit on the instrument panel).

  • Page 371: Maintenance Practices

    EQUIPMENT/ FURNISHINGS MAINTENANCE PRACTICES Emergency parachute system Magnum 601 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 22 1 pc Wrench 8 1 pc Socket set 10, 17 1 pc Hex key 3...
  • Page 372 EQUIPMENT/ FURNISHINGS From engine compartment unscrew the nuts (26), remove washers (25) and pull out the U bolts (10) from interior. Cut cable ties (28) fixing the main straps (5; 7) and stabilizing strap (6) and remove the straps (5; 6; 7) from the aircraft. Remove cable ties (27) securing the bowden from actuator to rocket.
  • Page 373 EQUIPMENT/ FURNISHINGS WARNING DURING INCORRECT MANIPULATION WITH UNLOCKED ACTUATOR THERE IS A DANGER ROCKET ACTIVATION! AVOID ROUGH MANIPULATION IF ACTUATOR OR BOWDEN HAS JAMMED DURING INSTALLATION! Unscrew bolts (21) and unscrew lateral actuator handle (12). Unlock actuator (11) by removing of lock (19) and carefully insert handle to central instrument panel from the rear side;...
  • Page 374 EQUIPMENT/ FURNISHINGS Secure looped strap (5) to rescue system board with one cable tie (28). Connect second U bolt (10) to second strap loop (7); secure loop with cable tie (28). Attach U bolt with strap to right side of firewall, put washers (25) and tighten nuts (26).
  • Page 375 EQUIPMENT/ FURNISHINGS Fixed gear version Fig. 25-7 Emergency Parachute System Magnum 601 Removal / Installation (page 1 of 2) EMERGENCY Chapter 25-60 14. 05. 2020 Effectivity: ALL Page 25-19...
  • Page 376 EQUIPMENT/ FURNISHINGS Retractable gear version 1 – 13 – Actuator protector 25 – Washer ø10.5 x 30 x 2.4 Parachute container 2 – 14 – Cable of rocket 26 – Self-locking nut M10 Rocket 3 – 15 – Parachute cable 27 –...
  • Page 377 EQUIPMENT/ FURNISHINGS EPS actuator (side installation version) removal: Make sure that the IGNITION switches are set to OFF. WARNING DURING INCORRECT MANIPULATION WITH UNLOCKED ACTUATOR THERE IS A DANGER ROCKET ACTIVATION! AVOID ROUGH MANIPULATION IF ACTUATOR OR BOWDEN HAS JAMMED DURING REMOVING! Cut seal and open actuator protector (13, Fig.
  • Page 378 EQUIPMENT/ FURNISHINGS 1 – 8 – Hex bolt M5 x 16 Actuator 2 – 9 – Spring Console of actuator EPS 3 – 10 – Pin ø 5 Bolt 4 – 11 – Cotter pin 1.2 x 10 Washer 5 – 12 –...

  • Page 379: Emergency Locator Transmitter

    EQUIPMENT/ FURNISHINGS Emergency locator transmitter Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 3/4 in 1 pc Wrench 5.4 1 pc Philips screwdriver 1 pc Persons Tab.
  • Page 380 EQUIPMENT/ FURNISHINGS ELT AMERI-KING AK-451 removal: Set switch on the unit to OFF position. Disconnect connectors (4, Fig. 25-10) from the unit. Unlock the toggle latch (3) on the bracket (2). Remove the unit (1) from the bracket (2). ELT AMERI-KING AK-451 installation: Install the unit (1, Fig.
  • Page 381 EQUIPMENT/ FURNISHINGS Carry out an operational test - refer to the Installation and Operation Manual ELT KANNAD 406 AF-COMPACT 406 AF-COMPACT (ER), Doc. No. DOC08038F (Revision 05 or later), or Operation Manual AMERI-KING AK-451, Doc. No. IM-451 (Revision NC-4.1e or later). ELT KANNAD 406 AF COMPACT battery replacement: The transmitter battery expiration date is fixed at 6 years after manufacturing.
  • Page 382 EQUIPMENT/ FURNISHINGS 1 – ELT unit 4 – Connectors 2 – Mounting bracket 5 – Central tunnel 3 – T oggle latch Fig. 25-9 ELT KANNAD 406 AF COMPACT Removal / Installation 1 – ELT unit 4 – Connectors 2 – Mounting bracket 5 –...
  • Page 383 EQUIPMENT/ FURNISHINGS 1 – ELT antenna For information: 2 – Connector 5 – Bracket 3 – Nut 6 – Foam block 4 – Serrated washer Fig. 25-11 ELT Antenna Removal / Installation EMERGENCY Chapter 25-60 14. 05. 2020 Effectivity: ALL Page 25-27...
  • Page 384 EQUIPMENT/ FURNISHINGS This page is left blank intentionally Chapter 25-60 EMERGENCY Page 25-28 Effectivity: ALL 14. 05. 2020...
  • Page 385 FLIGHT CONTROLS 27 FLIGHT CONTROLS CONTENTS Chapter Description Page 27-00 GENERAL ................. 3 INTRODUCTION ............... 3 MAINTENANCE PRACTICES ........... 3 General principles ............. 3 ADJUSTMENT / TEST ............... 4 Values for deflection adjustment .......... 4 INSPECTION / CHECK ............. 5 Check of plays in flight controls .........
  • Page 386 FLIGHT CONTROLS Electrical pitch trim system with electrical indicating ..54 Electrical pitch trim control ..........58 27-50 FLAPS ................61 DESCRIPTION ................ 61 MAINTENANCE PRACTICES ..........63 Flap control system FG / RG (manually) ......63 Flap control system (electrical) ........68 Pedestal panel ..............

  • Page 387: General

    FLIGHT CONTROLS 27-00 GENERAL INTRODUCTION This chapter describes operation and the adjustment of the flight controls. It also describes the assembly of the flight controls. Refer to the related chapter for the data on a specified system. The aircraft is equipped with dual control systems for elevator, ailerons and rudder. MAINTENANCE PRACTICES General principles WARNING...

  • Page 388: Adjustment / Test

    FLIGHT CONTROLS unscrewing and dropping out the nut during operation. Use the same principle also when securing the nuts with locking pins or cotter pins. After installing control elements, always check them for free motion without any jamming and verify proper safety of all nuts and bolts. Prior to installing new push-pull rods, adjust their lengths to correspond to their nominal sizes.

  • Page 389: Inspection / Check

    FLIGHT CONTROLS INSPECTION / CHECK Check of plays in flight controls At the aircraft operation the flight control and elements become worn-out under the influence of loading, vibrations etc. This wear is shown by increase of plays. When the maximum allowable operating play is reached, the worn-out parts (bearings, bolts, pins, guides etc.) must be replaced.
  • Page 390 FLIGHT CONTROLS This page is left blank intentionally Chapter 27-00 GENERAL Page 27-6 Effectivity: ALL 14. 05. 2020...
  • Page 391 FLIGHT CONTROLS 27-10 AILERON DESCRIPTION Ailerons are controlled through the control sticks, attached to the control stick's torsion tube (7, Fig. 27-1). Movement from control sticks is transferred to the ailerons through the push-pull rod 1 (1), push-pull rod 2 (2), bellcrank (3) and push-pull rod 3 (4).
  • Page 392 FLIGHT CONTROLS 1 – Push-pull rod 1 5 – Aileron root rib 2 – Push-pull rod 2 6 – Guide bearing 3 – Bellcrank 7 – Torsion tube 4 – Push-pull rod 3 8 – Stop Fig. 27-1 Aileron Control System Chapter 27-10 AILERON Page 27-8...
  • Page 393 FLIGHT CONTROLS MAINTENANCE PRACTICES Aileron control Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Special wrench 10 (see Fig. 27-2) 1 pc Wrench 9 1 pc...

  • Page 394: Aileron

    FLIGHT CONTROLS Remove the bellcrank (4) from bracket (26), by removing nut (13), washers (15; 6) and bolt (11). Aileron control installation: Thoroughly clean and lubricate all the aileron movable points and other movable parts with Vaseline before each assembling (Chapter 12-20).
  • Page 395 FLIGHT CONTROLS Carry out test and check: • That the castle nuts are secured with cotter pins. • If all bolt connections are tight. • That all lock nuts are tight. • Free movement of aileron control system. • Alignment of the trailing edge of aileron and wing. •...
  • Page 396 FLIGHT CONTROLS Fig. 27-3 Aileron Control Removal / Installation (page 1 of 2) Chapter 27-10 AILERON Page 27-12 Effectivity: ALL 14. 05. 2020...
  • Page 397 FLIGHT CONTROLS 1 – 14 – Castle nut M6 Push-rod 1 2 – 15 – Washer ø6.4 x 12 x 1.6 Push-rod 2 3 – 16 – Serrated locking washer ø6.4 Push-rod 3 4 – 17 – Washer ø6.4 x 12 x 0.5 Bellcrank 5 –...
  • Page 398 FLIGHT CONTROLS Torsion tube with control sticks Torsion tube with control sticks removal: Remove laminated seats (Chapter 25-10). Remove pedestal panel (Chapter 27-50, 2.B.(1)). Disconnect ailerons push-pull rods (1, Fig. 27-3) from both control sticks (21) by removing nut (13), washer (15) and bolt (8). Disconnect elevator control push-pull rod 1 (1, Fig.
  • Page 399 FLIGHT CONTROLS Torsion tube with control sticks installation: Before assembling check push rods for cracks and condition of rivets. Check parallel alignment of swivel bearings; on new push rods, release lock nuts. Assemble connecting push rod (11, Fig. 27-4) with control sticks (2;...
  • Page 400 FLIGHT CONTROLS Fig. 27-4 Torsion Tube with Control Sticks Removal / Installation (page 1 of 2) Chapter 27-10 AILERON Page 27-16 Effectivity: ALL 14. 05. 2020...
  • Page 401 FLIGHT CONTROLS 1 – 15 – Torsion tube Bolt M6x46 2 – 16 – Left control stick Bolt M6x22 3 – 17 – Bolt M5x8 Bolt M6x16 18 – 4 – Bolt M4x20 Left handle 19 – 5 – Bolt M6x16 Push-To-Talk (PTT) Button 20 –...
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  • Page 403: Description

    FLIGHT CONTROLS 27-20 RUDDER DESCRIPTION The rudder is controlled by foot control pedals. The position of pedals for pilot and co-pilot can be remotely adjustable. The rudder is controlled through steel cables. Nose gear steering controlled through push-pull rods version) or through control bowdens (RG version).
  • Page 404 FLIGHT CONTROLS 1 – Torsion tube Turnbuckle 2 – Holder Nose landing gear leg 3 – Pedal Push-pull rod (FG only) 4 – Control cables Control handle 5 – Rudder root lever 10 - Control bowdens (RG only) Fig. 27-5 Rudder Control System (Illustrative figure) Chapter 27-20 RUDDER Page 27-20...
  • Page 405 FLIGHT CONTROLS MAINTENANCE PRACTICES Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Wrench 9 1 pc Hex key 5 1 pc Nicopress tool 1 pc Steel wire cutter...
  • Page 406 FLIGHT CONTROLS Control cables FG Control cables FG removal: On both ends of steel cable (1, Fig. 27-7), remove nuts (11; 12), washers (9; 10) bolts (6; 7) and distance tubes (15; 16); cut steel cable (1) and pull it out. Remove second steel cable (1).
  • Page 407 FLIGHT CONTROLS Fig. 27-6 Straighten of Steel Cable Disconnect steel cable (1, Fig. 27-7) with sleeve (2) and thimble (3) from rudder operating lever by removing bolt (7). NOTE Take care to not move positions of items (1; 2; 3) during removal of bolt (7).
  • Page 408 FLIGHT CONTROLS Adjustment / test - rudder deflections: Deflections of rudder are mentioned in Tab. 27-5. These deflections are not adjustable. The neutral position of the rudder can be adjusted. CONTROL SURFACE DEFLECTIONS Distance measurement point Control surface Left Right from the point of rotation 25 ±2°...

  • Page 409: Control Cables Fg

    FLIGHT CONTROLS Control cables RG Control cables RG removal: Disconnect the both springs (20, Fig. 27-7) and steel cables (1) from the torsion tubes by removing nuts (12), washers (19) and distance tubes (16, 17). Remove the springs (20). Disconnect the steel cables (1) from the rudder by removing nuts (12), washers (9), bolts (7) and distance tubes (16).
  • Page 410 FLIGHT CONTROLS Press the sleeve (2) with Nicopress tool at 3 points, cut unnecessary end of steel cable (1) and shrink the shrink tube on the sleeve (2). (m) Make the eye on the second steel cable (1) by the same method. Connect control cable eyes (1) to the rudder operating levers, using distance tubes (16), bolts (7), washers (9) and nuts (12).
  • Page 411 FLIGHT CONTROLS Fig. 27-7 Control Cable Removal / Installation (1 of 2) RUDDER Chapter 27-20 14. 05. 2020 Effectivity: ALL Page 27-27...
  • Page 412 FLIGHT CONTROLS 1 – Control cable ø3.2 11 - Self-locking nut M5 2 – Sleeve 3.0-3.2 12 - Self-locking nut M6 3 – Thimble 3.1-4.0 13 - Castle nut M6 4 – 14a - Cotter pin ø1.6 x 25 Turnbuckle assembly 5a –...

  • Page 413: Remote Control Of Pedals Fg / Rg

    FLIGHT CONTROLS Remote control of pedals FG / RG Remote control of pedals FG / RG removal: Remove spiral hoses (14, Fig. 27-8) and cable ties. Remove the nuts (8; 12), washers (6; 7), distance tube (13) and pull out thread rod (11) with handle (10). Pull out inner cables (2) and bowdens (1).
  • Page 414 FLIGHT CONTROLS 1 – Bowden 10 - Black handle 2 – Inner cable ø1.2 11 - Thread rod M5 x 42 3 – Screw shackle 12 - Nut M5 4 – Nut M6 Low 13 - Distance tube 5 – Serrated locking washer ø6.4 14 - Spiral hose ø1 6 –...

  • Page 415: Foot Control Fg

    FLIGHT CONTROLS Foot control FG Foot control FG removal: Remove control cables (see 2.A.(1)). Remove remote control of pedals (see 2.C.(1)). Remove steering push rods (Chapter 32-50). Remove foot control, by unscrewing the nuts (13, Fig. 27-9) and removing the washers (15). Pull out consoles (3;...
  • Page 416 FLIGHT CONTROLS The inner consoles (4) have elliptical holes and have direction out. Outer consoles (3) have direction in. Connect bronze bushing (5) with console (4), by using bolt (11), washer (15) and nut (13). Put foot control on screws laminated in floor; put washers (15) and tighten nuts (13).

  • Page 417: Foot Control Rg

    FLIGHT CONTROLS Foot control RG Foot control RG removal: Remove control cables (see 2.B.(1)). Remove remote control of pedals (see 2.C.(1)). Remove foot control bowdens (Chapter 32-50). Remove foot control, by unscrewing the nuts (13, Fig. 27-9) and removing the washers (22, 23), bolts (25) and pads (24). Pull out consoles (3;...
  • Page 418 FLIGHT CONTROLS NOTE The inner consoles (4) have elliptical holes and have direction out. Outer consoles (3) have direction in. Connect bronze bushing (5) with console (4), by using bolt (11), washer (15) and nut (13). Put foot control with pads (24) on holes in floor; insert bolts (25) with washers (23, 22) and tighten it with nuts (13).
  • Page 419 FLIGHT CONTROLS Fig. 27-9 Foot Control Removal / Installation (page 1 of 3) RUDDER Chapter 27-20 14. 05. 2020 Effectivity: ALL Page 27-35...
  • Page 420 FLIGHT CONTROLS Fig. 27-9 Foot Control Removal / Installation (page 2 of 3) Chapter 27-20 RUDDER Page 27-36 Effectivity: ALL 14. 05. 2020...
  • Page 421 FLIGHT CONTROLS Torsion tube R 14a - Cotter pin 2 x 16 Torsion tube L 14b - Self-locking nut M8 15 - Washer ø6.4 x 12 x 1.6 Outer console 16 - Washer ø8.4 x 16 x 1.6 Inner console Bronze bushing 17 - Left lever spring Pedal LL...
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  • Page 423: Description

    FLIGHT CONTROLS 27-30 ELEVATOR AND PITCH TRIM DESCRIPTION Both control sticks (1, Fig. 27-10) are fitted with bearings, attached to the control stick's torsion tube (2) and linked inside of torsion tube with connecting push-pull rod (3). Torsion tube turns in sliding / balling bearings (4) which are attached to the central section main spar.
  • Page 424 FLIGHT CONTROLS Control stick Push-pull rod 3 Torsion tube 10 - Elevator lever Push-pull rod 11 - Elevator root hinge Sliding bearing 12 - Aft stop Push-pull rod 1 13 - Trim spring Two-armed lever 14 - Trim lever Push-pull rod 2 15 - Adjustable push-pull rod Support lever 16 - Connecting push-pull rod...

  • Page 425: Maintenance Practices

    FLIGHT CONTROLS MAINTENANCE PRACTICES Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Wrench 9 1 pc Wrench 8 2 pcs Wrench 7 2 pcs Hex key 5...
  • Page 426 FLIGHT CONTROLS Disconnect push rod (1) from torsion tube (21), by removing nut (16), washer (12) and bolt (11). Remove the root hinge (4), by removing split pin (19), nut (18), washers (12; 13) and bolt (10). Remove support lever (5), by removing split pin (19), nut (18), washer (12) and bolt (8).
  • Page 427 FLIGHT CONTROLS Connect push rod (1) to torsion tube (21), using bolt (11), washer (12) and nut (16). If using new push rod (1): • Replace washer (14) and fully screw bearing ends (20) and tighten locking nuts (17). • Pay attention to parallel alignment of bearing ends (20). •...
  • Page 428 FLIGHT CONTROLS Unfix elevator and keep in neutral position. Put protractor on the trailing edge of elevator. Set the protractor to 0° - starting value of measuring. Check deflection values according to the Tab. 27-7. If deflections are not within range listed in Tab. 27-7, screw stop bolts (25;...
  • Page 429 FLIGHT CONTROLS Fig. 27-11 Push Rods and Levers Removal / Installation (page 1 of 2) ELEVATOR AND PITCH TRIM Chapter 27-30 14. 05. 2020 Effectivity: ALL Page 27-45...
  • Page 430 FLIGHT CONTROLS 1 – 14 – Serrated locking washer ø6.4 Push rod 2 – 15 – Tab washer ø6.4 Push rod 3 – 16 – Self-locking nut M6 Push rod 4 – 17 – Nut M6 Root hinge 5 – 18 –...

  • Page 431: Manual Pitch Trim System

    FLIGHT CONTROLS Manual pitch trim system Pitch trim system removal: Remove pedestal panel (Chapter 27-50, 2.C.(1)). Disconnect trim system from torsion tube (16, Fig. 27-12), by removing nut (13), washers (11) and bolt (8). Disconnect trim control (3) from central tunnel, by removing nut (13), washers (10) and bolt (7).
  • Page 432 FLIGHT CONTROLS Fig. 27-12 Manual Trim System Removal / Installation (page 1 of 2) Chapter 27-30 ELEVATOR AND PITCH TRIM Page 27-48 Effectivity: ALL 14. 05. 2020...
  • Page 433 FLIGHT CONTROLS 1 – 10 - Washer ø6.4 x 18 x 1.6 Trim spring 19 - Plywood Insert 2 – 11 - Washer ø6.4 x 12 x 1.6 Connecting push rod 20 - Bracket 3 – 12 - Washer ø4.3 x 9 x 0.8 Trim control 4 –...

  • Page 434: Electrical Pitch Trim System With Manual Indicating

    FLIGHT CONTROLS Electrical pitch trim system with manual indicating (1) Pitch trim system removal: Remove pedestal panel (Chapter 27-50, 2.C.(1)). Disconnect the adjustment trim push rod from torsion tube (1, Fig. 27-13), by removing cotter pin (36), nut (26), washer (30) and bolt (17).
  • Page 435 FLIGHT CONTROLS Connect the adjustment trim push rod (2) to torsion tube (1) by using the bolt (17), washer (30), nut (26) and cotter pin (36). Connect the adjustment trim push rod (2) to trim spring (10), by using the nuts (22) and washer (31). (m) Carry out test and check: •...
  • Page 436 FLIGHT CONTROLS Fig. 27-13 Electrical Trim System Removal / Installation (page 1 of 2) Chapter 27-30 ELEVATOR AND PITCH TRIM Page 27-52 Effectivity: ALL 14. 05. 2020...
  • Page 437 FLIGHT CONTROLS 1 – Torsion tube 12 - Plywood 26 - Castle nut M6 2 – 28 - Washer ø3.2 x 7 x 0.5 Adjustment trim push rod 13 - Plywood bracket 3 – 30 - Washer ø6.4 x 12 x 1.6 Position indicator 14 - Deflector 4 –...

  • Page 438: Electrical Pitch Trim System With Electrical Indicating

    FLIGHT CONTROLS Electrical pitch trim system with electrical indicating Pitch trim system removal: Remove pedestal panel (Chapter 27-50, 2.C.(1)). Disconnect the adjustment trim push rod (2) from torsion tube (1, Fig. 27-14), by removing cotter pin (37), nut (29), washer (33) and bolt (23).
  • Page 439 FLIGHT CONTROLS Assembly the potentiometer (38) with potentiometer cover (17), by using bolts (19). Install the assembled potentiometer on potentiometer holder (16), by using bolts (20), washers (31) and nuts (26). Attach the assembled electromotor on plywood (12) into central tunnel, by using the bolts (24), washers (34) and nuts (27).
  • Page 440 FLIGHT CONTROLS Fig. 27-14 Electrical Trim System Removal / Installation (page 1 of 2) Chapter 27-30 ELEVATOR AND PITCH TRIM Page 27-56 Effectivity: ALL 14. 05. 2020...
  • Page 441 FLIGHT CONTROLS Torsion tube 14 - Limit switch holder 3 28 - Self-locking nut M5 Adjustment trim push rod 15 - Electromotor bolt 29 - Castle nut M6 31 - Washer ø3.2 x 7 x 0.5 Position indicator 16 - Potentiometer holder 32 - Washer ø4.3 x 9 x 0.8 Electromotor bracket 17 - Potent.

