Aquila AT01-300 Maintenance Manual

Table of Contents

Quick Links

Download this manual

MAINTENANCE MANUAL

This document is protected by copyright. All associated rights, in particular those of translation, reprinting, reproduction

by photo mechanical or similar means and storing in data processing facilities in whole or part are reserved.

The technical content of this document is approved under the authority of the DOA ref. EASA.21J.025.

AQUILA Aviation International GmbH

Flugplatz

14959 Schönhagen

AQUILA AT01-100

MAINTENANCE MANUAL

AQUILA AT01-100 (A211)

AQUILA AT01-200 (A212)

AQUILA AT01-300 (A211i)

Doc.-No. MM-AT01-1020-110

AQUILA Aviation International GmbH

Phone:+49 33 731 707 - 0

Fax:

+49 33 731 707 - 11

e-mail:

support@aquila-aviation.de

occurence@aquila-aviation.de

Table of Contents

Troubleshooting

Need help?

Do you have a question about the AT01-300 and is the answer not in the manual?

Questions and answers

Summary of Contents for Aquila AT01-300

Page 1 AQUILA AT01-100 AQUILA Aviation International GmbH MAINTENANCE MANUAL MAINTENANCE MANUAL AQUILA AT01-100 (A211) AQUILA AT01-200 (A212) AQUILA AT01-300 (A211i) Doc.-No. MM-AT01-1020-110 This document is protected by copyright. All associated rights, in particular those of translation, reprinting, reproduction by photo mechanical or similar means and storing in data processing facilities in whole or part are reserved.
Page 2 AQUILA AT01-100 MAINTENANCE MANUAL...
Page 3 AQUILA AT01-100/200/300 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS Cha/Sec/Sub Title Pages TABLE OF CONTENTS INTRODUCTION LIST OF EFFECTIVE CHAPTERS AIRWORTHINESS LIMITATIONS 04-00-00 Airworthiness Limitations - General TIME LIMITS / MAINTENANCE CHECKS 05-00-00 Time Limits / Maintenance Checks - General...
Page 4 AQUILA AT01-100/200/300 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages PLACARDS AND MARKINGS 11-00-00 Placards and Markings - General 11-20-00 Exterior Placards and Markings 201-207 11-30-00 Interior Placards and Markings 201-209 SERVICING 12-00-00 Servicing - General...
Page 5 AQUILA AT01-100/200/300 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages ELECTRICAL POWER 24-00-00 Electrical Power - General 24-00-00 Electrical Power - Troubleshooting 101-102 24-20-01 Alternator System - Description (Rotax 912S) 24-20-02 Alternator System - Description (Rotax 914F)
Page 6 AQUILA AT01-100/200/300 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 28-41-02 Fuel Quantity Indication - Maintenance (Garmin G3X) 201-203 28-41-03 Fuel Quantity Indication - Maintenance (E.I. MVP-50) 201-203 28-44-01 Fuel Pressure Indication - Maintenance (Analog / G3X & Rotax 912S) 28-44-02 Fuel Pressure Indication - Maintenance (G3X &...
Page 7 AQUILA AT01-100/200/300 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages DOORS 52-00-00 Doors - General 52-10-00 Canopy - Maintenance 201-204 52-30-00 Baggage Door - Maintenance FUSELAGE 53-00-00 Fuselage - General 53-10-00 Fuselage Main Frame - Description...
Page 8 AQUILA AT01-100/200/300 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages IGNITION SYSTEM 74-00-01 Ignition System - General (Rotax 912S / 914F) 74-00-02 Ignition System - General (Rotax 912iS) 74-00-01 Ignition System - Maintenance (Rotax 912S / 914F)
Page 9 AQUILA AT01-100/200/300 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages CHARTS AND DIAGRAMS 91-00-00 Charts and Diagrams - General 1-40 Page 7 31.05.24...
Page 10 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 11 AQUILA AT01-100/200/300 Record of Revisions MAINTENANCE MANUAL RECORD OF REVISIONS Revision Date of Date Revision Date of Date Number Revision Inserted Number Revision Inserted A.01 30.04.13 A.02 26.08.13 A.03 24.10.13 A.04 02.03.15 A.05 20.08.15 A.06 29.02.16 A.07 10.06.16 A.08 09.10.18 A.09...
Page 12 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 13 AQUILA AT01-100/200/300 Record of Temp. Revisions MAINTENANCE MANUAL RECORD OF TEMPORARY REVISIONS Temp. Revision Date of Date Page Number Revision Removed 05-10-00 p.1 & 3 11.06.14 20.08.15 05-20-00 p.7 14.08.14 20.08.15 76-00-00 p.203 & 204...
Page 14 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 15 SB-AT01-027 A.12 01.02.23 New variant AT01-200A; Garmin G3X autopilot A.03 24.10.13 FAA validation A.13 31.05.24 New model AT01-300 (airworthiness limitations, wire routing diagrams); lubrication revised; standard torque ROTAX engine mount revised A.04 02.03.15 Life time limit, 6000 hour inspection A.05 20.08.15...
Page 16 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 17 AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL INTRODUCTION 1. General This maintenance manual provides to maintenance personnel all information necessary for the maintenance of the aircraft. It contains detailed descriptions of the systems, troubleshooting and maintenance practices. This handbook only contains maintenance practices to be carried out on the aircraft, e.g.
Page 18 AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL Table 1 - List of Technical Publications (Cont.) Title Manual No. / Part No. Supplier Operator’s Manual for OM-914 BRP-Powertrain GmbH & Co KG ROTAX 914 Series 899706 Operator’s Manual for OM-912 i BRP-Powertrain GmbH & Co KG...
Page 19 AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL Table 1 - List of Technical Publications (Cont.) Title Manual No. / Part No. Supplier Garmin GTN 6xx/7xx (Xi) Garmin International Inc. GTN 6XX/7XX System Maintenance Manual 190-01007-A1 GTN Xi Series Maintenance Manual 190-02327-01 Flymap L...
Page 20 AQUILA AT01-100/200/300 Introduction Introduction MAINTENANCE MANUAL Table 1 - List of Technical Publications (Cont.) Title Manual No. / Part No. Supplier Andromeda Aurora Aveo Engineering Installation Manual Ultra Galactica AVE-WPST-54G-IM Aveo Engineering Installation Manual Parmetheus PAR-36 Plus LED Landing Light...
Page 21 AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL 3. Structure of the Maintenance Manual The MM has been prepared in accordance with the Air Transport Association (ATA) Specification Number 100 for Manufacturer’s Technical Data. Classification of Subject Matter The MM is divided into 5 major sections. Each of these sections is sub-divided into chapters.
Page 22 AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL (2) When the chapter/system element number is followed by zeros in the section/subsystem and subject/unit element number (28-00-00), the information is applicable to the entire system. (3) When the section/subsystem element number is followed by zeros in the subject/unit element number (28-20-00), the information is applicable to subsystem within the system.
Page 23 AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL Record of Temporary Revisions Highlights of Revisions Introduction List of Effective Chapters (2) Each chapter begins with: Title Table of Contents Figures The figures within the sections of a chapter are numbered in accordance with the appropriate page number block.
Page 24 AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL Effectivity This maintenance manual is "customized". It includes the following effectivity identification system to show modification and/or configuration differences. (1) The MM starts with a list of effective chapters. Each chapter is listed with date of issue or revision.
Page 25: Warnings, Cautions, And Notes
AQUILA AT01-100/200/300 Introduction MAINTENANCE MANUAL (4) Incorporating revisions into the manual (a) In order to keep track of revisions and to facilitate the use of the manual, a revision always affects the entire chapter, i.e. all pages of a chapter have the same date of issue or revision and the entire chapter is replaced during a revision.
Page 26 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 27 AQUILA AT01-100/200/300 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* GENERAL Table of Contents 31.05.24 Introduction 31.05.24 Airworthiness Limitations 31.05.24 Time Limits / Maintenance Checks 31.05.24 Dimensions and Areas 31.05.24 Lifting & Shoring 28.02.20 Leveling and Weighing 28.02.20...
Page 28 AQUILA AT01-100/200/300 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* POWER PLANT Power Plant 31.05.24 Ignition 31.05.24 Cooling System 31.05.24 Engine Controls 31.05.24 Engine Indicating 31.05.24 Exhaust 31.05.24 31.05.24 Starting 31.05.24 Charts and Wiring Diagrams 24.10.13 * The date refers to the issue / revision date of the respective chapter.
Page 29: Airworthiness Limitations
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS...
Page 30 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 31: Record Of Revisions
02.03.15 Life time limit / EASA Major Change Approval 10052527 6000h inspection A.04 28.02.20 New model AT01-200 EASA Major Change Approval 10072382 A.05 31.05.24 New model AT01-300 EASA Major Change Approval 10084831 Page 1 04 - RECORD OF REVISIONS 31.05.24...
Page 32 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 33 AQUILA AT01-100/200/300 Airworthiness Limitations MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page AIRWORTHINESS LIMITATIONS - GENERAL ..........04-00-00 Introduction 04-00-00 Airworthiness Limitations 04-00-00 Page 1 04 - TOC 31.05.24...
Page 34 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 35 2. Airworthiness Limitations Life Time Limit The airframe of the AQUILA AT01 is limited to 6000 h of flight time. An inspection program to reach an extension of replacement time can be obtained from AQUILA Aviation. NOTE: The life time limit of 6000 h of flight time will be kept for all models listed in the data sheet.
Page 36 / shade is Cromax Imron Fleet Line Elite Topcoat / RAL 9016 (PT101). Before painting the aircraft with a different coating AQUILA Aviation must be contacted. For aircraft registered in Europe or countries where the EASA-TC has been accepted, the approved shade is RAL 9016.
Page 37: Time Limits / Maintenance Checks
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS / MAINTENANCE CHECKS...
Page 38 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 39: Table Of Contents
AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page TIME LIMITS / MAINTENANCE CHECKS - GENERAL ......05-00-00 Introduction 05-00-00 General Description 05-00-00 COMPONENT TIME LIMITS .................05-10-00 General 05-10-00 Component Time Limits 05-10-00 SCHEDULED MAINTENANCE CHECKS............05-20-00...
Page 40 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 41: Time Limits / Maintenance Checks - General
AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL TIME LIMITS / MAINTENANCE CHECKS - GENERAL 1. Introduction This chapter provides scheduled and unscheduled maintenance checks and inspections, recommended by the type certificate holder as well as the time limits for service life limited components and parts.
Page 42 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 43: Component Time Limits
2,3) Fuel system check valves 2000 h or 15 years Nose landing gear spring 5 years package rubber elements Main landing gear struts 6000h 1) AT01-100 only 2) AT01-200 only Page 1 3) AT01-300 only 05-10-00 31.05.24...
Page 44 / fuel system Flexible hoses of the 5 years cooling system Flexible silicone hoses 2000 h or 15 years of the air intake system AQUILA engine mount 6000 h and attachment bolts Engine shock mounts with engine and attachment bolts overhaul...
Page 45 Refer to latest issue of the mt-propeller Service Bulletin No. 1.-( ), and to the mt-Propeller E-124 Operation and Installation Manual. 1) AT01-100 only 2) AT01-200 only Page 3 3) AT01-300 only 05-10-00 15) Time limit does not apply to silicone hoses 31.05.24...
Page 46 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Note 3: Refer to the latest issues of BRP-Rotax documentation, i.e. Service Bulletins, Service Information and to the ROTAX Aircraft Engines Maintenance Manual for ROTAX Engine Type 912 Series, Type 912 i Series respectively Type 914 Series.
Page 47: Scheduled Maintenance Checks
Annual inspections and 100 hour inspections on the AQUILA AT01 must include all inspection items as required by FAR 43, Appendix D, “Scope and detail of annual/100h inspections”.
Page 48 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL For intervals between maintenance work, the following tolerances must not be exceeded: Interval Tolerance up to and including 100 h 10% of interval >100 h up to and including 1000 h 5% of interval >1000 h...
Page 49 Airworthiness Directives - Verify all Airworthiness Directives have been complied with. Service Letters, Service Bulletins, and Service Information - Verify all AQUILA GmbH and suppliers Service Letters, Service Bulletins and Service Information have been complied with. Service time records, equipment list and weight and balance records - Check.
Page 50 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Engine Ground Test Rotax 912S Reference Interval Initials 100h other Perform an engine test run as follows. MML* 12-20-00 (RPM in this point are specified as propeller RPM) Start engine and warm-up at 800 RPM for approx. 2 minutes, Airplane Flight continue at 1050 RPM until oil temperature reaches 50°...
Page 51 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Engine Ground Test Rotax 912iS Reference Interval Initials 100h other Perform an engine test run as follows. MML* 12-20-00 (RPM in this point are specified as engine RPM) Fuel system restricting orifice - Check orifice is not blocked.
Page 52 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Engine Ground Test Rotax 914F Reference Interval Initials 100h other Perform an engine test run as follows. MML* 12-20-00 (RPM in this point are specified as propeller RPM) Fuel pumps - Check fuel pressure with MAIN / AUX / both 28-20 fuel pumps running for at least 5 seconds each.
Page 53 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Engine Reference Interval Initials 100h other Engine cowling - Remove engine cowling. Check for cracks, overheated areas, deformation, loose or missing fasteners. Check condition of fire protect paint and heat resistance shielding. Engine oil change - Remove oil drain screw from oil tank.
Page 54 Check for damage and correct installation (arrow on valve shows correct flow direction). Fuel selector / shut-off valve - Check for security of attachment. Check that the valve engages noticeable into the positions LEFT, RIGHT and OFF. 3) AT01-300 only Page 8 05-20-00 31.05.24...
Page 55 Sensors - Check for tight fit, condition and security of attachment. 1) AT01-100 only 2) AT01-200 only 3) AT01-300 only 7) If more than 30% of operation hours have been flown with leaded fuel e.g.: AVGAS 100LL 8) N/VFR equipped aircraft only Page 9 16) First 100h since engine replacement / overhaul or fuel system work only.
Page 56 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Engine (Cont.) Reference Interval Initials 100h other Exhaust system - Check attachment screws and springs for security and fit. Inspect system for damage and missing parts. Visual inspection of the muffler, turbo charger , exaust pipes and mounting flanges for cracks, corrosion and leakage.
Page 57 Other external engine accessories - Inspect screws and nuts of all other external engine parts and accessories for tight fit. Inspect safety wiring if applicable, replace as necessary. Engine mounts (manufactured by ROTAX and AQUILA) - MML* 12-20-00 Check mounts for deformation, cracks, corrosion, SB-912-028 security and damage from heat.
Page 58 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Propeller Reference Interval Initials 100h other Spinner - Remove from aircraft and check for delamination 61-10 and cracks. Spinner plate - Check for cracks and fit. Blade root and hub area - Examine for oil and grease leaks.
Page 59 Inspect gas spring struts for oil leakage or other damage. Seats - Check ease of movement - if required remove seats, 25-10 annual clean and lubricate seat rails. 2) AT01-200 only 3) AT01-300 only Page 13 05-20-00 31.05.24...
Page 60 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Fuselage / Cabin (Cont.) Reference Interval Initials 100h other Center Console - Visually examine the parts of the engine annual controls, lines and cables, located in the center console. Engine and propeller controls - Check for proper function, security of attachment and for evidence of wear.
Page 61 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Fuselage / Cabin (Cont.) Reference Interval Initials 100h other Rudder control - Check rudder control weldment and rudder bellcrank for cracks, distortion, chafing and security. Examine rudder control support brackets, rudder pedal pivot brackets and connection of the rudder controls with the nose gear steering tubes for security, condition and correct splintering.
Page 62 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Wings, Ailerons, Flaps Reference Interval Initials 100h other Wings with winglets, ailerons, and flaps - Visual inspection for paint coat damage, dents, cracks, holes, distortion and other evidence of failure. Examine all unpainted parts for delamination (white spots).
Page 63 Fuel filler caps - Check for proper function and leakage. Upper wing shell in the fuel tank area - Check wing skin for annual bubble formation or bulging. Contact AQUILA Aviation if there are any findings. Tank inlet - Check sealing of the bore hole in the tank inlet.
Page 64 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Empennage, Elevator, Rudder Reference Interval Initials 100h other Empennage - Inspect complete surface of the vertical and horizontal stabilizers, the elevator and the rudder for dents, cracks, holes and delamination. Rudder hinge, elevator hinge and bellcranks - Check brackets and bellcranks for security of attachment and corrosion.
Page 65 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Nose and Main Landing Gear Reference Interval Initials 100h other Wheel fairings - Check condition and correct fit. Remove and clean. Check for paint coat damage, cracks, dents and delamination. Fairing mounts - Inspect for cracks, distortion or other damage.
Page 66 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Nose and Main Landing Gear (Cont.) Reference Interval Initials 100h other Nose gear strut and elastomer package - Check strut for deformation, stress marks, and cracks. Inspect correct installation of the nose wheel fork. Inspect elastomer package for wear, deterioration, cracks, correct fit and security.
Page 67 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Electrical System / Avionics Reference Interval Initials 100h other Electrical wiring system - Check the complete electrical MML* 12-20-00 annual wiring system for security, damage, wear and secure fit. Check all cable connections for tight fit, good contact, corrosion and condition.
Page 68 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Return to Service Reference Interval Initials 100h other Install wheels and wheel fairings. 32-40 Install seats (if removed). Install cabin floor boards. Install baggage compartment floorboard. Install access panel of the baggage compartment bulkhead.
Page 69: 6000-Hour Inspection
MAINTENANCE MANUAL 3. 6000-Hour Inspection The airframe of the type AQUILA AT01 is limited to 6.000 hours of flight time (refer to 04-00). An inspection program to reach an extension of replacement time can be obtained from the type certificate holder on request.
Page 70 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL 6000-Hour Inspection Checklist Aircraft S/N Operating Hours Registration TTSN Number Engine S/N Operating Hours Date TTSN / TTSO Propeller S/N Operating Hours Date TTSN / TTSO Inspection Items Inspection Finding / Initials Left Wing...
Page 71 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Left Wing (Cont.) Method Condition Areas around inspection openings - delamination, cracks. Wing leading edge bonding area - disbonds, cracks. V, T Area around pitot-static tube opening - delamination, cracks.
Page 72 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Right Wing (Cont.) Method Condition Inner Flap Hinge Support Rib Bonding area of rib to the wing shell - delamination, cracks. V, T Condition of rib laminate, delamination, cracks.
Page 73 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Right Wing (Cont.) Method Condition Flap hinge levers - delamination at bolt area, bolt corrosion. Tank Rib Bonding area of rib to the wing shell - delamination, cracks.
Page 74 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Control Surfaces (Cont.) Method Condition Areas around hinge fasteners - delamination from skin, cracks. Condition of control horn bearing, corrosion, play. Condition of hinges (bushings), corrosion, play. Inspect for previously performed repairs and repaintings.
Page 75 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Control Surfaces (Cont.) Method Condition Condition of hinges (bushings), corrosion, play. Inspect for previously performed repairs and repaintings. If so, check elevator mass and static moment to be within specified limits (refer to 55-20).
Page 76 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Fuselage (Cont.) Method Condition Fuselage / Wing Interconnection Root ribs and intersection to fuselage - Check for cracks in paint and structure. Area around wing attachment bolt bushings - Check for cracks and disbonding.
Page 77 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Fuselage (Cont.) Method Condition Area around pedal control brackets - delamination, cracks. Cockpit Area and Baggage Compartment Front cockpit floor - Check for delamination and cracks. V, T Check bonding area to the fuselage structure for disbonding.
Page 78 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Fuselage (Cont.) Method Condition Elevator control lever mounting supports on baggage bulkhead - Check for delamination and cracks. Check bonding area to the fuselage structure for disbonding. Flap actuator mounting supports in middle tunnel - Check for delamination and cracks.
Page 79 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL Inspection Items Inspection Finding / Initials Landing Gear (Cont.) Method Condition Engine mount attachment bolts - Check for cracks and wear. Nose wheel axle - Check for cracks and distortion. The aircraft is airworthy and meets the condition specified in the aircraft data sheet.
Page 80 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 81: Daily Inspections
Pre-flight checks are essential for flight safety as numerous accidents can be traced back to inadequate pre-flight checks. The scope of the pre-flight check is listed in the AQUILA AT01-100/200/300 Airplane Flight Manual, section 4.
Page 82 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 83: Unscheduled Maintenance Checks
AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL UNSCHEDULED MAINTENANCE CHECKS 1. General Special checks are to be carried out when an incident has occurred that may have caused damage to the aircraft or impaired airworthiness. In addition, a 25-hour inspection must be carried out on new aircraft and its engine, on overhauled engines and after extensive airframe repairs.
Page 84 AQUILA AT01-100/200/300 Maintenance Checks MAINTENANCE MANUAL (3) Inspect nose landing gear. (a) Check wheel fairing for cracks, dents and delamination. (b) Inspect fairing mounts for cracks, distortion and other damage. (c) Check nose gear strut mount for deformation and cracks. Check nose gear strut journal bearing for proper operation and play.
Page 85: Dimensions And Areas
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS AND AREAS...
Page 86 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 87 AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page DIMENSIONS AND AREAS - GENERAL .............06-00-00 Introduction 06-00-00 General Description 06-00-00 AIRCRAFT DIMENSIONS AND AREAS............06-10-00 General 06-10-00 Dimensions and Areas 06-10-00 Weight and Static Moments of Control Surfaces 06-10-00 AIRCRAFT ZONING ..................06-20-00...
Page 88 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 89: Dimensions And Areas - General
AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL DIMENSIONS AND AREAS - GENERAL 1. Introduction This chapter provides information about dimensions and control surface travel and tolerances. Furthermore, this chapter contains information about aircraft zoning and access and inspection plates. Dimensions are presented to aid the operator and/or maintenance personnel in the ground handling of the aircraft, e.g.
Page 90 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 91: Aircraft Dimensions And Areas
AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL AIRCRAFT DIMENSIONS AND AREAS 1. General The wing and tail spans are measured parallel to the relevant reference level. Refer to figure 1 for an illustration of aircraft dimensions. 2. Dimensions and Areas...
Page 92: Weight And Static Moments Of Control Surfaces
AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL Horizontal Stabilizer and Elevator: Profile FX 71/L150-30 Area (entire) 2,0 m² 21.64 ft² 0,68 m 2.24 ft Elevator area 0,58 m² 6.28 ft² Up travel 23 ° ±1,5 ° Down travel 24 ° ±1,5 °...
Page 93 AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL 2,4 (7.9) 1,69 (5.54) 7,4 (24.2) 10,3 (33.8) 1,94 (6.36) MAC 1,07 (3.52) MAC 0,68 (2.24) 3,0 (9.87) Aircraft Dimensions [m (ft.)] Figure 1 Page 3 06-10-00 31.05.24...
Page 94 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 95: Aircraft Zoning
AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL AIRCRAFT ZONING 1. General The aircraft is divided into numbered zones to facilitate the location of aircraft components and parts. The zoning used here is standard. The zones are identified by a three-digit number. The first digit in the sequence denotes the major...
Page 96 AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL (Interior) Instrument Panel Firewall Aircraft Zones Figure 1 Page 2 06-20-00 31.05.24...
Page 97 AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL ACCESS & INSPECTION PLATES 1. General Access / inspection plates are used to gain access to various systems, components and parts of structure during maintenance and for inspection. The access and inspection plates are designated logically.
Page 98: Access/Inspection Plates
AQUILA AT01-100/200/300 Dimensions and Areas MAINTENANCE MANUAL 610AB 510AB 210BB 210AB 520AB 620AB 610BB 510BB Access / Inspection Plates Figure 1 Page 2 06-30-00 31.05.24...
Page 99: Lifting And Shoring
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 07 LIFTING AND SHORING...
Page 100 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 101: General
AQUILA AT01-100/200/300 Lifting and Shoring MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page LIFTING AND SHORING - GENERAL............07-00-00 Introduction 07-00-00 General Description 07-00-00 JACKING......................07-10-00 General 07-10-00 Tools, Equipment and Material 07-10-00 Jacking 07-10-00 Hoisting 07-10-00 Page 1 07 - TOC...