  • Page 442: Electrical Pitch Trim Control

    FLIGHT CONTROLS Electrical pitch trim control Pitch trim control removal: Remove the upper handle (1) from control stick by removing the handle (2), rivets (3), screw (4), plastic tube (5) and shrink tubes (6). Pitch trim control installation: Install the upper handle (1) on control stick, by using the handle (2), rivets (3), screw (4), plastic tube (5) and shrink tubes (6).
  • Page 443 FLIGHT CONTROLS 1 – 3 – Rivet 3x6 Upper handle Plastic tube 2 – Handle Screw M3x10 Shrink tube Fig. 27-15 Electrical Trim Control Removal / Installation ELEVATOR AND PITCH TRIM Chapter 27-30 14. 05. 2020 Effectivity: ALL Page 27-59...
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  • Page 445: Flaps

    FLIGHT CONTROLS 27-50 FLAPS DESCRIPTION The aircraft (with fixed gear – FG; or retractable gear – RG) may be equipped with manually or electrically operated wing flaps. The manually operated wing flaps are controlled by a lever (1, Fig. 27-16) on the pedestal panel between pilot and co-pilot.
  • Page 446 FLIGHT CONTROLS Lever Bearing Pedestal panel Wing flap lever Push-pull rod 1 Push-pull rod Bellcrank Wing flap Torsion tube 10 - Gas strut Fig. 27-16 Wing Flap Control System Chapter 27-50 FLAPS Page 27-62 Effectivity: ALL 14. 05. 2020...

  • Page 447: Maintenance Practices

    FLIGHT CONTROLS MAINTENANCE PRACTICES Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Wrench 8 1 pc Screwdriver 1 pc Puller on small pins M4 1 pc Pliers 1 pc...
  • Page 448 FLIGHT CONTROLS Flap control system FG / RG installation: Before installation check main parts for cracks and condition. Carefully rotate and slide torsion tube (1, Fig. 27-18) from right side of centre section wing root through all holes to other side (wings have to be removed).
  • Page 449 FLIGHT CONTROLS Carry out test and check: • That the pins are secured with cotter pins. • If all bolt connections are tight. • Free plays. • Free movement of flap control system. • If deflections of wing flaps are symmetrical. •...
  • Page 450 FLIGHT CONTROLS Set protractor on trailing edge of wing flap root. Set wing flaps to fully retracted position. Set the protractor to 0°- starting value for measurement. Check deflections at first position 15°, second position 24° and third position 35°, see Tab. 27-9. Check if deflections are symmetrical on both wing flaps.
  • Page 451 FLIGHT CONTROLS 1 – Torsion tube 12 - Nut M6 2 – 13 - Washer ø6.4 x 12 x 1.6 Bellcrank 3 – 14 - Washer ø6.4 x 18 x 1.6 Push-pull rod 4 – 15 – Washer ø6.4 x 12 x 0.5 5 –...

  • Page 452: Flap Control System (Electrical)

    FLIGHT CONTROLS Flap control system (electrical) Flap control system removal: Remove wings (Chapter 57-10) Disconnect push rod (13, Fig. 27-19) from torsion tube (5), by removing nut (23), washer (29) and bolt (16). Remove second push rod (13). Remove pedestal panel (Chapter 27-50, 2.C.(1)). In baggage compartments, remove flaps actuator cover (10) by removing screws (22).
  • Page 453 FLIGHT CONTROLS Stick cover on centre section roots with silicone (remove old silicone). Install pedestal panel (Chapter 27-50, 2.C.(2)). Install wings (Chapter 57-10). Install the flaps lever (2) to torsion tube (5) by using bolt (17), washer (29) and nut (25). In baggage compartment install the upper hinge (3) and flaps actuator (37) by using the bearing end (11), bushings (7), bolt (18), washers (31, 33) and nuts (25, 27).
  • Page 454 FLIGHT CONTROLS Carry out test and check: • That the pins are secured with cotter pins. • If all bolt connections are tight. • Free plays. • Free movement of flap control system. • If deflections of wing flaps are symmetrical. •...
  • Page 455 FLIGHT CONTROLS Fig. 27-19 Electrical Flap Control System Removal / Installation (page 1 of 3) FLAPS Chapter 27-50 14. 05. 2020 Effectivity: ALL Page 27-71...
  • Page 456 FLIGHT CONTROLS Fig. 27-19 Electrical Flap Control System Removal / Installation (page 2 of 3) Chapter 27-50 FLAPS Page 27-72 Effectivity: ALL 14. 05. 2020...
  • Page 457 FLIGHT CONTROLS Potentiometer holder 21 - Bolt M6 x 60 Flaps lever assembly 22 - Screw M4 x 12 Upper hinge assembly 23 - Nut M6 lower Potentiometer console 24 - Nut M6 Flaps torsion tube 25 - Self locking nut M6 Potentiometer assembly axle 26 - Self locking nut M5 Flaps actuator bushing...

  • Page 458: Pedestal Panel

    FLIGHT CONTROLS Pedestal panel Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Wrench 8 1 pc Screwdriver 10 1 pc Philips screwdriver 1 pc Vaseline...
  • Page 459 FLIGHT CONTROLS WARNING CHECK CONTROL TUNNEL VERY CAREFULLY FOR FOREIGN OBJECTS TOOLS AFTER REASSEMBLY! Connect the trim rocker switches (18) (if installed). Place the pedestal panel (1) on the central tunnel and install attaching bolts (7). Install the trim lever handle (19) by using bolt (20) (only manual trim control).
  • Page 460 FLIGHT CONTROLS 1 – Slotted link 11 – Bolt M6 x 25 2 – Arm rest 12 – Washer ø6.4 x 12 x 1.6 3 – Upholstery 13 – Washer ø6.4 x 10 x 1.6 4 – Push rod 14 – Washer ø5.3 x 10 x 1 5 –...
  • Page 461 FUEL 28 FUEL CONTENTS Chapter Description Page 28-00 GENERAL ................. 3 INTRODUCTION ............... 3 Fuel Distribution System A – Rotax 912 ......3 Fuel Distribution System B – Rotax 912 ......3 Fuel Distribution System C – Rotax 912 ......4 Fuel Distribution System D –...
  • Page 462 FUEL MAINTENANCE PRACTICES ..........26 Electric fuel pump in fuel distribution system A ....26 Electric fuel pump in fuel distribution system B, C, D, E, F ................. 29 One-way valve ..............32 Coarse filter cleaning ............33 Fine fuel filter ..............34 Fuel selector FS16x2-F ...........

  • Page 463: General

    FUEL 28-00 GENERAL INTRODUCTION Fuel Distribution System A – Rotax 912 Fuel is supplied to the engine in dependence of fuel selector position (LEFT - RIGHT - OFF) (22, Fig. 28-1). From fuel tanks (16; 17; 18; 19) the fuel flows through the socket with coarse filter (23) and fuel filters (21) to the fuel selector (22) inlets.

  • Page 464: Fuel Distribution System C - Rotax 912

    FUEL jets in its outlets to the 4-way distributor (4). Both monitor the actual pressure in the fuel supply line. Signal from the fuel pressure sensor is carried to the engine monitoring system unit (8) and from there to the EFIS display (10). Wing fuel tanks (16;...

  • Page 465: Fuel Distribution System D - Rotax 912

    FUEL Fuel Distribution System D – Rotax 912 Fuel is supplied to the engine in dependence of fuel selector position (LEFT - RIGHT - OFF) (22, Fig. 28-4). From fuel tanks (16; 17; 18; 19) the fuel flows through the socket with coarse (23) and fuel filters (21) to the fuel selector.

  • Page 466: Fuel Distribution System F - Rotax 912

    FUEL discharge through the hoses protruding under aircraft through the fuselage skin inside of central tunnel. Fuel tank (16) in the left wing is an option. There is fuel level sensor (15) in the both left and right fuel tank. Fuel level sensors are installed in the root rib of fuselage fuel tanks.
  • Page 467 FUEL supplied to right tanks (18, 19) through the fuel filter (21), fuel pump (12) and check valve (13). Signal from the differential pressure sensor is carried to the EMS module (8) and from there to the EFIS display (10). Wing fuel tanks (16;...
  • Page 468 FUEL 1 – Engine fuel pump 9 – Fuel pressure sensor 17 – LH center section fuel tank 2 – LH carburetor 10 – EFIS display 18 – RH center section fuel tank 3 – RH carburetor 11 – Standby fuel pressure indicator 19 – RH wing fuel tank 4 –...
  • Page 469 FUEL 1 – Engine fuel pump 9 – Fuel pressure sensor 17 – LH center section fuel tank 2 – LH carburetor 10 – EFIS display 18 – RH center section fuel tank 3 – RH carburetor 11 – Standby fuel pressure indicator 19 – RH wing fuel tank 4 –...
  • Page 470 FUEL 1 – Engine fuel pump 9 – Fuel pressure sensor 17 – LH center section fuel tank 2 – LH carburetor 10 – EFIS display 18 – RH center section fuel tank 3 – RH carburetor 11 – N/A 19 –...
  • Page 471 FUEL 1 – Engine fuel pump 10 – EFIS display 19 – RH wing fuel tank 2 – LH carburetor 11 – Standby fuel pressure indicator 20 – Drain valve 3 – RH carburetor 12 – Electric fuel pump 21 – Fuel filter 4 –...
  • Page 472 FUEL 1 – Engine fuel pump 9 – N/A 17 – LH center section fuel tank 2 – LH carburetor 10 – Fuel level indicator 18 – RH center section fuel tank 3 – RH carburetor 11 – Fuel pressure indicator 19 –...
  • Page 473 FUEL 1 – Engine fuel pump 10 – EFIS display 19 – RH wing fuel tank 2 – LH carburetor 11 – Standby fuel pressure indicator 20 – Drain valve 3 – RH carburetor 12 – Electric fuel pump 21 – Fuel filter 4 –...

  • Page 474: Fuel Distribution System G - Rotax 914

    FUEL Fig. 28-7 Fuel Distribution System G – Rotax 914 (1 of 2) Chapter 28-00 GENERAL Page 28-14 Effectivity: ALL 04. 05. 2021...
  • Page 475 FUEL 1 – Fuel pressure 11 – N/A 19 – RH wing fuel tank regulator 2 – LH carburetor 12a – Electric fuel pump (main) 20 – Drain valve 3 – RH carburetor 12b – Electric fuel pump (auxiliary) 21 – Fuel filter 4 –...

  • Page 476: Fuel Distribution System H - Rotax 914

    FUEL Fig. 28-8 Fuel Distribution System H – Rotax 914 (1 of 2) Chapter 28-00 GENERAL Page 28-16 Effectivity: ALL 04. 05. 2021...
  • Page 477 FUEL 1 – Fuel pressure regulator 10 – EFIS display 18 – RH center section fuel tank 2 – LH carburetor 11 – N/A 19 – RH wing fuel tank 3 – RH carburetor 12a – Electric fuel pump (main) 20 –...

  • Page 478: Troubleshooting

    FUEL TROUBLESHOOTING TROUBLE POSSIBLE CAUSE REMEDY Filler cap improperly Install filler cap properly. installed. Filler cap leaks. Filler cap seal improperly Replace filler cap seal. installed. Deteriorated filler cap seal. Replace filler cap seal. Loose connector(s). Inspect and tighten connector(s). Fuel connector(s) leak.
  • Page 479 FUEL TROUBLE POSSIBLE CAUSE REMEDY Malfunction of engine fuel Replace engine fuel pump. pump or fuel system. Fuel starvation after start up (cont.). Fuel vents plugged. Remove obstruction. Water in fuel. Drain water. Defective fuel quantity Replace fuel quantity Erratic fuel quantity indicator.
  • Page 480 FUEL This page is left blank intentionally Chapter 28-00 GENERAL Page 28-20 Effectivity: ALL 04. 05. 2021...

  • Page 481: Storage

    FUEL 28-10 STORAGE DESCRIPTION The aircraft has integral fuel tanks with a total capacity of approx. 100 or 126 liters. The integral fuel tanks are located in the forward box of the fuselage central section and in right (100 l) or both (126 l) halves of wing. The wing and central section tanks are connected by a simple hose connection with clamps.
  • Page 482 FUEL Drain valve removal: Make sure that the IGNITION switches are set to OFF. Remove engine cowlings (Chapter 71-10). Disconnect negative terminal of battery (Chapter 24-30). Electrically ground the aircraft (use the exhaust pipe outlet) to the grounding point. Drain fuel tanks (Chapter 12-10). Unscrew and remove the drain valve (1, Fig.
  • Page 483 FUEL 1 – Drain valve For information: 2 – O-ring ø7.66 x 1.78 3 – Wing bottom surface Fig. 28-9 Drain Valve Removal / Installation STORAGE Chapter 28-10 04. 05. 2021 Effectivity: ALL Page 28-23...
  • Page 484 FUEL This page is left blank intentionally Chapter 28-10 STORAGE Page 28-24 Effectivity: ALL 04. 05. 2021...
  • Page 485 FUEL 28-20 DISTRIBUTION DESCRIPTION Fuel Distribution System A – Rotax 912 For fuel distribution system description see Chapter 28-00 (Fig. 28-1). Fuel Distribution System B – Rotax 912 For fuel distribution system description see Chapter 28-00 (Fig. 28-2). Fuel Distribution System C – Rotax 912 For fuel distribution system description see Chapter 28-00 (Fig.

  • Page 486: Electric Fuel Pump In Fuel Distribution System A

    FUEL MAINTENANCE PRACTICES Electric fuel pump in fuel distribution system A Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Wrench 10 1 pc Screwdriver 1 pc...
  • Page 487 FUEL Electric fuel pump installation: Make sure that the IGNITION switches are set to OFF. WARNING BEWARE ENSURE CORRECT DIRECTION OF FLOW! Put the clamp (3, Fig. 28-10) on el. fuel pump (1). Put the hose clamps (12) on the fuel hoses (14, 15) and connect to the el.
  • Page 488 FUEL 1 – El. fuel pump 9 – Bolt M6 x 18 17 – Fuel hose 2 – One way valve 10 – Self-locking nut M5 18 – Wires 3 – Clamp 11 – Washer ø5.3 x 10 x 1 19 – Nut M5 4 –...

  • Page 489: Electric Fuel Pump In Fuel Distribution System B, C, D, E, F

    FUEL Electric fuel pump in fuel distribution system B, C, D, E, F Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Screwdriver 1 pc Pliers...
  • Page 490 FUEL Electric fuel pump installation: Make sure that the IGNITION switches are set to OFF. WARNING BEWARE ENSURE CORRECT DIRECTION OF FLOW! Put the clamp (3, Fig. 28-11) on el. fuel pump (1). Put the hose clamps (12) on the fuel hoses (14, 15) and connect to the el.

  • Page 491: One-Way Valve

    FUEL 1 – El. fuel pump 9 – N/A 17 – Fuel hose 2 – One-way valve 10 – Self-locking nut M5 18 – Wires 3 – Clamp 11 – Washer ø5.3 x 10 x 1 19 – Nut M5 4 –...
  • Page 492 FUEL One-way valve Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Oetiker pliers 1 pc Persons Tab. 28-4 Recommended tools, materials, persons and documentation WARNING GROUND THE EXHAUST PIPE OUTLET AND FUEL SERVICE EQUIPMENT PRIOR TO AIRCRAFT REFUELING/DEFUELING!

  • Page 493: Coarse Filter Cleaning

    FUEL Replenish the fuel system (Chapter 12-10). Install engine cowlings (Chapter 71-10). Remove the ground cable from the aircraft. Carry out engine ground test; check fuel system for leaks. Coarse filter cleaning Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher.

  • Page 494: Fine Fuel Filter

    FUEL Fine fuel filter Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Wrench 13 1 pc Screwdriver 1 pc Pliers 1 pc Oetiker pliers 1 pc...
  • Page 495 FUEL Fine fuel filter installation: Make sure that the IGNITION switches are set to OFF. WARNING BEWARE ENSURE CORRECT DIRECTION OF FLOW! Put the fuel filter clamp (2, Fig. 28-12) on the fuel filter (1) and hose clamps (7) on the fuel hoses (8; 9). Connect fuel hoses (8;...
  • Page 496 FUEL 1 – Fuel filter 6 – Distance tube 2 – Clamp 7 – Hose clamp 3 – Self-locking nut M6 8 – Fuel hose 4 – Washer ø6.4 x 12 x 0.5 9 – Fuel hose 5 – Washer ø6.4 x 12 x 1.6 10 –...

  • Page 497: Fuel Selector Fs16X2-F

    FUEL Fuel selector FS16x2-F Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 9 2 pcs Screwdriver 1 pc Hex key 2 1 pc Pliers 1 pc Oetiker pliers...
  • Page 498 FUEL Fuel selector FS16x2-F installation: Make sure that the IGNITION switches are set to OFF. Prepare fuel selector: • Screw elbow fittings (5, Fig. 28-13) into fuel selector (1) secured with Loctite 542. • Install hose fitting nuts (6) with hose sockets (7) and olives (9). •...
  • Page 499 FUEL 1 – Fuel selector body 8 – Hose clamp 14.5 2 – Flange 9 – Olive 3 – Fuel selector handle 10 – Fuel hose (from LH fuel tank) 4 – Screw M4 x 15 11 – Fuel hose (to engine) 5 –...

  • Page 500: Fuel Selector Fs15X2

    FUEL Fuel selector FS15x2 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 9 2 pcs Screwdriver 1 pc Hex key 2 1 pc Pliers 1 pc Oetiker pliers...
  • Page 501 FUEL Fuel selector FS15x2 installation: Make sure that the IGNITION switches are set to OFF. Prepare fuel selector: • Screw elbow fittings (5, Fig. 28-14) into fuel selector (1) secured with Loctite 542. • Install hose fitting nuts (6) with hose sockets (7) and olives (9). •...
  • Page 502 FUEL 1 – Fuel selector body 8 – Hose clamp 14.5 2 – Flange 9 – Olive 3 – Fuel selector handle 10 – Fuel hose (from LH fuel tank) 4 – Screw M4 x 15 11 – Fuel hose (to engine) 5 –...

  • Page 503: Fuel Selector 05-01042

    FUEL Fuel selector 05-01042 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 22 1 pc Pliers 1 pc Oetiker pliers 1 pc Lockwire ø0.8 mm Persons Tab.
  • Page 504 FUEL Connect fuel hoses (5; 6; 7, Fig. 28-15) to the hose sockets of fuel selector (1) and secure them with hose clamps (4). Put fuel selector (1) into central console (8), install the washer (2) and attach it using nut (3). Check if fuel selector is firmly secured and sealed.

  • Page 505: Fuel Lines Fg / Rg Rotax 912

    FUEL Fuel lines FG / RG Rotax 912 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Socket 12 1 pc Screwdriver 5 1 pc Phillips screwdriver 1 pc Cable tie 2.6...
  • Page 506 FUEL Fuel lines FG / RG Rotax 912 removal: Make sure that the IGNITION switches are set to OFF. Remove engine cowlings (Chapter 71-10). Disconnect negative terminal of battery (Chapter 24-30). Electrically ground the aircraft (use the exhaust pipe outlet) to the grounding point.
  • Page 507 FUEL Fuel lines FG / RG Rotax 912 installation: Make sure that the IGNITION switches are set to OFF. Put the pyro jacket (fire sleeve) coverings along the length of fuel hoses in the engine compartment. On engine fuel pump, slide fuel hoses (1; 2, Fig. 28-16) and secure them with hose clamps (20;...
  • Page 508 FUEL NOTE Hose (12) belongs to ventilation line and hose (13) connecting wing and fuselage fuel tanks. Installing of fuel hoses between left wing and fuselage fuel tank is described. The right side is analogous. Check if all hoses are firmly secured and sealed. Check correct orientation of fuel system components.
  • Page 509 FUEL Fig. 28-16 Fuel Line FG Rotax 912 Removal / Installation (page 1 of 3) DISTRIBUTION Chapter 28-20 04. 05. 2021 Effectivity: ALL Page 28-49...
  • Page 510 FUEL Fig. 28-16 Fuel Line RG Rotax 912 Removal / Installation (page 2 of 3) Chapter 28-20 DISTRIBUTION Page 28-50 Effectivity: ALL 04. 05. 2021...
  • Page 511 FUEL 1 – Fuel hose 1 13 – Fuel hose 13 25 – Hose clamp ø6-12 2 – Fuel hose 2 14 – Fuel hose 14 26 – Hose clamp ø16-27 3 – Fuel hose 3 15 – Fuel hose 15 27 –...

  • Page 512: Ventilation Line

    FUEL Ventilation line Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 5 1 pc Phillips screwdriver 1 pc Pliers 1 pc Oetiker Pliers 1 pc Cable tie 2.6 Hose clamps (as appropriate)
  • Page 513 FUEL Cut and scarf the end of ventilation hoses 60 mm under fuselage skin. Connect negative terminal of the battery (Chapter 24-30) Install engine cowlings (Chapter 71-10). Remove the ground cable from the aircraft. 1L – Ventilation hose (left tank) 2 –...

  • Page 514: Electric Fuel Pumps For Rotax 914

    FUEL Electric fuel pumps for Rotax 914 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Screwdriver 1 pc Pliers 1 pc Oetiker pliers 1 pc Persons...
  • Page 515 FUEL Electric fuel pumps for Rotax 914 installation: Make sure that the IGNITION switches are set to OFF. WARNING BEWARE ENSURE CORRECT DIRECTION OF FLOW! Check the correct orientation of el. fuel pumps. Put the hose clamps (12; 13, Fig. 28-18) on the fuel hoses (14, 15; 16;...
  • Page 516 FUEL 1 – El. fuel pump 9 – Fuel hose 17 – Fuel hose 2 – Fuel filter 10 – Coarse filter socket 18 – Wires 3 – 11 – Fuel hose 19 – Nut M5 4 – 12 – Hose clamp 15.5 20 –...

  • Page 517: Transfer Electric Fuel Pump For Rotax 914

    FUEL Transfer electric fuel pump for Rotax 914 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Wrench 13 1 pc Screwdriver 1 pc Pliers...
  • Page 518 FUEL Electric fuel pump for Rotax 914 installation: Make sure that the IGNITION switches are set to OFF. WARNING BEWARE ENSURE CORRECT DIRECTION OF FLOW! Check the correct orientation of el. fuel pumps. Slide the clamp (11, Fig. 28-19) on the fuel pump (6). Put the hose clamps (12, 13) on the fuel hoses (14, 8) and connect to the el.
  • Page 519 FUEL 1 – Fuel filter 9 – Fuel hose 17 – N/A 2 – Clamp 10 – N/A 18 – Wires 3 – Self-locking nut M6 11 – Clamp RSGU 19 – Nut M5 4 – One-way valve 12 – Hose clamp 15.5 20 –...

  • Page 520: Fuel Pump's Unit For Rotax 914

    FUEL Fuel pump’s unit for Rotax 914 Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Allen key 5 1 pc Screwdriver 1 pc Pliers 1 pc Oetiker pliers 1 pc...
  • Page 521 FUEL Fuel pump’s unit for Rotax 914 installation: Make sure that the IGNITION switches are set to OFF. WARNING BEWARE ENSURE CORRECT DIRECTION OF FUEL FLOW! Put the fuel pump’s unit (1, Fig. 28-20) on firewall in correct position and attach it by using the bolts (6), washers (8; 9), silentblocks (2) and nuts (7).
  • Page 522 FUEL 1 – El. fuel pump unit 6 – Bolt M6 x 12 11 – Hose clamp 15.5 2 – Silentblock 7 – Self-locking nut M6 12 – Fuel hose 3 – Hose adaptor 8 – Washer 6.4 x 18 x 1.6 13 – Fuel hose 4 –...