Page 102 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 103: Lifting And Shoring - General
AQUILA AT01-100/200/300 Lifting and Shoring MAINTENANCE MANUAL LIFTING AND SHORING - GENERAL 1. Introduction This chapter describes procedures used to jack the aircraft. The equipment required to jack the aircraft and the procedures to be followed are described. 2. General Description In the following, a brief description and intended purpose of each section of this chapter is given.
Page 104 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 105: Jacking
AQUILA AT01-100/200/300 Lifting and Shoring MAINTENANCE MANUAL JACKING 1. General The aircraft is jacked at two points and supported at the tail. The jack points are located at the bottom of the fuselage root ribs (see figure 201). Special adapters must be installed prior to jacking.
Page 106: Hoisting
AQUILA AT01-100/200/300 Lifting and Shoring MAINTENANCE MANUAL (5) Remove tail stand. (6) Remove adapters from jack points. 4. Hoisting Hoisting Procedure (1) The aircraft may be lifted with a one metric ton (2205 lbs) hoist for maintenance purposes. The front sling is hooked to the two upper engine mount bars. The aft sling is positioned around the aft fuselage forward the vertical stabilizer.
Page 107: Leveling And Weighing
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 08 LEVELING AND WEIGHING...
Page 108 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 109 AQUILA AT01-100/200/300 Leveling and Weighing MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page LEVELING AND WEIGHING - GENERAL..........08-00-00 Introduction 08-00-00 General Description 08-00-00 WEIGHING ......................08-10-00 General 08-10-00 Tools, Equipment and Material 08-10-00 Weighing Procedure 08-10-00 LEVELING......................08-20-00 General 08-20-00...
Page 110 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 111: Leveling And Weighing - General
AQUILA AT01-100/200/300 Leveling and Weighing MAINTENANCE MANUAL LEVELING AND WEIGHING - GENERAL 1. Introduction This chapter provides all the necessary information to properly level the aircraft and prepare it for weighing. 2. General Description In the following, a brief description and intended purpose of each section of this chapter is given.
Page 112 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 113: Weighing
C.G. position in flight. Essential condition for a correct function is the input of the latest weighing data. Refer to Electronics International MVP-50 operating instructions for the appropriate procedures. The necessary password can be obtained from AQUILA on request. 2. Tools, Equipment and Material...
Page 114 AQUILA AT01-100/200/300 Leveling and Weighing MAINTENANCE MANUAL AIRCRAFT WEIGHING REPORT MODEL: SERIAL NUMBER: REGISTRATION NUMBER: DATE: Data in accordance with airplane flight manual Reference datum: Leading edge of wing root rib. Horizontal reference line: Refer to 08-20-00 for information on longitudinal leveling.
Page 115 AQUILA AT01-100/200/300 Leveling and Weighing MAINTENANCE MANUAL After these preparations have been completed, place scales under each wheel. Be sure that no side forces act on the scales to avoid incorrect readings. Once the scales are in place, level the aircraft as described in section 08-20-00 "Leveling".
Page 116 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 117: Leveling
AQUILA AT01-100/200/300 Leveling and Weighing MAINTENANCE MANUAL LEVELING 1. General Before every weighing process, the aircraft has to be leveled. 2. Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer Spirit level commercially at least 1 m available (3.28 ft) length...
Page 118 AQUILA AT01-100/200/300 Leveling and Weighing MAINTENANCE MANUAL Longitudinal Leveling Wedge Positioning Figure 201 Page 202 08-20-00 28.02.20...
Page 119: Towing And Taxiing
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 09 TOWING AND TAXIING...
Page 120 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 121 AQUILA AT01-100/200/300 Towing and Taxiing MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page TOWING AND TAXIING - GENERAL ............09-00-00 Introduction 09-00-00 General Description 09-00-00 TOWING......................09-10-00 General 09-10-00 Tools, Equipment and Material 09-10-00 Towing Procedure 09-10-00 TAXIING ......................09-20-00 General...
Page 122 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 123: Towing And Taxiing - General
AQUILA AT01-100/200/300 Towing and Taxiing MAINTENANCE MANUAL TOWING AND TAXIING - GENERAL 1. Introduction This chapter describes towing and taxiing procedures. It contains instructions as to how the aircraft can be moved without a tow bar. 2. General Description In the following, a brief description and intended purpose of each section of this chapter is given.
Page 124 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 125: Towing
AQUILA AT01-100/200/300 Towing and Taxiing MAINTENANCE MANUAL TOWING 1. General The aircraft may be moved by hand with or without a tow bar. The towing procedure is described below. 2. Tools, Equipment and Materials Quantity Equipment Parts No. Manufacturer 3.A.
Page 126 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 127: Taxiing
AQUILA AT01-100/200/300 Towing and Taxiing MAINTENANCE MANUAL TAXIING 1. General The aircraft is directionally controlled during taxiing by the steerable nose wheel linked through the rudder pedals and toe operated brakes. During taxiing the engine should be operated as described in section 4 of the airplane flight manual.
Page 128 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 129: Parking, Mooring, Storage And Return To Service
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE...
Page 130 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 131 AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page PARKING, MOORING, STORAGE AND RETURN TO SERVICE - GENERAL ..............10-00-00 Introduction 10-00-00 General Description 10-00-00 PARKING ......................10-10-00 General 10-10-00 Parking 10-10-00 STORAGE ......................10-11-00 Storage with a Duration up to 30 Days...
Page 132 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 133: Parking, Mooring, Storage And Return To Service - General
AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL PARKING, MOORING, STORAGE AND RETURN TO SERVICE - GENERAL 1. Introduction This chapter provides instructions on how to park, moor, store and transport the aircraft. 2. General description The chapter is divided into different sections to help maintenance personnel to find any information required more easily.
Page 134 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 135: Parking
AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL PARKING 1. General In order to protect the aircraft when it is parked in the open, the following parking instructions should be followed. The extent of the measures depends on park duration and weather conditions.
Page 136 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 137: Storage
AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL STORAGE 1. Storage with a Duration up to 30 Days The following procedures should be followed if the aircraft is be stored for 7 to 30 days to prevent deterioration during periods of non-use.
Page 138 AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL (5) Brakes (a) Apply brakes at least once a week. (6) Pitot tube (a) Put on a pitot tube cover. (7) Ventilation of the aircraft (a) Ventilate aircraft well before storage. (b) In the open, depending on external conditions (high humidity, high temperatures etc.) ventilate the aircraft several times during storage.
Page 139: Mooring
2. Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer 3.B. Ropes AQUILA Aviation GmbH 3.B. Tie-down AQUILA Aviation GmbH rings 3. Mooring The aircraft has three tie-down points; two are located on the underside of the wings and the third is located on the lower fin.
Page 140 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 141: Return To Service
AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL RETURN TO SERVICE 1. Storage between 5 and 30 Days After storage lasting between 5 and 30 days, the following should be carried out before returning to service: (1) Perform a thorough pre-flight check 2.
Page 142 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 143: Transport
AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL TRANSPORT 1. General The aircraft may be transported in open or closed trailers. It is recommended to use a standard semi-trailer container or an ISO container for transportation over greater distances. Container dimensions have to be at least: length = 12 000 mm, width = 2300 mm, height = 2350 mm.
Page 144 AQUILA AT01-100/200/300 Parking, Mooring . . MAINTENANCE MANUAL NOTE: Stow wing close to the container sidewall in order to have the entire diagonal of the container cross-section available to store the fuselage. NOTE: If sufficient space is available, the wing may also be transported lying on pads and a pallet-like support to match or compensate wing dihedral.
Page 145: Placards And Markings
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS...
Page 146 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 147 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page PLACARDS AND MARKINGS - GENERAL ..........11-00-00 Introduction 11-00-00 General Description 11-00-00 EXTERIOR PLACARDS AND MARKINGS...........11-20-00 General 11-20-00 Tools, Equipment and Material 11-20-00 Removal/Installation 11-20-00 Maintenance/Care 11-20-00 INTERIOR PLACARDS AND MARKINGS ...........11-30-00...
Page 148 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 149: Placards And Markings - General
AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL PLACARDS AND MARKINGS - GENERAL 1. Introduction This chapter provides information about interior and exterior graphics, placards, labels and interior markings, their maintenance and repair. 2. General Description Below a brief description and intended purpose of each section of this chapter is given.
Page 150 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 151: Exterior Placards And Markings
AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL EXTERIOR PLACARDS AND MARKINGS 1. General This section gives maintenance and care instructions for exterior graphics, markings, etc.. Figure 201 shows the locations of the exterior placards and markings. 2. Tools, Equipment and Material...
Page 152 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL (4) Do not allow fuel to spill on to graphics. If fuel spills on to graphics, wipe off with a cloth and rinse with water thoroughly. (5) Do not remove snow and ice from surfaces using sharp-edged instruments.
Page 153 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Detail- The unusable amount of fuel depends on the model. The shown placard is only valid for the AT01-100/200. Exterior Placards and Markings Figure 201 (1)
Page 154 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. KRAFTSTOFF FUEL DRAIN ABLASS Detail- VERZURRPUNKT TIE DOWN Detail- 2,5 bar 36 psi Detail- 2,5 bar 36 psi Detail- 2,0 bar 29 psi Detail- (red jack point markings)
Page 155 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Detail- (flap position markings ) Detail- HIER EINGEBAUT INSTALLED HERE Detail- NICHT SCHIEBEN Detail- NO PUSH Detail- Exterior Placards and Markings Figure 201 (3) Page 205 11-20-00 31.05.24...
Page 156 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated not in scale. ! ACHTUNG ! ! CAUTION ! Kein Flugmotorenöl einfüllen. Detail- DO NOT use aviation grade oil Siehe Flughandbuch Refer to POH ! ACHTUNG ! ! CAUTION ! Keine Automobilbremsflüssigkeit...
Page 157 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Externe GROUND Stromversorgung POWER 12 V DC 12 VDC Detail- Exterior Placards and Markings Figure 201 (5) EFFECTIVITY Page 207 Aircraft equipped with external power receptacle 11-20-00 31.05.24...
Page 158 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 159: Interior Placards And Markings
AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL INTERIOR PLACARDS AND MARKINGS 1. General This section gives information about removal and installation of interior placards, markings etc.. Figure 201 shows the aircraft interior placards and markings. If the information on the placard is no longer legible or the placard is partially destroyed or is no longer in place, it must be replaced.
Page 160 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Close to receptacle. * Position of this placard can On the right side wall of the vary on the instrument panel. center pedestal adjacent to the adjusting knob. On both control sticks below the handle.
Page 161 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Fuel Kraftstoff Schalter Künstl. Switch Attitude Pumpe Audio Audio Pump Leiste Horizont Panel Indicator MAIN MAIN Wende Turn Schalter Switch Coordin. Zeiger Leiste (OAT) Panel (OAT)
Page 162 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. OIL TEMP. ÖLTEMPERATUR Detail- CYL. HEAD TEMP. ZYL. KOPF TEMP. Detail- OIL PRESS. ÖLDRUCK Detail- KRAFTSTOFF FUEL CAPACITY Detail- 109,6 LITER AUSFLIEGBAR 28.9 GAL / 109.6 LITER USABLE...
Page 163 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. KRAFTSTOFF FUEL AUSFLIEGBAR USABLE The unusable amount 109,6 LITER 109.6 LTR of fuel depends on the Detail- model. The shown 28.9 GAL placard is only valid...
Page 164 Interior Placards and Markings 1) AT01-100 only. Figure 201 (5) AT01-200 only. 3) AT01-300 only. 4) Aircraft equipped with analog engine instruments or Garmin G3X Touch only. 5) Aircraft equipped with pitot heating system only. 6) Aircraft equipped with non-(E)TSO’d GPS-receiver only.
Page 165 BAT2 for Flight BAT2 im Flug for Parking am Boden 1,2,3) Detail- ALT1 AMPS ALT2 Interior Placards and Markings Figure 201 (6) 1) Aircraft equipped with Garmin G3X Touch only. 2) AT01-200 only. Page 207 3) AT01-300 only. 11-30-00 31.05.24...
Page 166 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Speed range 60 KIAS to 150 KIAS with Flaps up (cruise) only Trim DN / FWD in intervals of if indicated max. 2 sec. Trim UP / AFT Detail- AP DISC Detail- Placard located on both control sticks.
Page 167 AQUILA AT01-100/200/300 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. LANE A LANE B Detail- ENG BACKUP PWR Detail- ENG START PWR Detail- Kraftst. Fuel Pumpe Pump Detail- Test Test ALTERNATE AIR ALTERNATE AIR Detail- ZIEHEN EIN...
Page 168 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 169 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 12 SERVICING...
Page 170 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 171 AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page SERVICING - GENERAL..................12-00-00 Introduction 12-00-00 General Description 12-00-00 REPLENISHING - DESCRIPTION..............12-10-00 General 12-10-00 Fuel 12-10-00 Engine Oil 12-10-00 Hydraulic Fluid 12-10-00 FUEL - SERVICING...................12-11-00 General 12-11-00 Safety and Maintenance Precautions...
Page 172 AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page BATTERY - SERVICING ...................12-17-00 General 12-17-00 Battery Servicing 12-17-00 SCHEDULED SERVICING - DESCRIPTION ..........12-20-00 General 12-20-00 LUBRICANTS - DESCRIPTION..............12-21-00 General 12-21-00 Service Notes 12-21-00 Definition of „As Needed“...
Page 173: Servicing - General
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL SERVICING - GENERAL 1. Introduction This chapter gives information on the replenishment of fluids and the lubrication of components. The chapter also contains instructions required to carry out scheduled servicing. 2. General Description The chapter is designed to help authorized personnel to correctly service the aircraft.
Page 174 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 175: Replenishing - Description
10,4 AT01-300: 23,0 Fuel Specification The following fuel is approved for use in the AQUILA AT01. The minimum RON should be 95 (ASTM D4814: min. AKI 91). EN 228 Super (Premium) EN 228 Super plus (Premium plus) AVGAS 100 LL (Grade ASTM-D910, blue color)
Page 176: Engine Oil
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL 3. Engine Oil Engine Oil Capacity Liters U.S. Quarts Engine oil capacity 3.17 Initial filling 3.70 Minimum 2.64 Oil Specification CAUTION: DO NOT USE AVIATION GRADE ENGINE OIL. IF MORE THAN 30% OF OPERATION HOURS HAVE BEEN FLOWN WITH LEADED FUEL (E.G.
Page 177: Fuel - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL FUEL - SERVICING 1. General Fuel Tanks (1) The aircraft is equipped with two integral wing fuel tanks. The fuel tanks are located inside each wing between the front and rear spars. Each fuel tank has a filler cap on the top wing surface.
Page 178: Fueling And Defueling
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL Maintenance Precautions (1) Use designated equipment for fuel loading / unloading to prevent contamination. (2) Only use approved anti-icing additive. (3) Blend fuel in accordance with prescribed procedures. (4) Document all fuel blending. 3. Fueling and Defueling Fueling (1) Move aircraft to a designated fuel loading / fuel unloading area.
Page 179: Engine Oil - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL ENGINE OIL - SERVICING 1. General This chapter provides information for checking and changing engine oil. The oil filler cap of the oil tank is located on the right side of the engine behind cylinder no. 3 (AT01-100/300) / on the left side of the engine behind cylinder no.
Page 180: Oil Changing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL CAUTION: UNDER SEVERE OPERATING CONDITIONS, THE FREQUENCY OF OIL CHANGES MUST BE INCREASED REGARDLESS OF THE TYPE OF FUEL USED (MOGAS OR AVGAS). Oil Change Intervals (1) Under normal operating conditions, oil must be changed every 100 hours.
Page 181: Induction Air Filter - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL INDUCTION AIR FILTER - SERVICING 1. General The air filter in the air induction system keeps dust and dirt particles from entering the system. It is located in the air filter box on the left (AT01-100/300) / right (AT01-200) inside of the lower cowling.
Page 182 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 183: Cooling System - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL COOLING SYSTEM - SERVICING 1. General The cooling system of the engine is designed for liquid cooling of the cylinder heads and ram air cooling of the cylinders. The cooling system of the cylinder heads is a closed circuit with an expansion tank.
Page 184: Renewal Of The Coolant
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL 3. Renewal of the Coolant Servicing Procedure (1) When engine is cold, open pressure cap of the expansion tank and lowest coolant hose on the radiator and drain the coolant. (2) Reconnect coolant hose. (3) Refill freshly mixed coolant into expansion tank (highest point of the cooling system).
Page 185: Brake System - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL BRAKE SYSTEM - SERVICING 1. General Ground service for the brake system is limited to the replenishment of brake fluid. The brake fluid reservoir is located at the upper left firewall in the engine compartment.
Page 186 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 187: Tires - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL TIRES - SERVICING 1. General The landing gear is equipped with 5.00-5 tires. Depending on the wheel/brake system installed, either 8 or 10 PLY rated tubeless tires (Beringer wheels) or 6 PLY rated tube-type tires (Cleveland / Grove wheels) are mounted.
Page 188 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 189: Battery - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL BATTERY - SERVICING 1. General The battery should be serviced every 100 hours. In the case of heavy-duty operation or operation in cold regions, service intervals should be shorter. On aircraft equipped with Rotax 914F engine, an additional battery (BAT2) is installed. This battery has to be replaced annually.
Page 190 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 191: Scheduled Servicing - Description
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL SCHEDULED SERVICING - DESCRIPTION 1. General This section provides instructions necessary to carry out scheduled servicing, such as the periodic lubrication of aircraft components; external and internal cleaning. Service intervals are also provided. This section does not include lubrication procedures required to complete maintenance measures.
Page 192 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 193: Lubricants - Description
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL LUBRICANTS - DESCRIPTION 1. General This section assists with the selection of proper lubricants used to maintain the aircraft. To ensure a long service life of the lubricated components, it is recommended to always use pure and authorized lubricants.
Page 194: Recommended Lubricants
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL 4. Recommended Lubricants: Categories of lubricants, their specifications and typical areas of application are provided below. Abbreviation Specification Description MIL-PRF-81322 Grease, wide temperature range MIL-PRF-23827 Grease, aircraft and instrument, Gear and actuator screw MIL-L-7870 Oil, general purpose...
Page 195: Lubrication - Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL LUBRICATION - SERVICING 1. General This section contains information on lubrication intervals for components or parts. 2. Lubrication Chart Figure 201 shows the location of components or parts to be regularly lubricated. The following chart contains detailed information about the lubrication interval, the recommended lubricant and the dispensing equipment.
Page 196 AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL Lubrication Chart Figure 301 (1) Page 302 12-22-00 31.05.24...
Page 197 AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL ACCESS ZONE INDEX ITEM LUBE TYPE (APPL.) INTERVAL PLATE Cleveland / Grove: 721, GR (Hand) Main wheel bearings 500 h or GR (Hand) Nose wheel bearings annual Battery terminals PL (Hand) 100 h annual or...
Page 198 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 199: Aircraft Exterior - Cleaning And Care
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL AIRCRAFT EXTERIOR - CLEANING AND CARE 1. General The good flight performance of the aircraft is achieved due to the modern construction and the use of specific materials. For efficient laminar flow, a clean surface is very important. Therefore, one should always keep the entire aircraft clean, but especially the leading edges of the wing.
Page 200: Cleaning And Care Of The Aircraft Exterior Surfaces
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL 4. Cleaning and Care of the Aircraft Exterior Surfaces Procedure for cleaning the exterior surface of the aircraft (1) Park the aircraft in a hangar or in the shadows, avoid places with a lot of dust caused by wind or vehicles.
Page 201: Cleaning The Engine
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL 6. Cleaning the Engine Safety and Maintenance Precautions (1) The engine should be cleaned during every 100-hour inspection. (2) Handle chemical cleaners and solvents with caution. Always read the manufacturer ’s instruction and follow them carefully.
Page 202: Cleaning And Care Of The Propeller
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL CAUTION: DO NOT ROTATE THE PROPELLER CLOCKWISE. (11) Before starting the engine, rotate the propeller by hand no less than five complete revolutions. 7. Cleaning and Care of the Propeller Clean propeller if necessary with any car wash solution or equivalent. This should be done at least every 50 hours.
Page 203: Aircraft Interior - Cleaning And Care
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL AIRCRAFT INTERIOR - CLEANING AND CARE 1. General This section provides the information required to clean the aircraft interior properly. Several recommended types of cleaning agents for different materials and the relevant cleaning and care procedures are also described below.
Page 204 AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL Blot up any liquid spilled promptly with an absorbent tissue or cloth. Press the blotting material firmly against the upholstery and hold for several seconds. Continue blotting until no more liquid is absorbed. Scrape off sticky materials cautiously with a dull knife, then clean area as required.
Page 205: Unscheduled Servicing
AQUILA AT01-100/200/300 Servicing MAINTENANCE MANUAL UNSCHEDULED SERVICING 1. General This section contains those instructions necessary to carry out unscheduled servicing for example: removing ice and snow from a parked aircraft. 2. Removing Snow and Ice CAUTION: DO NOT REMOVE SNOW AND ICE FROM SURFACES USING SHARP-EDGED INSTRUMENTS.
Page 206 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 207: Standard Practices - Airframe
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES - AIRFRAME...
Page 208 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 209 AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page STANDARD PRACTICES AIRFRAME - GENERAL........20-00-00 Introduction 20-00-00 General Description 20-00-00 FASTENER IDENTIFICATION AND TORQUE DATA .......20-10-00 General 20-10-00 Bolt Types 20-10-00 Torques 20-10-00 CONVERSION DATA..................20-11-00 General...
Page 210 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 211: Standard Practices Airframe - General
Maintenance procedures which are unique to a specific system / component / part are described in the corresponding chapter. As far as the maintenance of the AQUILA AT01 is concerned, there are no standard practices or relevant safety regulations, which require special knowledge other than that which is commonly expected for the maintenance of small aircraft.
Page 212 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 213: Fastener Identification And Torque Data
AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL FASTENER IDENTIFICATION AND TORQUE DATA 1. General This section contains information concerning the identification of bolts, the correct usage of bolts and nuts and torque data. CAUTION: OBSERVE STANDARD OR TORQUE VALUES RECOMMENDED BY THE MANUFACTURER AND MAKE SURE THE RECOMMENDED SAFETYING DEVICE FOR EVERY FASTENER IS APPLIED.
Page 214: Torques
AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL 3. Torques NOTE: When a specific torque is not provided in the maintenance instructions contained in this maintenance manual, use the standard torque patterns shown in table 201 respectively the special torques in table 202.
Page 215 AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL Table 201: Standard Torques DIN and LN specifications Torque values Torque values Thread size in.lbs 15.9 31.9 56.6 141.6 283.2 NOTE: Castellated nuts (DIN 935, 937) 531.1 should be finger tightened. Table 202: Special Torques Torque (Nm / in.lbs)
Page 216 AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL 1. Variant - The adapter increases the effective length of the torque wrench. adapter drive centerline handgrip centerline wrench drive centerline Y = apparent (indicated) torque T x L formula: T = actual (desired) torque...
Page 217: Conversion Data
AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL CONVERSION DATA 1. General This chapter is designed to assist the operator with the conversion of commonly used measuring units found in this manual from Imperial, US and metric measuring systems. 2. Conversion Factors Subsequent conversion factors of units of measurement are given from the metric system to the US / Imperial systems and vice versa.
Page 218 AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL (3) Cubic measures Table 3 - Conversion of Cubic Measures Unit m³ Cu. in. Cu. ft. Imp.-Gallons U.S.-Gallons 1 Liter 0,001 61,03 0,05332 0,22 0,2642 1 m³ 1000 61023 35,315 219,97 264,175 1 cu. in.
Page 219: Equivalents For Standard Values
AQUILA AT01-100/200/300 Standard Practices MAINTENANCE MANUAL 3. Equivalents for Standard Values For conversion data to convert standard drill sizes to inch and millimeter equivalents refer to figure 1. Drill Drill Drill 0,34 0,0135 1,85 0,0730 4,09 0,1610 0,37 0,0145 1,93...
Page 220 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 221: Ventilation And Heating
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 21 VENTILATION AND HEATING...
Page 222 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 223 AQUILA AT01-100/200/300 Ventilation and Heating MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page VENTILATION AND HEATING - GENERAL..........21-00-00 Introduction 21-00-00 General Description 21-00-00 FRESH AIR DISTRIBUTION - MAINTENANCE .........21-20-00 General 21-20-00 Eyeball Ventilator Removal/Installation 21-20-00 Heat Relief Valve Removal/Installation 21-20-00 HEATING - MAINTENANCE .................21-40-00...
Page 224 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 225: Ventilation And Heating - General
AQUILA AT01-100/200/300 Ventilation and Heating MAINTENANCE MANUAL VENTILATION AND HEATING - GENERAL 1. Introduction This chapter describes those systems and components used to heat and ventilate the cabin. Fresh air for ventilation (outside air temperature) and heated fresh air for heating and windshield defrosting is supplied to the cabin.
Page 226 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 227: Fresh Air Distribution - Maintenance
AQUILA AT01-100/200/300 Ventilation and Heating MAINTENANCE MANUAL FRESH AIR DISTRIBUTION - MAINTENANCE 1. General Maintenance is limited to the removal and installation of the components. 2. Eyeball Ventilator Removal/Installation (Ref. Fig. 201) NOTE: Removal/installation of the left and right eyeball ventilator is analogous.
Page 228 AQUILA AT01-100/200/300 Ventilation and Heating MAINTENANCE MANUAL flexible air duct to air inlet hose clamp eyeball ventilator Detail- Eyeball Ventilator Installation Figure 201 Page 202 21-20-00 30.04.13...
Page 229 AQUILA AT01-100/200/300 Ventilation and Heating MAINTENANCE MANUAL cabin heat control knob flexible air duct to windscreen heating manifold Detail- heated air distributor actuating lever control cable to relief valve flexible air duct to heat exchanger Detail- heat relief valve flexible air duct...
Page 230 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 231: Heating - Maintenance
AQUILA AT01-100/200/300 Ventilation and Heating MAINTENANCE MANUAL HEATING - MAINTENANCE 1. General Fresh air is heated when it passes through the heat exchanger at the engine. The heat exchanger consists of a shroud, which is set around the exhaust muffler. Flexible ducts are connected to the heat exchanger through which the air enters and exits.
Page 232 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 233: Auto Flight
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 22 AUTO FLIGHT...
Page 234 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 235 AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity AUTO FLIGHT - GENERAL ................22-00-00 GFC 500 Introduction 22-00-00 GFC 500 General Description 22-00-00 GFC 500 AUTO FLIGHT - GENERAL ................22-00-00 Introduction 22-00-00 General Description 22-00-00 AUTOPILOT - MAINTENANCE ..............22-10-00...
Page 236 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 237: Auto Flight - General
1. Introduction This chapter contains information on the Garmin GFC 500 autopilot system available for the AQUILA AT01-100 and AT01-200. The GFC 500 autopilot system consists of the following major components: - G5 (autopilot computer; refer to 34-25-00 for inspection/maintenance)
Page 238 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 239: Auto Flight - General
MAINTENANCE MANUAL AUTO FLIGHT - GENERAL 1. Introduction This chapter contains information on the Garmin G3X autopilot system available for the AQUILA AT01-100 and AT01-200. The G3X autopilot system consists of the following major components: - G3X Touch (autopilot computer; refer to 34-25-00 for inspection/maintenance) - GMC 507 (certified version) mode controller - 2x (or 3x) GSA 28 servos (certified version;...
Page 240 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 241: Autopilot - Maintenance
The actual software version is documented in the aircraft equipment list, located in chapter 6 of the airplane flight manual. All service information released from AQUILA and related to software versions has to be attached to this maintenance manual for continuing airworthiness! For bonding checks on the AQUILA AT01-100/200 no procedures or equipment are necessary other than that which are commonly expected for bonding measurements on small aircraft.
Page 242: Inspection/Check
AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL 2. Inspection/Check Servicing of the GFC 500 / G3X autopilot equipment is ‘on condition’ only. ’ On condition’ replacement and/or servicing should occur when an item exhibits conditions, symptoms, and/or abnormalities defined in section 5 of the Garmin GFC 500 Part 23 AML STC Maintenance Manual.
Page 243: Roll Servo Removal/Installation/Inspection
AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL 4. Roll Servo Removal/Installation/Inspection (Ref. Fig. 201) Remove Roll Servo (1) Ensure electrical power to aircraft and AP main switch are OFF. (2) Remove access panel 210 AB (refer to 06-30-00). (3) Remove access panels 211BB, 211HL and 211HR (refer to 25-12-00).
Page 244 AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL Detail- pushrod servo crank arm servo bracket Detail- servo electrical connector Roll Servo Installation Figure 201 EFFECTIVITY Page 204 Aircraft equipped with Garmin GFC 500 or G3X 22-10-00 autopilot 01.02.23...
Page 245: Pitch Servo Removal/Installation/Inspection
AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL 5. Pitch Servo Removal/Installation/Inspection (Ref. Fig. 202) Remove Pitch Servo (1) Ensure electrical power to aircraft and AP main switch are OFF. (2) Remove access panel 211KC (refer to 25-12-00). (3) Disconnect pushrod at bell crank.
Page 246 AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL Detail- servo bracket electrical connector servo servo crank arm pushrod Detail- Pitch Servo Installation Figure 202 EFFECTIVITY Page 206 Aircraft equipped with Garmin GFC 500 or G3X 22-10-00 autopilot 01.02.23...
Page 247 AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL 6. Yaw Servo Removal/Installation/Inspection (Ref. Fig. 203 / Optional) KS_Syst_Loc_R914.iso Remove Yaw Servo (1) Ensure electrical power to aircraft and AP main switch are OFF. (2) Remove access panel 211 JB (refer to 25-12-00).
Page 248 AQUILA AT01-100/200/300 Auto Flight MAINTENANCE MANUAL Detail- electrical connector servo 5 Nm 45 in.lbs servo bracket cable clamp bridle cable capstan cable clamp Detail- Yaw Servo Installation Figure 203 EFFECTIVITY Page 208 Aircraft equipped with Garmin GFC 500 or G3X...
Page 249 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 23 COMMUNICATIONS...
Page 250 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 251 AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity COMMUNICATIONS - GENERAL ............23-00-00 Introduction 23-00-00 General Description 23-00-00 SPEECH COMMUNICATION - DESCRIPTION ......23-10-00 GNS 430W / GTN 650 Introduction 23-10-00 GNS 430W / GTN 650...
Page 252 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 253: Communications - General
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL COMMUNICATIONS - GENERAL 1. Introduction This chapter describes and provides maintenance instructions for components and systems used to communicate between occupants of the aircraft and between the aircraft and other aircraft or ground stations. Technical publications available from the manufacturer or vendor of the various components and systems, which are not covered in this manual, must be utilized as necessary for the maintenance of those components and systems.
Page 254 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 255: Speech Communication - Description
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION – DESCRIPTION 1. Introduction This section covers the portion of the system which utilizes voice communication from air-to-air or air-to-ground installations. It includes the VHF speech communications portion of the NAV/COM radio Garmin GNS 430W or GTN 650.
Page 256 AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL GNS 430 unit jackscrew access hole GTN 650 unit jackscrew access hole GNS 430, GTN 650 Front View Figure 1 EFFECTIVITY Page 2 Aircraft equipped with Garmin 23-10-00 GNS 430W / GTN 650 30.04.13...
Page 257: Speech Communication - Maintenance
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION – MAINTENANCE 1. General The scope of maintenance is limited to the removal and installation of the components. For removal and installation procedures for the GNS 430W / GTN 650 GPS antenna, refer to 34-40-00.
Page 258: Inspection/Check
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL Install Antenna CAUTION: WIRING MUST NOT INTERFERE WITH THE OPERATION OF MOVEABLE AIRCRAFT COMPONENTS. (1) Position antenna with gasket to fuselage. (2) Install mounting plate from inside the fuselage. (3) Secure antenna base to fuselage using screws, nuts and washers. Reinstall ground wire.
Page 259: Speech Communication - Description
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION - DESCRIPTION 1. Introduction This section covers the portion of the system which utilizes voice communication from air-to-air or air-to-ground installations. It includes the VHF speech communications portion of the NAV/COM radio Garmin SL30 or SL40.
Page 260 AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL transmit function to/from annunciator annunciators indication active standby standby Graphic large outer frequency symbol frequency Bearing photocell knob SL30 118.00 s136.00 PULL SQUELCH COM NAV power / frequency ident enter small inner flip/flop radio volume /...
Page 261: Speech Communication - Maintenance
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL SPEECH COMMUNICATION – MAINTENANCE 1. General The scope of maintenance is limited to the removal and installation of system components. For further information, refer to Garmin SL30 NAV/COM installation manual, P/N 560-0404-XX, latest revision, or Garmin SL40 NAV/COM installation manual, P/N 560-0956-XX, latest revision, as well as any other appropriate manufacturer publications.
Page 262 AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL Install Antenna CAUTION: WIRING MUST NOT INTERFERE WITH THE OPERATION OF MOVEABLE AIRCRAFT COMPONENTS. (1) Position antenna with gasket to fuselage. (2) Install mounting plate from inside the fuselage. (3) Secure antenna base to fuselage using screws, nuts and washers. Reinstall ground wire.
Page 263: Audio Integrating - Maintenance
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL AUDIO INTEGRATING - MAINTENANCE 1. General This section covers that portion of the system which controls the output of the communication and navigation receivers to crew member headphones and speakers, and the output of the crew member microphones to the communication transmitters.
Page 264: Audio Control Unit Removal/Installation
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL 2. Audio Control Unit Removal/Installation Remove Audio Control Unit (1) Ensure electrical power to aircraft is OFF. (2) Disconnect the plug at the back of the audio control unit. (3) Remove control knob caps on the front panel of the audio control unit.
Page 265: Audio Integrating - Maintenance
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL AUDIO INTEGRATING - MAINTENANCE 1. General This section covers that portion of the system which controls the output of the communication and navigation receivers to crew member headphones and speakers, and the output of the crew member microphones to the communication transmitters.
Page 266: Gma 340 / Gma 350
AQUILA AT01-100/200/300 Communications MAINTENANCE MANUAL (3) Turn the wrench clockwise until the unit is secured in the rack. Continue turning until tight, but do not over-tighten. (4) Conduct a functional test of the unit. MKR/BCN A O M NAV1 NAV2...
Page 267: Electrical Power
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER...
Page 268 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 269 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity ELECTRICAL POWER - GENERAL ...............24-00-00 Introduction 24-00-00 General Description 24-00-00 ELECTRICAL POWER - TROUBLESHOOTING.........24-00-00 Troubleshooting 24-00-00 ALTERNATOR SYSTEM - DESCRIPTION ............24-20-01 Rotax 912S Introduction 24-20-01...
Page 270 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Effectivity ELECTRICAL LOAD DISTRIBUTION - DESCRIPTION......24-60-00 Introduction 24-60-00 Description and Operation 24-60-00 CIRCUIT BREAKER - MAINTENANCE ............24-61-00 General 24-61-00 Circuit Breaker Removal/Installation 24-61-00 Circuit Breaker Current Ratings 24-61-00 ELECTRICAL SYSTEM WIRING - MAINTENANCE........24-97-00...
Page 271: Electrical Power - General
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ELECTRICAL POWER - GENERAL 1. Introduction This chapter describes the units and components, which generate, control and supply AC and DC electrical power for other systems. 2. General Description The aircraft is equipped with a 12V DC electrical system. It is powered by a belt driven 600W alternator (ALT 1) and a 12V battery which is installed on the front-right side of the firewall.
Page 272 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 273: Electrical Power - Troubleshooting
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ELECTRICAL POWER - TROUBLESHOOTING 1. Troubleshooting If a power problem or a complete blackout occurs, first check all connections to the components and the circuit breakers. Troubleshooting Chart: TROUBLE POSSIBLE CAUSE REMEDY No alternator ALT1 switch OFF Turn switch ON.
Page 274 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL If a voltage reading is obtained, replace battery relay. Defective wiring or electrical Step 5: connection between battery With switch BAT in ON position, relay and starter relay. measure voltage between starter side relay terminal, and starter relay.
Page 275: Alternator System - Description
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ALTERNATOR SYSTEM - DESCRIPTION 1. Introduction The alternator system supplies the electrical equipment with electrical power when the engine is running and is the main current source in the power supply design. The alternator system consists of the following components:...
Page 276 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL warning light “ALT 1” circuit breaker “Warning Lights” external alternator Ammeter circuit breaker “ALT 1” circuit breaker “ALT 1 Excitation” ALT 1 External Alternator System (Schematic) Figure 1 warning light “ALT 2” ROTAX circuit breaker internal alternator “Warning Lights”...
Page 277: Alternator System - Description
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ALTERNATOR SYSTEM - DESCRIPTION 1. Introduction The alternator system supplies the electrical equipment with electrical power when the engine is running and is the main current source in the power supply design. The alternator system consists of the following components:...
Page 278 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL BAT 2 is protected from loads (incl. the main fuel pump) by a Schottky diode and charged by the internal alternator with charging overcurrent protection. The battery is switched OFF via the ALT2/BAT2 switch whenever the aircraft is parked to prevent discharge of the battery.
Page 279 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL warning light “ALT 1” circuit breaker “Warning Lights” external alternator Ammeter circuit breaker “ALT 1” circuit breaker “ALT 1 Excitation” ALT 1 External Alternator System (Schematic) Figure 1 warning light circuit breaker “ALT 2”...
Page 280 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 281: Alternator System - Description
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ALTERNATOR SYSTEM - DESCRIPTION 1. Introduction The alternator system supplies the electrical equipment with electrical power when the engine is running and is the main current source in the power supply design. The alternator system consists of the following components:...
Page 282 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL Ammeters measure the current from the external (ALT 1) and internal (ALT 2) alternators and the current to/from the battery, a voltmeter is connected with the aircraft bus bar. All instruments are found in the digital engine monitor.
Page 283 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL warning light “ALT 1” circuit breaker “Warning Lights” external alternator Ammeter circuit breaker “ALT 1” circuit breaker “ALT 1 Excitation” ALT 1 External Alternator System (Schematic) Figure 1 Regulator B Internal Alternator B (ALT 2)
Page 284 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 285: Alternator System - Maintenance
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ALTERNATOR SYSTEM - MAINTENANCE 1. General Maintenance is limited to the removal and installation of the (external) alternator, drive belt and rectifier-regulator unit (only Rotax 912S Night-VFR or Rotax 914 equipped aircraft). Refer to the appropriate ROTAX publications for maintenance procedures on the internal alternator(s).
Page 286 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL Detail- External Alternator Installation Figure 201 Page 202 24-20-00 31.05.24...
Page 287 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL (4) Cut safety wire and loosen adjusting bolt and alternator mounting bolts. (5) Slip drive belt off alternator pulley. (6) Remove propeller (refer to 61-10). (7) Remove alternator drive belt. Install Alternator Drive Belt (1) Install alternator drive belt around drive pulley.
Page 288 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL “Nordlock” washer Detail- nut M8 (2ea) rectifier-regulator unit Detail- “Nordlock” washer (4ea) bolt M8x20 (2ea) Rectifier-Regulator Unit Installation ( Night-VFR equipped aircraft only) Figure 202 EFFECTIVITY Page 204 Aircraft equipped with Rotax 912S engine 24-20-00 31.05.24...
Page 289 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL “Nordlock” washer Detail- Schottky diodes Cover battery BAT 2 fuse holder Detail- rectifier-regulator unit bolt M8x20 “Nordlock” washer (4ea) Rectifier-Regulator Unit Installation Figure 202 EFFECTIVITY Page 205 Aircraft equipped with Rotax 914F engine 24-20-00...
Page 290: Bat 2 Battery Removal/Installation
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL 5. BAT 2 Battery Removal/Installation Remove BAT 2 Battery (1) Ensure electrical power to aircraft is OFF. (2) Remove engine cowling (refer to 71-10). (3) Disconnect main battery (refer to 24-30). (4) Disconnect BAT 2 battery cables.
Page 291: Main Battery System - Description
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL MAIN BATTERY SYSTEM - DESCRIPTION 1. Introduction The battery system supplies power to the electrical equipment if the alternator fails. It represents the auxiliary electrical power source. The battery system consists of the following components:...
Page 292 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL BATTERY SYSTEM (SCHEMATIC) to aircraft bus bar battery AMPS ALT 1 ammeter DC VOLTS voltmeter to clock (optional) firewall battery- relay battery Battery System (Schematic) Figure 1 Page 2 24-30-00 31.05.24...
Page 293: Main Battery System - Maintenance
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL MAIN BATTERY SYSTEM - MAINTENANCE 1. General CAUTION: ALWAYS DISCONNECT THE BATTERY BEFORE DOING ANY MAINTENANCE ON THE ELECTRICAL SYSTEM. DISCONNECT THE NEGATIVE LEAD FIRST. RECONNECT THE NEGATIVE LEAD LAST. SECURE THE BATTERY LEADS FROM ACCIDENTAL CONNECTION DURING MAINTENANCE WORKS.
Page 294 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL Install Battery Relay (1) Position and secure battery relay to engine mount using bolts, washers and nuts. (2) Identify and reconnect wires to relay. CAUTION: DO NOT REMOVE INNER NUT WHEN ASSEMBLING. USE WRENCH TO HOLD INNER NUT IN PLACE WHEN APPLYING OUTER NUT.
Page 295: Battery Condition Check
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL 4. Battery Condition Check For Night-VFR equipped aircraft or aircraft equipped with Rotax 914F or 912iS engine, check the battery condition according to one of the following methods: Measure „state of health“ (SOH) according to SAE using specialized test equipment (Schumacher PTI900X or similar).
Page 296 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 297: External Power - Maintenance
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL EXTERNAL POWER - MAINTENANCE 1. General This section covers that portion of the system which connects external electrical power to the aircraft's electrical systems. It includes items such as external power receptacle and relays.
Page 298 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL 1,4-2 Nm 12-18 in.lbs external power relay 5-6 Nm 44-55 in.lbs Detail- ground 4 Pl. power 8212A04N 8212B04 Signal Detail- External Power Receptacle Installation Figure 201 8212A20 EFFECTIVITY Page 202 Aircraft equipped with an external power receptacle 24-40-00 31.05.24...
Page 299: Adjustment/Test
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL Install External Power Relay (1) Position and secure external power relay to engine mount using bolts, washers and nuts. (2) Identify and reconnect wires to external power relay. CAUTION: DO NOT REMOVE INNER NUT WHEN ASSEMBLING. USE WRENCH TO HOLD INNER NUT IN PLACE WHEN APPLYING OUTER NUT.
Page 300 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 301: Electrical Load Distribution - Description
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ELECTRICAL LOAD DISTRIBUTION - DESCRIPTION 1. Introduction Distribution of electrical power supplied by the external and optional the internal alternator and the battery is accomplished by bus bars. The bus architecture allows power to be routed to the essential circuitry if any one of the main power sources fails.
Page 302 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 303: Circuit Breaker - Maintenance
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL CIRCUIT BREAKER - MAINTENANCE 1. General The circuit breaker panel is equipped with circuit breakers of the "push to reset" type. One terminal of each switch/breaker is directly connected to the appropriate bus bar, the other is wired to the component/system it protects.
Page 304 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL Table 201: Circuit Breaker Current Ratings (Cont.) Current Rating Circuit Breaker Effectivity Flap Actuator COM1 & 2 GTN 650, GNS 430W, GTR 225, GNC 255 GTR 205 COM/NAV 1 & 2 GNC215 Landing Light...
Page 305 AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL Table 201: Circuit Breaker Current Ratings (Cont.) Current Rating Circuit Breaker Effectivity Warning Lights Trim Control up to S/N 326 Flap Control Starter Relay Rotax 912S, Rotax 914F Stall Warning CHT (OAT) Fuel Gauge...
Page 306 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 307: Electrical System Wiring - Maintenance
AQUILA AT01-100/200/300 Electrical Power MAINTENANCE MANUAL ELECTRICAL SYSTEM WIRING - MAINTENANCE 1. General Repairs of the electrical system wiring are limited to the replacement and splicing of electrical wires. In general all repairs have to be carried out by certified repair stations or properly certified and trained persons.
Page 308 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 309: Equipment / Furnishings
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT / FURNISHINGS...
Page 310 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 311 AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity EQUIPMENT / FURNISHINGS - GENERAL..........25-00-00 Introduction 25-00-00 General Description 25-00-00 SEATS - MAINTENANCE ................25-10-00 General 25-10-00 Seat Removal/Installation 25-10-00 Gas Spring Strut Assembly Removal/Installation 25-10-00 RESTRAINT SYSTEM - MAINTENANCE.............25-11-00...
Page 312 AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL Page 02 25 - TOC 15.09.09...
Page 313: Equipment / Furnishings - General
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL EQUIPMENT / FURNISHINGS - GENERAL 1. Introduction This chapter describes removable items of equipment and interior furnishings contained in the cabin and baggage compartment. 2. General Description The seats can be adjusted back and forward. The restraint system of each seat is attached to the fuselage structure.
Page 314 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 315: Seats - Maintenance
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL SEATS - MAINTENANCE 1. General The seats are made from fiber composite materials and equipped with integrated safety head rests and removable, hard-wearing seat cushions. An infinitely adjustable seat meets the requirements of a wide range of pilots. The seat track is angled upward for forward travel so that shorter people will be positioned slightly higher as they adjust the seat forward.
Page 316 AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL Detail- Seat Installation Figure 201 Page 202 25-10-00 28.02.20...
Page 317: Gas Spring Strut Assembly Removal/Installation
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL 4. Gas Spring Strut Assembly Removal/Installation Remove Gas Spring Strut Assembly (1) Remove seat cushion. (2) Remove control knob at the remote control of the gas spring locking valve and then the retaining nut which secures the remote control to attachment bracket.