  • Page 523: Gascolator For Rotax 914

    FUEL Gascolator for Rotax 914 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Wrench 8 1 pc Screwdriver 1 pc Pliers 1 pc Oetiker pliers...
  • Page 524 FUEL Gascolator installation: Make sure that the IGNITION switches are set to OFF. WARNING BEWARE ENSURE CORRECT DIRECTION OF FUEL FLOW! Assembly the gascolator (1, Fig. 28-21) with holder (2), washers (6) and bolts (4). Apply Loctite 243 on thread of bolts. Put the gascolator assy on firewall in the correct position.
  • Page 525 FUEL 1 – Gascolator 5 – Bolt M5 x 20 9 – Self-locking nut M5 2 – Holder 6 – Washer ø6.4 x 12 x 1.6 10 – Fuel hose 3 – Hose clamp 7 – Washer ø5.3 x 15 x 1.2 11 –...

  • Page 526: Fuel Selector Fs20 For Rotax 914

    FUEL Fuel selector FS20 for Rotax 914 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Screwdriver 1 pc Hex key 2 1 pc Pliers 1 pc...
  • Page 527 FUEL Fuel selector FS20 TYPE 1 for Rotax 914 installation: Make sure that the IGNITION switches are set to OFF. Prepare fuel selector: • Remove the protective caps from fuel selector sockets. • Install the hose banjos (7; 9, Fig. 28-22) in correct position together with gasket rings (6) and banjo bolts (5).
  • Page 528 FUEL 1 – Fuel selector body 10 – N/A 2 – Flange 11 – N/A 3 – Fuel selector handle 12 – Fuel hose (to engine) 4 – Screw M5 x 20 13 – N/A 5 – Banjo bolt NPT 1/8” 14 –...

  • Page 529: Fuel Selector Fs2020 For Rotax 914

    FUEL Fuel selector FS2020 for Rotax 914 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Screwdriver 1 pc Hex key 2 1 pc Pliers 1 pc...
  • Page 530 FUEL Fuel selector FS2020 for Rotax 914 installation: Make sure that the IGNITION switches are set to OFF. Fuel selector preparation: • Remove the protective caps from fuel selector sockets. • Install the banjos (7; 9, Fig. 28-23) in correct position together with gasket rings (6) and banjo bolts (5) to the fuel selector (1).
  • Page 531 FUEL 1 – Fuel selector body 10 – Fuel hose (to engine) 2 – Flange 11 – Fuel hose (from engine) 3 – Fuel selector handle 12 – Fuel hose (to RH fuel tank) 4 – Screw M5 x 20 13 –...
  • Page 532 FUEL Fuel lines RG Rotax 914 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Socket 12 1 pc Screwdriver 5 1 pc Phillips screwdriver 1 pc Cable tie 2.6 Cable tie 4.8...

  • Page 533: Fuel Lines Rg Rotax 914

    FUEL Fuel lines RG Rotax 914 (fuel system G) removal: Make sure that the IGNITION switches are set to OFF. Remove engine cowlings (Chapter 71-10). Disconnect negative terminal of battery (Chapter 24-30). Electrically ground the aircraft (use the exhaust pipe outlet) to the grounding point.
  • Page 534 FUEL Fuel lines RG Rotax 914 (fuel system G) installation: Make sure that the IGNITION switches are set to OFF. Put the pyro jacket (fire sleeve) coverings along the length of fuel hoses in the engine compartment. Connect the fuel hoses to the transfer fuel pump and fuel filter (2.L.). Connect the fuel hoses to the fuel pumps and fuel filter (2.K).
  • Page 535 FUEL Fuel lines RG Rotax 914 (fuel system H) removal: Make sure that the IGNITION switches are set to OFF. Remove engine cowlings (Chapter 71-10). Disconnect negative terminal of battery (Chapter 24-30). Electrically ground the aircraft (use the exhaust pipe outlet) to the grounding point.
  • Page 536 FUEL Fuel lines RG Rotax 914 (fuel system H) installation: Make sure that the IGNITION switches are set to OFF. Put the pyro jacket (fire sleeve) coverings along the length of fuel hoses in the engine compartment. Connect the fuel hoses (7; 8; 9; 10; 11; 12, Fig. 28-24) to the fuel selector FS2020 and fuel tanks sockets and secure with the hose clamps (16;...
  • Page 537 FUEL Fuel system RG Rotax 914 leak test: NOTE Fuel system must be drained. Make sure that the IGNITION switches are set to OFF. Remove the engine cowlings (Chapter 71-10). Disconnect negative terminal of battery (Chapter 24-30). Electrically ground the aircraft (use the exhaust pipe outlet) to the grounding point.
  • Page 538 FUEL Fig. 28-24 Fuel Lines RG Rotax 914 Removal / Installation (page 1 of 2) Chapter 28-20 DISTRIBUTION Page 28-78 Effectivity: ALL 04. 05. 2021...
  • Page 539 FUEL 1 – Fuel hose 1 11 – Fuel hose 11 21 – Banjo bolt 2 – Fuel hose 2 12 – Fuel hose 12 22 – Banjo eye 3 – Fuel hose 3 13 – Fuel hose 13 23 – Banjo extended 4 –...
  • Page 540 FUEL This page is left blank intentionally Chapter 28-20 DISTRIBUTION Page 28-80 Effectivity: ALL 04. 05. 2021...

  • Page 541: Indicating

    FUEL 28-40 INDICATING DESCRIPTION The fuel level sensor is installed in the both left and right fuel tank on the root rib of fuselage fuel tank. The fuel tank sensor value is displayed on the instrument panel by the EFIS Display or analogue gauge. Low fuel quantity (less than 16 liters in the appropriate fuel tank) is signalized on the instrument panel by the LH FUEL RES / RH FUEL RES red warning lamps (Chapter 39-10).

  • Page 542: Fuel Level Sensors Road / Vdo

    FUEL Fuel level sensors ROAD / VDO Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 8 1 pc Screwdriver 1 pc Pliers 1 pc Oetiker Pliers 1 pc Loctite 577...
  • Page 543 FUEL Fuel level sensor ROAD/VDO installation: Make sure that the IGNITION switches are set to OFF. Put the fuel level sensor (1, Fig. 28-25) with seal (2) to the fuel tank in correct position. WARNING DO NOT CHANGE LEFT AND RIGHT FUEL LEVEL SENSORS! Attach the fuel level sensors with washers (4) and bolts (3) secured with Loctite 577.

  • Page 544: Calibration Of Fuel Quantity Indication

    FUEL Calibration of fuel quantity indication Adjustment Test – calibration check correct function of the measurement system and indication of fuel quantity. Carry out this procedure on the aircraft with completely finished fuel installation. Perform the procedure in a suitable and exactly defined space. In this space and in its vicinity don´t carry out, in the course of the calibration, any other work than the work necessary for performing the calibration.
  • Page 545 FUEL By turning the rotary switch, select the calibrated tank – FUEL TANK 1 or 2 (LEFT or RIGHT) and then move the rotary switch to the right. If you want to edit the calibration, select EDIT; if you want to do a recalibration, select RECAL.
  • Page 546 FUEL 1 – Fuel level sensor 5 – Electrical connector 2 – Rubber seal For information: 3 – Bolt M5 x 36 6 – Wing rib 4 – Washer ø5.3 x 10 x 1 Fig. 28-25 Illustrative variants of fuel level sensor Removal / Installation Chapter 28-40 INDICATING Page 28-86...

  • Page 547: Fuel Pressure Sensor

    FUEL Fuel pressure sensor Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 8 2 pcs Wrench 14 1 pc Pliers 1 pc Oetiker Pliers 1 pc Philips screwdriver 2 1 pc...
  • Page 548 FUEL ROAD (A): Disassemble the fuel pressure sensor (1), sealing ring (8) and hose socket (7). Kavlico (B): Disassemble the fuel pressure sensor (13), lock plate (14), console (15) and hose socket (7). VDO (C): Disassemble the fuel pressure sensor (16) and hose socket (7).
  • Page 549 FUEL 1 – Fuel pressure sensor (ROAD) 11 – Electrical connector / Wires 2 – Bracket 12 – Bolt M5 3 – Bolt M5 x 20 13 – Fuel pressure sensor (Kavlico) 4 – Washer ø5.3 x 15 x 1.2 14 –...

  • Page 550: Fuel Flow Transducer Fg / Rg

    FUEL Fuel flow transducer FG / RG Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 14 1 pc Pliers 1 pc Oetiker Pliers 1 pc Cable tie 4.8 5 pcs...
  • Page 551 FUEL Fuel flow transducer FG / RG installation: Make sure that the IGNITION switches are set to OFF. Remove the caps from the transducer ports and hose. Assemble fuel flow transducer (1; Fig. 28-27) by screwing the hose sockets (4) secured with Loctite 542. WARNING BEWARE ENSURE...
  • Page 552 FUEL 1 – Fuel flow transducer 8 – Electrical connector 2 – Rubber plate 9 – Cable tie 4.8 3 – Rubber distant hose 10 – Cable tie 2.6 4 – Hose socket 11 – Pyrojacket (fire sleeve) 5 – Hose clamp 14.5 For information: 6 –...

  • Page 553: Fuel Flow Transducers Rg Rotax 914

    FUEL Fuel flow transducers RG Rotax 914 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 14 1 pc Pliers 1 pc Oetiker Pliers 1 pc Screwdriver 1 pc...
  • Page 554 FUEL Fuel flow transducers RG Rotax 914 installation: Make sure that the IGNITION switches are set to OFF. Remove the caps from the transducer ports and hose. Assemble fuel flow transducer (1; Fig. 28-28) by using the bolts (10), rings (11), hose banjos (9) and hose sockets (8; 7; 6). Socket secured with Loctite 542.
  • Page 555 FUEL 1 – Fuel flow transducer 11 – Gasket ring 10 2 – Holder 12 – Self-locking nut M6 3 – Clamp 70-90 13 – Bolt M6x85 4 – Hose clamp 15.5 14 – Washer 6,4 x 12 x 1,6 5 –...
  • Page 556 FUEL This page is left blank intentionally Chapter 28-40 INDICATING Page 28-96 Effectivity: ALL 04. 05. 2021...
  • Page 557 INDICATING/ RECORDING SYSTEMS 31 INDICATING / RECORDING SYSTEMS CONTENTS Chapter Description Page 31-00 GENERAL ................. 3 INTRODUCTION ............... 3 TROUBLESHOOTING ............... 3 31-30 RECORDERS..............5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 5 Flying hours counter ............5 Engine hours meter Hobbs ..........5 31-50 CENTRAL WARNING SYSTEMS ........
  • Page 558 INDICATING/ RECORDING SYSTEMS This page is left blank intentionally Chapter 31 CONTENTS Page 31-2 Effectivity: ALL 14. 05. 2020...

  • Page 559: General

    INDICATING/ RECORDING SYSTEMS 31-00 GENERAL INTRODUCTION This chapter describes equipment which provides visual and aural warning of conditions in unrelated systems. This includes the hour meters, control / warning lamps, low value warning unit and stall warning system. All equipment must be installed according to specific equipment OEM installation manual.
  • Page 560 INDICATING/ RECORDING SYSTEMS TROUBLE POSSIBLE CAUSE REMEDY Defective LVW unit. Replace the LVW unit. Fuel reserve warning lamp Defective fuel reserve Replace the fuel reserve does not operate correctly. switch. switch. Defective LVW unit. Replace the LVW unit. Oil pressure warning lamp Defective oil pressure Replace the oil pressure does not operate correctly.

  • Page 561: Recorders

    INDICATING/ RECORDING SYSTEMS 31-30 RECORDERS DESCRIPTION The aircraft can be equipped with the flying hours counter and engine operation Hobbs hours meter. The flying hours counter has an electrically driven counter mechanism and the readings are in hours and minutes. It is connected to the aircraft's total pressure sensor and automatically switches on when the airspeed reaches 60 km/h (32 kts).
  • Page 562 INDICATING/ RECORDING SYSTEMS This page is left blank intentionally Chapter 31-30 RECORDERS Page 31-6 Effectivity: ALL 14. 05. 2020...
  • Page 563 INDICATING/ RECORDING SYSTEMS 31-50 CENTRAL WARNING SYSTEMS DESCRIPTION The aircraft may equipped with the Low Value Warning (LVW) system for oil minimum pressure and fuel quantity. The system triggers a warning indicated by the warning lamps when the oil minimum pressure or fuel quantity decreases below the critical level.
  • Page 564 INDICATING/ RECORDING SYSTEMS 1 – ACI stall warner 4 – LH Dynon SkyView 2 – Buzzer 5 – RH Dynon SkyView 3 – ADAHRS module 6 – Stall warning lamp Fig. 31-1 Stall Warning System Chapter 31-50 CENTRAL WARNING SYSTEMS Page 31-8 Effectivity: ALL 14.
  • Page 565 INDICATING/ RECORDING SYSTEMS Fig. 31-2 Stall Warning System Scheme without Dynon SkyView Fig. 31-3 Stall Warning System Scheme with Dynon SkyView CENTRAL WARNING SYSTEMS Chapter 31-50 14. 05. 2020 Effectivity: ALL Page 31-9...

  • Page 566: Maintenance Practices

    INDICATING/ RECORDING SYSTEMS MAINTENANCE PRACTICES Low value warning unit Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Screwdriver 1 pc Persons Tab.
  • Page 567 INDICATING/ RECORDING SYSTEMS 1 – Screw M4 x 16 5 – Washer ø4.3 x 9 x 0.9 2 – LVW unit For information: 3 – LVW connector 6 – Instrument floor 4 – Self-locking nut M4 Fig. 31-4 Low Value Warning Unit Removal / Installation CENTRAL WARNING SYSTEMS Chapter 31-50 14.
  • Page 568 INDICATING/ RECORDING SYSTEMS Fuel reserve switch Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Soldering gun 1 pc Pliers 1 pc Persons Tab. 31-2 Recommended tools, materials, persons and documentation Fuel reserve switch removal: Set the MASTER SWITCH to OFF position.
  • Page 569 INDICATING/ RECORDING SYSTEMS Oil pressure switch Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Soldering gun 1 pc Pliers 1 pc Persons Tab. 31-3 Recommended tools, materials, persons and documentation Oil pressure switch removal: Set the MASTER SWITCH to OFF position.
  • Page 570 INDICATING/ RECORDING SYSTEMS ACI stall warner Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Knife 1 pc Double sided tape 3M VHB 5925 F or equivalent Persons Tab.

  • Page 571: Aci Stall Warner

    INDICATING/ RECORDING SYSTEMS 1 – ACI stall warner 3 – Cover film 2 – Double sided tape Fig. 31-5 ACI Stall Warner Removal / Installation SV-ADAHRS-200 module For removal / installation procedures refer to Chapter 34-10. SV-D1000 display For removal / installation procedures refer to Chapter 39-10. Stall warning lamp For removal / installation procedures refer to Chapter 39-10.
  • Page 572 INDICATING/ RECORDING SYSTEMS This page is left blank intentionally Chapter 31-50 CENTRAL WARNING SYSTEMS Page 31-16 Effectivity: ALL 14. 05. 2020...
  • Page 573 MAINTENANCE PRACTICES OF FIXED GEAR ....... 6 Main wheel fairing ............. 6 Main wheels Beringer ............8 Main wheels Aerospool ........... 11 Main landing gear leg ............13 DESCRIPTION OF MAIN RETRACTABLE GEAR ....17 MAINTENANCE PRACTICES OF MAIN RETRACTABLE GEAR ..................
  • Page 574 32-40 WHEELS AND BRAKES ..........71 DESCRIPTION ................ 71 Beringer wheels and brake system ......... 71 Aerospool wheels and brake system ......72 MAINTENANCE PRACTICES ..........76 Main wheels Beringer ............. 76 Main wheels Aerospool ........... 79 Nose wheel Beringer............81 Nose wheel Aerospool ............

  • Page 575: General

    LANDING GEAR 32-00 GENERAL INTRODUCTION Introduction to landing gear The aircraft is equipped with a fixed tricycle landing gear with steerable nose wheel (Fig. 32-1). Fixed gear version: The main wheels are mounted on composite spring legs, the nose leg is made of metal with the composite fork made of carbon. The wheels are equipped with the wheel fairings.
  • Page 576 LANDING GEAR Retractable landing gear 1 – Left main landing gear 3 – Nose landing gear 2 – Right main landing gear 4 – Hydraulic system Fig. 32-1 Landing Gear (page 2 of 2) Chapter 32-00 GENERAL Page 32-4 Effectivity: ALL 14.

  • Page 577: Main Gear

    LANDING GEAR 32-10 MAIN GEAR DESCRIPTION OF MAIN FIXED GEAR The main landing gear consists of two composite landing gear legs (1, Fig. 32-2). The main landing gear legs are fixed in the inner (4) and outer ribs (5) inside of the fuselage in the wing central section.

  • Page 578: Maintenance Practices Of Fixed Gear

    LANDING GEAR MAINTENANCE PRACTICES OF FIXED GEAR Main wheel fairing The aircraft may be equipped with main wheel fairing Model 2005 or Model 2011. They differ in design but removal/installation instructions are the same. Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher.
  • Page 579 LANDING GEAR On the inner side of the main landing gear, install the inner cover (2) using the bolt (6); apply Loctite 243 on the bolt (5) thread, install the washer (7) and screw the bolt (5) in. Install the cable tie (8) around the upper part of the inner cover (2) and the fairing (1).

  • Page 580: Main Wheels Beringer

    LANDING GEAR Main wheels Beringer Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Phillips screwdriver 1 pc Pliers 1 pc Wrench 32 1 pc Persons Tab.
  • Page 581 LANDING GEAR Main wheel installation: Before assembling the main landing gear, ensure the wheel axle connection is not damaged. Align the brake disc (3, Fig. 32-4) with the gap in the brake caliper; install the wheel (1) on the wheel axle (7). NOTE Tabs of the brake disc (3) must fit between the wheel disc tabs.
  • Page 582 LANDING GEAR 1 – Main wheel 5 – Distance tube 2 – Safety stainless wire ø1 mm 6 – Split pin ø0.8 mm 3 – Brake disc 7 – Brake caliper with wheel axle 4 – Nut M25 Fig. 32-4 Main Wheel Removal / Installation Chapter 32-10 MAIN GEAR Page 32-10...

  • Page 583: Main Wheels Aerospool

    LANDING GEAR Main wheels Aerospool The procedure for removal of the left main wheel is described. Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY...
  • Page 584 LANDING GEAR Main wheel installation: Install brake disc (145) and distance tube (3). Install the main wheel (7) on the wheel axle and attach the brake disc (15) to the main wheel by washers (14) and screws (13) secured by Loctite 243. Bent the tabs of washers (14).
  • Page 585 LANDING GEAR Main landing gear leg Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Wrench 13 1 pc Hex key 6 1 pc Screwdriver 1 pc...
  • Page 586 LANDING GEAR Main landing gear leg installation: Before assembly of the main landing gear leg, check the outer surface of the landing gear leg for any cracks and ensure the wheel axle connection is not damaged. Insert the main landing gear leg (1, Fig. 32-6) into the fuselage. On the inner attachment (23) install the bolts (20), washers (7) and slightly tighten the nuts (19).
  • Page 587 LANDING GEAR Fig. 32-6 Main Landing Gear Leg Removal / Installation (page 1 of 2) MAIN GEAR Chapter 32-10 14. 05. 2020 Effectivity: ALL Page 32-15...

  • Page 588: Main Landing Gear Leg

    LANDING GEAR 1 – Main landing gear leg 15 - Spacer washer 2 – Wheel axle with brake caliper 16 - Rubber plate 3 – Bolt M8 x 52 17 - Lower bracket 4 – Bolt M8 x 57 18 - Bolt M8 x 58 5 –...

  • Page 589: Description Of Main Retractable Gear

    LANDING GEAR DESCRIPTION OF MAIN RETRACTABLE GEAR The main landing gear consists of two metal landing gear legs with elastomer damping elements (1, Fig. 32-7). The main landing gear legs are attached in the brackets to the main spar (3) and auxiliary spar (4) inside of the fuselage in the wing central section.

  • Page 590: Maintenance Practices Of Main Retractable Gear

    LANDING GEAR MAINTENANCE PRACTICES OF MAIN RETRACTABLE GEAR Main landing gear door Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Pliers 1 pc Wrench 10 2 pcs Persons Tab.
  • Page 591 LANDING GEAR 1 – Spring 3 – Trailing arm’s lever 2 – Main landing gear door Fig. 32-8 Main Landing Gear Door Spring Removal / Installation MAIN GEAR Chapter 32-10 14. 05. 2020 Effectivity: ALL Page 32-19...

  • Page 592: Main Landing Gear Door

    LANDING GEAR 1 – Main landing gear door 4 – Bolt M5 x 26 2 – Hinge 1 5 – Washer ø5.4 3 – Hinge 2 6 – Self-locking nut M5 Fig. 32-9 Main Landing Gear Door Removal / Installation Chapter 32-10 MAIN GEAR Page 32-20...

  • Page 593: Main Wheels Beringer

    LANDING GEAR Main wheels Beringer Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Phillips screwdriver 1 pc Pliers 1 pc Slotted nut wrench 1 pc Persons Tab.
  • Page 594 LANDING GEAR 1 – Wheel axle 6 – Ring 2 – Wheel adaptor 7 – Tab washer 3 – Safety stainless steel wire ø1 mm 8 – Slotted nut 4 – Brake disc 9 – Trailing arm 5 – Main wheel Fig.