Page 318 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 319: Restraint System - Maintenance
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL RESTRAINT SYSTEM - MAINTENANCE 1. General The seats are equipped with automatic, four point seat belts/shoulder harness assemblies. A central rotary buckle is used to fasten the seat belts/shoulder harness. The design incorporates an inertia reel system for the shoulder portion.
Page 320 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 321: Cabin Interior - Maintenance
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL CABIN INTERIOR - MAINTENANCE 1. General The panels, coverings and carpets can be removed for maintenance purposes. For cabin interior cleaning and care refer to chapter 12, section "Cabin interior - Cleaning and Care".
Page 322 AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL 211 BB 211 AB 211 FT 211 FB remove 211 FT 211 EC 211 LT remove 211 FT disconnect fuel lines remove 211 FB remove 211 BB 211 GT 211 CC 211 DR...
Page 323 AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL 211 IR 211 IC remove 211 IL remove 211 IR 211 IL 211 KC Detail- 211 JB Panels and Covers Figure 201 (2) Page 203 25-12-00 28.02.20...
Page 324 AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL...
Page 325: Cargo Tie-Downs - Maintenance
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL CARGO TIE-DOWNS - MAINTENANCE 1. General Eight cargo tie-down rings are provided to secure baggage. Baggage nets may be used to hold baggage in position during flight. The cargo tie-down rings are secured directly to the floorboard by nutplates or they secure the floorboard to the supports.
Page 326 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 327: Emergency Equipment - Description
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL EMERGENCY EQUIPMENT - DESCRIPTION 1. Introduction This section describes those items of equipment carried for use in emergencies and includes the emergency locator transmitter (ELT) and a fire extinguisher. As standard the aircraft is equipped with a Kannad 406 AF Compact / Integra ELT. Due to the multiplicity of equipment coming onto the market a different ELT may be installed.
Page 328 AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL Detail- ELT remote control panel / indicator (RCPI) Detail- Detail- ELT antenna BNC connector red LED main switch RC connector Detail- mounting bracket Velcro strap ELT Main Components (Kannad 406 AF Compact) Figure 1...
Page 329: Emergency Locater Transmitter - Maintenance
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL EMERGENCY LOCATER TRANSMITTER - MAINTENANCE 1. General This section covers removal and installation procedures of ELT components as well necessary periodic maintenance. Consider all publications / requirements of the appropriate national authority regarding ELT operation and maintenance.
Page 330: Battery Replacement
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL Install ELT Antenna (1) Position antenna with gasket on topside of fuselage. (2) From inside the fuselage install mounting plate. (3) Secure antenna base to topside of fuselage using screws, nuts and washers. Reinstall ground wire.
Page 331: Fire Extinguisher - Maintenance
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL FIRE EXTINGUISHER - MAINTENANCE 1. General The aircraft is equipped with a liquefied-gas type fire extinguisher AIR TOTAL HAL 1 mounted in a quick-release bracket attached to the floor board of the baggage compartment, behind the right seat.
Page 332 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 333: Description And Operation
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL FIRE EXTINGUISHER - MAINTENANCE 1. General The aircraft is equipped with a liquefied-gas type fire extinguisher H3R Aviation RT A400 or A344T mounted in a quick-release bracket attached to the floor board of the baggage compartment, behind the right seat.
Page 334: Fire Extinguisher Removal/Installation
AQUILA AT01-100/200/300 Equipment / Furnishings MAINTENANCE MANUAL 4. Fire Extinguisher Removal/Installation Remove Fire Extinguisher (1) Release quick-release clamp. (2) Remove fire extinguisher from bracket assembly. Install Fire Extinguisher (1) Position fire extinguisher in bracket assembly. (2) Secure with quick release clamp.
Page 335: Flight Controls
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS...
Page 336 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 337 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page FLIGHT CONTROLS - GENERAL ..............27-00-00 Introduction 27-00-00 General Description 27-00-00 AILERON CONTROL SYSTEM - DESCRIPTION........27-10-00 Introduction 27-10-00 Description and Operation 27-10-00 AILERON CONTROL SYSTEM - MAINTENANCE ........27-10-00...
Page 338 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Inspection/Check 27-30-00 Adjustment/Test 27-30-00 ELEVATOR TRIM CONTROL - DESCRIPTION..........27-31-00 Introduction 27-31-00 Description and Operation 27-31-00 ELEVATOR TRIM CONTROL - MAINTENANCE ........27-31-00 General 27-31-00 Trim Actuator Removal/Installation...
Page 339: Flight Controls - General
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL FLIGHT CONTROLS - GENERAL 1. Introduction This chapter contains information about the flight controls used to manually control the aircraft in flight. It also includes functional and maintenance information about the flaps. 2. General Description The conventionally designed flight control system is divided into aileron control, rudder control, elevator control and the wing flaps system.
Page 340 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 341: Aileron Control System - Description
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL AILERON CONTROL SYSTEM - DESCRIPTION 1. Introduction This section describes that portion of the flight control system which controls the position and movement of the ailerons. The rigging procedure for the aileron control system is also provided.
Page 342 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL pushrod 4 pushrod 3 pushrod 2 pushrod 1 roll servo (optional) Aileron Control System Design and Function Figure 1 Page 2 27-10-00 05.03.21...
Page 343: Aileron Control System - Maintenance
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL AILERON CONTROL SYSTEM - MAINTENANCE 1. General For a breakdown of components, refer to figure 201, 202 and 203. WARNING: WHEN INSTALLING COMPONENTS OF CONTROL SYSTEM, NEW SELF-LOCKING NUTS SHOULD ALWAYS BE USED. NEVER USE A SELF-LOCKING NUT MORE THAN ONCE.
Page 344 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL left side shown (right side analogous) Detail- Detail- Roll servo (optional) pushrod, refer to chapter 22-10-00 Component Installation Figure 201 Page 202 27-10-00 05.03.21...
Page 345: Pushrod 2 Removal/Installation
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Install Front Bellcrank (1) Position front bellcrank between brackets and secure using bolt, washer and nut. (2) Connect pushrods to front bellcrank (optional roll servo pushrod: refer to 22-10-00). (3) Perform aileron control system inspection/check (refer to “Inspection/Check” below).
Page 346 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL left side shown (right side analogous) Detail- Detail- Component Installation Figure 202 Page 204 27-10-00 05.03.21...
Page 347: Pushrod 4 Removal/Installation
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL 8. Pushrod 4 Removal/Installation Remove Pushrod 4 (1) Remove wing (refer to 57-10-00). (2) Open access panel 520 (620) AB (refer to 06-30-00). (3) Disconnect pushrod at aileron bellcrank. (4) Remove rod end bearing.
Page 348 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- left side shown (right side analogous) Detail- Aileron Bellcrank Installation Figure 203 Page 206 27-10-00 05.03.21...
Page 349: Adjustment/Test
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL (2) Verify minimum rod end thread engagement of 8 mm (0.312 in.). (3) Verify ailerons can be moved smoothly through the full travel. No grinding is audible. (4) Check ailerons for correct travel using an inclinometer. If necessary perform aileron control system adjustment/test (refer to “Adjustment/Test”...
Page 350 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 351: Rudder Control System - Description
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL RUDDER CONTROL SYSTEM - DESCRIPTION 1. Introduction This section describes that portion of the flight control system which controls the position and movement of the rudder. The rigging procedure for the rudder control system is also provided.
Page 352 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL yaw damper (optional) Rudder Control Design and Function Figure 1 Page 2 27-20-00 05.03.21...
Page 353: Rudder Control System - Maintenance
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL RUDDER CONTROL SYSTEM - MAINTENANCE 1. General For a breakdown of the components, refer to figure 201 and 202. WARNING: WHEN INSTALLING COMPONENTS OF THE CONTROL SYSTEM, NEW SELF- LOCKING NUTS SHOULD ALWAYS BE USED. NEVER USE A SELF-LOCKING NUT MORE THAN ONCE.
Page 354 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- Rudder Control Installation Figure 201 Page 202 27-20-00 05.03.21...
Page 355: Control Cable Removal/Installation
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Install Rudder Pedal Assembly (1) Position rudder bars in left and right bearing blocks and secure bearing blocks to firewall using bolts. (2) Reinstall lower half of middle bearing block. (3) Reconnect steering tubes to rudder bars.
Page 356 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- Rudder Pedal / Master Cylinder Installation Figure 202 Page 204 27-20-00 05.03.21...
Page 357: Inspection/Check
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL 5. Inspection/Check Inspection/Check (1) Perform a visual inspection of the rudder control system. Check all components for proper installation and security. No signs of excessive play. NOTE: The maximum permissible value of rudder play at hinge pins is 1,0 mm (0.04 in.) axial play and 0,3 mm (0.01 in.) radial play.
Page 358 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 359: Elevator Control System - Description
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL ELEVATOR CONTROL SYSTEM - DESCRIPTION 1. Introduction This section describes that portion of the flight control system which controls the position and movement of the elevator. The rigging procedure for the elevator control system is also provided.
Page 360 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL pitch servo (optional) pushrod 2 pushrod 1 Elevator Control System Design and Function Figure 1 Page 2 27-30-00 05.03.21...
Page 361: Elevator Control System - Maintenance
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL ELEVATOR CONTROL SYSTEM - MAINTENANCE 1. General For a breakdown of the components, refer to figure 201 and 202. WARNING: WHEN INSTALLING COMPONENTS OF THE CONTROL SYSTEM NEW SELF- LOCKING NUTS SHOULD ALWAYS BE USED. NEVER USE A SELF-LOCKING NUT MORE THAN ONCE.
Page 362 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- Fuselage structure omitted for clarity. left side shown (right side analogous) Detail- Component Installation Figure 201 Page 202 27-30-00 05.03.21...
Page 363: Elevator Bellcrank Removal/Installation
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL (4) Check elevator control system and elevator trim system for proper operation and rig if necessary (refer to 27-30-00 and 27-31-00). (5) Install baggage compartment floor panel (refer to 25-12-00). (6) Install seats (refer to 25-10-00).
Page 364 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Fuselage structure omitted for clarity. Detail- pitch servo (optional) control rod, refer to chapter 22-10-00 Detail- Component Installation Figure 202 Page 204 27-30-00 05.03.21...
Page 365: Adjustment/Test
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL 6. Adjustment/Test Adjustment/Test (1) Remove baggage compartment floor panel (refer to 25-12-00). (2) Remove access plate 211 HL and HR (refer to 25-12-00). (3) Lock elevator bellcrank in neutral position in a suitable manner (the line between pushrod attach points on bellcrank is perpendicular to the pushrod 2).
Page 366 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 367: Elevator Trim Control - Description
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL ELEVATOR TRIM CONTROL - DESCRIPTION 1. Introduction The aircraft isequipped with an electrical spring-force trim system. An electrical trim actuator changes the pre-load of a pair of springs that applies a defined force to the elevator pushrod.
Page 368 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- elevator pushrod trim position sensor Fuselage structure omitted for clarity. trim actuator Elevator Trim System Design And Function Figure 1 Page 2 27-31-00 05.03.21...
Page 369: Elevator Trim Control - Maintenance
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL ELEVATOR TRIM CONTROL - MAINTENANCE 1. General For a breakdown of the components, refer to figure 201. 2. Trim Actuator Removal/Installation Remove Trim Actuator (1) Set the elevator trim system to neutral. (2) Place the BAT switch in OFF position.
Page 370 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- Fuselage structure Fuselage structure omitted for clarity. omitted for clarity. Elevator Trim System Installation Figure 201 Page 202 27-31-00 05.03.21...
Page 371: Flap Control System - Description
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL FLAP CONTROL SYSTEM - DESCRIPTION 1. Introduction This section describes that portion of the flight control system which controls the position and movement of the flaps. The rigging procedure forthe flap control system is also provided.
Page 372 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL flap actuator torque tube Flap Control System Design and Function Figure 1 Page 2 27-50-00 05.03.21...
Page 373: Flap Control System - Maintenance
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL FLAP CONTROL SYSTEM - MAINTENANCE 1. General This section provides instructions for removal and installation of components and instruction for flap control system rigging. For a breakdown of the components, refer to figure 201, 202, 203, and 204.
Page 374 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- Fuselage structure omitted for clarity. Flap Control System Installation Figure 201 Page 202 27-50-00 05.03.21...
Page 375: Flap Pushrod Removal/Installation
AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL (2) Secure both halves to pivot bracket using bolt, washer and nut. (3) Install spacer and bolt, washer and nut connecting halves. (4) Connect torque tube assembly to flap actuator pushrod. (5) Perform flap control system inspection/check and rig system, if necessary (refer to “Inspection/Check”...
Page 376 AQUILA AT01-100/200/300 Flight Controls MAINTENANCE MANUAL Detail- Wing structure omitted for clarity. Flap Control System Installation Figure 201 Page 204 27-50-00 05.03.21...
Page 377: Adjustment/Test
06-10-00. (e) Repeat check on right flap. NOTE: If the results of inspection do not fall within the tolerance specified in 06-10-00, contact AQUILA Aviation for disposition. (4) Install all items removed for access. 6. Adjustment/Test Adjustment/Test (1) Remove access plate 210 AB (refer to 06-30-00).
Page 378 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 379 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 28 FUEL...
Page 380 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 381 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity FUEL - GENERAL .....................28-00-01 Rotax 912S Introduction 28-00-01 Rotax 912S General Description 28-00-01 Rotax 912S FUEL - GENERAL .....................28-00-02 Rotax 914F Introduction 28-00-02 Rotax 914F General Description...
Page 382 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Effectivity FUEL PRESSURE INDICATION - MAINTENANCE ........28-44-01 Analog / G3X General 28-44-01 Analog / G3X Fuel Pressure Switch Removal/Installation 28-44-01 Analog / G3X FUEL PRESSURE INDICATION - MAINTENANCE ........28-44-02...
Page 383: Fuel - General
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL - GENERAL 1. Introduction This chapter covers those units and components which are not part of the engine but store or deliver fuel to the engine or indicate fuel quantity and pressure. For further information on the internal engine fuel system components, refer to applicable ROTAX publications.
Page 384 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL fuel vent lines wing fuel tanks drain valve drain valve dual fuel level indicator return line FUEL LEFT RIGHT LIFT LIFT KNOB KNOB fuel selector / shut-off valve fuel filter return line aux. fuel pump drain valve “Fuel Pump”...
Page 385: Fuel - General
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL - GENERAL 1. Introduction This chapter covers those units and components which are not part of the engine but store or deliver fuel to the engine or indicate fuel quantity and pressure. For further information on the internal engine fuel system components, refer to applicable ROTAX publications.
Page 386 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL fuel vent lines wing fuel tanks drain valve drain valve dual fuel level indicator return line FUEL LEFT RIGHT LIFT LIFT KNOB KNOB fuel selector / shut-off valve gascolator return line main fuel pump fuel flow meters...
Page 387: Fuel - General
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL - GENERAL 1. Introduction This chapter covers those units and components which are not part of the engine but store or deliver fuel to the engine or indicate fuel quantity and pressure. For further information on the internal engine fuel system components, refer to applicable ROTAX publications.
Page 388 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL fuel vent lines wing fuel tanks right tank left tank drain valve drain valve dual fuel level indicator return line FUEL LEFT RIGHT LIFT LIFT KNOB KNOB fuel selector / shut-off valve gascolator return line...
Page 389: Fuel Storage - Maintenance
The inboard fuel tank ribs are easily accessible for maintenance work through access panel 610 BB / 510 BB in the lower wing skin. The wing fuel tanks are maintenance-free. However, if a leak is suspected, AQUILA Aviation should be consulted.
Page 390 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 391: Fuel Distribution - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL DISTRIBUTION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General The fuel distribution system consists primarily of the fuel selector / shut-off valve, electrical fuel pump(s), fuel filter(s), check valves, fuel lines and the AUX fuel pump switch.
Page 392 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL Notes: Fuel system components Detail- in left wing analogous. Fuselage structure omitted fuel return line for clarity. fuel line reducer fitting (only with Ø8mm fuel return lines) Fuel Selector / Shut-Off Valve Installation Figure 201...
Page 393 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL fuel return line fuel supply line Detail- 2 Nm 17.7 in.lbs Fuel Level Sensor / Fuel Tank Outlet Strainer Installation Figure 202 Page 203 28-20-00 31.05.24...
Page 394 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL firewall hardpoints Detail- fuel line fuel return line Electrical Fuel Pump Installation Figure 203 EFFECTIVITY Page 204 Aircraft equipped with Rotax 912S engine 28-20-00 31.05.24...
Page 395 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL KS_Syst_Loc_R914.iso check valve main fuel pump from fuel selector / shut-off valve check valve aux. fuel pump Detail- gascolator Electrical Fuel Pump Installation to engine Figure 203 KS-Pumpen_Inst_Expl_R914.iso EFFECTIVITY Page 204 Aircraft equipped with Rotax 914F engine 28-20-00 31.05.24...
Page 396 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL check valve main fuel pump from fuel selector / shut-off valve check valve aux. fuel pump Detail- Electrical Fuel Pump Installation to engine Figure 203 gascolator EFFECTIVITY Page 204 Aircraft equipped with Rotax 912iS engine 28-20-00 31.05.24...
Page 397: Fuel Selector / Shut-Off Valve Removal/Installation
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL A clean fuel distribution system is very important for the secure and continuous supply of fuel to KS_Syst_Loc_R914.iso the engine. The fuel system is equipped with drain valves with which fuel in the system can be examined for contamination and grade.
Page 398: Electrical Fuel Pump Removal/Installation (Rotax 912S)
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL 3. Electrical Fuel Pump Removal/Installation (Rotax 912S only) Remove Electrical Fuel Pump (1) Ensure electrical power to aircraft is OFF. (2) Remove engine cowling (refer to 71-10). (3) Disconnect battery (refer to 24-30). (4) Close fuel selector / shut-off valve.
Page 399: Fuel Filter Maintenance (Rotax 912S)
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL (5) Perform leakage check: Plug outlet of fuel pump assembly. Connect inlet to air compressor and pressure gauge. Rotax 914F: Apply 2 bar (29 psi) / Rotax 912iS: Apply 6 bar (87 psi) air pressure and check system for leaks. No pressure loss is allowed.
Page 400: Fuel Fine Filter Removal/Installation (Rotax 912Is)
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL (11) Reinstall filter element. Gently grip at the top of the filter element and screw to hand tight. (12) Fit new O-ring to the bowl. (13) Line up arrow on sediment bowl and engraved line on the gascolator body. Carefully push bowl into gascolator body and tighten the retaining ring.
Page 401: Fuel Quantity Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General The fuel quantity indicating system consists of two resistive float type fuel quantity sensors, one in each tank, a dual fuel quantity indicator and wiring connecting the components.
Page 402: Fuel Quantity Indicating System Test/Calibration
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL Install Fuel Quantity Sensor (1) Verify battery is disconnected and electrical power to aircraft is OFF. (2) Check ease of movement of the float arm before installing the sensor. (3) Place sensor with new gasket on to the threaded studs at inboard fuel tank rib.
Page 403 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL (16) Turn BAT switch to the OFF position. (17) Repeat steps (13) thru (16) for RH wing fuel tank. Fuel Quantity Indicating System Calibration NOTE: A calibration module is necessary to perform the steps described below.
Page 404 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 405: Fuel Quantity Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Fuel quantity indication is included in the Garmin G3X Touch system. Fuel quantity is measured by two resistive type fuel quantity sensors, one in each tank, electrically connected to the GEA 24 engine interface at the back of the instrument panel.
Page 406: Fuel Quantity Indicating System Test/Calibration
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL 3. Fuel Quantity Indicating System Test/Calibration NOTE: When a fuel quantity sensor is replaced, the fuel quantity indicating system must be calibrated. NOTE: Due to the dihedral angle of the wing and the position of the fuel quantity sensor (total) fuel levels above approx.
Page 407 AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL (2) Ensure electrical power to aircraft is OFF. (3) Fill unusable amount of fuel into each wing fuel tank. (4) Wait approx. 30 seconds. Then gently shake wing to assure fuel quantity sensors settle in their final position.
Page 408 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 409: Fuel Quantity Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Fuel quantity indication is included in the engine monitoring system. Fuel quantity is measured by two resistive type fuel quantity sensors, one in each tank, electrically connected to the engine data converter (EDC) via an interface module (RFLM-4) at the back of the instrument panel.
Page 410: Resistive Fuel Module Removal/Installation
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL 3. Resistive Fuel Module Removal/Installation Remove Resistive Fuel Module (1) Ensure electrical power to aircraft is OFF. (2) Disconnect battery (refer to 24-30). (3) Remove glare shield (refer to 31-10). (4) Disconnect electrical connectors from back of module.
Page 411 NOTE: Refer to Electronics International MVP-50 operating instructions for further information on the fuel tank calibration procedure. The necessary password can be obtained from AQUILA Aviation on request. (1) Prepare aircraft (a) Drain fuel from wing tanks (refer to 12-11).
Page 412 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 413: Fuel Pressure Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL PRESSURE INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Low fuel pressure is indicated by a warning light. Fuel pressure is measured by a pressure switch at the fuel manifold on top of the engine.
Page 414 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 415: Fuel Pressure Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL PRESSURE INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Fuel pressure indication is included in the Garmin G3X Touch. It is indicated as difference between the absolute fuel pressure and the boost pressure in the airbox.
Page 416 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 417: Fuel Pressure Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL PRESSURE INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Fuel pressure indication is included in the engine monitoring system. Fuel pressure is measured by a pressure sensor (PT-30GA) electrically connected to the engine data converter (EDC).
Page 418 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 419: Fuel Pressure Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL PRESSURE INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Fuel pressure indication is included in the Garmin G3X Touch. It is indicated as difference between the absolute fuel pressure and the pressure in the airbox.
Page 420 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 421: Fuel Flow Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL FLOW INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Fuel flow is measured by two FT-60 fuel flow sensors: One installed in the fuel supply line, the other one in the return line.
Page 422: Fuel Flow Differential Module Removal/Installation
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL (7) Reconnect electrical connector to sensor. (8) Reconnect battery (refer to 24-30). (9) Run both fuel pumps and check system for leaks and fuel flow indication. Fuel flow indication should read zero with fuel pumps running and the engine switched OFF.