  • Page 595: Main Landing Gear Leg

    LANDING GEAR Main landing gear leg Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 1 pc Wrench 13 1 pc Hex key 6 1 pc Screwdriver 1 pc...
  • Page 596 LANDING GEAR Trailing arm removal: Remove nut (39), washer (40) and bolt (41). Remove split pin (42), nut (43), washer (44) and bolt (45). Remove trailing arm (2). Remove grounding wire (46) by removing nut (47) washer (48) and bolt (49). Damper removal: Remove nuts (50, 51), silent block plate (52) and strop rubber (53) and pull out the damper.
  • Page 597 LANDING GEAR Main landing gear leg installation: NOTE All movable joints need to be grease before installation. Before assembly of the main landing gear leg, check the outer surface of the landing gear leg parts for any cracks and ensure the wheel axle connection is not damaged.
  • Page 598 LANDING GEAR Damper installation: Assemble damper body (56), silent blocks (54), damper rings (55), bearing rod end (59), washer (57) and nut (58). Attach the damper body (56) to the main landing gear leg (1), using stop rubber (53), silent block plate (52), and nuts (51, 50). Trailing arm installation: Attach trailing arm (2) to main landing gear leg (1) by using screw (45), washer (44), nut (43) and secure with split pin (42).
  • Page 599 LANDING GEAR Carry out a test of retracting and extending of landing gear by hand and check: • Collision of all movable parts. In case of collision adjust the bearing rod ends by unscrewing or screwing to achieve straight and smooth movement. •...
  • Page 600 LANDING GEAR Fig. 32-11 Main Landing Gear Leg Removal / Installation (page 1 of 5) Chapter 32-10 MAIN GEAR Page 32-28 Effectivity: ALL 14. 05. 2020...
  • Page 601 LANDING GEAR Fig. 32-11 Main Landing Gear Leg Removal / Installation (page 2 of 5) MAIN GEAR Chapter 32-10 14. 05. 2020 Effectivity: ALL Page 32-29...
  • Page 602 LANDING GEAR Fig. 32-11 Main Landing Gear Leg Removal / Installation (page 3 of 5) Chapter 32-10 MAIN GEAR Page 32-30 Effectivity: ALL 14. 05. 2020...
  • Page 603 LANDING GEAR 1 – Main landing gear leg 16 – Main strut console 2 – Trailing arm 17 – Serrated washer Ø6.4 3 – Short strut 18 – Bolt M6 x 15 4 – Main strut 19 – Side strut eye hinge 5 –...
  • Page 604 LANDING GEAR 31 – Nut M8 62 – Washer Ø30 x 10 32 – Washer Ø8.4 63 – Spring 33 – Bolt M8 x 28 64 – Bolt M10 x 46 Adapted 34 – Bolt M6 x 16 65 – Bearing rod end 1040 35 –...
  • Page 605 LANDING GEAR Fig. 32-12 Main Landing Gear Leg Geometry Adjustment (illustrative figure) Fig. 32-13 Main and Short Struts Geometry Adjustment MAIN GEAR Chapter 32-10 14. 05. 2020 Effectivity: ALL Page 32-33...
  • Page 606 LANDING GEAR This page is left blank intentionally Chapter 32-10 MAIN GEAR Page 32-34 Effectivity: ALL 14. 05. 2020...

  • Page 607: Nose Gear

    LANDING GEAR 32-20 NOSE GEAR DESCRIPTION OF NOSE FIXED GEAR The metal nose landing gear leg (1, Fig. 32-14) with carbon fork (2) is attached to the firewall in the lower (3) and upper (4) supports. The nose landing gear incorporates bungees (5) (nose leg - lower support) and rubber damper (nose leg - upper support).

  • Page 608: Maintenance Practices Of Nose Fixed Gear

    LANDING GEAR MAINTENANCE PRACTICES OF NOSE FIXED GEAR Nose wheel fairing Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Hex key 6 1 pc Wrench 10...

  • Page 609: Nose Wheel Fairing

    LANDING GEAR 1 – Nose wheel fairing 6 – Bolt M5 x 12 2 – Cover 7 – Washer ø8.4 x 24 x 2 3 – Bolt M8 x 35 8 – Washer ø6.4 x 18 x 1.6 4 – Bolt M6 x 16 9 –...

  • Page 610: Nose Wheel Beringer/Aerospool

    Unscrew the axle bolt (5), remove the washer (6) and pull the nose wheel axle (2) out. Remove the nose wheel (1) with the short distance tube (4) and the adaptor (3a) for Beringer wheel / distance tube (3b) for Aerospool wheel. Nose wheel Beringer/Aerospool installation: Insert the nose wheel (1, Fig.
  • Page 611 LANDING GEAR Fig. 32-16 Nose Wheel Removal / Installation (page 1 of 3) WHEELS AND BRAKES Chapter 32-40 14. 05. 2020 Effectivity: ALL Page 32-39...
  • Page 612 LANDING GEAR Fig. 32-16 Nose Wheel Removal / Installation (page 2 of 3) Chapter 32-40 WHEELS AND BRAKES Page 32-40 Effectivity: ALL 14. 05. 2020...
  • Page 613 7 – Wheel fairing bracket Nose wheel axle 3a – Adaptor (Beringer wheel) 8 – Bolt M8 x 12 3b – Short distance tube (Aerospool wheel) 9 – Washer ø8.4 x 16 x 1.6 4a – Short distance tube (Beringer wheel) 10 – Fork 4b –...
  • Page 614 LANDING GEAR Nose landing gear leg Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Wrench 13 1 pc Wrench 24 2 pcs Screwdriver 10 1 pc...
  • Page 615 LANDING GEAR NOTE Housing assembly consists of items (7), (8) and (9). Remove housing assembly by removing nuts (16), washers (15) and bolts (14). Remove the nose landing gear leg (1). Remove the upper and lower supports (see 2.D.(1)). (m) As necessary, remove the carbon fork (18) by removing the nuts (16), washers (15), bolts (19) and fork plate (20).
  • Page 616 LANDING GEAR Tighten all nuts (8, Fig. 32-20) fastening upper support assembly (1) and lower support (3). (m) Tighten all nuts (16, Fig. 32-19) on the bearing housing (7). Secure the bolts (9) by Loctite 243. Check free movement of the nose landing gear leg (1). At one end of the rubber ropes (12) make loop ...

  • Page 617: Nose Landing Gear Leg

    LANDING GEAR Nose landing gear inspection / check In the following table the permissible plays for nose landing gear attachment are shown. These values should not be exceeded in operation. PROCEDURE MAX. MAX. PROCEDURE TO FIND SYSTEM TO REMEDY A PRODUCT.
  • Page 618 LANDING GEAR 1 – Nose landing gear leg 9 – 17 – Split pin ø2 x 32 Bolt M4 x 5 2 – 10 – Tube 18 – Carbon fork Upper support assy 3 – 11 – Rubber plate 19 – Bolt M6 x 28 Lower support 4 –...

  • Page 619: Upper And Lower Supports

    LANDING GEAR Upper and lower supports Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Wrench 8 1 pc Loctite 243 Persons Tab.
  • Page 620 LANDING GEAR 1 – Upper support casing 7 – Bolt M6 x 28 2 – Upper support 8 – Self-locking nut M6 3 – Lower casing 9 – Washer ø6.4 x 18 x 1.6 4 – Bushing 10 – Washer ø6.4 x 12 x 1.6 5 –...

  • Page 621: Description Of Nose Retractable Gear

    LANDING GEAR DESCRIPTION OF NOSE RETRACTABLE GEAR The nose landing gear leg is metal (1, Fig. 32-21) with metal trailing arm (2) and elastomer damping elements. It is attached to the engine mount (7). Front drag strut (3), rear drag strut (4), gas strut (5) and hydraulic actuator (6) ensure the operation of nose landing gear leg.

  • Page 622: Maintenance Practices Of Nose Retractable Gear

    LANDING GEAR MAINTENANCE PRACTICES OF NOSE RETRACTABLE GEAR Nose wheel Beringer Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 22 1 pc Slotted nut wrench 1 pc Persons Tab.
  • Page 623 LANDING GEAR 1 – Trailing arm 5 – Wheel 2 – Axle 6 – Washer 3 – Ring 7 – Tab washer 4 – Wheel adaptor 8 – Nut Fig. 32-22 Nose wheel Removal / Installation WHEELS AND BRAKES Chapter 32-40 14.
  • Page 624 LANDING GEAR Nose landing gear Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 10 2 pcs Wrench 13 1 pc Wrench 17 2 pcs Screwdriver 10 1 pc Loctite 243...
  • Page 625 LANDING GEAR Trailing arm removal: Remove split pin (11), nut (15), washer (14) and bolt (9). Remove nut (15), washer (14) and bolt (13) to release the trailing arm (2). Damper removal: Remove screws (29) and cover (28). Remove nuts (27), silentblock plate (51) and rubber stops (25, 26). Pull damper out of nose gear leg (1).
  • Page 626 LANDING GEAR Damper installation: Put the damping elements (17, 18) and inner rings (19) on damper body (16). Put assembled damper into nose gear leg (1). Install rubber stops (25, 26), silentblock plate (51) and nut (27). Tight the nut to adjust the geometry according to Fig. 32-24 and lock the position with second nut (27, Fig.
  • Page 627 LANDING GEAR (aa) Carry out a test of retracting and extending of landing gear by hand and check: • Collision of all movable parts. In case of collision adjust the bearing rod ends by unscrewing or screwing to achieve straight and smooth movement. •...
  • Page 628 LANDING GEAR Fig. 32-23 Nose Landing Gear Removal / Installation (page 1 of 2) Chapter 32-40 WHEELS AND BRAKES Page 32-56 Effectivity: ALL 14. 05. 2020...
  • Page 629 LANDING GEAR 1 – Nose gear leg 27 – Self-locking nut M10 DIN985 2 – Trailing arm 28 – Cover 3 – Front drag strut 29 – Screw M4 x 6 4 – Rear drag strut 30 – Split pin 1.6 x 16 5 –...
  • Page 630 LANDING GEAR Fig. 32-24 Nose Landing Gear Leg Geometry Adjustment Fig. 32-25 Drag Strut Geometry Adjustment Chapter 32-40 WHEELS AND BRAKES Page 32-58 Effectivity: ALL 14. 05. 2020...
  • Page 631 LANDING GEAR 1 – Hydraulic actuator 5 – Ball stud 2 – Bearing end 6 – Ball socket 3 – Gas strut 7 – Safety clip 4 – Extension Fig. 32-26 Gas Strut and Hydraulic Actuator Assembly / Disassembly WHEELS AND BRAKES Chapter 32-40 14.
  • Page 632 LANDING GEAR This page is left blank intentionally Chapter 32-40 WHEELS AND BRAKES Page 32-60 Effectivity: ALL 14. 05. 2020...

  • Page 633: Nose Landing Gear

    LANDING GEAR 32-30 EXTENSION AND RETRACTION DESCRIPTION The aircraft with retractable landing gear is equipped with hydraulic extension and retraction system. Hydraulic system is installed under the co-pilot seat and consists of hydraulic unit (1, Fig. 32-27), hydraulic hoses and hydraulic actuators, which operate extending and retracting of landing gear legs.

  • Page 634: Maintenance Practices

    LANDING GEAR MAINTENANCE PRACTICES Hydraulic system Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 13 1 pc Persons Tab. 32-17 Recommended tools, materials, persons and documentation CAUTION THE HYDRAULIC SYSTEM OPERATES AT HIGH PRESSURE.
  • Page 635 LANDING GEAR 1 – Banjo fitting HK40 3 – Socket 2 – Olive 4 – Hydraulic hose Fig. 32-28 Banjo Fitting Installation WHEELS AND BRAKES Chapter 32-40 14. 05. 2020 Effectivity: ALL Page 32-63...
  • Page 636 LANDING GEAR Hydraulic hoses removal from hydraulic actuator: Remove banjo bolt (4, Fig. 32-29), sealing rings (2), banjo fitting (1) and extension (3) from hydraulic actuator’s rear fitting (6). Remove banjo bolt (4), sealing rings (2) and banjo fitting (1) from hydraulic actuator’s front fitting (7).
  • Page 637 LANDING GEAR Hydraulic hoses removal from hydraulic unit: Remove the right laminate seat (Chapter 25-10). Remove banjo bolt (4, Fig. 32-30), sealing rings (2) and banjo fitting (1) from distribution box (4) of hydraulic unit. Hydraulic hoses installation to hydraulic unit: CAUTION NEW SEALING RINGS MUST BE ALWAYS INSTALLED! Install banjo fitting (1, Fig.
  • Page 638 LANDING GEAR Hydraulic system bleeding: Set MASTER SWITCH to OFF position. Set HYDRAULIC PUMP switch to OFF position. Remove the right laminate seat (Chapter 25-10). Open cap of hydraulic fluid reservoir (1, Fig. 32-31) and remove all possible amount of hydraulic fluid by using syringe. Disconnect hydraulic hoses form hydraulic actuators and put the disconnected ends to containers.
  • Page 639 LANDING GEAR 1 – Hydraulic fluid reservoir 5 – Left main landing gear - Front inlet 2 – Nose landing gear – Rear inlet 6 – Right main landing gear - Rear inlet 3 – Nose landing gear – Front inlet 7 –...
  • Page 640 LANDING GEAR Gear blocking Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Pliers 1 pc Persons Tab. 32- 18 Recommended tools, materials, persons and documentation NOTE The gear blocking and gear blocking switch is installed behind the instrument panel.
  • Page 641 LANDING GEAR 1 – Gear blocking unit 6 – Screw M4 x 12 2 – Connector 7 – Washer ø4.3 x 9 x 0.9 3 – Hose clamp 8 – Self-locking nut M4 4 – Static pressure hose 9 – Panel 5 –...
  • Page 642 LANDING GEAR 1 – Gear blocking test switch 4 – Console 2 – Nut 5 – Serrated washer 3 – External tab washer 6 – Wires Fig. 32-33 Gear Blocking TEST Switch Installation / Removal Chapter 32-40 WHEELS AND BRAKES Page 32-70 Effectivity: ALL 14.

  • Page 643: Wheels And Brakes

    LANDING GEAR 32-40 WHEELS AND BRAKES DESCRIPTION Beringer wheels and brake system This chapter describes the wheels and brake system Beringer and its operation. The main landing gear may be equipped with an aluminium Beringer wheel discs (1, Fig. 32-34) with tires 15x6.00-6 (2). The wheel discs consist of split rim with two ball bearings.

  • Page 644: Aerospool Wheels And Brake System

    13x5.00-6 (4) including inner tube. The wheel disc consists of split rim with two ball bearings. The main gear wheels are equipped with Aerospool hydraulic brakes which are controlled by the brake lever (10) located on the central console. The brake lever acts through the push rod and double-arm lever on the master cylinder (7) located under the left seat.
  • Page 645 LANDING GEAR 1 – Main wheel disc 7 – Master cylinder 2 – Main wheel tire 8 – Pressure limiter 3 – Nose wheel disc 9 – Brake fluid reservoir 4 – Nose wheel tire 10 – Brake lever 5 – Brake caliper 11 –...
  • Page 646 4 – Nose wheel tire (including inner tube) 10 – Brake lever 5 – Brake caliper 11 – Brake hose 6 – Brake disc Fig. 32-35 Brake System Aerospool (illustrative figure) Chapter 32-40 WHEELS AND BRAKES Page 32-74 Effectivity: ALL...
  • Page 647 3 – Brake lever Fig. 32-36 Beringer Brake System Scheme 1 – Master cylinder 3 – Brake caliper 2 – Brake lever Fig. 32-37 Aerospool Brake System Scheme WHEELS AND BRAKES Chapter 32-40 14. 05. 2020 Effectivity: ALL Page 32-75...

  • Page 648: Maintenance Practices

    LANDING GEAR MAINTENANCE PRACTICES All wheels (with tires fitted) must be balanced before the installation. If a new tire is installed, the wheel must be re-balanced (with the tire fitted) before the installation. Unbalanced wheels can cause vibration to the landing gear. Main wheels Beringer Type of maintenance: Line...
  • Page 649 LANDING GEAR Main wheel bearings replacement: Remove the main wheel (Chapter 32-10). Deflate the tire to zero pressure. Separate the tire (1, Fig. 32-38) from the discs (2; 3). Remove the bolts (5) and disassemble discs (2; 3). Remove the O ring (4). Use Circlip pliers to remove the circlips (8;...
  • Page 650 LANDING GEAR Fig. 32-39 Order of Bolts Tightening and Beringer Jig Chapter 32-40 WHEELS AND BRAKES Page 32-78 Effectivity: ALL 14. 05. 2020...

  • Page 651: Main Wheels Aerospool

    LANDING GEAR Main wheels Aerospool Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: QUANTITY ITEM Wrench 10 2 pcs Circlip pliers 1 pc Persons Aerospool documentation Tab.
  • Page 652 4 – Distance tube wheel 10 – Bearing 5 – Internal disc 11 – Retaining ring 6 – Washer 6 x 12 x 0.5 Fig. 32-40 Main Wheel Aerospool Chapter 32-40 WHEELS AND BRAKES Page 32-80 Effectivity: ALL 14. 05. 2020...
  • Page 653 LANDING GEAR Nose wheel Beringer Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Hex key 5 1 pc Beringer jig 1 pc Circlip pliers 1 pc O ring 2 pcs...

  • Page 654: Nose Wheel Beringer

    LANDING GEAR Nose wheel bearings replacement: Remove the wheel (Chapter 32-20). Deflate the tire to zero pressure. Separate the tire (1, Fig. 32-41) from the discs (2; 3). Remove the bolts (4) and disassemble discs (2; 3). Remove the O ring (5). Use Circlip pliers to remove the circlips (7;...
  • Page 655 LANDING GEAR Nose wheel Aerospool Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Fork wrench 10 2 pcs Circlip pliers 1 pc Persons Aerospool documentation Tab.

  • Page 656: Nose Wheel Aerospool

    4 – Distance tube wheel 10 – Bearings 5 – Internal disc 11 – Retaining rings 6 – Washer 6 x 12 x 0.5 Fig. 32-42 Nose Wheel Aerospool Chapter 32-40 WHEELS AND BRAKES Page 32-84 Effectivity: ALL 14. 05. 2020...

  • Page 657: Brake System Beringer

    LANDING GEAR Brake system Beringer Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 12 1 pc Wrench 10 1 pc Socket set 14 1 pc Screwdriver 5 1 pc...
  • Page 658 LANDING GEAR Fig. 32-43 Beringer Brake System Components Removal / Installation (Page 1 of 2) Chapter 32-40 WHEELS AND BRAKES Page 32-86 Effectivity: ALL 14. 05. 2020...
  • Page 659 LANDING GEAR 1 – 16 – Brake hose L 31 – Washer ø6.4 x 12 x 1.6 Brake fluid reservoir 2 – 17 – Connecting brake hose 32 – Washer ø6.4 x 10 x 1.6 Master cylinder assembly 3 – 18 –...
  • Page 660 LANDING GEAR Master cylinder assembly and brake lever removal: Drain the brake fluid from the brake system (see 2.E.(11)). Remove the pedestal panel (Chapter 27-50). Remove the left laminated seat (Chapter 25-10). Remove the elevator push rod in the central tunnel (Chapter 27-30). Remove the hose clamp (35, Fig.
  • Page 661 LANDING GEAR Assemble the brake hoses (15; 17) with banjo fittings (23) (see 2.E.(10)). Connect the brake hoses (15; 17) to the master cylinder (3), using banjo bolt (21) and gasket rings (24). CAUTION A NEW GASKET RINGS MUST BE INSTALLED AT EACH MASTER CYLINDER ASSEMBLY.
  • Page 662 LANDING GEAR Install the pedestal panel (Chapter 27-50). Carry out a test and check: • If all bolt connections are tight. • Tightness and function of the brake system. • That no foreign objects remain in the aircraft. Brake caliper removal: Jack the aircraft and secure the tail (Chapter 07-10).
  • Page 663 LANDING GEAR Install the main wheel (Chapter 32-10). Fill the brake system with the brake fluid (see 2.C.(11)). Carry out a test and check: • If all bolt connections are tight. • Tightness and function of the brake system. • That no foreign objects remain in the aircraft. Brake hoses removal: Cut the hose fittings at the end of hoses and pull them out.
  • Page 664 LANDING GEAR Push the olive against a flat solid surface, make sure that the PTFE tube is fully settled on the olive (Fig. 32-46). Fig. 32-46 Settled PTFE Tube on the Olive Insert the main fitting body, lubricate the thread, screw the socket in and tighten using a Vice (Fig.
  • Page 665 LANDING GEAR (11) Brake system draining, filling and bleeding: Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Beringer jig 1 pc Cloth 2 pcs Draining hose ø6 x 300 mm 3 pcs Container...
  • Page 666 LANDING GEAR Pump on the Beringer jig until all brake fluid has been drained into the containers. Remove the Beringer jig from brake fluid reservoir. Install the bleeding container on the brake fluid reservoir (Fig. 32-50). Remove drain hoses from caliper’s bleeding screws and install the Beringer jigs on both caliper’s bleeding screws (1, Fig.
  • Page 667 LANDING GEAR (aa) Carry out a test and check: • If all bleeding screws are tight. • Tightness of the brake system. (bb) That no foreign objects remain in the aircraft. Fig. 32-48 Bleeding Points (illustrative figure) WHEELS AND BRAKES Chapter 32-40 14.
  • Page 668 LANDING GEAR Fig. 32-49 Beringer Jig (illustrative figure) Fig. 32-50 Bleeding Container (illustrative figure) Chapter 32-40 WHEELS AND BRAKES Page 32-96 Effectivity: ALL 14. 05. 2020...
  • Page 669 LANDING GEAR (12) Brake pads replacement: The brake pads must be replaced when the thickness of the braking layer is under 2 mm. The brake pads must be replaced on both brake calipers. Type of maintenance: Line Personnel qualification: Independent certifying staff qualified...
  • Page 670 LANDING GEAR 1 – Bolt M8 x 41 4 – Brake pad 2 – Bolt M8 x 30 5 – Brake caliper body 3 – Brake pad support Fig. 32-51 Beringer Brake Pads FG Chapter 32-40 WHEELS AND BRAKES Page 32-98 Effectivity: ALL 14.
  • Page 671 LANDING GEAR 1 – Bolt M6 x 15 4 – Brake pad 2 – Locking plate 5 – Brake caliper body 3 – Brake pad support Fig. 32-52 Beringer Brake Pads RG WHEELS AND BRAKES Chapter 32-40 14. 05. 2020 Effectivity: ALL Page 32-99...

  • Page 672: Brake System Aerospool

    2 pcs Vaseline Sealing adhesive tape Persons Aerospool documentation - Assembly instructions for hose and banjo fittings Tab. 32-26 Recommended tools, materials, persons and documentation Master cylinder and brake lever removal: Drain the brake fluid from the brake system (see 2.F.(7)).
  • Page 673 LANDING GEAR • Remove the brake lever-short (8), by unscrew the bolt (13), nut (21) with washers (24). • Remove the mount brake drum (4), by unscrew the screw (17) and nut (21). • Remove the mount grid cubes (11) and grid cube (5) by unscrew the bolts (14;...
  • Page 674 LANDING GEAR Install the elevator push rod in the central tunnel (Chapter 27-30). Fill the brake system with the brake fluid (see 2.F.(7)). Install the left laminated seat (Chapter 25-10). Install the pedestal panel (Chapter 27-50). (m) Carry out a test and check: •...
  • Page 675 1 pc Brake fluid Wheel chocks 4 pcs Persons Aerospool documentation - Brake system bleeding procedure Tab. 32-27 Recommended tools, materials, persons and documentation Put the aircraft on levelled surface, secure against moving and release the brake lever. Remove the main landing gear fairings (Chapter 32-10).
  • Page 676 1 pc Phillips screwdriver 1 pc Brake fluid Persons Aerospool documentation - Brake system bleeding procedure Tab. 32-28 Recommended tools, materials, persons and documentation Put the aircraft on levelled surface, secure against moving and release the brake lever. Remove the main landing gear fairings (Chapter 32-10).
  • Page 677 LANDING GEAR Brake system bleeding: Put the aircraft on leveled surface and release the brake lever. Remove the main landing gear fairings (Chapter 32-10). Install wheel chocks. Remove the left laminated seat (Chapter 25-10). Unscrew the cap on the fluid tank (31, Fig. 32-53) and pour the brake fluid.
  • Page 678 LANDING GEAR Fig. 32-53 Aerospool Brake System Components Removal / Installation (page 1 of 2) Chapter 32-40 WHEELS AND BRAKES Page 32-106 Effectivity: ALL 14. 05. 2020...
  • Page 679 39 – O-ring 25 x 2 59 – Banjo bolt 20 – Self-locking nut M6 40 – Cuff Fig. 32-53 Aerospool Brake System Components Removal / Installation (page 2 of 2) WHEELS AND BRAKES Chapter 32-40 14. 05. 2020 Effectivity: ALL...
  • Page 680 LANDING GEAR This page is left blank intentionally Chapter 32-40 WHEELS AND BRAKES Page 32-108 Effectivity: ALL 14. 05. 2020...