Page 423: Fuel Flow Indication - Maintenance
AQUILA AT01-100/200/300 Fuel MAINTENANCE MANUAL FUEL FLOW INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11! 1. General Fuel flow is calculated by the engine control unit (ECU) based on the injection times and forwarded to the G3X Touch system via CAN interface.
Page 424 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 425: Indicating / Recording Systems
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 31 INDICATING / RECORDING SYSTEMS...
Page 426 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 427 AQUILA AT01-100/200/300 Indicating / Recording MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity INDICATING / RECORDING SYSTEMS - GENERAL........31-00-00 Analog Introduction 31-00-00 Analog General Description 31-00-00 Analog INDICATING / RECORDING SYSTEMS - GENERAL........31-00-00 Introduction 31-00-00 General Description 31-00-00 INDICATING / RECORDING SYSTEMS - GENERAL........31-00-00...
Page 428 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 429: Indicating / Recording Systems - General
Basically the instruments and avionic equipment can be chosen by the customer, but it cannot be installed in any arbitrary combination. Before removing or installing equipment the aircraft manufacturer AQUILA Aviation must be contacted, with the exception of replacing a unit by an identical one.
Page 430 AQUILA AT01-100/200/300 Indicating / Recording MAINTENANCE MANUAL Dimmer Airspeed indicator COM/NAV Attitude gyro Transponder Altimeter Manifold pressure indicator Turn coordinator Tachometer Directional gyro Fuel level indicator Vertical speed indicator CHT indicator Ignition switch Voltmeter ALT1 / BAT switch Oil temperature indicator...
Page 431: Indicating / Recording Systems - General
Basically the instruments and avionic equipment can be chosen by the customer, but it cannot be installed in any arbitrary combination. Before removing or installing equipment the aircraft manufacturer AQUILA Aviation must be contacted, with the exception of replacing a unit by an identical one.
Page 432 AQUILA AT01-100/200/300 Indicating / Recording MAINTENANCE MANUAL 15 16 Warning lights Garmin G3X Touch ELT remote control Attitude indicator (optional) Dimmer Autopilot control panel (optional) COM/NAV Ignition switch Transponder ALT1 / BAT switch ALT2 / BAT2 switch (AT01-200 only) Circuit breaker panel...
Page 433: Indicating / Recording Systems - General
Basically the instruments and avionic equipment can be chosen by the customer, but it cannot be installed in any arbitrary combination. Before removing or installing equipment the aircraft manufacturer AQUILA Aviation must be contacted, with the exception of replacing a unit by an identical one.
Page 434 AQUILA AT01-100/200/300 Indicating / Recording MAINTENANCE MANUAL Transponder Garmin G500 TXi Manifold pressure indicator Attitude indicator (optional) Tachometer Autopilot control panel (optional) Fuel level indicator Ignition switch CHT indicator ALT1 / BAT switch Voltmeter AUX fuel pump switch Oil temperature indicator...
Page 435: Indicating / Recording Systems - General
Basically the instruments and avionic equipment can be chosen by the customer, but it cannot be installed in any arbitrary combination. Before removing or installing equipment the aircraft manufacturer AQUILA Aviation must be contacted, with the exception of replacing a unit by an identical one.
Page 436 AQUILA AT01-100/200/300 Indicating / Recording MAINTENANCE MANUAL Warning lights Garmin G500 TXi ELT remote control Attitude indicator (optional) Dimmer Autopilot control panel (optional) COM/NAV Ignition switch Transponder ALT1 / BAT switch Engine monitoring system ALT2 / BAT2 switch (AT01-200 only)
Page 437: Instrument Panel - Maintenance
AQUILA AT01-100/200/300 Indicating / Recording MAINTENANCE MANUAL INSTRUMENT PANEL - MAINTENANCE 1. General The instrument panel is made from aluminum alloy and is formed in one piece with a shelf. The shelf fits between the panel and the firewall. The panel shelf is attached on the left and right sides to support consoles and secured to the fuselage with bolts.
Page 438 AQUILA AT01-100/200/300 Indicating / Recording MAINTENANCE MANUAL Install Instrument Panel (1) Put instrument panel assembly in position and secure to fuselage using bolts, spacers, washers and nuts. (2) Secure instrument panel to center console using bolts, spacers, washers, and nuts.
Page 439: Landing Gear
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 32 LANDING GEAR...
Page 440 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 441 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectifity LANDING GEAR - GENERAL 32-00-00 Introduction 32-00-00 General Description 32-00-00 MAIN LANDING GEAR - DESCRIPTION..........32-10-00 Introduction 32-10-00 Description and Operation 32-10-00 MAIN LANDING GEAR - MAINTENANCE ..........32-10-00...
Page 442 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL TABLE OF CONTENTS - CONTINUED Chapter Section Title Subject Page Effectivity WHEELS AND BRAKES - MAINTENANCE ..........32-40-00 Cleveland/Grove Main Gear Wheel Removal/Installation 32-40-00 Cleveland/Grove Main Gear Wheel Disassembly/Assembly 32-40-00 Cleveland/Grove Nose Gear Wheel Removal/Installation...
Page 443: Landing Gear - General
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL LANDING GEAR - GENERAL 1. Introduction This chapter describes units and components which furnish a means of supporting and steering the aircraft on the ground, including the main and nose landing gears, brakes, wheels and tires.
Page 444 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 445: Main Landing Gear - Description
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL MAIN LANDING GEAR - DESCRIPTION 1. Introduction The main landing gear consists of the main landing gear struts, the wheels with brakes and the wheel fairings. The wheel fairings are standard equipment. The main gear struts are cantilever spring legs made of spring steel and carry the landing loads.
Page 446 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 447: Main Landing Gear - Maintenance
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL MAIN LANDING GEAR - MAINTENANCE 1. Main Gear Leg Removal/Installation Remove a Main Gear Leg (1) Gain access to the appropriate landing gear mounting brackets (refer to 25-00-00). (2) Lift aircraft (refer to 07-10-00).
Page 448 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL 45 Nm 398 in.lbs Detail- UHMW-insert UHMW-insert UHMW-insert UHMW-insert Main Gear Leg Installation Figure 201 Page 202 32-10-00 01.06.22...
Page 449: Nose Landing Gear - Description
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL NOSE LANDING GEAR - DESCRIPTION 1. Introduction The aircraft has a steerable nose landing gear which is equipped with a shock absorber and wheel fairing. 2. Description and Operation The nose gear consists of a welded tubular steel strut pivotally attached to the engine mount.
Page 450 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 451: Nose Landing Gear - Maintenance
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL NOSE LANDING GEAR - MAINTENANCE 1. Nose Gear Leg Removal/Installation (Figure 201) Remove Nose Gear Leg (1) Jack aircraft or weight tail of aircraft to raise nose wheel (refer to 07-00-00). (2) Remove engine cowling (refer to 71-10-00).
Page 452 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL 32 Nm 283 in.lbs Detail- Detail- NOTE: Right steering rod assembly omitted for clarity. Rivet (blind) 3ea 28 Nm 248 in.lbs Nose Gear Leg Installation Figure 201 322014 Page 202 32-20-00 01.06.22...
Page 453 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL Secured with safety wire. 10 Nm 88 in.lbs Detail- Damper Assy and Nose Wheel Fork Installation Figure 202 Page 203 32-20-00 01.06.22...
Page 454 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL NOTE: Damper assembly with 4 rubber elements shown. If a reinforced nose wheel fork is installed, a damper assembly with 3 rubber elements has to be used (refer to SB-AT01-037). Detail- Damper Assembly Figure 203...
Page 455: Wheels And Brakes - Description
AQUILA AT01-100/200/300 MAINTENANCE MANUAL WHEELS AND BRAKES - DESCRIPTION 1. Introduction This section describes components and maintenance of the wheels and the brake system. For tire specifications, refer to “Landing Gear - General”. For more detailed information on the installed wheels and brakes, refer to the maintenance guide for Beringer products, P/N SM-00, latest revision (www.beringer-aero.com).
Page 456 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 457: Wheels And Brakes - Maintenance
Equipment Parts No. Manufacturer 3.B. and 4.B. waterproof grease commercially available 5.B. plywood tool with OT-002 Beringer Aero / AQUILA conical bushing 5.A. and B. tire lubricant commercially available (silicone free) 12.A. and B. brake bleeding kit ONC01 Beringer Aero / AQUILA 3.
Page 458 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL 28 Nm 248 in.lbs 10 Nm 88 in.lbs Detail- 30 Nm 265 in.lbs Main Gear Wheel Installation / Disassembly Figure 201 (1) EFFECTIVITY Page 202 Aircraft equipped with Beringer wheel/brake system 32-40-00 01.06.22...
Page 459 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL **On A/C with RF-005 main wheels 14(3ea) Detail- Inner circlip Detail- Inner bearing Inner wheel half 11(8ea) Large O-ring Tire Central spacer Outer wheel half Outer bearing Outer circlip 10 Valve 10 Nm 11 Bolt (8ea) 88 in.lbs...
Page 460 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL **On A/C with RF-018 main wheels Detail- 10(8ea) Inner circlip Inner bearing Inner wheel half Large O-ring 10 Nm Tire 88 in.lbs Outer wheel half Outer bearing Outer circlip Valve 10 Bolt (8ea) Main Gear Wheel Installation / Disassembly...
Page 461 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL 5 Nm 44 in.lbs Detail- Nose Gear Wheel Installation / Disassembly Figure 202(1) 322023 EFFECTIVITY Page 205 Aircraft equipped with Beringer wheel / brake system 32-40-00 01.06.22...
Page 462 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL **On A/C with RA-002 nose wheels 14(3ea) Detail- Inner circlip Detail- Inner bearing Inner wheel half 11(8ea) Large O-ring Tire Central spacer Outer wheel half Outer bearing Outer circlip 10 Valve 11 Bolt (8ea) 10 Nm 88 in.lbs...
Page 463 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL **On A/C with RA-014 nose wheels Detail- 10(8ea) Inner circlip Inner bearing Inner wheel half 10 Nm Large O-ring 88 in.lbs Tire Outer wheel half Outer bearing Outer circlip Valve 10 Bolt (8ea) Nose Gear Wheel Installation / Disassembly...
Page 464: Wheel Disassembly/Assembly/Tire Change
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL Install Nose Gear Wheel (1) Greasing the axle on the bearing surfaces (e.g. Bel-Ray waterproof grease) is recommended for corrosion protection. (2) Slide axle into wheel and spacer sleeve onto axle. (3) Slide the whole wheel assembly between wheel fork arms.
Page 465 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL **On A/C with RF-005 and RA-002 wheels connector small O-ring central spacer axle Ø 3 mm with- out sharp edges small O-ring large O-ring outer wheel half plywood tool (lower part with supports) Wheel Assembly...
Page 466 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL conical bushing outer wheel half Tire arrangement: red spot in front of valve Wheel Assembly Figure 203 (2) EFFECTIVITY Page 210 Aircraft equipped with Beringer wheel/brake system 32-40-00 01.06.22...
Page 467 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL wheel assembly screws (8ea) large O-ring inner wheel half Wheel Assembly Figure 203 (3) EFFECTIVITY Page 211 Aircraft equipped with Beringer wheel/brake system 32-40-00 01.06.22...
Page 468 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL Assemble a Wheel NOTE: Plywood tool with conical bushing made from polished aluminium required for wheel assembly. Additionally an axle with diameter 3 mm (3/32 in.) without sharp edges is required for positioning the central spacer on RF-005 / RA-002 wheels.
Page 469: Disc Clip Removal/Installation
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL (11) Install wheel assembly screws. Secure screws using medium strength threadlocker (Loctite 243 recommended). Screw to contact and torque tighten to 10 Nm (88 in.lbs). Respect order when torque tightening. Torque all screws to 10 Nm (88 in.lbs) a second time.
Page 470: Wheel Bearing Removal/Installation
AQUILA AT01-100/200/300 Landing Gear Landing Gear MAINTENANCE MANUAL 7. Wheel Bearing Removal/Installation A. Removal of Wheel Bearings (1) Disassemble wheel (refer to “Wheel Disassembly” above). (2) Remove circlips on wheel half with a snap-ring plier. (3) Place wheel flange in an oven at 110°C to 120°C for 30 minutes (never exceed 150°C).
Page 471: Brake Pad Replacement
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL (3) Remove the old brake pads. NOTE: The disc has not to be removed during the pad change. It is recommended to leave the disc in place. (4) Clean all around pistons with a dry cloth to remove dust.
Page 472: Brake Disc Replacement
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL (6) Insert new brake pads. CAUTION: NEVER MIX OLD AND NEW PADS. ALL 4 PADS MUST BE REPLACED AT THE SAME TIME. NOTE: Pad insulator and grid should not be reused, they come together with new brake pads.
Page 473: Brake Master Cylinder Removal/Installation
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL CAUTION: WHEN NEW BRAKE DISCS ARE INSTALLED BRAKE PADS MUST BE CHANGED TO NEW ONES EVEN IF NOT WORN OUT. (1) Follow brake pad change procedure (refer to “Brake Pad Replacement” above). (2) Degrease new brake disc prior to installation.
Page 474 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL pedal shaft master brake cylinder Detail- pilot’s left pedal assembly Master Brake Cylinder Installation Figure 205 EFFECTIVITY Page 218 Aircraft equipped with Beringer wheel/brake system 32-40-00 01.06.22...
Page 475 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL (5) Dismantle the wheel axle to loosen the back plate. Remove 2 screws securing backplate to axle and remove backplate. (6) Remove pistons. NOTE: Air pressure can be used to remove pistons. Replace caliper back plate and blow air pressure into inlet.
Page 476 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL bleeder cylinder Detail- piston seals pistons brake pad assemblies back plate 25 Nm 220 in.lbs assembly screws Brake Caliper Assembly Figure 206 EFFECTIVITY Page 220 Aircraft equipped with Beringer wheel/brake system 32-40-00 01.06.22...
Page 477: Brake System Bleeding / Brake Fluid Change
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL (8) Install bleeding screw and reconnect brake line to caliper. CAUTION: COPPER SEALS MUST BE CHANGED AT EACH REMOVAL OF THE HYDRAULIC FITTING. (9) Reinstall main gear wheel (refer to “Main Landing Gear Wheel Installation” above).
Page 478: Brake System Conditioning
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL After component replacement or repair: (1) Check the brakes for firm pedal pressure and bleed the system if either brake feels spongy. (2) Perform a minimum of six stops from a speed of between 25 and 40 knots, using light pedal effort and letting the brakes cool partially (about one minute) between stops.
Page 479: Wheels And Brakes - Description
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL WHEELS AND BRAKES - DESCRIPTION 1. Introduction Nose and main landing gear wheels are of conventional design. The wheels of the main landing gear are each equipped with a single brake disc, floating cylinder brake assembly.
Page 480 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 481: Wheels And Brakes - Maintenance
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL WHEELS AND BRAKES - MAINTENANC 1. Main Gear Wheel Removal/Installation Remove a Main Gear Wheel (1) Jack aircraft or appropriate main gear wheel (refer to 7-00-00). (2) Remove screws securing wheel fairing and remove wheel fairing.
Page 482 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL 28 Nm 248 in.lbs Detail- Main Gear Wheel Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Cleveland/Grove wheel/brake 32-40-00 system 01.06.22...
Page 483: Nose Gear Wheel Removal/Installation
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL (4) Reassemble the wheel unit, including the brake disc, with bolts, washers, and nuts. Torque to 10 - 12 Nm (89 - 106 in.lbs.). (5) Inflate the tire as required (refer to “Landing Gear - General”).
Page 484 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL brake disc on main wheels only Detail- +/-2 Wheel Assembly Figure 202 EFFECTIVITY Page 204 Aircraft equipped with Cleveland/Grove wheel/brake 32-40-00 system 01.06.22...
Page 485: Brake Master Cylinder Removal/Installation
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL NOTE: When the wheel halves are joined, it is recommended to double check that the tube isn't pinched, using an inspection mirror and a flashlight. (4) Reassemble the wheel unit with bolts, washers, and nuts. Torque to 10 - 12 Nm.
Page 486 AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL back plate torque plate lining brake hose piston O-ring cylinder Detail- anchor bolt bleeder assy Brake Caliper Assembly Figure 203 324007 EFFECTIVITY Page 206 Aircraft equipped with Cleveland/Grove wheel/brake 32-40-00 system 01.06.22...
Page 487: Brake Disc Removal/Installation
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL Install a Caliper (1) Slide the caliper casing anchor pins into the torque plate bushings until the lining on the pressure plate contacts the brake disc. (2) Position the back plate against the other side of the disc and thread the two caliper casing bolts with their washers into the back plate from opposite side of the caliper casing.
Page 488: Brake System Bleeding
AQUILA AT01-100/200/300 Landing Gear MAINTENANCE MANUAL NOTE: Before setting the first rivet fully, start the other rivets to keep the lining aligned properly with the plate. (5) Set all the rivets fully. (6) Slide the pressure plate with its new lining material over the caliper casing anchor pins.
Page 489 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 33 LIGHTS...
Page 490 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 491 AQUILA AT01-100/200/300 Lights MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity LIGHTS - GENERAL..................33-00-00 Introduction 33-00-00 General Description 33-00-00 INTERIOR LIGHTS - MAINTENANCE ............33-10-00 General 33-10-00 Post Light Removal/Installation 33-10-00 Nulite Removal/Installation 33-10-00 Cockpit Light Removal/Installation 33-10-00 EXTERIOR LIGHTS - MAINTENANCE ............33-40-00...
Page 492 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 493: Lights - General
AQUILA AT01-100/200/300 Lights MAINTENANCE MANUAL LIGHTS - GENERAL 1. Introduction This chapter describes interior and exterior lighting systems used on the aircraft, including removal and installation procedures of components and light bulb replacement instructions. 2. General Description A cockpit light is installed for general cabin lighting, for emergency instrument panel lighting and as a reading light.
Page 494 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 495: Interior Lights - Maintenance
AQUILA AT01-100/200/300 Lights MAINTENANCE MANUAL INTERIOR LIGHTS - MAINTENANCE 1. General If instruments do not have internal lighting, they are illuminated by post lights or Nulites. Post lights are LED lights that illuminate the instrument panel and function as instrument mounting bolts.
Page 496 AQUILA AT01-100/200/300 Lights MAINTENANCE MANUAL Install Nulite (1) Put Nulite in position between the instrument panel and the instrument with the wires coming out of the top. (2) Install affected instrument as described in the apropriate chapter of this manual.
Page 497: Exterior Lights - Maintenance
AQUILA AT01-100/200/300 Lights MAINTENANCE MANUAL EXTERIOR LIGHTS - MAINTENANCE 1. General The aircraft is equipped with Aveo Engineering Andromeda Aurora (up to S/N AT01-326) / Ultra Galactica (from S/N AT01-327 or SI-AT01-018, annex 19) or Whelen Orion 660 (SI-AT01-026) navigation/position/anti-collision lights and a Hella 90mm module halogen / Whelen Parmetheus PAR-36 Plus LED landing light.
Page 498 AQUILA AT01-100/200/300 Lights MAINTENANCE MANUAL 3. Navigation/Position/Anti-Collision Light Removal/Installation/Check Remove Aveo Engineering Navigation/Position/Anti-Collision Light (1) Ensure BAT, NAV light and ACL light switches are in OFF position. (2) Remove screw(s) securing base plate to wing tip fairing. Carefully remove light.
Page 499 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 34 NAVIGATION...
Page 500 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 501 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity NAVIGATION - GENERAL ..............34-00-00 Introduction 34-00-00 General Description 34-00-00 PITOT/STATIC SYSTEM – DESCRIPTION........34-11-00 Introduction 34-11-00 Description and Operation 34-11-00 PITOT/STATIC SYSTEM – MAINTENANCE ........34-11-00 General 34-11-00...
Page 502 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Effectivity INTEGRATED FLIGHT SYSTEM – MAINTENANCE .....34-25-00 Garmin G500 General 34-25-00 Garmin G500 Garmin G500 Removal/Installation 34-25-00 Garmin G500 Inspection/Check 34-25-00 Garmin G500 INTEGRATED FLIGHT SYSTEM – MAINTENANCE.....34-25-00...
Page 503: Navigation - General
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL NAVIGATION - GENERAL 1. Introduction This chapter describes units and components that provide aircraft navigational information. 2. General Description Different instruments and devices offer a means of determining flight conditions, aircraft attitude and position of the aircraft over the ground.
Page 504 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 505: Pitot/Static System - Description
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL PITOT/STATIC SYSTEM - DESCRIPTION 1. Introduction Depending on the aircraft configuration, the static and pitot pressure system supplies static and pitot pressure for the airspeed indicator, altimeter, vertical speed indicator and air data computer. 2. Description and Operation...
Page 506 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL NOTE: Equipment installed may vary depending on aircraft configuration. Air Data Computer airspeed indicator altimeter vertical speed Indicator pitot pressure water traps pitot-static tube static pressure Pitot-Static System Schematic Figure 1 Page 2 34-11-00 01.02.23...
Page 507: Pitot/Static System - Maintenance
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL PITOT/STATIC SYSTEM - MAINTENANCE 1. General CAUTION: NEVER BLOW COMPRESSED AIR THROUGH PITOT OR STATIC LINES TOWARD INSTRUMENTS AS THIS CAN CAUSE DAMAGE TO INSTRUMENTS. Proper maintenance of the pitot/static system is essential for proper altimeter, airspeed and vertical speed indications.
Page 508: P/S Heat Control Box Removal/Installation (Optional)
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 4. P/S Heat Control Box Removal/Installation (optional) CAUTION: NEVER OPERATE PITOT HEATING WITHOUT THE CONTROL BOX AS THIS CAN DESTROY THE PITOT TUBE. Remove the Control Box (1) Ensure electrical power to aircraft is OFF.
Page 509 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL NOTE: Example View! Equipment installed on instrument panel may vary depending on aircraft configuration. cable ties electrical connector Detail- P/S Heat Control Box Figure 202 Page 203 34-11-00 01.02.23...
Page 510 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 7. Inspection/Check After any component replacement or repair, the system should be checked for proper function and a leakage test should be performed. Pitot System Leak Test (1) Fasten surgical hose and sphygmomanometer bulb over pitot head.
Page 511: Stall Warning System - Description
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL STALL WARNING SYSTEM - DESCRIPTION 1. Introduction The aircraft is equipped in with a stall warning system. It signals an approaching stall to the pilot by an audible alarm in the cockpit. 2. Description and Operation The stall warning system consists of a mechanical transmitter, located in the leading edge of the left wing and a warning buzzer behind the instrument panel.
Page 512 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 513: Stall Warning System - Maintenance
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL STALL WARNING SYSTEM - MAINTENANCE 1. General Maintenance is limited to the removal/installation of system components. In wintry conditions, make sure that the system transmitter microplate is always clear of ice and snow. 2. Transmitter Removal/Installation Remove Transmitter (1) Ensure electrical power to aircraft is OFF.
Page 514 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL...
Page 515: Attitude And Direction - Maintenance
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL ATTITUDE AND DIRECTION - MAINTENANCE 1. General CAUTION: GYROS ARE DELICATE AND CAN NOT WITHSTAND THE SHOCK OF BEING DROPPED, JARRED OR STRUCK BY PIECES OF EQUIPMENT. DO NOT PLACE GYROS ON ANY HARD SURFACE. PAD WITH GENEROUS FOAM.
Page 516: Attitude Indicator Removal/Installation
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 4. Attitude Indicator Removal/Installation Remove Attitude Indicator (1) Ensure electrical power to aircraft is OFF. (2) Disconnect battery (refer to 24-30-00). (3) Remove glare shield (refer to 31-10-00). (4) Disconnect electrical connector from attitude indicator.
Page 517 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL (e) Run engine and set throttle at cruise position. NOTE: When performing maintenance on the magnetic compass, use a non-magnetic or plastic screwdriver. (2) Remove screws securing access plate to compass casing to reveal adjustment screws.
Page 518 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 519: Integrated Flight System - Maintenance
If fasteners are deformed in any way, they must be replaced. The operation of the Aspen EFD1000 requires the software version given in the AQUILA Service Information SI-AT01-012.
Page 520: Efd Battery Replacement
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL Install EFD (1) Verify electrical power to aircraft is OFF. (2) Install 44 pin D-sub connector and tighten jacks crews until connector is fully seated. (3) Install pitot and static lines (EFD1000 only) to back of EFD by firmly pressing the fitting until fully seated (pitot and static quick connectors are keyed and cannot be crossed).
Page 521: Configuration Module (Cm) Removal/Installation
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL NOTE: It is critical that the screws are non-ferrous to avoid compass errors. (5) Connect the circular electrical connector and cable tie harness to prevent chafing and interference. (6) Connect shield ground wire to ground stud.