  • Page 681: Steering

    LANDING GEAR 32-50 STEERING DESCRIPTION The aircraft is equipped with a steerable nose gear. The steering is controlled by the rudder pedals. Fixed gear version: The rudder pedals are connected to the nose landing gear leg by means of push-pull rods fitted with bearing eyes. The hole in the firewall for push- pull rod is protected by a flange with sleeve.
  • Page 682 LANDING GEAR Steering push rods installation: Jack the aircraft and secure the tail (Chapter 07-10). If necessary, install the sleeves (3, Fig. 32-54) and sleeve flanges (4) using screws (7) on the firewall. Slide the push rods (1; 2) through the firewall and the sleeve. Then slide the hose clamp (14) on the sleeve (3).
  • Page 683 LANDING GEAR Fig. 32-54 Steering Push Rods Removal / Installation (page 1 of 2) STEERING Chapter 32-50 14. 05. 2020 Effectivity: ALL Page 32-111...
  • Page 684 LANDING GEAR 1 – Washer ø6.4 x 12 x 1.6 Push rod RH 2 – 10 - Washer ø6.4 x 30 x 1.6 Push rod LH 3 – 11 - Serrated locking washer ø6.4 Sleeve 4 – Sleeve flange 12 - Self-locking nut M6 5 –...

  • Page 685: Steering Push Rods (Fg)

    LANDING GEAR Steering bowdens (RG) Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 8 1 pcs Wrench 10 2 pcs Wrench 19 2 pcs Hex key 5 1 pc Screwdriver...
  • Page 686 LANDING GEAR Connect the steering bowdens (1; 2) to the foot control using bolts (7), washers (10) and nuts (15). Bolts insert from the aircraft axis. Attach the steering bowdens (1; 2) to the central tunnel (25) using Bowden pads (4), Bowden brackets (5), washers (12), bolts (9) and nuts (15).
  • Page 687 LANDING GEAR Fig. 32-55 Fig. 32-1 Steering Bowdens Removal / Installation (page 1 of 2) STEERING Chapter 32-50 14. 05. 2020 Effectivity: ALL Page 32-115...
  • Page 688 LANDING GEAR 1 – Bowden LH 15 - Self-locking nut M6 2 – Bowden RH 16 - Nut M6 3 – Bowden end 17 - Nut M5 4 – Bowden pad 18 - Bearing end 5 – Bowden bracket 19 - Nut M12 6 –...
  • Page 689 LIGHTS 33 LIGHTS CONTENTS Chapter Description Page 33-00 GENERAL ................. 3 INTRODUCTION ............... 3 TROUBLESHOOTING ............... 4 33-40 EXTERIOR LIGHTING ............5 DESCRIPTION ................5 AveoEngineering AveoFlash LSA ........5 AveoEngineering AveoFlashLP LSA ......... 5 AveoEngineering Ultra Galactica ........5 Whelen A600 ..............
  • Page 690 LIGHTS 33-60 INTERIOR LIGHTING............19 DESCRIPTION ................ 19 AveoEngineering Aveo EyeBeam touch ......19 LED light strip ..............19 MAINTENANCE PRACTICES ..........21 Aveo EyeBeam touch light ..........21 LED light strip ..............23 Chapter 33 CONTENTS Page 33-2 Effectivity: ALL 14.

  • Page 691: General

    LIGHTS 33-00 GENERAL INTRODUCTION This chapter describes the system and maintenance practices about the lighting on the airplane. GENERAL Chapter 33-00 14. 05. 2020 Effectivity: ALL Page 33-3...

  • Page 692: Troubleshooting

    LIGHTS TROUBLESHOOTING TROUBLE POSSIBLE CAUSE REMEDY Circuit-breaker not set or Set/replace the circuit- defective. breaker. Defective position light Replace the switch. switch. Both position lights do not Defective wiring Carry out a continuity test operate. of the wiring. Repair/replace defective wiring.

  • Page 693: Exterior Lighting

    LIGHTS 33-40 EXTERIOR LIGHTING DESCRIPTION This chapter contains information on servicing the anti-collision/position, anti-collision and landing lights. The anti-collision/position lights (1; 2, Fig. 33-1) are mounted to the outboard surface of each wing tip. The light assembly includes a LED anti-collision lights and position lights with forward (red-left, green-right) and white rear light.

  • Page 694: Halogen Mr16 12V/20W

    LIGHTS Installed variants of landing lights: Halogen MR16 12V/20W The aircraft may be equipped with Halogen MR16 12V/20W landing lights. The lights are located on bottom engine cowling. LED MR16 12V/4,5W The aircraft may be equipped with LED MR16 12V/4,5W landing lights. The lights are located on bottom engine cowling.

  • Page 695: Maintenance Practices

    LIGHTS MAINTENANCE PRACTICES ACL/POS lights AveoFlash LSA / AveoFlashLP LSA / Ultra Galactica Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Phillips screwdriver 1 pc Hex key 3 1 pc Knife...
  • Page 696 LIGHTS Anti-collision/position light polishing: Polish the lights after installation. NOTE Under no circumstances should any petroleum-based product be used to clean the lights. 1 – Anti-collision/position light 5 – Spiral hose ø6 2 – Gasket For information: 3 – Screw M3 x 20 / M5 x 45 6 –...
  • Page 697 LIGHTS ACL light MiniMax TS White / MiniMax TS Red Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Phillips screwdriver 1 pc Wrench 7 1 pc Knife 1 pc...
  • Page 698 LIGHTS NOTE Fig. 33-3 shows installation of anti-collision light on the upper surface of fuselage, installation on the lower surface of fuselage is analogic. 1 – Anti-collision light 5 – Nut 2 – Gasket For information: 3 – Screw 6 – Fuselage 4 –...
  • Page 699 LIGHTS ACL light Double Dual Magnum Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Phillips screwdriver 1 pc Wrench 7 1 pc Wrench 8 1 pc Knife 1 pc...
  • Page 700 LIGHTS NOTE Under no circumstances should any petroleum-based product be used to clean the lights. Double Dual Magnum module removal: Make sure that the ignition switch is set to OFF. Remove the left seat (Chapter 06-00). Disconnect the connectors. Loosen the nuts (10, Fig. 33-4), remove the washers (7; 8) and pull out the light module (3).
  • Page 701 LIGHTS Landing lights Halogen / LED Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Silicone Persons Tab. 33-4 Recommended tools, materials, persons and documentation WARNING ENGINE IGNITION MUST BE SWITCHED OFF.
  • Page 702 LIGHTS 1 – Landing light 5 – Washer ø4.3 x 9 x 0.8 2 – Holder 6 – Connector 3 – Screw M4 x 10 For information: 4 – Spring washer ø4.3 7 – Bottom engine cowling Fig. 33-5 Landing Light Halogen MR16 12V/20W / LED MR16 12V/4,5W Removal / Installation Chapter 33-40 EXTERIOR LIGHTING...

  • Page 703: Whelen A600

    LIGHTS Whelen A600 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Flat screwdriver 1 pc Knife 1 pc Soldering gun 1 pc Cable tie 2.6 1 pc Shrink tube ø3.2 x 1.6 Persons...
  • Page 704 LIGHTS Anti-collision/position light polishing: Polish the lights after installation. NOTE Under no circumstances should any petroleum-based product be used to clean the lights. 1 – Anti-collision/position light cover 5 – Spiral hose ø6 2 – Light base assembly 6 – Screw M4 x 16 3 –...
  • Page 705 LIGHTS Landing light AveoEngineering Hercules JP Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Wrench 7 1 pc Wrench 8 1 pc Knife 1 pc...
  • Page 706 LIGHTS 1 – Landing light 7 – Washer ø4.3 x 9 x 0.8 2 – Metal plate 1 8 – Self-locking nut M4 3 – Metal plate 2 9 – Clamp 50-70 4 – Holder For information: 5 – Screw M4 x 10 10 –...
  • Page 707 LIGHTS 33-60 INTERIOR LIGHTING DESCRIPTION This chapter contains information on servicing the interior lights. The interior lights (1; 2, Fig. 33-8) are mounted to the cockpit / cabin compartment. The instrument panel light – LED strip is mounted on the instrument panel cover bottom surface.
  • Page 708 LIGHTS 1 – Cockpit / cabin light 2 – LED light strip Fig. 33-8 Interior Lighting Chapter 33-40 EXTERIOR LIGHTING Page 33-20 Effectivity: ALL 14. 05. 2020...
  • Page 709 LIGHTS MAINTENANCE PRACTICES Aveo EyeBeam touch light Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Knife 1 pc Persons Tab. 33-7 Recommended tools, materials, persons and documentation WARNING ENGINE IGNITION MUST BE SWITCHED OFF.
  • Page 710 LIGHTS 1 – Light 4 – Screw M4 x 12 2 – Flange 5 – Connector Fig. 33-9 Aveo EyeBeam Touch Removal / Installation Chapter 33-40 EXTERIOR LIGHTING Page 33-22 Effectivity: ALL 14. 05. 2020...
  • Page 711 LIGHTS LED light strip Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Knife 1 pc Double sided tape Persons Tab. 33-8 Recommended tools, materials, persons and documentation WARNING ENGINE IGNITION MUST BE SWITCHED OFF.
  • Page 712 LIGHTS 1 – Double sided tape 2 – LED light strip Fig. 33-10 LED Light Strip Removal / Installation Chapter 33-40 EXTERIOR LIGHTING Page 33-24 Effectivity: ALL 14. 05. 2020...
  • Page 713 NAVIGATION 34 NAVIGATION CONTENTS Chapter Description Page 34-00 GENERAL ................. 3 INTRODUCTION ............... 3 34-10 FLIGHT ENVIRONMENTAL DATA ........5 DESCRIPTION ................5 TROUBLESHOOTING ............. 13 MAINTENANCE PRACTICES ..........15 Pitot-static probe ............. 15 SV-ADAHRS-200 module ..........17 Altitude encoder .............. 20 Airspeed indicator ............
  • Page 714 NAVIGATION Magnetic compass ............35 Standby bank indicator ........... 35 34-40 INDEPENDENT POSITION DETERMINING ....37 DESCRIPTION ................ 37 MAINTENANCE PRACTICES ..........38 FLARM Classic antenna, ADS-B antenna, Power FLARM Core antenna ............. 38 TRX-1500 traffic sensor ..........40 Power FLARM Core sensor ..........42 34-50 DEPENDENT POSITION DETERMINING .......

  • Page 715: General

    NAVIGATION 34-00 GENERAL INTRODUCTION This chapter describes the navigation systems, units, and components which provide aircraft navigational information. Included are pitot-static, compass, navigation systems, and indicators. The subjects to be covered in this chapter are as follows: The Flight Environmental Data/Pitot Static section describes systems which sense environmental conditions and use the data to influence navigation of the aircraft.
  • Page 716 NAVIGATION This page is left blank intentionally Chapter 34-00 GENERAL Page 34-4 Effectivity: ALL 14. 05. 2020...

  • Page 717: Flight Environmental Data

    NAVIGATION 34-10 FLIGHT ENVIRONMENTAL DATA DESCRIPTION Arrangements and schemes of the pitot-static systems are given on the Fig. 34-1, Fig. 34-2, Fig. 34-3, Fig. 34-4, Fig. 34-5, Fig. 34-6 and Fig. 34-7. The Pitot-static probe (1) is installed under the right wing. It receives total pressure (hoses marked “P”), static pressure (hoses marked “S”) and is equipped with AOA sensing (hoses marked “A”).

  • Page 718: Altitude Encoder

    NAVIGATION 1 – Pitot-static probe 6 – Flight hours counter 2 – ADAHRS module 7 – Altitude encoder 3 – Airspeed indicator 8 – Expansion bottle 4 – Altimeter 9 – Drain sumps 5 – Vertical speed indicator Fig. 34-1 Dynon SkyView Pitot-Static System with VSI and AoA (illustrated picture) Chapter 34-10 FLIGHT ENVIRONMENTAL DATA Page 34-6...
  • Page 719 NAVIGATION 1 – Pitot-static probe 6 – Flight hours counter 2 – ADAHRS module 7 – Altitude encoder 3 – Airspeed indicator 8 – Expansion bottle 4 – Altimeter 9 – Drain sumps 5 – Vertical speed indicator Fig. 34-2 Pitot-Static System with VSI without AoA (illustrated picture) FLIGHT ENVIRONMENTAL DATA Chapter 34-10 14.
  • Page 720 NAVIGATION 1 – Pitot-static probe 6 – Flight hours counter 2 – ADAHRS module 7 – Altitude encoder 3 – Airspeed indicator 8 – N/A 4 – Altimeter 9 – Drain sumps 5 – N/A Fig. 34-3 Dynon SkyView Pitot-Static System with AoA without VSI (illustrated picture) Chapter 34-10 FLIGHT ENVIRONMENTAL DATA Page 34-8...
  • Page 721 NAVIGATION 1 – Pitot-static probe 6 – N/A 2 – AHRS module 7 – Altitude encoder 3 – Airspeed indicator 8 – Expansion bottle 4 – Altimeter 9 – Drain sumps 5 – Vertical speed indicator Fig. 34-4 Flymap L Pitot-Static System with VSI without AoA (illustrated picture) FLIGHT ENVIRONMENTAL DATA Chapter 34-10 14.
  • Page 722 NAVIGATION 1 – Pitot-static probe 6 – N/A 2 – N/A 7 – Altitude encoder 3 – Airspeed indicator 8 – Expansion bottle 4 – Altimeter 9 – Drain sumps 5 – Vertical speed indicator Fig. 34-5 TruTrak Pitot-Static System with VSI without AoA (illustrated picture) Chapter 34-10 FLIGHT ENVIRONMENTAL DATA Page 34-10...
  • Page 723 NAVIGATION 1 – Pitot-static probe 6 – N/A 2 – N/A 7 – Altitude encoder 3 – Airspeed indicator 8 – Expansion bottle 4 – Altimeter 9 – Drain sumps 5 – Vertical speed indicator Fig. 34-6 Dynon D100 Pitot-Static System with VSI without AoA (illustrated picture) FLIGHT ENVIRONMENTAL DATA Chapter 34-10 14.
  • Page 724 NAVIGATION 1 – Pitot-static probe 6 – N/A 2 – N/A 7 – Altitude encoder 3 – Airspeed indicator 8 – N/A 4 – Altimeter 9 – Drain sumps 5 – N/A Fig. 34-7 Dynon D100 Pitot-Static System without VSI and AoA (illustrated picture) Chapter 34-10 FLIGHT ENVIRONMENTAL DATA Page 34-12...
  • Page 725 NAVIGATION TROUBLESHOOTING TROUBLE POSSIBLE CAUSE REMEDY Pitot static system Low or sluggish airspeed Pitot-static probe Repair or replace indication. Normal deformed. Leak or damaged component. altimeter and vertical obstruction in total line. speed indication. Incorrect or sluggish Leaks or obstruction in Repair or replace line.
  • Page 726 NAVIGATION TROUBLE POSSIBLE CAUSE REMEDY Airspeed indicator (cont.) Pointer vibrates. Excessive vibration Tighten mounting bolts. caused by loose mounting bolts. Excessive tube vibration. Tighten clamps and connections. Altimeter Excess scale error. Improper calibration Replace instrument. adjustment. Excessive pointer Defective instrument. Replace or repair oscillation.
  • Page 727 NAVIGATION MAINTENANCE PRACTICES WARNING AVOID OF IMPURITIES AND WATER INFILTRATION INTO PITOT-STATIC SYSTEM. CAUSE WRONG FUNCTION OR DAMAGE OF THE INSTRUMENTS! Pitot-static probe Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver...
  • Page 728 NAVIGATION 1 – Pitot-static probe 4 – Static pressure hose (S) 2 – Bolt (4 pcs) 5 – AoA hose (A), if is installed 3 – Total pressure hose (P) 6 – Hose clamp Fig. 34-8 Pitot-Static Probe Removal / Installation Chapter 34-10 FLIGHT ENVIRONMENTAL DATA Page 34-16...
  • Page 729 NAVIGATION SV-ADAHRS-200 module Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Oetiker pliers- Crimping pliers 1 pc Sealing Teflon tape Persons Tab.
  • Page 730 NAVIGATION SV-ADAHRS-200 Module installation: WARNING BEWARE THAT CORRECT A-P-S HOSES ARE INSTALLED TO CORRECT POSITIONS ON SV-ADAHRS-200 MODULE. INCORRECT INSTALLATION CAUSE LOSS OF AIRCRAFT! Remove the caps from the hoses and module ports. As necessary, screw hose socket (2, Fig. 34-9) sealed with Teflon tape.
  • Page 731 NAVIGATION 1 – SV-ADAHRS-200 Module 8 – Spring clamp ø9 2 – Hose socket 9 – Static pressure hose (S) 3 – Bolt M4 x 16 (4 pcs) 10 – Total pressure hose (P) 4 – Spring locking washer ø4.3 (4 pcs) 11 –...
  • Page 732 NAVIGATION Altitude encoder Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Oetiker pliers- Crimping pliers 1 pc Persons Tab. 34-3 Recommended tools, materials, persons and documentation Altitude encoder removal: Set MASTER SWITCH to OFF position.
  • Page 733 NAVIGATION 1 – Altitude encoder 4 – Electrical connector 2 – Mounting tray 5 – Static pressure hose 3 – Knurled nut 6 – Spring clamp ø9 Fig. 34-10 Altitude Encoder Removal / Installation Airspeed indicator For removal / installation procedures refer to Chapter 39-10. Altimeter For removal / installation procedures refer to Chapter 39-10.
  • Page 734 NAVIGATION Drain sumps Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Oetiker pliers- Crimping pliers 1 pc Clippers Persons Tab. 34-4 Recommended tools, materials, persons and documentation NOTE If you find impurities or water in pitot-static system drain sumps, these sumps must be drain.
  • Page 735 NAVIGATION 1 – Drain sump 3 – Hose 2 – Spring clamp ø9 Fig. 34-11 Drain Sumps Removal / Installation FLIGHT ENVIRONMENTAL DATA Chapter 34-10 14. 05. 2020 Effectivity: ALL Page 34-23...

  • Page 736: Pitot-Static System

    NAVIGATION Pitot-static system Adjustment / leak test Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY DPST-3500M testing device 1 pc Pitot-static probe adapter (P1-0011-00) 1 pc Persons Tab.
  • Page 737 NAVIGATION Pitot-static system leak test: Set the onboard altimeters to the reference pressure 1013.3 mbar (29.92 inHg). Monitor the values displayed on the DPST-3500M testing device. Slowly adjust the altitude on the display (3, Fig. 34-13) to the 4 000 ft. Monitor the values displayed on the DPST-3500M testing device.
  • Page 738 NAVIGATION 1 – Main switch 8 – Static pressure input 2 – Pump switch 9 – Total pressure input 10 – Pressure control 3– - Display 4 – Control panel 11 – Pressure vent 5 – Grounding 12 – Cross bleed control 6 –...
  • Page 739 NAVIGATION Flymap L AHRS module Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Socket 7 1 pc Oetiker pliers - Crimping pliers 1 pc Wrench 7 1 pc Persons...
  • Page 740 NAVIGATION SV-ADAHRS-200 Module installation: WARNING BEWARE THAT CORRECT P-S HOSES ARE INSTALLED TO CORRECT POSITIONS ON AHRS MODULE. INCORRECT INSTALLATION MAY CAUSE LOSS OF AIRCRAFT! Remove the caps from the hoses and module ports. Install the module (1, Fig. 34-14) using the bolts (4) and washers with nuts (5;...
  • Page 741 NAVIGATION 1 – Flymap AHRS Module 5 – Washer ø4.3 x 9 x 0.8 (4 pcs) 2 – Electrical connector 6 – Self-locking nut M4 (4 pcs) 3 – Hoses (S, P) 7 – Spring clamp ø9 4 – Bolt M4 x 16 (4 pcs) Fig.

  • Page 742: Trutrak Efis Display

    NAVIGATION TruTrak EFIS display For removal / installation procedures refer to Chapter 39-10. Dynon EFIS D100 display For removal / installation procedures refer to Chapter 39-10. Chapter 34-10 FLIGHT ENVIRONMENTAL DATA Page 34-30 Effectivity: ALL 14. 05. 2020...

  • Page 743: Attitude And Direction

    NAVIGATION 34-20 ATTITUDE AND DIRECTION DESCRIPTION This chapter contains information pertaining to those portions of the system which use magnetic, gyroscopic, and inertia forces. Included is the Dynon SkyView system, Flymap L system, TruTrak, Dynon D100, magnetic compass and standby bank indicator.
  • Page 744 NAVIGATION The Dynon D100 features a 7" diagonal, colour LCD high-resolution screen. The display enables split-screen viewing to augment the primary EFIS data with other pages of information called up by the pilot. Attitude information is obtained from 3 solid-state gyrometers, 3 solid-state accelerometers, and the airspeed pressure sensor.
  • Page 745 NAVIGATION Fig. 34-15 Dynon Skyview System Scheme ATTITUDE AND DIRECTION Chapter 34-20 14. 05. 2020 Effectivity: ALL Page 34-33...

  • Page 746: Troubleshooting

    NAVIGATION TROUBLESHOOTING TROUBLE POSSIBLE CAUSE REMEDY Pitot static system Compass not properly Compensate instrument. compensated. Excessive card error. External magnetic Locate magnetic interference. interference and eliminate if possible. Excessive card oscillation. Insufficient fluid. Replace instrument. Weak card magnet. Replace instrument. Card sluggish.