Page 522 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 6. I nspection/Check All units, brackets, installation hardware and wiring of the EFD1000 system should be checked as defined below during annual inspection. Items found to be defective should be repaired or replaced prior to returning the aircraft to service. The performance of this inspection should not create the need for additional protective treatment (Alodine, paint, etc) of surfaces within the aircraft.
Page 523: Integrated Flight System - Maintenance
The actual software version is documented in the aircraft equipment list, located in chapter 6 of the airplane flight manual. All service information released from AQUILA and related to software versions has to be attached to this maintenance manual for continuing airworthiness! For bonding checks on the AQUILA AT01-100/200 no procedures or equipment are necessary other than that which are commonly expected for bonding measurements on small aircraft.
Page 524 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL GMU 44 unit support bracket Detail- GMU 44 magnetometer G500 System Components Figure 201 (1) EFFECTIVITY Page 202 Aircraft equipped with Garmin G500 34-25-00 01.02.23...
Page 525 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL GDC 74A unit support bracket Detail- attachment clamp Detail- GTP 59 (OAT sensor) GDC 74A (air data computer) AHRS unit Detail- support bracket GRS 77 (AHRS sensor) G500 System Components Figure 201 (2) EFFECTIVITY Page 203...
Page 526 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 3. Inspection/Check G500 s ystem LRUs are designed to detect internal failures. A thorough self-test is executed automatically upon application of power to the units, and built-in tests are continuously executed. Detected errors are indicated on the GDU 620 display via failure annunciations.
Page 527: Integrated Flight System - Maintenance
The actual software version is documented in the aircraft equipment list, located in chapter 6 of the airplane flight manual. All service information released from AQUILA and related to software versions has to be attached to this maintenance manual for continuing airworthiness! For bonding checks on the AQUILA AT01-100/200 no procedures or equipment are necessary other than that which are commonly expected for bonding measurements on small aircraft.
Page 528 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 3. Inspection/Check G500 TXi s ystem LRUs are designed to detect internal failures. A thorough self-test is executed automatically upon application of power to the units, and built-in tests are continuously executed. Detected errors are indicated on the GDU 1060 display via failure annunciations, system messages, or a combination of the two.
Page 529: Integrated Flight System - Maintenance
The actual software version is documented in the aircraft equipment list, located in chapter 6 of the airplane flight manual. All service information released from AQUILA and related to software versions has to be attached to this maintenance manual for continuing airworthiness! For bonding checks on the AQUILA AT01-100/200 no procedures or equipment are necessary other than that which are commonly expected for bonding measurements on small aircraft.
Page 530 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL after G3X removal, installation or replacement. For autopilot settings refer to SB-AT01-042 and referenced documents. 3. Inspection/Check G3X Touch EFIS LRUs maintenance is “on condition” only. No component-level overhaul is required the G3X Touch. “On Condition” replacement and/or servicing should occur when an item exhibits conditions, symptoms, and/or abnormalities defined in section 5 of the G3X Touch EFIS Part 23 AML STC Maintenance Manual.
Page 531: Integrated Flight System - Maintenance
The actual software version is documented in the aircraft equipment list, located in chapter 6 of the airplane flight manual. All service information released from AQUILA and related to software versions has to be attached to this maintenance manual for continuing airworthiness! For bonding checks on the AQUILA AT01-100/200 no procedures or equipment are necessary other than that which are commonly expected for bonding measurements on small aircraft.
Page 532 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 3. Inspection/Check G5 LRUs maintenance is “on condition” only. No component-level overhaul is required the G5. “On Condition” replacement and/or servicing should occur when an item exhibits conditions, symptoms, and/or abnormalities defined in section 5 of the Garmin G5 Electronic Flight Instrument Part 23 AML STC Maintenance Manual.
Page 533: Independent Position Determining - Maintenance
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL INDEPENDENT POSITION DETERMINING – MAINTENANCE 1. General This section covers that portion of the system which provides information to determine position and is mainly independent of ground installations. This includes the GPS portion of the GNS 430W or GTN 650 (Xi) navigation management system (NMS).
Page 534 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 535: Independent Position Determining - Maintenance
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL INDEPENDENT POSITION DETERMINING – MAINTENANCE General A. This section covers that portion of the system which provides information to determine position and is mainly independent of ground installations. This includes the FlymapL multifunctional display/GPS. B. The scope of maintenance is limited to the removal and installation of the components. For further information on the FlymapL, refer to the FlymapL Installation Manual, doc.
Page 536 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL unit attachment screws Note: Surrounding components and parts Detail- omitted for clarity FlymapL Unit Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with FlymapL 34-40-00 01.02.23...
Page 537 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL Install glare shield (refer to 31-10-00). Reconnect battery (refer to 24-30-00). Conduct a functional test of the installed unit. GPS Antenna Removal/Installation (Ref. Fig. 202) A. Remove FlymapL GPS Antenna Ensure electrical power to aircraft is OFF.
Page 538 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL cable ties adhesive tape GPS antenna Detail- FlymapL GPS Antenna Installation Figure 202 EFFECTIVITY Page 204 Aircraft equipped with FlymapL 34-40-00 01.02.23...
Page 539: Dependent Positioning Determining - Maintenance
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL DEPENDENT POSITIONING DETERMINING - MAINTENANCE 1. General This section covers that portion of the system which provides information to determine position and is mainly dependent on ground installations. This includes the VOR/ILS receiver portion of...
Page 540: Transponder Removal/Installation
AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 2. Transponder Removal/Installation Remove Garmin GTX Transponder (1) Ensure electrical power to aircraft is OFF. (2) Insert a 3/32 hex wrench into the access hole at the unit face and engage hex bolt. (3) Turn wrench counterclockwise until the unit is forced out about 3/8” and can be freely pulled from the rack.
Page 541 AQUILA AT01-100/200/300 Navigation MAINTENANCE MANUAL 4. Inspection/Check Maintenance of the GTX has to be carried out in accordance with: - GTX 328 Transponder Maintenance Manual, P/N 190-00420-05, latest revision - Garmin GTX 33X and GTX 3X5 ADS-B Maintenance Manual, P/N 190-00734-11, latest revision Garmin GTX transponder maintenance is “on condition”...
Page 542 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 543 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 51 STRUCTURES...
Page 544 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 545 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page STRUCTURES - GENERAL................51-00-00 Introduction 51-00-00 General Description 51-00-00 Structure Classes 51-00-00 COMPOSITE DAMAGE INVESTIGATION ..........51-10-00 General 51-10-00 Inspection Methods 51-10-00 Damage Classification 51-10-00 COMPOSITE REPAIR..................51-20-00 General 51-20-00...
Page 546 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 547: Structures - General
Please contact AQUILA Aviation GmbH for support in case damage to the aircraft structure the cause of which is unknown or suspect, and prior to major repairs to obtain detailed information.
Page 548 Secondary Structure These parts are not important for the structural integrity of the aircraft. For example: panels, covers, access plates, fairings. AQUILA AT01 Primary Structure Figure 01 Page 2 51-00-00 29.02.16...
Page 549: Composite Damage Investigation
AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL COMPOSITE DAMAGE INVESTIGATION 1. General This section contains maintenance information and procedures such as investigation and damage classification applicable to fiber laminate structure components. 2. Inspection Methods Visual Inspection Most damage to a composite structure will be visually detectable. A wide variety of component surface discontinuities such as scratches, cracks, dimples, dents and creases may indicate damage.
Page 550 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL 3. Damage Classification Damage to composite structures can be divided into four classes: (1) Damage Class 1 Severe, extensive damage that requires partial component restoration or general component replacement. (2) Damage Class 2 Damage to primary or secondary structures with sandwich penetration such as holes or fractures.
Page 551 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL roll-over bar strip around the canopy frame stabilizer root area wing root area wing root area wing root area wing spar area 1350 fuel tank 1000 4500 stabilizer root area stabilizer spar area Damages - Critical Areas...
Page 552 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 553: Composite Repair
AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL COMPOSITE REPAIR 1. General This section covers required information to complete successful repairs to aircraft components that are made from fiber laminate. Necessary repair data, such as ply lay-up and ply orientation for various areas, as well as repair materials and procedures are provided. Not included are general practices used during most composite repairs, such as cleaning and preparing the damaged area, proper preparation of materials, mixing and applying resin or proper curing the repair.
Page 554 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL (4) Solvents used in repair processes are composed of a group of chemicals that often prove toxic. To avoid toxic poisoning, work in a well-ventilated area only and always be alert for symptoms of poisoning. If symptoms are observed, it is vital to immediately remove the person from the contaminated area.
Page 555 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL 4. Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer 6.A. sandpaper commercially required 30-grit to available 400 grit isopropyl commercially required alcohol available peel ply commercially required available release film commercially required available hot glue...
Page 556 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL 2k epoxy primer LE2001 DuPont required activator XK206 thinner EV301 8.B. cotton cloth commercially required available isopropyl commercially required alcohol available coating PUR EV310 DuPont reqired activator PUR EV313 thinner PUR EV303 5. Material Data Sheet...
Page 557 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (1) Page 205 51-20-00 29.02.16...
Page 558 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (2) Page 206 51-20-00 29.02.16...
Page 559 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL Remarks Item No. Layers Description Interglas 92110 width 110 mm Interglas 92125 Interglas 92125 width 100 mm strip, overlap in winglet area Interglas 92125 Interglas 92125 Interglas 92125 up to aileron Interglas 92125 up to y=1030 mm...
Page 560 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL filler y=1450 1030 1900 3000 3600 Upper Wing Shell Ply Lay-Up Figure 203 (1) Page 208 51-20-00 29.02.16...
Page 561 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL 1750 4100 4500 2350 1350 1350 1000 Upper Wing Shell Ply Lay-Up Figure 203 (2) Page 209 51-20-00 29.02.16...
Page 562 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL 1450 1030 1030 3472 1900 3600 Lower Wing Shell Ply Lay-Up Figure 203 (3) Page 210 51-20-00 29.02.16...
Page 563 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL left side only left side only drainer fitting plate tie down point 2350 1750 4050 1350 2350 1350 1000 Lower Wing Shell Ply Lay-Up Figure 203 (4) Page 211 51-20-00 29.02.16...
Page 564 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL Remarks Item No. Layers Description Interglas 90070 overall Interglas 98140 overall Interglas 98140 width 400 mm (on fuselage side) CST 240/60 DH60-03 rigid foam Interglas 98140 overall Ply lay-up for upper / lower flap shell and LH / RH flap symmetrical.
Page 565 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL Remarks Item No. Layers Description Interglas 92110 overall CST 240/30 Interglas 92125 DH60-03 rigid foam Interglas 92110 Interglas 92110 overall Ply lay-up for upper / lower aileron shell and LH / RH aileron symmetrical. 1343...
Page 566 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL Remarks Item No. Layers Description Interglas 92110 overall Interglas 92110 Interglas 92125 Interglas 92125 CST 240/30 DH60-03 rigid foam Interglas 92110 Interglas 92110 overall Ply lay-up for upper / lower elevator shell and LH / RH elevator symmetrical.
Page 567 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL Remarks Item No. Layers Description Interglas 92110 overall CST 240/60 Interglas 92110 Interglas 92110 Interglas 92125 Interglas 92125 DH60-03 rigid foam Interglas 92110 Interglas 92125 Interglas 92110 overall Ply lay-up for LH / RH rudder shell symmetrical.
Page 568 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL applies to LH shell / applies to RH shell Rudder Shell Ply Lay-Up Figure 207 (2) Page 216 51-20-00 29.02.16...
Page 569 (5) Lay up repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. (6) Pre-cure the repair at least 24 hours at 20°C (68°F) to 25°C (77°F).
Page 570 (8) Lay up repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. (9) Pre-cure the repair at least 24 hours at 20°C (68°F) to 25°C (77°F).
Page 571 (9) Lay up repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. (10) Pre-cure the repair at least 24 hours at 20°C (68°F) to 25°C (77°F).
Page 572 (10) Lay up outer repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. (11) Pre-cure the repair at least 24 hours at 20°C (68°F) to 25°C (77°F).
Page 573 (13) Apply a thin coat of resin to the scarfed edges of the repair area. (14) Lay up outer repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. Page 221 51-20-00 29.02.16...
Page 574 (4) Lay up repair plies according to the existing layer direction (refer to “Material Data Sheet” above). If the layer orientation is not clear please contact AQUILA Aviation GmbH. (5) Pre-cure the repair at least 24 hours at 20°C (68°F) to 25°C (77°F).
Page 575 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL 8. Exterior Finish Prior painting over a repair, inspect the repair to ensure that it has hardened completely and has been properly contoured. CAUTION: MASK OFF SURFACE AROUND REPAIR AREA THAT DOES NOT REQUIRE FILLING OR PAINT, PAY SPECIAL ATTENTION TO STATIC PORTS, ANTENNAS AND DRAIN HOLES.
Page 576 AQUILA AT01-100/200/300 Structures MAINTENANCE MANUAL...
Page 577 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 52 DOORS...
Page 578 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 579 AQUILA AT01-100/200/300 Doors MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page DOORS - GENERAL..................52-00-00 Introduction 52-00-00 General Description 52-00-00 CANOPY - MAINTENANCE ................52-10-00 General 52-10-00 Canopy Removal/Installation 52-10-00 Canopy Latching Mechanism Maintenance 52-10-00 BAGGAGE DOOR - MAINTENANCE............52-30-00 General...
Page 580 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 581: Doors - General
AQUILA AT01-100/200/300 Doors MAINTENANCE MANUAL DOORS - GENERAL 1. Introduction This chapter describes the canopy and the baggage door. It includes items such as structure, latching mechanism and maintenance instructions. 2. General Description The canopy consists of a composite frame and a large one-piece acrylic glass window which are bonded together.
Page 582 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 583 AQUILA AT01-100/200/300 Doors MAINTENANCE MANUAL CANOPY - MAINTENANCE 1. General The canopy consists of a frame fabricated from carbon fiber laminate and rovings, and a large one- piece acrylic glass window which are bonded together. The window has two direct-vision panels, one on each side.
Page 584 AQUILA AT01-100/200/300 Doors MAINTENANCE MANUAL Detail- Canopy Latching Mechanism Figure 201 (1) Page 202 52-10-00 30.04.13...
Page 585 AQUILA AT01-100/200/300 Doors MAINTENANCE MANUAL Detail- receiver latching pin push-pull road inner handle spacer locking pin canopy lock spacer shaft actuation lever spacer outer handle Detail- Canopy Latching Mechanism Figure 201 (2) Page 203 52-10-00 30.04.13...
Page 586 AQUILA AT01-100/200/300 Doors MAINTENANCE MANUAL Install/Adjust Locking Pin (1) Remove screws securing the covering to the canopy and remove covering. (2) Clean thread of hole and locking pin with ethyl alcohol. (3) Thoroughly apply epoxy resin to the thread tapped inside the GRP plate of the cover.
Page 587 AQUILA AT01-100/200/300 Doors MAINTENANCE MANUAL BAGGAGE DOOR - MAINTENANCE 1. General The baggage door is made of glass fiber laminate. It is hinged on the forward edge via two GFRP hinge arms and latched on the rear edge. The door is locked from the outside with a key lock.
Page 588 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 589 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 53 FUSELAGE...
Page 590 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 591 AQUILA AT01-100/200/300 Fuselage MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page FUSELAGE - GENERAL ...................53-00-00 Introduction 53-00-00 General Description 53-00-00 FUSELAGE MAIN FRAME - DESCRIPTION ..........53-10-00 Description and Operation 53-10-00 FUSELAGE MAIN FRAME - MAINTENANCE ..........53-10-00 General 53-10-00 AUXILIARY STRUCTURE - DESCRIPTION..........53-20-00...
Page 592 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 593: Fuselage - General
AQUILA AT01-100/200/300 Fuselage MAINTENANCE MANUAL FUSELAGE - GENERAL 1. Introduction This chapter provides a description of the general fuselage structure. For systems and components installed in the fuselage structure, refer to the respective chapters in this manual. 2. General Description The fuselage is a semi-monocoque structure made primarily of composite materials.
Page 594 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 595: Fuselage Main Frame - Description
AQUILA AT01-100/200/300 Fuselage MAINTENANCE MANUAL FUSELAGE MAIN FRAME - DESCRIPTION 1. Description and Operation This section describes those structural components which make up the main frame including firewall, bulkheads and ring frames. Firewall The firewall separates the engine compartment from the rest of the fuselage and supports various aircraft components on both the forward and aft sides.
Page 596 AQUILA AT01-100/200/300 Fuselage MAINTENANCE MANUAL ring frames baggage compartment bulkhead carbon fiber stringers carbon fiber stringers landing gear bulkhead firewall seat bulkhead side force bulkhead Fuselage Structure Figure 201 (1) Page 2 53-10-00 30.04.13...
Page 597 AQUILA AT01-100/200/300 Fuselage MAINTENANCE MANUAL vertical stabilizer rear web vertical stabilizer main spar carbon fiber stringers (4x) tail end bulkhead vertical stabilizer ribs ring frames Fuselage Structure Figure 201 (2) Page 3 53-10-00 30.04.13...
Page 598 AQUILA AT01-100/200/300 Fuselage MAINTENANCE MANUAL Vertical Stabilizer Ribs The vertical stabilizer front and rear ribs are of rigid GFRP molding and bonded to the fuselage shells and to the vertical stabilizer main spar. The rear rib also bonds to the rear web.
Page 599: Fuselage Main Frame - Maintenance
Refer to chapter 51 for standard repair procedures and for repair data for the fuselage shells. If the damage area is inside the fuselage AQUILA Aviation GmbH must be contacted prior to beginning repair work.
Page 600 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 601: Auxiliary Structure - Description
AQUILA AT01-100/200/300 Fuselage MAINTENANCE MANUAL AUXILIARY STRUCTURE - DESCRIPTION 1. Description and Operation This section describes those structural components which make up the auxiliary structure including fuselage floor structure, center console, access panels and entry step. Fuselage Floor Structure The floor structure of the aircraft consists of a forward floor, a left and right baggage compartment floor, a left and right control stick cover and a left, right and center cover of the well of the landing gear.
Page 602 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 603 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 55 STABILIZERS...
Page 604 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 605 AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page STABILIZERS - GENERAL................55-00-00 Introduction 55-00-00 General Description 55-00-00 HORIZONTAL STABILIZER - MAINTENANCE.........55-10-00 General 55-10-00 ELEVATOR - MAINTENANCE ...............55-20-00 General 55-20-00 Elevator Removal/Installation 55-20-00 Adjustment - Elevator Balancing 55-20-00 VERTICAL STABILIZER - MAINTENANCE..........55-30-00...
Page 606 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 607: Stabilizers - General
AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL STABILIZERS - GENERAL 1. Introduction This chapter describes the horizontal and vertical stabilizers as well as the structure of the elevator and rudder. Maintenance information is provided. 2. General Description The empennage consists of a horizontal stabilizer, a two-piece elevator, a vertical fin and a rudder.
Page 608 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 609: Horizontal Stabilizer - Maintenance
AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL HORIZONTAL STABILIZER - MAINTENANCE 1. General The horizontal stabilizer is of a fully cantilever, semi-monocoque design. The structure, made of composite materials, consists of a front spar, a rear shear web, root ribs and top and bottom shells.
Page 610 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 611: Elevator - Maintenance
AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL ELEVATOR - MAINTENANCE 1. General The two-piece elevator is made from composite materials. Each half has a top and a bottom shell which are bonded together. The shells have a sandwich structure with a rigid foam core. The following are bonded between the shells: a horn rip at the outer end, two hinge brackets in the front area and a rib at the inboard end.
Page 612 AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL Elevator Balancing NOTE: Calculate the static control surface moment as follows: M = F x r [Nm] (1) Disconnect elevator assembly from elevator push-pull rod (refer to 27-30-00). (2) Weigh by means of a conventional spring balance at the given weighing point (refer to figure 201).
Page 613 AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL (b) Raise the spring balance slowly until the control surface begins to move. Note the reading and the direction of the movement (i.e. 11,2 N up). (c) Lower the spring balance slowly until the control surface begins to move down. Note the reading and the direction of the movement to (i.e.
Page 614 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 615: Vertical Stabilizer - Maintenance
AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL VERTICAL STABILIZER - MAINTENANCE 1. General The vertical stabilizer is an integral part of the fuselage structure and is made from composite laminate materials. No servicing is required. For more information on fuselage structure, refer to 53-10-00.
Page 616 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 617: Rudder - Maintenance
AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL RUDDER - MAINTENANCE 1. General The rudder is made from composite materials. The assembly consists primarily of the left and right shells which are bonded together. The shells have a sandwich structure with a rigid foam core.
Page 618 AQUILA AT01-100/200/300 Stabilizers MAINTENANCE MANUAL Rudder Balancing NOTE: Calculate the static control surface moment as follows: M = F x r [Nm] (1) Remove rudder from aircraft (refer to “Rudder Removal/Installation” above). (2) Use any suitable method to support the rudder horizontally at the pivot axis so it can rotate freely around the pivot axis.
Page 619 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 56 WINDOWS...
Page 620 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 621 AQUILA AT01-100/200/300 Windows MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page WINDOWS - GENERAL ..................56-00-00 Introduction 56-00-00 General Description 56-00-00 FLIGHT COMPARTMENT WINDOWS - MAINTENANCE......56-10-00 General 56-10-00 Tools, Equipment and Materials 56-10-00 Window Repair 56-10-00 Page 1 56 - TOC...
Page 622 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 623: General
AQUILA AT01-100/200/300 Windows MAINTENANCE MANUAL WINDOWS - GENERAL 1. Introduction This chapter describes the acrylic glass windows of the canopy and the fuselage. Refer to 52-10-00 for information on the canopy structure. Refer to 12-23-00 for information on cleaning and care of acrylic glass windows.
Page 624 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 625: Flight Compartment Windows - Maintenance
AQUILA AT01-100/200/300 Windows MAINTENANCE MANUAL FLIGHT COMPARTMENT WINDOWS - MAINTENANCE 1. General This section describes the repair of damaged acrylic glass windows. A properly carried out repair is essential to preserve the optical properties of acrylic glass windows. Personnel must be familiar with repair practices prior to attempting acrylic glass repairs on the aircraft.
Page 626 AQUILA AT01-100/200/300 Windows MAINTENANCE MANUAL Temporary Repairs (1) Stop-drill the ends of short cracks. Use a 2,5 mm (3/32 in.) drill. stop-drill 2.5 mm (3/32 in.) window crack (2) Repair the crack not later than the next 100-hour inspection. Permanent Repairs (1) Remove canopy (refer to 52-10-00).
Page 627 AQUILA AT01-100/200/300 Windows MAINTENANCE MANUAL (11) Cut a groove along the crack in the inner surface of the window. NOTE: This groove is less deep than the outer surface groove. It must cut into the outer layer of filler. This prevents holes in the filler.
Page 628 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 629 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 57 WINGS...
Page 630 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 631 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page WINGS - GENERAL..................57-00-00 Introduction 57-00-00 General Description 57-00-00 WINGS - MAINTENANCE ................57-00-00 General 57-00-00 Tools, Equipment and Material 57-00-00 Wings Removal/Installation 57-00-00 Wing Attachment Bolt Removal/Installation 57-00-00 CONTROL SURFACES - MAINTENANCE ..........57-50-00...
Page 632 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 633: Wings - General
AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL WINGS - GENERAL 1. Introduction This chapter describes the wing, flaps and aileron structures. It also provides maintenance information. 2. General Description The wings are made from composite materials which provide very smooth and seamless flight surfaces.
Page 634 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 635: Wings - Maintenance
2. Tools, Equipment and Material Quantity Equipment Parts No. Manufacturer 3.A./B. Wing stand AQUILA Aviation Int. GmbH 3.A./4.A Wing attachment AQUILA Aviation Int. GmbH bolt removal tool 3. Wing Removal/Installation CAUTION: AT LEAST SEVEN PERSONS ARE NEEDED FOR WING REMOVAL OR INSTALLATION.
Page 636 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL wing spar root ribs wing fuel tank Detail- Wing Structure Figure 201 Page 202 57-00-00 10.06.16...
Page 637 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL (9) Disconnect electrical wires at connector inside the spar tunnel. (10) Disconnect fuel lines (four places). (11) Identify and disconnect pitot and static lines at water traps. (12) Disconnect aileron front from aileron rear bellcrank (refer to 27-10-00).
Page 638 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL fillister-head screw 11,5 in.lb Bolt must be secured with safety wire! Safety wire should be anchored to the shown fillister-head screw. Note: The rear right location is shown. Wing Bolt Installation Figure 201 EFFECTIVITY Page 204...
Page 639 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL safety plate Use adjusting washers under bolt head to assure correct torque and position of bolt head to safety plate. 11,5 in.lb Note: The rear right location is shown. Wing Bolt Installation Figure 201 EFFECTIVITY...
Page 640 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL (9) Install elevator pushrod 1 (refer to 27-30-00) f rom inside the cabin (10) Re-fuel wing tanks. Check fuel lines and fittings inside the spar tunnel for signs of leakage. (11) Reconnect battery (refer to 24-30-00).
Page 641: Control Surfaces - Maintenance
AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL CONTROL SURFACES - MAINTENANCE 1. General The flap structure is shown in figure 201. The top and bottom shells have a sandwich structure with a rigid foam core. GFRP molded ribs are bonded between the shells. A flap hinge arm is bonded to each rib.
Page 642 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL Detail- Detail- Flap/Aileron Structure Figure 201 Page 202 57-50-00 10.06.16...
Page 643 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL Install Aileron (1) Put the aileron in position and secure with washer and castellated nut at inboard hinge. Secure castellated nut with cotter pin. (2) Connect aileron push-pull rod to aileron horn. (3) Check proper aileron control system operation.
Page 644 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL wing Detail- right flap Flap Installation Figure 202 Page 204 57-50-00 10.06.16...
Page 645 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL Detail- Aileron Installation Figure 203 Page 205 57-50-00 10.06.16...
Page 646 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL hinge center line weighing point r=21,1 cm (8.3 in.) Detail- hinge center line weighing point r=21,1 cm (8.3 in.) Detail- Flap / Aileron Balancing Figure 204 Page 206 57-50-00 10.06.16...
Page 647 AQUILA AT01-100/200/300 Wings MAINTENANCE MANUAL (a) Attach spring balance at weighing point. The initial position of the flaps for each measurement should be 35° down. (b) Raise the spring balance slowly until the control surface begins to move. Note the reading and the direction of the movement (i.e.
Page 648 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 649 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 61 PROPELLER...
Page 650 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 651 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity PROPELLER - GENERAL ................61-00-00 Introduction 61-00-00 General Description 61-00-00 PROPELLER - TROUBLESHOOTING ............61-00-00 General 61-00-00 Troubleshooting 61-00-00 PROPELLER ASSEMBLY - MAINTENANCE..........61-10-00 General 61-10-00 Tools, Equipment and Material...
Page 652 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 653: Propeller - General
AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL PROPELLER - GENERAL 1. Introduction This chapter describes the propeller. Maintenance information is provided. Revs given in this chapter are propeller speeds. 2. General Description The aircraft uses a MT-Propeller MTV-21-A/170-05 (Rotax 912S) or MTV-21-A/175-05 (Rotax 914F / Rotax 912iS) variable pitch, two blade wood-composite propeller.
Page 654 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 655: Propeller - Troubleshooting
AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL PROPELLER - TROUBLESHOOTING 1. General The following chart lists some of the more common troubles which may occur with the propeller, their probable causes and remedies. 2. Troubleshooting Chart Trouble Probable Cause Remedy Static rpm too low Propeller limits engine speed.
Page 656 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL 2. Troubleshooting Chart (Cont.) Trouble Probable Cause Remedy Surging rpm 1. Trapped air in propeller Move propeller control at least twice piston. before flying at about 1800 rpm with a drop of about 500 rpm.
Page 657 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL 2. Troubleshooting Chart (Cont.) Trouble Probable Cause Remedy power to remain about 100 rpm below take-off rpm. Note that propeller rpm should be always lower than adjusted with the propeller control. This will hold the governor in an underspeed...
Page 658 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 659: Propeller Assembly - Maintenance
AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL PROPELLER ASSEMBLY - MAINTENANCE 1. General The aircraft is equipped with a MT-Propeller MTV-21-A/170-05 (Rotax 912S) or MTV-21-A/175-05 (Rotax 914F / Rotax 912iS) variable pitch, two blade wood-composite propeller. For more detailed information on the installed propeller, refer to MT-Propeller E-124 operation and installation manual for hydraulically controlled variable pitch propeller, latest revision.
Page 660 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL Spinner The spinner dome is a one-piece part made from fiber reinforced composite. The bulkhead is truncated aluminum alloy. Filler plates increase the stiffness of the dome on the cutouts for the blades. The dome is mounted to the bulkhead by means of screws.
Page 661: Cleaning
AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL 5. Inspection/Check Inspection/Check (1) Remove screws securing spinner dome to spinner bulkhead and remove spinner. (2) Check spinner for cracks and other damage. (3) Perform a visual inspection of the propeller blades. (a) Check for critical cracks (refer to MT-Propeller E-124 operation and installation manual for hydraulically controlled variable pitch propeller) (b) Inspect for notches, dents, nicks or other damage.
Page 662 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL Trailing edge splitting can arise from a stone hit. If the split is not longer than 40 mm (1.5 in.), it can be glued with epoxy cement. If some wood is missing (not deeper than 8 mm [0.25 in.]), fill damaged area with epoxy, let it harden, grind surface smooth and cover with water-resistant varnish, preferably polyurethane.
Page 663: Propeller Control - Maintenance
AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL PROPELLER CONTROL - MAINTENANCE 1. General The aircraft is equipped with a constant speed propeller. A MT-Propeller P-850-12 governor controls the blade pitch. For more detailed information on the installed governor, refer to MT-Propeller E-1048 operation and installation manual for hydraulically constant speed governor P-8( )( )-( ), latest revision.
Page 664 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL gasket governor 20-24 Nm 180-220 in.lbs Governor Installation Figure 201 Page 202 61-20-00 31.05.24...
Page 665 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL (5) Adjust governor (refer to “Adjustment/Test” below). (6) Install upper engine cowling (refer to 71-10). (7) Carry out a functional test (refer to “Adjustment/Test” below). 5. Inspection/Check Perform the following inspections frequently and in particular after any maintenance on the propeller / governor: (1) Remove upper engine cowling (refer to 71-10).
Page 666 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL CAUTION: AFTER ADJUSTMENT THE STOP SCREW MUST OVERLAP THE STOP SCREW SUPPORT BY AT LEAST 2 MM (0.08 IN.). CAUTION: CHECK POSITION OF CONTROL SHAFT WITH CONTROL LEVER AT THE MAX. RPM STOP . ENSURE THAT THE SPLINES ARE NOT BEYOND THE GOVERNOR CASING, OTHERWISE THE O-RING COULD BE DAMAGED.
Page 667 AQUILA AT01-100/200/300 Propeller MAINTENANCE MANUAL (27) Perform a test-flight. At 130-140 kts with propeller and power levers full forward propeller speed should be max. 2385 rpm ( Rotax 912S / 914F ) / max. 2260 rpm ( Rotax 912iS ). Slowly move propeller lever forward.
Page 668 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 669: Power Plant
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 71 POWER PLANT...
Page 670 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 671 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity POWER PLANT - GENERAL ................71-00-01 Rotax 912S Introduction 71-00-01 Rotax 912S General Description 71-00-01 Rotax 912S POWER PLANT - GENERAL ................71-00-02 Rotax 912iS Introduction 71-00-02...
Page 672 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 673: Power Plant - General
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL POWER PLANT - GENERAL 1. Introduction This chapter provides maintenance information for the power plant and associated components. Engine-related information is limited to the most important specifications. For further, more detailed information, refer to applicable ROTAX Aircraft Engines publications.
Page 674 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL Components (1) Starter The starter is mounted at the rear lower right side of the engine. It is a direct drive 12 V DC motor. Starting a pinion gear in the starter engages the crankshaft ring gear and turns the engine over.
Page 675: Power Plant - General
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL POWER PLANT - GENERAL 1. Introduction This chapter provides maintenance information for the power plant and associated components. Engine-related information is limited to the most important specifications. For further, more detailed information, refer to applicable ROTAX Aircraft Engines publications.
Page 676 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL Components (1) Electric System This system is responsible for supplying the engine management system (EMS) and the airframe with electrical power. It consists of the fusebox with regulators and the internal generators. (2) Internal Generators A and B The two generators (generator A and generator B) are electrically isolated and mounted on one stator.
Page 677 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL Nonredundant sensors (e. g. oil pressure sensors) are connected to one Lane only and serve for the expanded monitoring of the engine functionality. Due to an ECU internal communication, these sensor values will be exchanged between the two Lanes (assuming that both Lanes are active and free of errors).
Page 678 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 679: Power Plant - General
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL POWER PLANT - GENERAL 1. Introduction This chapter provides maintenance information for the power plant and associated components. Engine-related information is limited to the most important specifications. For further, more detailed information, refer to applicable ROTAX Aircraft Engines publications.
Page 680 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL Components (1) Starter The starter is mounted at the rear lower right side of the engine. It is a direct drive 12 V DC motor. Starting a pinion gear in the starter engages the crankshaft ring gear and turns the engine over.
Page 681: Power Plant - Troubleshooting
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL POWER PLANT - TROUBLESHOOTING 1. General The following chart lists some of the more common engine troubles, which may be encountered during maintenance, their probable causes and remedies. 2. Troubleshooting Safety Precautions: (1) Before beginning troubleshooting on engine, ensure that a fire extinguisher is available.
Page 682 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL Leak in induction Tighten all connections system in induction system. Replace any parts that are defective. Incorrect idle adjustment Adjust throttle stop to obtain correct idle. Uneven cylinder Check condition of piston compression rings and valve seats.
Page 683 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL and corrosion. Check cables for damage, for ground contact and security. Failure of engine Leak in induction system Tighten all connections and to develop full power replace defective parts. Throttle lever out of Adjust throttle lever.
Page 684 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL High oil Insufficient air cooling Check oil cooler for condition, temperature deformation or obstruction. Insufficient oil supply Fill to proper level with specified oil. Low grade of oil Replace with oil conforming to specifications.
Page 685: Power Plant - Maintenance
(16) Remove wiring harness and bonding cables from engine. (17) Lift engine just enough to relief weight from engine mounts. (18) Remove nuts, washers, and bolts securing engine to AQUILA engine mount. (19) Remove engine from aircraft. Page 201 71-00-00 31.05.24...
Page 686 The marking must also be replaced. Refer also to SI-AT01-008 and SI-AT01-018, annex 11. (1) Hoist engine into alignment with AQUILA engine mount attach points. (2) Assemble engine shock mounts. (3) Install bolts, washers, and nuts connecting both engine mounts. Torque to 25 Nm (221 in.lbs).
Page 687: Engine Cleaning
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL 3. Engine Cleaning For engine cleaning procedures, refer to 12-23. 4. Engine Storage If the engine is being removed for storage purposes, it should be preserved. The engine operator's manual, section 8, contains information on preservation techniques.
Page 688 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 689: Cowling - Maintenance
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL COWLING - MAINTENANCE 1. General The engine cowling is made from laminated fiberglass / carbon fiber and comprises an upper and a lower half. The oil access door is located on the side of the upper cowling. An air intake and the induction air filter casing are to be found on the lower cowling.
Page 690 AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL Install Engine Cowling (1) Close canopy. (2) Rotate propeller to horizontal position. CAUTION: DO NOT ROTATE THE PROPELLER CLOCKWISE. (3) Put lower cowl in position and fasten to fuselage with Camloc quick-release fasteners. (4) Position end cover plate on bottom of lower cowl and secure with Camloc quick-release fasteners.
Page 691: Engine Mount - Maintenance
The vibration dampers isolate engine noise and vibration from the airframe. This section is applicable to the engine mount made by AQUILA Aviation. Maintenance not covered by this chapter is possible, if carried out according to AC 43.13-1B, September 8, 1998.
Page 692 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 693: Air Induction System - Maintenance
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL AIR INDUCTION SYSTEM - MAINTENANCE 1. General Induction air enters the carburetors via the air intake, the induction air filter, the airbox and flexible ducts. The air intake and the induction air filter casing are located on the left side of the lower cowling.
Page 694 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 695: Air Induction System - Maintenance
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL AIR INDUCTION SYSTEM - MAINTENANCE 1. General Induction air enters the engine airbox via the air intake, the induction air filter and flexible ducts. The air intake and the induction air filter casing are located on the left side of the lower cowling.
Page 696 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 697: Air Induction System - Maintenance
AQUILA AT01-100/200/300 Power Plant MAINTENANCE MANUAL AIR INDUCTION SYSTEM - MAINTENANCE 1. General The Rotax 914 engine is equipped with an exhaust gas turbocharger, making use of the energy in the exhaust gas for precompression of the intake air (boost pressure).
Page 698 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 699 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 74 IGNITION SYSTEM...
Page 700 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 701 AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity IGNITION SYSTEM - GENERAL ..............74-00-01 Rotax 912S/914F Introduction 74-00-01 Rotax 912S/914F General Description 74-00-01 Rotax 912S/914F IGNITION SYSTEM - GENERAL ..............74-00-02 Rotax 912iS Introduction 74-00-02...
Page 702 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 703: Ignition System - General
AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM - GENERAL 1. Introduction This chapter describes those units and components which generate, distribute and control an electrical current to ignite the fuel air mixture in the engine cylinders. 2. General Description The engine is equipped with a breakerless dual ignition system (DCDI - Dual Capacitor Discharge Ignition).
Page 704: Ignition System
AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM ignition circuit A ignition circuit B Ignition System Electrical Schematic Figure 1 EFFECTIVITY Page 2 Aircraft equipped with Rotax 912S / 914F engine 74-00-01 31.05.24...
Page 705: Ignition System - General
AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM - GENERAL 1. Introduction This chapter describes those units and components which generate, distribute and control an electrical current to ignite the fuel air mixture in the engine cylinders. 2. General Description The engine is equipped with 4 double ignition coils.
Page 706 AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL Ignition System Electrical Schematic Figure 1 EFFECTIVITY Page 2 Aircraft equipped with Rotax 912iS engine 74-00-02 31.05.24...
Page 707: Ignition System - Maintenance
AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM - MAINTENANCE 1. General Maintenance of the ignition system is limited to the removal and installation of components. Information on verification and renewal of spark plugs is also provided. For information beyond the scope of this section pertaining to the ignition system, refer to the...
Page 708: Spark Plug Removal/Installation
AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL (3) Install spark plug connectors to spark plugs. (4) Install clamps and cable ties securing ignition cables to engine. (5) Install battery (refer to 24-30). (6) Install engine cowling (refer to 71-10). 4. Spark Plug Removal/Installation Remove Spark Plug (1) Remove engine cowling (refer to 71-10).
Page 709 AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL NOTE: New spark plug type: Due to the curved gap between the center electrode and the ground electrodes, it is suggested to use a wire type feeler gauge for accurate gap measurement. Refer to Rotax SI-912-027 respectively SI-914-028.
Page 710 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 711: Inspection/Check
AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM - MAINTENANCE 1. General Maintenance of the ignition system is limited to the removal and installation of components. Information on verification and renewal of spark plugs is also provided. For information beyond the scope of this section pertaining to the ignition system, refer to the maintenance manual for ROTAX Engine Type 912 i Series.
Page 712 AQUILA AT01-100/200/300 Ignition System MAINTENANCE MANUAL (4) Inspect plug face appearance. Face appearance: Indicates the following: Light tan-colored to brown: Plug and calibration are correct. Velvet black: - Mixture too rich; - Insufficient air intake (clogged air filter); - Operating temperature too low;...
Page 713: Cooling System
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 75 COOLING SYSTEM...
Page 714 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 715 AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity COOLING SYSTEM - GENERAL ..............75-00-00 Introduction 75-00-00 General Description 75-00-00 COOLING SYSTEM - MAINTENANCE ............75-00-00 General 75-00-00 Radiator Removal/Installation 75-00-00 Overflow Bottle Removal/Installation 75-00-00 Expansion Tank Removal/Installation...
Page 716 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 717: Cooling System - General
AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL COOLING SYSTEM - GENERAL 1. Introduction This chapter covers those units and components which are used for liquid cooling of the cylinder heads and are not part of the engine. For additional information on the internal engine cooling system components, refer to the respective engine manufacturer’s publications.
Page 718 AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL e coolant flow is forced by a camshaft driven water pump from the radiator to the cylinder heads. The coolant passes from the top of the cylinder heads on to the expansion tank. Since the radiator is installed below engine level, the expansion tank located on top of the engine allows for coolant expansion.
Page 719: Cooling System - Maintenance
AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL COOLING SYSTEM - MAINTENANCE 1. General WARNING: NEVER OPEN RADIATOR, EXPANSION TANK OR OVERFLOW BOTTLE CAP WHEN THE COOLING SYSTEM IS STILL HOT! FOR REASONS OF SAFETY, COVER CAP WITH A CLOTH AND OPEN SLOWLY. SUDDEN OPENING OF THE CAP WOULD PROVOKE EXIT OF BOILING COOLANT AND RESULT IN SEVERE SCALDS.
Page 720: Expansion Tank Removal/Installation
AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL Install Overflow Bottle (1) Place overflow bottle on bracket. Ensure the correct position of the protection rubbers. (2) Secure overflow bottle to bracket with clamps. (3) Connect hose at overflow bottle. (4) Replenish engine coolant as required (refer to 12-14).
Page 721 AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL Detail- overflow bottle with cap expansion tank with cap Detail- Detail- radiator EFFECTIVITY Page 203 Aircraft equipped with Rotax 912S engine 75-00-00 31.05.24...
Page 722 AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL Detail- overflow bottle with cap expansion tank with cap Detail- Detail- radiator EFFECTIVITY Page 203 Aircraft equipped with Rotax 914F engine 75-00-00 31.05.24...
Page 723 AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL Detail- overflow bottle with cap expansion tank with cap Detail- Detail- radiator EFFECTIVITY Page 203 Aircraft equipped with Rotax 912iS engine 75-00-00 31.05.24...
Page 724 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 725: Winterization Kit - Maintenance
AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL WINTERIZATION KIT - MAINTENANCE 1. General Optional winter kits are supplied for use in cold weather operations. The kits include a special air inlet cover with fasteners, a placard and the appropriate airplane flight manual supplement. The cover should be fitted in front of the oil and coolant radiators as shown in figure 201.
Page 726: Air Inlet Cover Removal/Installation
AQUILA AT01-100/200/300 Cooling System MAINTENANCE MANUAL 2. Air Inlet Cover Removal/Installation Install air inlet cover as shown in figure 201. 3. Inspection/Check Perform the following checks if the air inlet cover is installed. (1) Verify the cover is fastened correctly (both quick release fasteners are closed).
Page 727: Engine Controls
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 76 ENGINE CONTROLS...
Page 728 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 729 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectifity ENGINE CONTROLS - GENERAL ............76-00-01 Rotax 912S / 914F Introduction 76-00-01 Rotax 912S / 914F General Description 76-00-01 Rotax 912S / 914F ENGINE CONTROLS - GENERAL ............76-00-02...
Page 730 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 731: Engine Controls - General
AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL ENGINE CONTROLS - GENERAL 1. Introduction This chapter describes and provides maintenance instructions for components and systems used to control the engine. 2. General Description Engine controls include throttle, choke, propeller and carburetor heat / alternate air. The primary engine controls, the throttle and propeller controls, employ conventional push-pull type levers and are connected to a control quadrant mounted on the center console.
Page 732 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL Turbo Control Unit (TCU) The wastegate is controlled by the TCU and actuated by an electric servo motor via a bowden cable. It regulates the speed of the turbocharger and consequently the boost pressure. The position of the wastegate is determined from the following sensors: throttle position, airbox pressure, ambient pressure, wastegate position, rev counter and airbox temperature.
Page 733: Engine Controls - General
AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL ENGINE CONTROLS - GENERAL 1. Introduction This chapter describes and provides maintenance instructions for components and systems used to control the engine. For additional information on engine system components, refer to the respective engine manufacturer’s publications.