  • Page 747: Maintenance Practices

    NAVIGATION MAINTENANCE PRACTICES SV-D1000 display For removal / installation procedures refer to Chapter 39-10. Flymap L EFIS display For removal / installation procedures refer to Chapter 39-10. TruTrak EFIS display For removal / installation procedures refer to Chapter 39-10. Dynon EFIS D100 display For removal / installation procedures refer to Chapter 39-10.
  • Page 748 NAVIGATION This page is left blank intentionally Chapter 34-20 ATTITUDE AND DIRECTION Page 34-36 Effectivity: ALL 14. 05. 2020...

  • Page 749: Independent Position Determining

    NAVIGATION 34-40 INDEPENDENT POSITION DETERMINING DESCRIPTION This chapter covers that portion of the system that provides information to determine position from sources that are mainly independent of ground installations. This includes the GPS and TRX-1500 traffic sensor. GPS signals are received by an SV-GPS-250 antenna mounted inside the fuselage under the left part of the instrument panel (Fig.

  • Page 750: Maintenance Practices

    NAVIGATION MAINTENANCE PRACTICES FLARM Classic antenna, ADS-B antenna, Power FLARM Core antenna Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons Wrench 9, 19 1 pc Cable ties 2.6 Tab.
  • Page 751 NAVIGATION Power FLARM Core antenna installation: Put the antenna base (3, Fig. 34-16) to installation hole in fuselage skin. Connect the cable (4) to the antenna base (3). Screw the nut (9) and antenna (8) from the outside. Install the pedestal panel (Chapter 27-50). Set MASTER SWITCH to ON position and carry out an operational test.
  • Page 752 NAVIGATION TRX-1500 traffic sensor Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Persons Tab. 34-8 Recommended tools, materials, persons and documentation TRX-1500 traffic sensor removal: Set MASTER SWITCH to OFF position.
  • Page 753 NAVIGATION 1 – TRX-1500 unit 6 – Bolt (4 pcs) 2 – Main connector 7 – Washer (4 pcs) 3 – ADS-B antenna connector 8 – Washer (4 pcs) 4 – FLARM antenna connector For information: 5 – GPS antenna connector 9 –...
  • Page 754 NAVIGATION Power FLARM Core sensor Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Screwdriver 1 pc Wrench 7 1 pc Persons Tab.
  • Page 755 NAVIGATION 1 – Power FLARM unit 5 – Bolt (4 pcs) 2 – Connectors For information: 3 – Nut (4 pcs) 6 – Bracket 4 – Washer (4 pcs) Fig. 34-18 Power FLARM Core Sensor a Removal / Installation INDEPENDENT POSITION DETERMINING Chapter 34-40 14.
  • Page 756 NAVIGATION This page is left blank intentionally Chapter 34-40 INDEPENDENT POSITION DETERMINING Page 34-44 Effectivity: ALL 14. 05. 2020...

  • Page 757: Dependent Position Determining

    NAVIGATION 34-50 DEPENDENT POSITION DETERMINING DESCRIPTION This chapter covers that portion of the system which provides information to determine position from sources which are mainly dependent on ground installations. This includes the GNC 255A NAV / COMM, Garmin GTX 328 Transponder system, and VOR/LOC antenna and transponder antenna.

  • Page 758: Maintenance Practices

    NAVIGATION MAINTENANCE PRACTICES Garmin GNC 255A NAV/COMM For removal / installation procedures refer to Chapter 39-10. FUNKWERK ATR 833 NAV/COM For removal / installation procedures refer to Chapter 39-10. Garmin GTX 328 transponder For removal / installation procedures refer to Chapter 39-10. FUNKWERK TRT 800H For removal / installation procedures refer to Chapter 39-10.

  • Page 759: Transponder Antenna

    NAVIGATION Transponder antenna AV-22 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 19 1 pc Persons Tab. 34-10 Recommended tools, materials, persons and documentation Transponder antenna removal (old installation): CAUTION DO NOT ACTIVATE ELT WHEN REMOVING COVER.
  • Page 760 NAVIGATION Transponder antenna removal (new installation): CAUTION DO NOT ACTIVATE ELT WHEN REMOVING COVER. IT IS SENSITIVE FOR SHOCKS. Set MASTER SWITCH to OFF position. Remove baggage bulkhead cover. Disconnect coaxial cable (6, Fig. 34-19) from transponder antenna (1). Unscrew the nut (3), remove washer (4), aluminium tape (5) and pull out transponder antenna (1) with gasket ring (2) from the fuselage bottom part (7).
  • Page 761 NAVIGATION 1 – Transponder antenna 5 – Label 2 – Gasket ring 6 – Coaxial cable 3 – Nut For information: 4 – Serrated locking washer 7 – Fuselage bottom part Fig. 34-19 Antenna Removal / Installation (old installation) XPDR DEPENDENT POSITION DETERMINING Chapter 34-50 14.
  • Page 762 NAVIGATION 1 – Transponder antenna 5 – Aluminium tape 2 – Gasket ring 6 – Coaxial cable 3 – Nut For information: 4 – Serrated locking washer 7 – Fuselage bottom part Fig. 34-20 Antenna Removal / Installation (new installation) XPDR Chapter 34-50 DEPENDENT POSITION DETERMINING...
  • Page 763 NAVIGATION TED 104-12 Transponder antenna For removal / installation procedures refer to Transponder antenna AV-22. RAMI AV-74 Transponder antenna Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 19 1 pc Persons Tab.
  • Page 764 NAVIGATION Transponder antenna removal (new installation): CAUTION DO NOT ACTIVATE ELT WHEN REMOVING COVER. IT IS SENSITIVE FOR SHOCKS. Set MASTER SWITCH to OFF position. Remove baggage bulkhead cover. Disconnect coaxial cable (7, Fig. 34-21) from transponder antenna (1). Unscrew the nuts (3), remove washers (4; 5), aluminium tape (6) and pull out transponder antenna (1) with gasket (2) from the fuselage bottom part (8).
  • Page 765 NAVIGATION 1 – Transponder antenna 6 – Label 2 – Gasket 7 – Coaxial cable 3 – Nut For information: 4 – Large washer 8 – Fuselage bottom part 5 – Split lock washer Fig. 34-21 Antenna Removal / Installation (old installation) XPDR DEPENDENT POSITION DETERMINING Chapter 34-50...
  • Page 766 NAVIGATION 1 – Transponder antenna 6 – Aluminium tape 2 – Gasket 7 – Coaxial cable 3 – Nut For information: 4 – Large washer 8 – Fuselage bottom part 5 – Split lock washer Fig. 34-22 Antenna Removal / Installation (new installation) XPDR Chapter 34-50 DEPENDENT POSITION DETERMINING...
  • Page 767 NAVIGATION CI-105 Transponder antenna For removal / installation procedures refer to Transponder antenna AV-74. SV-GPS-250 antenna Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Cable ties 2.6...

  • Page 768: Gps-250 Antenna

    NAVIGATION 1 – SV-GPS-250 antenna 5 – Cable 2 – Cable For information: 3 – Bolt (4 pcs) 6 – Bracket 4 – TRX GPS antenna 7 – Bracket Fig. 34-23 SV-GPS-250 and TRX GPS Antennas Removal / Installation Chapter 34-50 DEPENDENT POSITION DETERMINING Page 34-56 Effectivity: ALL...

  • Page 769: Garmin Ga25 Mcx

    NAVIGATION Garmin GA25 MCX For removal / installation procedures refer to SV-GPS-250 antenna. TRX GPS antenna Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Knife 1 pc Double side tape...
  • Page 770 NAVIGATION This page is left blank intentionally Chapter 34-50 DEPENDENT POSITION DETERMINING Page 34-58 Effectivity: ALL 14. 05. 2020...
  • Page 771 INSTRUMENT AND CONTROL PANELS 39 INSTRUMENT AND CONTROL PANELS CONTENTS Chapter Description Page 39-00 GENERAL ................. 5 INTRODUCTION ............... 5 39-10 INSTRUMENT AND CONTROL PANELS......7 DESCRIPTION ................7 MAINTENANCE PRACTICES ........... 8 Instrument panel cover ............8 Instrument panel .............. 10 EFIS/EMS/GPS/AP Dynon SV-D1000 ......
  • Page 772 INSTRUMENT AND CONTROL PANELS Engine hours Honeywell Hobbs 85094 ......47 Engine RPM indicator Rotax 966408 ......49 Engine RPM indicator Road IF61.2B35.2301 ....51 Propeller regulator Flybox PR1-P ........53 Manifold pressure indicator UMA 7-100-20 ..... 55 Fuel pressure indicator Skydrive FP-912/10 ....57 Oil pressure indicator Road XIE4.0013.00 / Oil temperature indicator Road XIH4.0010.00 / Cylinder head temperature indicator Road XIH4.0018.00 .....
  • Page 773 INSTRUMENT AND CONTROL PANELS WW. Exhaust gas temperature indicator Westach 2DA2 ..108 XX. Colision avoidance Flarm V3 indicator ......110 YY. Dynon D100 ..............112 ZZ. Dynon EMS-D120 ............114 AAA. GPS AV-MAP-EKP IV ........... 116 BBB. AP TruTrak DigiFlight II VS ........... 118 CCC.
  • Page 774 INSTRUMENT AND CONTROL PANELS This page is left blank intentionally Chapter 39 CONTENTS Page 39-4 Effectivity: ALL 14. 05. 2020...

  • Page 775: General

    INSTRUMENT AND CONTROL PANELS 39-00 GENERAL INTRODUCTION The instrument panel is arranged primarily for use by the pilot in the left seat; however, it can be viewed from the co-pilot in the right seat. Primary flight display and warning and control lights are located on the left side of the panel and engine monitoring system is located on the right side of the instrument panel.
  • Page 776 INSTRUMENT AND CONTROL PANELS This page is left blank intentionally Chapter 39-00 GENERAL Page 39-6 Effectivity: ALL 14. 05. 2020...

  • Page 777: Instrument And Control Panels

    INSTRUMENT AND CONTROL PANELS 39-10 INSTRUMENT AND CONTROL PANELS DESCRIPTION Instrument panel is made of glass/carbon fabric laminate and is attached to the central tunnel and both sides of fuselage. In the middle of top edge is the panel supported with composite bar. The instrument panel is covered with glass laminate cover.

  • Page 778: Maintenance Practices

    INSTRUMENT AND CONTROL PANELS MAINTENANCE PRACTICES Instruments panels shown in this maintenance practices are illustrative only. The instrument panel layouts of specific aircraft are shown in their POH. Instrument panel cover Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher.
  • Page 779 INSTRUMENT AND CONTROL PANELS 1 – Instrument panel cover 2 – Screw M4 x 10 Fig. 39-1 Instrument Panel Cover Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-9...
  • Page 780 INSTRUMENT AND CONTROL PANELS Instrument panel Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Wrench 8 1 pc Wrench 10 1 pc Phillips screwdriver 2 1 pc...

  • Page 781: Instrument Panel

    INSTRUMENT AND CONTROL PANELS 1 – 7 – Support bar 2 – 8 – Nut 3 – Instrument panel 9 – Bolt 4 – 10 – Washer 5 – Screw 11 – Central tunnel 6 – Washer Fig. 39-2 Instrument Panel Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.

  • Page 782: Efis/Ems/Gps/Ap Dynon Sv-D1000

    INSTRUMENT AND CONTROL PANELS EFIS/EMS/GPS/AP Dynon SV-D1000 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Hex key 5/64” 1 pc Persons Tab.
  • Page 783 INSTRUMENT AND CONTROL PANELS SV-D1000 installation: Remove protective covers from rear connectors of the display. Connect the connectors (2; 3; 4, Fig. 39-3) to the display (1). Put the display (1) to the panel (9) and fasten it by means of the screws (5), washers (7;...
  • Page 784 INSTRUMENT AND CONTROL PANELS The second screen will be automatically synchronized through the internal network, once it has been activated. A recommended 4GB USB flash drive intended for the files transfer during the actualization procedure is supplied with every SkyView display SV-D1000.
  • Page 785 INSTRUMENT AND CONTROL PANELS 1 – EFIS/EMS/GPS/AP (1 pc) 6 – Nut (6 pcs) 2 – DB37 display connector (1 pc) 7 – Spring locking washer ø4.3 (6 pcs) 3 – SkyView network connector (2 pcs) 8 – Washer ø4.3 x 9 x 0.8 (6 pcs) 4 –...

  • Page 786: Efis/Ems/Gps/Ap Flymap L / Xl

    INSTRUMENT AND CONTROL PANELS EFIS/EMS/GPS/AP Flymap L / XL Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Persons Tab. 39-4 Recommended tools, materials, persons and documentation WARNING UNAUTHORIZED ENTRY TO THE SYSTEM SETTINGS AND A FAILURE...
  • Page 787 INSTRUMENT AND CONTROL PANELS 1 – EFIS/EMS/GPS/AP (1 pc) For information: 2 – Screw M4 (4 pcs) 3 – Instrument panel Fig. 39-4 EFIS/EMS/GPS/AP Flymap L / XL Removal / Installation (Illustrative figure) INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-17...
  • Page 788 INSTRUMENT AND CONTROL PANELS EFIS/AP TruTrak III Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Persons Tab. 39-5 Recommended tools, materials, persons and documentation WARNING UNAUTHORIZED ENTRY TO THE SYSTEM SETTINGS AND FAILURE...
  • Page 789 INSTRUMENT AND CONTROL PANELS 1 – EFIS/AP (1 pc) 5 – Connector (1 pc) 2 – Screw (4 pcs) For information: 3 – Total pressure hose (P) (1 pc) 6 – Instrument panel 4 – Static pressure hose (S) (1 pc) Fig.

  • Page 790: Gps Garmin 695

    INSTRUMENT AND CONTROL PANELS GPS Garmin 695 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Persons Tab. 39-6 Recommended tools, materials, persons and documentation WARNING UNAUTHORIZED ENTRY TO THE SYSTEM SETTINGS AND FAILURE...
  • Page 791 INSTRUMENT AND CONTROL PANELS 1 – GPS (1 pc) 5 – Connection terminal (1 pc) 2 – Washer (4 pcs) For information: 3 – Spring washer (4 pcs) 6 – Instrument panel 4 – Screw (4 pcs) Fig. 39-6 GPS Garmin 695 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.

  • Page 792: Traffic Information Display Bd57

    INSTRUMENT AND CONTROL PANELS Traffic information display BD57 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Persons Tab. 39-7 Recommended tools, materials, persons and documentation BD57 removal: Set the MASTER SWITCH to OFF position.
  • Page 793 INSTRUMENT AND CONTROL PANELS 1 – Traffic information display (1 pc) For information: 2 – Screw (4 pcs) 3 – Instrument panel Fig. 39-7 Traffic Information Display BD57 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-23...

  • Page 794: Elt Remote Control Kannad 406 Af-Compact

    INSTRUMENT AND CONTROL PANELS ELT remote control Kannad 406 AF-Compact Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Wrench 7 1 pc Persons Tab.
  • Page 795 INSTRUMENT AND CONTROL PANELS 1 – ELT remote control (1 pc) ø 5 – Washer 3.2 x 7 x 0.5 (4 pcs) 2 – Connector (1 pc) For information: 3 – Screw M3 x 10 (4 pcs) 6 – Instrument panel 4 –...
  • Page 796 INSTRUMENT AND CONTROL PANELS ELT remote control Ameri-King AK-451 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Wrench 5.5 1 pc Persons Tab.
  • Page 797 INSTRUMENT AND CONTROL PANELS 1 – ELT remote control (1 pc) 5 –Connector (1 pc) 2 – Screw M3 x 10 (4 pcs) For information: ø 6 – Instrument panel 3 – Washer 3.2 x 7 x 0.5 (4 pcs) 4 –...

  • Page 798: Flaps Controller Flybox Efc-P

    INSTRUMENT AND CONTROL PANELS Flaps controller Flybox EFC-P Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-10 Recommended tools, materials, persons and documentation EFC-P removal: Set the MASTER SWITCH to OFF position.
  • Page 799 INSTRUMENT AND CONTROL PANELS 1 – Flaps controller (1 pc) For information: 2 – Screw M3 (4 pcs) 4 – Instrument panel 3 – Connector (1 pc) Fig. 39-10 Flaps Controller Flybox EFC-P Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.

  • Page 800: Airspeed Indicator Winter 7Fms511 / 7Fms513 / 7Fms421, Altimeter Winter 4Fgh20 / 4Fgh40

    INSTRUMENT AND CONTROL PANELS Airspeed indicator Winter 7FMS511 / 7FMS513 / 7FMS421, Altimeter Winter 4FGH20 / 4FGH40 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc...
  • Page 801 INSTRUMENT AND CONTROL PANELS 4FGH20 / 4FGH40 removal: Remove the instrument panel cover (Chapter 39-10, 2.A.). Remove the clamps (4, Fig. 39-11). Disconnect the hose (5) from the port of the altimeter (2). Remove the mounting screws (3); hold the altimeter (2). Remove the altimeter (2) from the instrument panel (7).
  • Page 802 INSTRUMENT AND CONTROL PANELS 1 – Airspeed indicator (1 pc) 5 – Static pressure hose (2 pcs) 2 – Altimeter (1 pc) 6 – Total pressure hose (1 pc) 3 – Screw M4 x 10 (4 + 3 pcs) For information: 4 –...

  • Page 803: Vertical Speed Indicator Winter 5Stvm10

    INSTRUMENT AND CONTROL PANELS Vertical speed indicator Winter 5STVM10 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Oetiker pliers- Crimping pliers 1 pc Persons Tab.
  • Page 804 INSTRUMENT AND CONTROL PANELS 1 – Vertical speed indicator (1 pc) 5 – Static pressure hose (1 pc) 2 – Screw M4 x 10 (4 pcs) For information: 3 – Spring clamp ø9 (2 pcs) 6 – Instrument panel 4 – Differential pressure hose (1 pc) Fig.

  • Page 805: Slip Indicator Winter Qmi And Qmii

    INSTRUMENT AND CONTROL PANELS Slip indicator Winter QMI and QMII Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Wrench 7 1 pc Persons Tab.

  • Page 806: Magnetic Compass Precision Aviation Pai-700 (On Instrument Panel)

    INSTRUMENT AND CONTROL PANELS Magnetic compass Precision Aviation PAI-700 (on instrument panel) Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Loctite 243 Persons Tab.
  • Page 807 INSTRUMENT AND CONTROL PANELS 1 – Magnetic compass (1 pc) For information: 2 – Screw M4 (brass) (4 pcs) 3– Instrument panel Fig. 39-14 Magnetic Compass Precision Aviation PAI-700 (on instrument panel) Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.
  • Page 808 INSTRUMENT AND CONTROL PANELS Magnetic compass adjustment / test: Carry out a test for correct operation of the compass (compass swing): • After replacing a major component • After replacing the compass • After modification to the aircraft. Compass swing must be performed on the approved compass swing area, which is at least 100 m (300 ft) from steel structures, electric leading or other over ground or underground steel equipment or objects.
  • Page 809 INSTRUMENT AND CONTROL PANELS MAGNETIC COMPASS COMPENSATION RECORD Aircraft: S/N: Compass: S/N: Measurement 1 Measurement 2 A. Aircraft stands on landing gear. A. Aircraft stands on landing gear. B. All electrical equipment ON and B. Switched ON only those Conditions: operating.
  • Page 810 INSTRUMENT AND CONTROL PANELS Magnetic compass Precision Aviation PAI-700 (on instrument panel cover) Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Wrench 7 1 pc Loctite 243...
  • Page 811 INSTRUMENT AND CONTROL PANELS 1 – Magnetic compass (1 pc) 5 – Washer (aluminium or bronze) (8 pcs) 2 – Screw M4 (brass) (4 pcs) 6 – Nut M4 (brass) (4 pcs) 3 – Compass holder (1 pc) For information: 4 –...
  • Page 812 INSTRUMENT AND CONTROL PANELS Magnetic compass Airpath C-2400-P Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Non-magnetic Philips screwdriver 1 pc Non-magnetic wrench 7 1 pc Persons Tab.
  • Page 813 INSTRUMENT AND CONTROL PANELS Magnetic compass adjustment / test: Carry out a test for correct operation of the compass (compass swing): • After replacing a major component • After replacing the compass • After modification to the aircraft. Compass swing must be performed on the approved compass swing area, which is at least 100 m (300 ft) from steel structures, electric leading or other over ground or underground steel equipment or objects.
  • Page 814 INSTRUMENT AND CONTROL PANELS 1 – Magnetic compass (1 pc) 4 – Washer 4.3 x 9 x 0.8 brass (3 pcs) 2 – Screw M4x10 aluminium (3 pcs) For information: 3 –Low nut M4 (brass) (3 pcs) 5 – Instrument panel cover Fig.
  • Page 815 INSTRUMENT AND CONTROL PANELS Flight hours Winter FSZM 1510 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Oetiker pliers- Crimping pliers 1 pc Persons Tab.
  • Page 816 INSTRUMENT AND CONTROL PANELS 1 – Flight hours (1 pc) 5 – Electrical connector (1 pc) 2 – Screw M4 x 10 (4 pcs) For information: 3 – Spring clamp ø9 (1 pc) 6 – Instrument panel 4 – Static pressure hose (1 pc) Fig.
  • Page 817 INSTRUMENT AND CONTROL PANELS Engine hours Honeywell Hobbs 85094 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-18 Recommended tools, materials, persons and documentation Hobbs 85094 removal: Set the MASTER SWITCH to OFF position.
  • Page 818 INSTRUMENT AND CONTROL PANELS 1 – Engine hours (1 pc) 5 –Connectors (2 pcs) ø For information: 2 – Washer 4. x 9 x 0.8 (adapted) (2 pcs) 3 – Self-locking nut M4 (2 pcs) 6 – Instrument panel 4 – Screw M4 x 16 (2 pcs) Fig.
  • Page 819 INSTRUMENT AND CONTROL PANELS Engine RPM indicator Rotax 966408 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-19 Recommended tools, materials, persons and documentation 966408 removal: Set the MASTER SWITCH to OFF position.
  • Page 820 INSTRUMENT AND CONTROL PANELS 1 – Engine RPM indicator (1 pc) For information: 2 – Screw M4 (4 pcs) 4 – Instrument panel 3 – Connector Fig. 39-20 Engine RPM Indicator Rotax 966408 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-50 Effectivity: ALL 14.
  • Page 821 INSTRUMENT AND CONTROL PANELS Engine RPM indicator Road IF61.2B35.2301 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons Tab. 39-20 Recommended tools, materials, persons and documentation IF61.2B35.2301 removal: Set the MASTER SWITCH to OFF position.
  • Page 822 INSTRUMENT AND CONTROL PANELS 1 – Engine RPM indicator (1 pc) For information: 2 – Retaining ring (1 pc) 4 – Instrument panel 3 – Electrical connector Fig. 39-21 Engine RPM Indicator Road IF61.2B35.2301 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-52 Effectivity: ALL 14.
  • Page 823 INSTRUMENT AND CONTROL PANELS Propeller regulator Flybox PR1-P Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-21 Recommended tools, materials, persons and documentation PR1-P removal: Set the MASTER SWITCH to OFF position.
  • Page 824 INSTRUMENT AND CONTROL PANELS 1 – Propeller regulator (1 pc) For information: 2 – Electrical connector (1 pc) 4 – Instrument panel 3 – Screw M4 (4 pcs) Fig. 39-22 Propeller Regulator Flybox PR1-P Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-54 Effectivity: ALL 14.
  • Page 825 INSTRUMENT AND CONTROL PANELS Manifold pressure indicator UMA 7-100-20 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 1 pc Philips screwdriver 1 pc Combinating pliers 1 pc Persons...
  • Page 826 INSTRUMENT AND CONTROL PANELS 1 – Manifold pressure indicator (1 pc) 4 – Clamp (1 pc) 2 – Screw (4 pcs) For information: 3 – Hose (1 pc) 5 – Instrument panel Fig. 39-23 Manifold Pressure Indicator UMA 7-100-20 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-56...
  • Page 827 INSTRUMENT AND CONTROL PANELS Fuel pressure indicator Skydrive FP-912/10 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 9 1 pc Oetiker pliers- Crimping pliers 1 pc Persons Tab.
  • Page 828 INSTRUMENT AND CONTROL PANELS 1 – Fuel pressure indicator (1 pc) 5 – Spring clamp ø9 (1 pc) 2 – Holder (1 pc) For information: 3 – Special nut NPT1/8 (1 pc) 6 – Instrument panel 4 – Hose (1 pc) Fig.
  • Page 829 INSTRUMENT AND CONTROL PANELS Oil pressure indicator Road XIE4.0013.00 / Oil temperature indicator Road XIH4.0010.00 / Cylinder head temperature indicator Road XIH4.0018.00 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons...
  • Page 830 INSTRUMENT AND CONTROL PANELS 1 – Indicator (1 pc) 4 – Electrical connector 2 – Bracket (1 pc) For information: 3 – Nut (2 pcs) 5 – Instrument panel Fig. 39-25 Oil Pressure Indicator Road XIE4.0013.00 / Oil Temperature Indicator Road XIH4.0010.00 / Cylinder Head Temperature Indicator Road XIH4.0018.00 Removal / Installation Chapter 39-10...
  • Page 831 INSTRUMENT AND CONTROL PANELS Oil pressure indicator Road IE61.2B35.2201 / Oil temperature indicator Road IH61.2B35.2201 / Cylinder head temperature indicator Road IH71.2B35.2201 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons...
  • Page 832 INSTRUMENT AND CONTROL PANELS 1 – Indicator (1 pc) For information: 2 – Retaining ring (1 pc) 4 – Instrument panel 3 – Electrical connector Fig. 39-26 Oil Pressure Indicator Road IE61.2B35.2201 / Oil Temperature Indicator Road IH61.2B35.2201 / Cylinder Head Temperature Indicator Road IH71.2B35.2201 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS...
  • Page 833 INSTRUMENT AND CONTROL PANELS Fuel level indicator VDO 301 010 002 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons Tab. 39-26 Recommended tools, materials, persons and documentation 301 010 002 removal: Set the MASTER SWITCH to OFF position.
  • Page 834 INSTRUMENT AND CONTROL PANELS 1 – Fuel level indicator (1 pc) For information: 2 – Retaining ring (1 pc) 4 – Instrument panel 3 – Electrical connector Fig. 39-27 Fuel Level Indicator VDO 301 010 002 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-64 Effectivity: ALL...
  • Page 835 INSTRUMENT AND CONTROL PANELS AA. Fuel level indicator PAL Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Persons Tab. 39-27 Recommended tools, materials, persons and documentation PAL removal: Set the MASTER SWITCH to OFF position.
  • Page 836 INSTRUMENT AND CONTROL PANELS 1 – Fuel level indicator (1 pc) 5 – Electrical connectors 2 – Holder (1 pc) For information: 3 – Washer (2 pcs) 6 – Instrument panel 4 – Nut M4 (2 pcs) Fig. 39-28 Fuel Level Indicator PAL Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-66...
  • Page 837 INSTRUMENT AND CONTROL PANELS BB. Airbox temperature indicator Voltcraft TCM 220 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons Tab. 39-28 Recommended tools, materials, persons and documentation TCM 220 removal: Set the MASTER SWITCH to OFF position.
  • Page 838 INSTRUMENT AND CONTROL PANELS 1 – Airbox temperature indicator (1 pc) 5 – Surrounding wires 2 – Wire to battery (1 pc) 6 – Wire to sensor (1 pc) 3 – Cable tie (1 pc) For information: 4 – Battery tray (1 pc) 7 –...
  • Page 839 INSTRUMENT AND CONTROL PANELS CC. Radiostation Funke ATR 833 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 1 pc Flat screwdriver 1 pc Persons Tab.
  • Page 840 INSTRUMENT AND CONTROL PANELS 1 – Radiostation (1 pc) 5 – COM connector (1 pc) 2 – Screw (4 pcs) 6 – COM antenna connector (1 pc) 3 – Knob with securing screw (4 pcs) For information: 4 – Cover (4 pcs) 7 –...
  • Page 841 INSTRUMENT AND CONTROL PANELS DD. Transponder Funke TRT 800H Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 1 pc Flat screwdriver 1 pc Combinating pliers 1 pc Persons...
  • Page 842 INSTRUMENT AND CONTROL PANELS 1 – Transponder (1 pc) 6 – XPDR antenna connector (1 pc) 2 – Screw (4 pcs) 7 – Static pressure hose (1 pc) 3 – Knob with securing screw (4 pcs) 8 – Clamp (1 pc) 4 –...
  • Page 843 INSTRUMENT AND CONTROL PANELS EE. Radiostation Garmin GNC 255A / GTR 225A Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Allen wrench 3/32” 1 pc Persons Tab.
  • Page 844 INSTRUMENT AND CONTROL PANELS Set MASTER SWITCH to ON position and carry out an operational test - refer to the Garmin GTR 225 / GNC 255 TSO Installation Manual, P/N 190-01182-02 (revision B or later). 1 – Radiostation (1 pc) For information: 2 –...
  • Page 845 INSTRUMENT AND CONTROL PANELS FF. Transponder Garmin GTX 328 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Allen wrench 3/32” 1 pc Persons Tab. 39-32 Recommended tools, materials, persons and documentation GTX 328 removal: Set MASTER SWITCH to OFF position.
  • Page 846 INSTRUMENT AND CONTROL PANELS Set MASTER SWITCH to ON position and carry out an operational test - refer to the Garmin GTX 328 Transponder Installation Manual, P/N 190-00420-04 (revision C or later). 1 – Transponder (1 pc) For information: 2 – Access hole for locking screw 4 –...
  • Page 847 INSTRUMENT AND CONTROL PANELS GG. Intercom PS Engineering PM-1000 / PM-1000 II / PM-3000 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Persons Tab.
  • Page 848 INSTRUMENT AND CONTROL PANELS Verify proper transmit and receive operation on the co-pilot position, noting that the co-pilot PTT switch allows proper transmission. Verify proper Intercom system operation in the ALL, ISO modes. Verify that the intercom system does not adversely affect any other aircraft system by systematically switching the unit on and off, while monitoring the other avionics and electrical equipment on the aircraft.
  • Page 849 INSTRUMENT AND CONTROL PANELS HH. Intercom Sigtronics SPA-4S Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Persons Tab. 39-34 Recommended tools, materials, persons and documentation SPA-4S removal: Set MASTER SWITCH to OFF position.
  • Page 850 INSTRUMENT AND CONTROL PANELS 1 – Intercom (1 pc) 5 – Nut (1 pc) 2 – Face plate (1 pc) 6 – Electrical connector (2 pcs) 3 – Screw (2 pcs) For information: 4 – Knob (2 pcs) 7 – Instrument panel Fig.
  • Page 851 INSTRUMENT AND CONTROL PANELS Audio input PS Engineering / Sigtronics Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Persons Tab.
  • Page 852 INSTRUMENT AND CONTROL PANELS 1 – Audio input (1 pc) For information: 2 – Nut (1 pc) 4 – Instrument panel 3 – Wires Fig. 39-36 Audio Input PS Engineering / Sigtronics Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-82 Effectivity: ALL 14.
  • Page 853 INSTRUMENT AND CONTROL PANELS JJ. Ignition switches Miyama MS-500M Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Socket wrench 10 1 pc Soldering gun 1 pc Shrink tube ø3.2 x 1.6 mm Knife...
  • Page 854 INSTRUMENT AND CONTROL PANELS Fig. 39-37 Ignition Switches Miyama MS-500M And Keyed Ignition Switch Hella 6JK 007 232-001 Removal / Installation (page 1 of 2) Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-84 Effectivity: ALL 14. 05. 2020...
  • Page 855 INSTRUMENT AND CONTROL PANELS 1 – Keyed ignition switch (2 pcs) 8 – Washer (2 pcs) 2 – Nut (1 pc) 9 – Serrated washer (2 pcs) 3 – Washer (1 pc) 10 – Nut (2 pcs) 4 – Knurled ring (1 pc) 11 –...
  • Page 856 INSTRUMENT AND CONTROL PANELS KK. Keyed ignition switch Hella 6JK 007 232-001 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 22 1 pc Pliers 1 pc Philips screwdriver 2...
  • Page 857 INSTRUMENT AND CONTROL PANELS LL. Keyed ignition switch ACS A-510-2 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 22 1 pc Pliers 1 pc Philips screwdriver 2 1 pc Persons...
  • Page 858 INSTRUMENT AND CONTROL PANELS 1 – Keyed ignition switch (1 pc) 5 – Wires 2 – Nut (1 pc) For information: 3 – Face plate (1 pc) 6 – Instrument panel 4 – Nut (1 pc) Fig. 39-38 Keyed Ignition Switch ACS A-510-2 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-88...
  • Page 859 INSTRUMENT AND CONTROL PANELS MM. Master switch Bulgin C3960BB Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 14 1 pc Pliers 1 pc Persons Tab.
  • Page 860 INSTRUMENT AND CONTROL PANELS 1 – Master switch (1 pc) 5 – Nut (1 pc) 2 – Nut (1 pc) 6 – Wire 3 – Protector (1 pc) For information: 4 – Plate (1 pc) 7 – Instrument panel Fig. 39-39 Master Switch Bulgin C3960BB Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-90...
  • Page 861 INSTRUMENT AND CONTROL PANELS NN. Master switch Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 7 1 pc Pliers 1 pc Philips screwdriver 1 pc Persons Tab.
  • Page 862 INSTRUMENT AND CONTROL PANELS 1 – Master switch (1 pc) 5 – Nut (2 pcs) 2 – Protector (1 pc) 6 – Wire 3 – Screw (2 pcs) For information: 4 – Washer (2 pcs) 7 – Instrument panel Fig. 39-40 Master Switch Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-92...
  • Page 863 INSTRUMENT AND CONTROL PANELS OO. Switches Miyama MS-500F Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Socket wrench 10 1 pc Soldering gun 1 pc Shrink tube 3.2 x 1.6 mm Ø...
  • Page 864 INSTRUMENT AND CONTROL PANELS 1 – Switch 5 – Wires 2 – Washer For information: 3 – Serrated washer 6 – Instrument panel 4 – Fig. 39-41 Switches Miyama MS-500F Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-94 Effectivity: ALL 14.
  • Page 865 INSTRUMENT AND CONTROL PANELS PP. Circuit breakers Klixon 7277-2 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Wrench 1/2 in 1 pc Persons Tab.
  • Page 866 INSTRUMENT AND CONTROL PANELS 1 – Circuit breaker 6 – Locking washer 2 – Nut 7 – Wire 3 – Keyway washer For information: 4 – Serrated washer 8 – Instrument panel 5 – Bolt Fig. 39-42 Circuit Breakers Klixon 7277-2 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-96...
  • Page 867 INSTRUMENT AND CONTROL PANELS QQ. Circuit breakers ETA 106-P10 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Persons Tab.
  • Page 868 INSTRUMENT AND CONTROL PANELS 1 – Circuit breaker 4 – Wire 2 – Washer For information: 3 – Ring 5 – Instrument panel Fig. 39-43 Circuit Breakers ETA 106-P10 Removal / Installation Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-98 Effectivity: ALL 14.
  • Page 869 INSTRUMENT AND CONTROL PANELS RR. Lamp Eleco SMS95 12DC P30 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Narrow flat screwdriver 1 pc Persons Tab.
  • Page 870 INSTRUMENT AND CONTROL PANELS 1 – Lamp body 6 – Nut 2 – Lamp cover 7 – Rubber washer 3 – Rubber washer 8 – Wire 4 – Wire For information: 5 – Test button body 9 – Instrument panel Fig.
  • Page 871 INSTRUMENT AND CONTROL PANELS SS. Autopilot OFF / Test button Ninigi PS10B2BK Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Wrench 11 1 pc Soldering gun 1 pc Shrink tube ø3.2 x 1.6...
  • Page 872 INSTRUMENT AND CONTROL PANELS TT. Power socket DC12V SCI A13-65A Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Persons Tab.
  • Page 873 INSTRUMENT AND CONTROL PANELS 1 – Power socket DC12V For information: 2 – Wires 3 – Instrument panel Fig. 39-45 Power Socket DC12V SCI A13-65A Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-103...
  • Page 874 INSTRUMENT AND CONTROL PANELS UU. Power socket DC12V 02226 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Persons Tab.
  • Page 875 INSTRUMENT AND CONTROL PANELS 1 – Power socket DC12V For information: 2 – Nut 4 – Instrument panel 3 – Wires Fig. 39-46 Power Socket DC12V 02226 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-105...
  • Page 876 INSTRUMENT AND CONTROL PANELS VV. USB connector AK674 1M Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Persons Tab.
  • Page 877 INSTRUMENT AND CONTROL PANELS 1 – USB connector For information: 2 – Screw 3 – Instrument panel Fig. 39-47 USB Connector AK674 1M Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-107...
  • Page 878 INSTRUMENT AND CONTROL PANELS WW. Exhaust gas temperature indicator Westach 2DA2 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-49 Recommended tools, materials, persons and documentation 2DA2 removal: Set the MASTER SWITCH to OFF position.
  • Page 879 INSTRUMENT AND CONTROL PANELS 1 – Exhaust gas temperature indicator (1 pc) For information: 2 – Screw M4 (4 pcs) 4 – Instrument panel 3 – Connector Fig. 39-48 Exhaust Gas Temperature Indicator Westach 2DA2 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.
  • Page 880 INSTRUMENT AND CONTROL PANELS XX. Colision avoidance Flarm V3 indicator Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-50 Recommended tools, materials, persons and documentation Flarm V3 indicator removal: Set the MASTER SWITCH to OFF position.
  • Page 881 INSTRUMENT AND CONTROL PANELS 1 – Flarm indicator (1 pc) 4 – Connector 2 – Double side tape (optional) For information: 3 – Screws (2 pcs) 5 – Instrument panel Fig. 39-49 Flarm V3 Indicator Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.
  • Page 882 INSTRUMENT AND CONTROL PANELS YY. Dynon D100 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Allen wrench 7/64” 1 pc Persons Tab.
  • Page 883 INSTRUMENT AND CONTROL PANELS 1 – Dynon D100 7 – Hose (static pressure 2 – Rack 8 – Hose (total pressure) 3 – Screws 9 – Hose (AoA) 4 – Washers 10 – Retaining screw 5 – Nuts For information: 6 –...
  • Page 884 INSTRUMENT AND CONTROL PANELS ZZ. Dynon EMS-D120 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Allen wrench 7/64” 1 pc Persons Tab.
  • Page 885 INSTRUMENT AND CONTROL PANELS 1 – Dynon EMS-D120 6 – Connector 2 – Rack 7 – Connector 3 – Screws 8 – Retaining screw 4 – Washers For information: 5 – Nuts 9 – Instrument panel Fig. 39-51 Dynon EMS-D120 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.
  • Page 886 INSTRUMENT AND CONTROL PANELS AAA. GPS AV-MAP-EKP IV Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Wrench 7 1 pc Persons Tab.
  • Page 887 INSTRUMENT AND CONTROL PANELS 1 – GPS AV-MAP-EKP IV 6 – Washer 4.3 x 9 x 0.8 2 – Bracket 1 7 – Spring washer 4.1 x 7.6 x 1.5 3 – Bracket 2 8 – Connectors 4 – Bolt M4 x 12 For information: 5 –...
  • Page 888 INSTRUMENT AND CONTROL PANELS BBB. AP TruTrak DigiFlight II VS Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-54 Recommended tools, materials, persons and documentation WARNING UNAUTHORIZED ENTRY TO THE SYSTEM SETTINGS AND FAILURE...
  • Page 889 INSTRUMENT AND CONTROL PANELS 1 – AP TruTrak DigiFlight II VS 5 – Hose (total pressure) 2 – Screw For information: 3 – Connector 6 – Instrument panel 4 – Hose (static pressure) Fig. 39-53 AP TruTrak DigiFlight II VS Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.
  • Page 890 INSTRUMENT AND CONTROL PANELS CCC. Trim indicator RP3 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Wrench 5 1 pc Persons Tab.
  • Page 891 INSTRUMENT AND CONTROL PANELS 1 – Trim indicator RP3 5 – Cables 2 – Screw For information: 3 – Washers 6 – Instrument panel 4 – Nuts Fig. 39-54 Trim indicator RP3 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14.
  • Page 892 INSTRUMENT AND CONTROL PANELS DDD. Winch control switch Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons Tab. 39-56 Recommended tools, materials, persons and documentation Winch control switch removal: Set MASTER SWITCH to OFF position.
  • Page 893 INSTRUMENT AND CONTROL PANELS 1 – Winch control switch For information: 2 – Pins 3 – Instrument panel Fig. 39-55 Winch Control Switch Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-123...
  • Page 894 INSTRUMENT AND CONTROL PANELS EEE. Landing gear controller Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-57 Recommended tools, materials, persons and documentation Landing gear controller removal: Set MASTER SWITCH to OFF position.
  • Page 895 INSTRUMENT AND CONTROL PANELS 1 – Landing gear controller 3 – Terminals 2 – Screws 4 – Instrument panel Fig. 39-56 Landing gear controller Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-125...
  • Page 896 INSTRUMENT AND CONTROL PANELS FFF. TRX-2000 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-58 Recommended tools, materials, persons and documentation TRX-2000 removal: Set MASTER SWITCH to OFF position.
  • Page 897 INSTRUMENT AND CONTROL PANELS 1 – TRX-2000 3 – Terminals 2 – Screws 4 – Instrument panel Fig. 39-57 TRX-2000 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-127...
  • Page 898 INSTRUMENT AND CONTROL PANELS GGG. TM250 traffic monitor Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-59 Recommended tools, materials, persons and documentation TM250 removal: Set MASTER SWITCH to OFF position.
  • Page 899 INSTRUMENT AND CONTROL PANELS 1 – TRX-2000 3 – Terminals 2 – Screws 4 – Instrument panel Fig. 39-58 TM250 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-129...
  • Page 900 INSTRUMENT AND CONTROL PANELS HHH. Attitude indicator TruTrak ADI 26 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-60 Recommended tools, materials, persons and documentation Attitude indicator TruTrak ADI 26 removal: Set MASTER SWITCH to OFF position.
  • Page 901 INSTRUMENT AND CONTROL PANELS 1 – ADI 26 3 – Terminal 2 – Screws 4 – Instrument panel Fig. 39-59 Attitude indicator TruTrak ADI 26 Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 14. 05. 2020 Effectivity: ALL Page 39-131...
  • Page 902 INSTRUMENT AND CONTROL PANELS III. Rocker switch A8L-21-15N2 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Persons Tab. 39-61 Recommended tools, materials, persons and documentation Rocker switch A8L-21-15N2 removal: Set MASTER SWITCH to OFF position.
  • Page 903 INSTRUMENT AND CONTROL PANELS 1 – Rocker switch For information: 2 – Connectors 3 – Instrument panel Fig. 39-60 Rocker Switch Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 04. 05. 2021 Effectivity: ALL Page 39-133...
  • Page 904 INSTRUMENT AND CONTROL PANELS JJJ. Radiostation TRIG TY96 Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Allen wrench 3/32” 1 pc Persons Tab. 39-62 Recommended tools, materials, persons and documentation Radiostation TRIG TY96 removal: Set MASTER SWITCH to OFF position.
  • Page 905 INSTRUMENT AND CONTROL PANELS Set MASTER SWITCH to ON position and carry out an operational test - refer to the TRIG TY96/96A Installation Manual (the latest issue). 1 – Radiostation (1 pc) For information: 2 – Access hole for locking screw 4 –...
  • Page 906 INSTRUMENT AND CONTROL PANELS KKK. LED panel control lamps Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Philips screwdriver 1 pc Narrow flat screwdriver 1 pc Persons Tab.
  • Page 907 INSTRUMENT AND CONTROL PANELS 1 – Lamp body 5 – Washer 3.1 x 6.2 x 0.8 2 – Thrust plates 6 – Screw M3x5 3 – Lamp nut 7 – Wires 4 – PCB panel Fig. 39-62 LED Panel control lamps Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 04.
  • Page 908 INSTRUMENT AND CONTROL PANELS LLL. TFT display CTF700-SHM Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Persons Tab. 39-64 Recommended tools, materials, persons and documentation TFT display CTF700-SHM removal: Set the MASTER SWITCH to OFF position.
  • Page 909 INSTRUMENT AND CONTROL PANELS 1 – Display 5 – Connectors 2 – Washers 6 – Holders 3 – Spring washers 7 – Instrument panel 4 – Screws M4 Fig. 39-63 TFT Display CTF700-SHM Removal / Installation INSTRUMENT AND CONTROL PANELS Chapter 39-10 04.
  • Page 910 INSTRUMENT AND CONTROL PANELS This page is left blank intentionally Chapter 39-10 INSTRUMENT AND CONTROL PANELS Page 39-140 Effectivity: ALL 04. 05. 2021...
  • Page 911 STANDAR PRACTICES AND STRUCTURES- GENERAL 51 STANDARD PRACTICES AND STRUCTURES - GENERAL CONTENTS Chapter Description Page 51-00 GENERAL ................. 3 INTRODUCTION ............... 3 General safety information ..........3 Aircraft description ............. 4 Spare parts source ............4 51-10 REPAIRS ................5 GENERAL ..................
  • Page 912 STANDAR PRACTICES AND STRUCTURES- GENERAL REPAIR PREPARATION ............11 Repair Class 4 ..............11 Repair Class 3 ..............11 Repair Class 2 ..............12 Repair Class 1 ..............13 PLY LAY-UP SCHEME ............14 REPAIRS OF METAL PARTS ..........29 REPAIRS OF PLEXIGLASS ...........
  • Page 913 STANDAR PRACTICES AND STRUCTURES- GENERAL 51-00 GENERAL INTRODUCTION This chapter contains information and procedures applicable to all composite repairs as well as information and procedures for aircraft painting and priming. The basic elements of successful repair are; preparation of the laminate and repair material, proper mixing of resin, technique, and a complete cure cycle.
  • Page 914 VFR day. Spare parts source Spare parts can be ordered from www.aerospool.sk under “Products / Dynamic WT9 / Spare Parts” or writing by an e-mail spareparts@aerospool.sk. E-mail must contain the following information: • Aircraft S/N •...
  • Page 915 STANDAR PRACTICES AND STRUCTURES- GENERAL 51-10 REPAIRS GENERAL Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY See Chapter 51-10, par. 4. Persons Tab. 51-1 Recommended tools, materials, persons and documentation The described procedures concern only to relatively minor damage.
  • Page 916 STANDAR PRACTICES AND STRUCTURES- GENERAL When the elevator, rudder, aileron and wing flaps were repaired, the static moments and weights must be checked, whether they are within the permissible range according to Tab. 51-2-1 or 51-2-2. Airplanes can be classified according to added mass balance weight in the control surfaces.
  • Page 917 STANDAR PRACTICES AND STRUCTURES- GENERAL CONSTRUCTION WT9 Dynamic LSA airframe consists of a sandwich shells from composite material. The shell is of three-layer construction. The external and internal shell layers are made of a glass and carbon fibre fabrics, which are saturated with a resin. Between them there is a filling from a hard foam panels (polyurethane foam HEREX from 3 to 15 mm thick).
  • Page 918 STANDAR PRACTICES AND STRUCTURES- GENERAL MATERIALS Epoxy system The laminates are made using following epoxy system type: ITEM TYPE MANUFACTURER Resin L 285 Hexion Inc. Hardener H 287 Hexion Inc. Mixing ratio of resin and hardener: ITEM RESIN : HARDENER Parts by weight 100 : 40±2 Parts by volume...
  • Page 919 STANDAR PRACTICES AND STRUCTURES- GENERAL Reinforcements WEIGHT MARKING WEAVE PER AREA APPLICATION (g/m GLASS FABRICS 91111 Cross twill 1/3 Outer skin, inner skin, aileron, wing, fuselage, wheel cover, canopy frame, fin 92110 Cross twill 2/2 Outer skin, inner skin, aileron, wing, fuselage, stabilizer, engine cowling, fin, rudder, landing gear leg cover...
  • Page 920 STANDAR PRACTICES AND STRUCTURES- GENERAL Foams and fillers Rigid Foam: HEREX C70.55 Resin Fillers: Aerosil Cotton flakes Microballoons white (brown) Paints ITEM Mipa 4+1 2K HS - Filler Mipa OC Mischlack-Konzentrat - Paint Mipa 2K-Härter H5 - Hardener Mipa 2K - Thinner Mipa C85 2K-HS - Clearcoat Chapter 51-10 REPAIRS...
  • Page 921 STANDAR PRACTICES AND STRUCTURES- GENERAL REPAIR PREPARATION For all repairs, it is important to know the number of layers of the laminate, density of weave and directional fabrics fibers orientation relative to the main part dimensions. The first step is removing all damage parts and all portion of the shell that has become delaminated from a damage area.
  • Page 922 STANDAR PRACTICES AND STRUCTURES- GENERAL Repair Class 2 If there is a through hole in the sandwich shell, then remove all delaminated parts and sand the edge of the hole. Enlarge the hole until good bonding to the foam is evidenced. Then remove the foam next 20 mm around the hole while the inner fabric remains undamaged.
  • Page 923 STANDAR PRACTICES AND STRUCTURES- GENERAL Repair Class 1 These repairs have serious character and can be carried out only by the aircraft manufacturer or a repair workshop approved by local Civil Aviation Authority (CAA). In any case contact the aircraft manufacturer. REPAIRS Chapter 51-10 14.
  • Page 924 STANDAR PRACTICES AND STRUCTURES- GENERAL PLY LAY-UP SCHEME Fig. 51-5 Ply Lay-up FG (page 1 of 2) Chapter 51-10 REPAIRS Page 51-14 Effectivity: ALL 14. 05. 2020...
  • Page 925 STANDAR PRACTICES AND STRUCTURES- GENERAL Fig. 51-5 Ply Lay-up FG (page 2 of 2) REPAIRS Chapter 51-10 14. 05. 2020 Effectivity: ALL Page 51-15...
  • Page 926 STANDAR PRACTICES AND STRUCTURES- GENERAL Fig. 51-6 Ply Lay-up RG (page 1 of 2) Chapter 51-10 REPAIRS Page 51-16 Effectivity: ALL 14. 05. 2020...
  • Page 927 STANDAR PRACTICES AND STRUCTURES- GENERAL Fig. 51-6 Ply Lay-up RG (page 2 of 2) Each fabric must be properly oriented with respect to the long side of the aircraft. The patch must be composed of an equal number of layers as a repair area plus one technology layer that prevents damage of the top layer due to finishing.
  • Page 928 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer EE50P Technological layer Outer EE50P Outer CF80 Outer CF80 Gluing collar Outer CF80 Gluing collar Outer CF140 Winglet aft section Herex 3 mm Inner CF80 Outer 92110 Technological layer Outer 92110...
  • Page 929 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer 92110 Technological layer Outer 92110 Outer 92110 Herex 6 mm Inner 92110 Inner 92110 Inner 91111 Outer 92110 Technological layer Outer 92110 Outer 92110 Herex 6 mm Inner 92110 Inner...
  • Page 930 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer 91111 Technological layer Outer 91111 Herex 3 mm Inner 91111 Root / tip rib leading edge Inner 91111 Root / tip rib leading edge Inner 91111 Root / tip rib leading edge Inner 91111 Leading edge collar...
  • Page 931 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer CF80 Technological layer Outer CF80 Herex 5 mm Inner 90070 Outer hinges – only Inner 92125 bottom shell Outer CF80 Technological layer Outer CF80 Outer CF140 Herex 5 mm Inner 90070...
  • Page 932 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer 92110 Technological layer Outer 92110 Outer 92110 Herex 3 mm Inner 92110 Inner 92110 Leading edge Inner 90070 Outer 92110 Technological layer Outer 92110 Outer 92110 Tip rib Herex 3 mm Inner...
  • Page 933 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer 92110 Technological layer Outer 92110 Outer 92110 Rudder rope outlets Outer 92110 Rudder rope outlets Outer CF140 Outer CF200 Keel lower part Outer CF200 Keel lower part Outer CF200 Keel lower part...
  • Page 934 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION 92110 Technological layer 92110 92110 92110 91111 92110 Technological layer 92110 92110 92110 CF140 91111 Outer 92110 Technological layer Outer 92110 Outer CF140 Herex 5 mm Inner 91111 Outer 92110 Technological layer...
  • Page 935 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer 92110 Technological layer Outer 92110 Outer 92110 Outer 92110 Flaps S-cover Outer CF140 Main gear leg rib Outer CF140 Main gear leg stiffeners Outer CF200 Main gear leg rib Outer 92125 Herex...
  • Page 936 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer 91111 Technological layer Outer 91111 Outer CF200 Outer CF200 Outer CF140 Inner CF200 Gas struts anchorings Inner CF140 Inner 92110 Ball vents Inner 92110 Ball vents Inner CF200 Inner 91111...
  • Page 937 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION Outer 91111 Technological layer Outer 91111 Outer CF200 Outer CF200 Outer CF140 Outer CF140 NACA opening Guide pins / canopy Inner CF200 attachment Inner CF140 Inner CF200 Inner CF200 Inner 91111...
  • Page 938 STANDAR PRACTICES AND STRUCTURES- GENERAL LAYER WEAVE ITEM LAYER NOTE POSITION DIRECTION 91111 Technological layer 91111 92125 Wheel cutout / Wheel 92125 attachment 92125 Wheel cover attachment – 92125 only side with cutout Wheel cover attachment – 92125 only side with cutout 91111 Technological layer 91111...
  • Page 939 STANDAR PRACTICES AND STRUCTURES- GENERAL REPAIRS OF METAL PARTS In case of a damage of any fittings, if a damage reason was not designate immediately, contact the aircraft manufacturer. It is necessary take account to an element function, a material composition, a processing technology and etc. The aircraft manufacturer can evaluate all these factors only.
  • Page 940 STANDAR PRACTICES AND STRUCTURES- GENERAL Test flight flying time: Test flight flying time takes approx.. 40 minutes, if the test flight is performed according to the Flight Test Record. Aircraft inspection before a Test flight: Prior to the test flight the aircraft shall be thoroughly inspected, weighed, found faults debugged and the aircraft shall be prepared for the flight (replenishing etc.).
  • Page 941 STANDAR PRACTICES AND STRUCTURES- GENERAL 51-20 EXTERIOR FINISH REPAIR REPAIR SURFACES During the operational life of the aircraft, small scratches and dents may appear on the composite surfaces. This damage needs to be repaired. Refinishing of the damage is permitted as long as there is no damage to the fiber fabrics. When control surfaces are painted, they must comply with weight and static moment range according to Tab.
  • Page 942 STANDAR PRACTICES AND STRUCTURES- GENERAL Painting Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Airbrush 1 pc Brush 1 pc Polishing pad Sandpapers 400-2000 Mipa 4+1 2K HS -Filler MIPA OC MISCHLACK-KONZENTRAT-Paint MIPA 2K-HÄRTER H5- Hardener...
  • Page 943 DOORS 52 DOORS CONTENTS Chapter Description Page 52-00 GENERAL ................. 3 INTRODUCTION ............... 3 52-10 CANOPY FRAME ............. 5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 6 Canopy frame ..............6 Gas spring ................. 8 Canopy closing mechanism ..........8 Canopy lock ..............11 CONTENTS Chapter 52 14.
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  • Page 945: General

    DOORS 52-00 GENERAL INTRODUCTION The WT9 aircraft LSA is equipped with the canopy which enables access to the cockpit. GENERAL Chapter 52-00 14. 05. 2020 Effectivity: ALL Page 52-3...
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  • Page 947: Canopy Frame

    DOORS 52-10 CANOPY FRAME DESCRIPTION The aircraft has a one-piece tilting canopy (Fig. 52-1). Canopy frame is attached in front section to the fuselage using two hinges (2) and supported by two gas springs. It is opened in upside-forward direction. Guide pins located on both sides of the canopy frame ensures positioning of the canopy during the closing.

  • Page 948: Maintenance Practices

    DOORS MAINTENANCE PRACTICES Canopy frame Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Wrench 10 1 pc Blind ø 25 mm 2 pcs Persons Tab.

  • Page 949: Canopy Frame

    DOORS 1 – Canopy 6 – Safety pin 1.4 x 20 2 – Gas spring 7 – Ball socket 3 – Hinge bolt 8 – Safety clip 4 – Castle nut M6 9 – Ball stud 5 – Washer 6 10 –...

  • Page 950: Canopy Closing Mechanism

    DOORS Gas spring Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Screwdriver 1 pc Pliers 1 pc Persons Tab. 52-2 Recommended tools, materials, persons and documentation Gas spring removal: Open the canopy frame (1, Fig.
  • Page 951 DOORS Canopy closing mechanism removal: Remove the handle plug (18, Fig. 52-3). Remove the nut (20), washers (19), screw (15) and canopy mechanism handle (interior) (12). Remove the split pin (17) and mark ring (6). Carefully remove the screws (13), washers (19), closing mechanism flange (7) and spring (16).
  • Page 952 DOORS Fig. 52-3 Canopy Frame (page 1 of 2) Chapter 52-10 CANOPY FRAME Page 52-10 Effectivity: ALL 14. 05. 2020...

  • Page 953: Canopy Lock

    DOORS 1 – 13 – Screw M4 x 10 Canopy frame 2 – 14 – Screw M4 x 12 Canopy lock 3 – 15 – Screw M4 x 25 Latch screw 4 – 16 – Spring 1.25 x 11.5 x 45 x 12 Lock nut 5 –...
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  • Page 955 FUSELAGE 53 FUSELAGE CONTENTS Chapter Description Page 53-00 GENERAL ................. 3 INTRODUCTION ............... 3 53-10 FUSELAGE STRUCTURE ..........5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 7 CONTENTS Chapter 53 14. 05. 2020 Effectivity: ALL Page 53-1...
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  • Page 957: General

    FUSELAGE 53-00 GENERAL INTRODUCTION The fuselage is a monocoque structure made primarily of glass and carbon fibre composite materials. Chapter 53-10 gives the data for the fuselage structure. GENERAL Chapter 53-00 14. 05. 2020 Effectivity: ALL Page 53-3...
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  • Page 959: Fuselage Structure

    FUSELAGE 53-10 FUSELAGE STRUCTURE DESCRIPTION Fuselage for fixed gear (FG) or retractable gear (RG) is monocoque glass/carbon composite construction consisting of three parts that are bonded together: left side (1, Fig. 53-1), right side (2) and lower section (3). The fuselage sandwich shell is stiffened with firewall, bulkheads, ribs, stiffeners and interior components creating cockpit.
  • Page 960 FUSELAGE 1 – Left side 7 – Central tunnel 2 – Right side 8 – Backrest 3 – Lower (wing central) section 9 – Baggage bulkhead 4 – Main spar 10 – Vertical stabilizer 5 – Auxiliary spar 11 – Rear windows (Model 2011 is shown) 6 –...

  • Page 961: Maintenance Practices

    FUSELAGE MAINTENANCE PRACTICES Fuselage is made from composite material and no servicing is required. Repairs of the fuselage are described in Chapter 51. FUSELAGE STRUCTURE Chapter 53-10 14. 05. 2020 Effectivity: ALL Page 53-7...
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  • Page 963 STABILIZERS 55 STABILIZERS CONTENTS Chapter Description Page 55-00 GENERAL ................. 3 INTRODUCTION ............... 3 55-10 HORIZONTAL STABILIZER ..........5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 5 Horizontal stabilizer ............5 55-20 ELEVATOR ............... 7 DESCRIPTION ................7 MAINTENANCE PRACTICES ........... 7 Elevator ................
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  • Page 965: General

    STABILIZERS 55-00 GENERAL INTRODUCTION The aircraft has conventional tail configuration, with horizontal stabilizer located in bottom part of fin. The empennage consists of vertical stabilizer with rudder and horizontal stabilizer with elevator. Vertical stabilizer is integral part of fuselage. The horizontal stabilizer is bonded into the fuselage.
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  • Page 967: Horizontal Stabilizer

    STABILIZERS 55-10 HORIZONTAL STABILIZER DESCRIPTION Horizontal stabilizer is a glass/carbon composite sandwich construction. It consists of upper and lower skin, auxiliary web and a web inside of stabilizer up to ¼ of stabilizer span from the plane of symmetry. MAINTENANCE PRACTICES Horizontal stabilizer Because the horizontal stabilizer is made from composite materials and is bonded into the fuselage, no servicing is required.
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  • Page 969: Elevator

    STABILIZERS 55-20 ELEVATOR DESCRIPTION Elevator is a glass/carbon composite sandwich construction. It consists of upper and lower skin and ribs. Each half of the elevator is attached to the horizontal stabilizer through two carbon hinges. Both halves of the elevator are connected together with elevator root hinge located in the aircraft’s plane of symmetry.
  • Page 970 STABILIZERS Align trailing edges of both elevator halves and tighten nuts (4; 5). Connect the push-pull rod to the root fitting (6) (Chapter 27-30). Install the rudder (Chapter 55-40). Carry out test and check: • Screw and nuts connections are tight. •...

  • Page 971: Vertical Stabilizer

    STABILIZERS 55-30 VERTICAL STABILIZER DESCRIPTION Vertical stabilizer is a sandwich shell construction and is integral part of the fuselage. There is an auxiliary web to which the rudder hinges are glued and the tip rib. MAINTENANCE PRACTICES Vertical stabilizer Because the vertical stabilizer is made from composite materials and is integral part of fuselage, no servicing is required.
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  • Page 973: Rudder

    STABILIZERS 55-40 RUDDER DESCRIPTION The rudder is a glass/carbon composite sandwich construction. The rudder is attached to the fin through two hinges and one root hinge. Rudder is fitted with a mass balance weight located in its horn. MAINTENANCE PRACTICES Rudder Type of maintenance: Heavy...
  • Page 974 STABILIZERS Rudder installation: Thoroughly clean and lubricate all the rudder hinges and other movable parts with Vaseline before each assembling. (Chapter 12-20). Do not lubricate the thread of the rudder root hinge. Put the washer (10, Fig. 55-2) on the rudder root hinge. Put the rudder (1) on hinges.
  • Page 975 STABILIZERS Fig. 55-2 Rudder Removal / Installation (page 1 of 2) RUDDER Chapter 55-40 14. 05. 2020 Effectivity: ALL Page 55-13...
  • Page 976 STABILIZERS 1 – 7 – Castle nut M6 Rudder 2 – 8 – Split pin ø1.6 x 16 Bolt M6 x 22 3 – 9 – Rudder control arm Self-locking nut M6 4 – 10 – Washer ø6.4 x12 x 0.5 Distance tube 5 –...
  • Page 977 WINDOWS 56 WINDOWS CONTENTS Chapter Description Page 56-00 GENERAL ................. 3 INTRODUCTION ............... 3 56-10 FLIGHT COMPARTMENT ..........5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 6 Windshield ................. 6 Vent windows Weiss ............11 Vent windows Mecaplex ..........13 Side windows ..............15 CONTENTS Chapter 56 14.
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  • Page 979: General

    WINDOWS 56-00 GENERAL INTRODUCTION The aircraft is equipped with a windshield and can be equipped (depending on the airplane equipment) with two side windows (one on left and one on right side). The side windows may be shaped in design Model 2005 or Model 2011. The windshield and side windows are made of stretched Plexiglas.
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  • Page 981: Flight Compartment

    WINDOWS 56-10 FLIGHT COMPARTMENT DESCRIPTION The aircraft has a one-piece tilting canopy, which is equipped with Plexiglas windshield (1, Fig. 56-1) and (option) side windows (2) on both sides of fuselage. 1 – Windshield 2 – Side windows (option) Fig. 56-1 Windows FLIGHT COMPARTMENT Chapter 56-10 14.

  • Page 982: Maintenance Practices

    WINDOWS MAINTENANCE PRACTICES Windshield Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Grinding tool 1 pc Masking tape Cover foil Sandpaper 80 grit Cleaner Isopropyl alcohol Adhesive Swiftbond 9622 Hardener Swifthardener 9533 Cotton flakes...
  • Page 983 WINDOWS Windshield removal: Remove canopy (Chapter 52-10). Remove vent windows (5.B.(1)). Use a grinding tool and a cut-off disk to cut out the inner portion of the windshield to gain access to the bonding flange. The windshield should be cut as close as possible to the canopy frame.
  • Page 984 WINDOWS Fig. 56-2 Windshield Removal Chapter 56-10 FLIGHT COMPARTMENT Page 56-8 Effectivity: ALL 14. 05. 2020...
  • Page 985 WINDOWS Windshield installation: CAUTION EXERCISE CARE TO PROTECT THE INNER AND OUTER WINDSHIELD SURFACES FROM DAMAGE DURING THE INSTALLATION PROCESS. Inspect canopy frame bonding flange for any remaining adhesive or contaminates, remove and clean if necessary. Cover the flight compartment and instrument panel with a foil to prevent contamination.
  • Page 986 WINDOWS Fig. 56-3 Windshield Installation Chapter 56-10 FLIGHT COMPARTMENT Page 56-10 Effectivity: ALL 14. 05. 2020...
  • Page 987 WINDOWS Vent windows Weiss Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Allen key 2 1 pc Persons Tab. 56-2 Recommended tools, materials, persons and documentation NOTE Described is removal and installation of one of vent windows.

  • Page 988: Windshield

    WINDOWS 1 – 5 – Slider Windshield 2 – 6 – Spring Side window 3 – 7 – Bolt M3 x 10 Upper rail 4 – 8 – Stop plate Lower rail Fig. 56-4 Vent Windows Weiss Installation Chapter 56-10 FLIGHT COMPARTMENT Page 56-12 Effectivity: ALL...
  • Page 989 WINDOWS Vent windows Mecaplex Type of maintenance: Line Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Allen key 2 1 pc Persons Tab. 56-3 Recommended tools, materials, persons and documentation NOTE Described is removal and installation of one of vent windows.
  • Page 990 WINDOWS 1 – 4 – Windshield Lower rail 2 – 5 – Spring Vent window 3 – 6 – Bolt M3 x 10 Upper rail Fig. 56-5 Vent Windows Mecaplex Installation Chapter 56-10 FLIGHT COMPARTMENT Page 56-14 Effectivity: ALL 14. 05. 2020...
  • Page 991 WINDOWS Side windows Type of maintenance: Heavy Personnel qualification: Independent certifying staff qualified in accordance with Part-66 or higher. Recommended tools, materials, persons and documentation: ITEM QUANTITY Grinding tool 1 pc Masking tape Cover foil Sandpaper 80 grit Cleaner Isopropyl alcohol Adhesive Swiftbond 9622 Hardener Swifthardener 9533 Cotton flakes...
  • Page 992 WINDOWS Side window removal: Use a grinding tool and a cut-off disk to cut out the inner portion of the side window to gain access to the bonding flange. The window should be cut as close as possible to the fuselage flange. Use care to prevent damage to the fuselage.
  • Page 993 WINDOWS Fig. 56-6 Side Windows Removal FLIGHT COMPARTMENT Chapter 56-10 14. 05. 2020 Effectivity: ALL Page 56-17...
  • Page 994 WINDOWS Side window installation: CAUTION EXERCISE CARE TO PROTECT THE INNER AND OUTER SIDE OF THE SIDE WINDOW SURFACES FROM DAMAGE DURING INSTALLATION PROCESS. Inspect fuselage bonding flange for any remaining adhesive or contaminates, remove and clean if necessary. Cover the interior with a foil to prevent contamination. Attach the cover foil to the side window in the distance of 30 mm from the edge of the window.
  • Page 995 WINDOWS Fig. 56-7 Side Windows Installation FLIGHT COMPARTMENT Chapter 56-10 14. 05. 2020 Effectivity: ALL Page 56-19...
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  • Page 997 WINGS 57 WINGS CONTENTS Chapter Description Page 57-00 GENERAL ................. 3 INTRODUCTION ............... 3 57-20 OUTER WING ..............5 DESCRIPTION ................5 MAINTENANCE PRACTICES ........... 5 Wings ................5 57-40 LEADING EDGE DEVICES ..........11 DESCRIPTION ................ 11 MAINTENANCE PRACTICES ..........11 Stall strips ................
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  • Page 999: General

    WINGS 57-00 GENERAL INTRODUCTION The WT9 Dynamic LSA is low-wing aircraft with cantilever wings. Each wing has a flap inboard and aileron on the outboard trailing edge. The wings are glass or glass/carbon composite sandwich construction. Refer to Chapter 27 for data on the control systems for the flaps and ailerons; refer to Chapter 28 for data on the wing tanks.
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