Page 734 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL A huge quantity of sensors (e. g. sensors for measuring the pressure in the airbox) and actuators (e. g. ignition coils) of the engine are designed with redundancy. In this case, each of the sensors or actuators is connected to a Lane, so that the two Lanes have the same measurement values and send the same output signals.
Page 735: Engine Controls - Maintenance
AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL ENGINE CONTROLS - MAINTENANCE 1. General For propeller speed control adjustment/test procedures, refer to 61-20. For carburetor heat / alternate air control adjustment/test procedures, refer to 71-60. 2. Control Quadrant Disassembly/Assembly For control quadrant disassembly/assembly, refer to figure 201.
Page 736 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL Rotax 912iS: Only the left throttle control cable is installed. rear stop adjusting bolts Detail- Control Quadrant Assembly Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 912S / 912iS engine 76-00-00 31.05.24...
Page 737 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL max. cont. power detent adjusting nut Detail- rear stop adjusting bolts Control Quadrant Assembly Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 914F engine 76-00-00 31.05.24...
Page 738: Governor Control Cable Removal/Installation
AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL 4. Governor Control Cable Removal/Installation Remove Governor Control Cable (1) Remove engine cowling (refer to 71-10). (2) Remove access panels 211 FT, 211 FB, 211 EC (refer to 25-12) in the cabin. (3) Disconnect governor control cable from governor control arm.
Page 739 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL Detail- Detail- Choke Control Assembly Figure 202 EFFECTIVITY Page 204 Aircraft equipped with Rotax 912S / 914F engine 76-00-00 31.05.24...
Page 740: Throttle Control Adjustment/Test
AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL 6. Throttle Control Adjustment/Test Idle Speed Adjustment (Rotax 912S / 914F only) NOTE: Always perform idle speed adjustment at operating temperature of the engine. (1) Close idle mixture control screw by turning clockwise. (2) Open idle mixture control screw again 1.5 turns counterclockwise.
Page 741 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL (8) Loosen nut that clamps lever with detent for max. continuous power (refer to figure 201 above). Adjust detent for max. continuous power to 100% (max. 103%) throttle position via communication program and tighten clamp nut.
Page 742 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL Install Turbo Control Unit (TCU) (1) Put TCU in position on lower left side of instrument panel and secure using 4 nuts. (2) Reconnect electrical connector to TCU. (3) Reconnect battery (refer to 24-30).
Page 743 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL Install/Adjust Wastegate Control Cable NOTE: When installing the wastegate control cable, ensure the cable is routed exactly as previously installed. Grease control cable wire with engine oil prior to installation. (1) Put throttle lever into idle position.
Page 744 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL Remove Engine Control Unit (ECU) NOTE: The wire connectors of the ECU must not be opened and closed more than 20 times! This must be shown on the device by a clearly visible label with a printed numerical sequence (1-20) and by documentation conforming to selfmonitoring guidelines.
Page 745 AQUILA AT01-100/200/300 Engine Controls MAINTENANCE MANUAL Install Fuse Box NOTE: Ensure the regulator connector brackets are installed on the fuse box prior to installation. Refer to Rotax Aircraft Engines Service Instruction SI-PAC-011 for further information. NOTE: Ensure the optional heat sink set is installed on regulator B of the fuse box prior to installation.
Page 746 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 747: Engine Indicating
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 77 ENGINE INDICATING...
Page 748 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 749 AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity ENGINE INDICATING - GENERAL..............77-00-00 Introduction 77-00-00 General Description 77-00-00 POWER INDICATION - MAINTENANCE...........77-10-01 Analog General 77-10-01 Analog Tachometer Removal/Installation 77-10-01 Analog Manifold Pressure Gauge Removal/Installation...
Page 750 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 751: Engine Indicating - General
AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL ENGINE INDICATING - GENERAL 1. Introduction This chapter describes those systems and components which indicate engine operation. Refer to 28-00 for further information on fuel pressure, fuel quantity and fuel flow measuring systems. Refer to 79-00 for further information on oil pressure and oil temperature measuring systems.
Page 752 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 753: Power Indication - Maintenance
AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL POWER INDICATION - MAINTENANCE 1. General Propeller speed is indicated by a tachometer which is mounted on the instrument panel. The tachometer receives an electrical signal from a sensor mounted on the internal alternator casing at the rear end of the engine.
Page 754 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 755: Power Indication - Maintenance
AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL POWER INDICATION - MAINTENANCE 1. General Propeller / engine speed is indicated via the Garmin G3X Touch system. Rotax 912iS: Engine speed measurement is included in the engine management system (EMS). Rotax 912S / 914F: Propeller / engine speed is measured by a sensor mounted on the internal alternator casing at the rear end of the engine.
Page 756 AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL (3) Rotax 912S/914F: Install sensor to manifold block at the back of the instrument panel (Rotax 912S) / on the right side of the intercooler (Rotax 914F). Torque two full turns past hand tight.
Page 757: Power Indication - Maintenance
If the manifold pressure sensor is replaced, the new calibration offset for the new sensor will need to be stored in the MVP-50. This offset is noted on the yellow sticker on its side, and in the paper in the box it came in. Contact AQUILA Aviation for the password required. 2. Manifold Pressure Sensor Removal/Installation Remove Manifold Pressure Sensor (1) Ensure electrical power to aircraft is OFF.
Page 758 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 759: Temperature Indication - Maintenance
AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL TEMPERATURE INDICATION - MAINTENANCE 1. General Cylinder head temperature is measured by a temperature-sensitive sensor that is mounted in the no. 3 cylinder head. The indicator is located in the cluster of engine gauges on the right side of the instrument panel.
Page 760 AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL (4) Connect electrical connector to sensor. (5) Reconnect battery (refer to 24-30). (6) Install engine cowling (refer to 71-10). 4. Carburetor Temperature Sensor Removal/Installation (optional) Remove Carburetor Temperature Sensor (1) Ensure electrical power to aircraft is OFF.
Page 761: Temperature Indication - Maintenance
AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL TEMPERATURE INDICATION - MAINTENANCE 1. General Cylinder head temperature (CHT) / coolant temperature indication is included in the MVP-50 engine monitoring system / G3X Touch system. Temperature is measured by a temperature- sensitive sensor electrically connected to the engine data converter (MVP-50) / GEA 24 engine interface (G3X).
Page 762: Cht / Coolant Temperature Sensor Removal/Installation
AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL 2. CHT / Coolant Temperature Sensor Removal/Installation Remove CHT / Coolant Temperature Sensor (1) Ensure electrical power to aircraft is OFF. (2) Remove engine cowling (refer to 71-10). (3) Disconnect battery (refer to 24-30).
Page 763 AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL 4. Exhaust Gas Temperature Sensor Removal/Installation (optional) Remove Exhaust Gas Temperature Sensor (1) Ensure electrical power to aircraft is OFF. (2) Remove engine cowling (refer to 71-10). (3) Disconnect battery (refer to 24-30). (4) Disconnect electrical lead to sensor.
Page 764 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 765: Engine Monitoring System - Maintenance
AQUILA AT01-100/200/300 Engine Indicating MAINTENANCE MANUAL ENGINE MONITORING SYSTEM - MAINTENANCE 1. General The aircraft is equipped with an Electronics International MVP-50 glass panel engine monitor. The system consists of four major components: - the MVP display, - the EDC-33 engine data converter, - the probes and sensors and - the wiring and extension cables.
Page 766: Engine Data Converter (Edc) Removal/Installation
Engine Indicating MAINTENANCE MANUAL AQUILA Aviation or Electronics International support will provide the necessary level 2 password to allow this process. The unit and tracking IDs are needed for password generation. The engine hours and tach time can be restored to the new MVP-50 display using the maintenance password.
Page 767 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 78 EXHAUST...
Page 768 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 769 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity EXHAUST SYSTEM - GENERAL ..............78-00-00 Introduction 78-00-00 General Description 78-00-00 EXHAUST SYSTEM - MAINTENANCE ............78-00-01 Rotax 912S/iS General 78-00-01 Rotax 912S/iS Exhaust System Removal/Installation 78-00-01 Rotax 912S/iS...
Page 770 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 771 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL EXHAUST SYSTEM - GENERAL 1. Introduction This chapter describes such systems and components which direct the engine exhaust gases out of the engine compartment. 2. General Description The exhaust system comprises four exhaust bends, a main muffler, a rear muffler, a tail pipe and an exhaust-driven turbocharger (aircrraft equipped with Rotax 914F engine only).
Page 772 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 773: Exhaust System - Maintenance
AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL EXHAUST SYSTEM - MAINTENANCE 1. General Each engine cylinder has an exhaust bend leading down to the main muffler that is located beneath the engine. The exhaust bends and a tail pipe with rear muffler are connected to the main muffler over ball joints.
Page 774 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL (6) Install lower engine cowling and set up the exhaust system to ensure sufficient clearance from adjacent assemblies and the cowling. Torque nuts on cylinders to 15 Nm (133 in.lbs). Remove lower engine cowling again.
Page 775 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL exhaust bend RH rear exhaust bend LH rear Detail- exhaust bend RH front main muffler exhaust bend LH front Main Muffler Installation Figure 201 EFFECTIVITY Page 203 Aircraft equipped with Rotax 912S / 912iS engine 78-00-01 31.05.24...
Page 776 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL support bracket Detail- Detail- heat shroud tail pipe main muffler Detail- Heat Shroud / Tail Pipe Installation Figure 202 EFFECTIVITY Page 204 Aircraft equipped with Rotax 912S / 912iS engine 78-00-01 31.05.24...
Page 777 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL EXHAUST SYSTEM - MAINTENANCE 1. General Exhaust gases are routed from the engine cylinders via exhaust bends and exhaust manifold to the exhaust turbocharger and from there to the main muffler and the tail pipe with rear muffler.
Page 778 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL 3. Tail Pipe Removal/Installation Remove Tail Pipe (1) Remove engine cowling (refer to 71-10). (2) While supporting the tail pipe, remove screws, washers, nuts, cotter pins and springs securing tail pipe to exhaust bend on main muffler.
Page 779 AQUILA AT01-100/200/300 Exhaust MAINTENANCE MANUAL heat shroud Detail- support main muffler bracket Detail- Detail- tail pipe exhaust bend Heat Shroud / Tail Pipe Installation Figure 201 EFFECTIVITY Page 203 Aircraft equipped with Rotax 914F engine 78-00-02 31.05.24...
Page 780 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 781 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 79...
Page 782 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 783 AQUILA AT01-100/200/300 MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity OIL - GENERAL ....................79-00-01 Rotax 912S/iS Introduction 79-00-01 Rotax 912S/iS General Description 79-00-01 Rotax 912S/iS OIL - GENERAL ....................79-00-02 Rotax 914F Introduction 79-00-02 Rotax 914F General Description...
Page 784 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 785: Oil - General
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL - GENERAL 1. Introduction This chapter covers those units and components which are not part of the engine but store and/or supply lubricating oil to/from the engine or indicate oil condition. For additional information on the internal engine oil system components, refer to the respective engine manufacturer’s publications.
Page 786 AQUILA AT01-100/200/300 MAINTENANCE MANUAL Oil Circuit The oil pump sucks the engine oil from the oil tank via the oil cooler and forces it through the oil filter to the points of lubrication in the engine. Surplus oil emerging from the points of lubrication accumulates on the bottom of the crankcase and is forced back to the oil tank by the blow-by gases.
Page 787: Oil - General
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL - GENERAL 1. Introduction This chapter covers those units and components which are not part of the engine but store and/or supply lubricating oil to/from the engine or indicate oil condition. For additional information on the internal engine oil system components, refer to the respective engine manufacturer’s publications.
Page 788 AQUILA AT01-100/200/300 MAINTENANCE MANUAL Oil Circuit The oil pump sucks the engine oil from the oil tank via the oil cooler and forces it through the oil filter to the points of lubrication in the engine. Surplus oil emerging from the points of lubrication accumulates on the bottom of the crankcase and is forced back to the oil tank by the blow-by gases.
Page 789: Oil Tank - Maintenance
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL TANK - MAINTENANCE 1. General The oil tank is attached to the engine mount. It can be removed and disassembled (figure 201) for maintenance. The oil tank must be removed, disassembled and cleaned when oil contamination is detected.
Page 790 AQUILA AT01-100/200/300 MAINTENANCE MANUAL clamp oil tank cover O-ring baffle insert partition sealing ring drain screw Oil Tank Disassembly Figure 201 Page 202 79-10-00 31.05.24...
Page 791: Oil Cooler - Maintenance
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL COOLER - MAINTENANCE 1. General The oil cooler is mounted in front of the radiator on the inner forward part of the lower engine cowling behind the main air intake (Rotax 912S/iS) or in the lower rear part of the lower engine cowling below / behind the exhaust muffler and behind an air duct (Rotax 914F).
Page 792 AQUILA AT01-100/200/300 MAINTENANCE MANUAL Detail- rubbing heat protection sleeve protection from/to engine mounting bracket Detail- oil cooler Oil Cooler Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 912S engine 79-20-00 31.05.24...
Page 793 AQUILA AT01-100/200/300 MAINTENANCE MANUAL Detail- Detail- Oil Cooler Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 914F engine 79-20-00 31.05.24...
Page 794 AQUILA AT01-100/200/300 MAINTENANCE MANUAL Detail- from/to engine heat protection sleeve rubbing protection mounting bracket Detail- oil cooler Oil Cooler Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 912iS engine 79-20-00 31.05.24...
Page 795: Oil Pressure Indication - Maintenance
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL PRESSURE INDICATION - MAINTENANCE 1. General The oil pressure indicating system consists of an oil pressure sensor, an oil pressure indicator and wiring connecting the two components. On aircraft equipped with Garmin G3X Touch system, oil pressure is indicated via the G3X displays.
Page 796 AQUILA AT01-100/200/300 MAINTENANCE MANUAL Install Oil Pressure Sensor (1) Clean sensor thread. (2) Lubricate sensor thread with Loctite 243. Rotax 912S / 914F: Do not use Loctite 243 if oil pump housing is not dry. Use a suitable new gasket ring instead.
Page 797: Oil Pressure Indication - Maintenance
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL PRESSURE INDICATION - MAINTENANCE 1. General Engine oil pressure indication is included in the engine monitoring system. Pressure is measured by a pressure sensor electrically connected to the engine data converter (EDC). Maintenance is limited to the removal and installation of the oil pressure sensor. Refer to 77-40 for further information on maintenance of the engine monitoring system.
Page 798 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 799: Oil Temperature Indication - Maintenance
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL TEMPERATURE INDICATION - MAINTENANCE 1. General The oil temperature indicating system consists of a temperature sensor, an oil temperature indicator and wiring connecting the two components. On aircraft equipped with Garmin G3X Touch system, oil temperature is indicated via the G3X displays. The oil temperature sensor is then connected with the GEA 24 engine interface.
Page 800 AQUILA AT01-100/200/300 MAINTENANCE MANUAL Install Oil Temperature Sensor (1) Clean sensor thread. (2) Lubricate sensor thread with Loctite 243. Rotax 912S / 914F: Do not use Loctite 243 if oil pump housing is not dry. Use a suitable new gasket ring instead.
Page 801: Oil Temperature Indication - Maintenance
AQUILA AT01-100/200/300 MAINTENANCE MANUAL OIL TEMPERATURE INDICATION - MAINTENANCE 1. General Engine oil temperature indication is included in the engine monitoring system. Temperature is measured by a type K thermocouple electrically connected to the engine data converter (EDC). Maintenance is limited to the removal and installation of the oil temperature sensor. Refer to 77-40 for further information on maintenance of the engine monitoring system.
Page 802 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 803 AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 80 STARTING...
Page 804 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 805 AQUILA AT01-100/200/300 Starting MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity STARTING - GENERAL..................80-00-00 Introduction 80-00-00 General Description 80-00-00 STARTER - MAINTENANCE................80-10-01 Rotax 912S/914F General 80-10-01 Rotax 912S/914F Starter Removal/Installation 80-10-01 Rotax 912S/914F Starter Relay Removal/Installation 80-10-01 Rotax 912S/914F STARTER - MAINTENANCE................80-10-02...
Page 806 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 807: Starting - General
AQUILA AT01-100/200/300 Starting MAINTENANCE MANUAL STARTING - GENERAL 1. Introduction This chapter describes the starter as a component of the starting system. 2. General Description The starting system comprises the starter, a relay and the ignition/starter switch. The starter is mounted at the rear lower right side of the engine. During the engine starting process, the starter pinion gear drives the crankshaft through a freewheel ring gear and turns the engine over.
Page 808 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 809 AQUILA AT01-100/200/300 Starting MAINTENANCE MANUAL STARTER - MAINTENANCE 1. General The aircraft is equipped with a direct-drive 12V DC starter. The starter is mounted at the rear lower right side of the engine. During starting, a starter relay is activated by the ignition key. Its contacts close and electrical current energizes the starter motor.
Page 810 AQUILA AT01-100/200/300 Starting MAINTENANCE MANUAL 10 Nm 89 in.lbs electric contact to aircraft ground: surface of engine mount below toothed washer Detail- metallically bright (remove paint) Starter Relay Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 912S / 914F engine 80-10-01 31.05.24...
Page 811 AQUILA AT01-100/200/300 Starting MAINTENANCE MANUAL STARTER - MAINTENANCE 1. General The aircraft is equipped with a direct-drive 12V DC starter. The starter is mounted at the rear lower right side of the engine. During starting, a starter relay is activated by the ignition key. Its contacts close and electrical current energizes the starter motor.
Page 812 AQUILA AT01-100/200/300 Starting MAINTENANCE MANUAL 10 Nm 89 in.lbs no electric contact to aircraft ground: Detail- insulating washers above / below engine mount and heat shrink tubing around the screw Starter Relay Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 912iS engine 80-10-02 31.05.24...
Page 813: Charts And Diagrams
AQUILA AT01-100/200/300 MAINTENANCE MANUAL CHAPTER 91 CHARTS AND DIAGRAMS...
Page 814 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 815 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity CHARTS AND DIAGRAMS - GENERAL ............91-00-00 Introduction 91-00-00 Electrical Symbols 91-00-00 Wiring Diagrams 91-00-00 Wire Routing Diagrams 91-00-00 Antenna Overview 91-00-00 Page 1 91 - TOC...
Page 816 AQUILA AT01-100/200/300 MAINTENANCE MANUAL...
Page 817 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL CHARTS AND WIRING DIAGRAMS - GENERAL 1. Introduction This chapter includes several wiring diagrams for reference purposes. 2. Electrical Symbols Below a collection of electrical symbols used in the wiring diagrams: connector, single pole,...
Page 818 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL 3. Wiring Diagrams The wiring diagrams listed below define the wiring of the basic electrical equipment. No. Wiring diagram Ref. Fig. Effectivity Ignition System and Fuel Pump Fig. 1 (2) Battery, External Alternator and Starter Fig.
Page 819 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL S I2 DEV582 LINE P724 7021AR18s-wh 7021AL18s-wh LOAD ignition switch 8050B16 GND M1a 7021BL18s-wh P1071 8050C16N GND M4 P1540 P1538 DEV664 brown brown violet DEV663 violet DEV662 7020D20 see: Battery, External Alternator and Starter...
Page 820 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL ALT 1 see: Ammeter battery relay starter relay battery Battery, External Alternator and Starter Figure 2 (1) Page 4 91-00-00 24.10.13...
Page 821 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL ALT 1 Starter Excitation Relay ground power auxiliary relay see: Warning Lights see: Warning Lights see: External Power see: External Power see: Ignition System and Fuel Pump see: Ignition System and Fuel Pump...
Page 822 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL LINE ALT 2 25 A LOAD 8213E12 8213A20 C M1 P1512 8213F12N X M1 8213G12-ye DEV667 8213H12-ye Internal Alternator Figure 3 EFFECTIVITY Page 6 Aircraft equipped for Night-VFR 91-00-00 24.10.13...
Page 823 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL GND M1b P1563 8212E20 P1564 J M1 P1595 P1566 P1569 P1596 8212B04 8212A04 see: Battery, External Alternator and Starter P1597 P1598 DEV674 P1594 P1567 P1568 ENABLE 8212A20 8212D20 RL M3 ground power relay...
Page 824 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Warning Lights voltage monitoring module ground terminals Voltage Monitoring Figure 5 EFFECTIVITY Page 8 Aircraft equipped for Night-VFR 91-00-00 24.10.13...
Page 825 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL P1018 P1020 fuel sensor LH fuel sensor RH Fuel Indicating System Figure 6 Page 9 91-00-00 24.10.13...
Page 826 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Warning Lights Circuit breaker ratings that are not shown depend on the configuration. Refer to the wiring diagram of the particular option. Stall Warning Trim Control Attitude Indicator Trim Actuator Turn Coordinator Flap Control...
Page 827 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Circuit Breakers and Switches Figure 7 (2) Page 11 91-00-00 24.10.13...
Page 828 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL X I1 P938 P939 ammeter TB I3 P1497 P1505 Ammeter Figure 8 EFFECTIVITY Page 12 Aircraft equipped with analog engine instruments 91-00-00 24.10.13...
Page 829 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL P1611 MVP-0000-or P1612 MVP-0000-br Ammeter Figure 9 EFFECTIVITY Page 13 Aircraft equipped with MVP-50 91-00-00 24.10.13...
Page 830 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL LINE Warning Lights LOAD 7030B20 7030C20 7030D20 7030E20 ALT 1 ALT 2 VOLT P/S HEAT FUEL L I1 L I2 L I3 L I4 L I5 Warning Lights Figure 10 EFFECTIVITY Page 14...
Page 831 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL LINE Warning Lights LOAD annunciator panel FUEL TEST ALT 1 ALT 2 VOLT PRESS (red) (amber) HEAT P1714 TB I4 TB I1 P1706 8260e22 * The warning light FUEL PRESS is not used if an MVP-50 is installed.
Page 832 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Dome Light cabin light NAV light LH Lights Figure 12 (1) Page 16 91-00-00 24.10.13...
Page 833 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL landing light NAV light RH Lights Figure 12 (2) Page 17 91-00-00 24.10.13...
Page 834 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Instruments 1 CHT (OAT) Oil temperature Engine Indicating Figure 13 (1) EFFECTIVITY Page 18 Aircraft equipped with analog engine instruments 91-00-00 24.10.13...
Page 835 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Instruments 2 Fuel Gauge Oil pressure Left Right see: Fuel Indicating System Engine Indicating Figure 13 (2) EFFECTIVITY Page 19 Aircraft equipped with analog engine instruments 91-00-00 24.10.13...
Page 836 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL LINE Panel Light dimmer IC 101 LOAD SP826 SP823 J585 P1732 9341Ba22 9341Ba22N TB I1 P1723 P 101 dimmer P1740 9341Bg22N 9341Bg22 P1739 P1733 J586 DEV708 P1742 9341Bf22N 9341Bf22 DEV709 P1741 Instrument Lighting...
Page 837 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL LINE Stall Warning LOAD warning buzzer J575 P1418 9410A20 9410B20-rd 9410C20-bk 9410D20 9410D20N TB I1 P1426 S F1 stall warning P1434 P1435 Stall Warning System Figure 15 Page 21 91-00-00 24.10.13...
Page 838 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL rear fuselage end switch spindle drive trim motor Elevator Trim System Figure 16 (1) Page 22 91-00-00 24.10.13...
Page 839 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL instrument panel Trim Control Trim Actuator center console trim indicator trim switch Elevator Trim System Figure 16 (2) Page 23 91-00-00 24.10.13...
Page 840 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Flap Flap Control Actuator Cruise Takeoff Landing Flap Control System Figure 17 (1) Page 24 91-00-00 24.10.13...
Page 841 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL LED takeoff position LED cruise position Cruise Takeoff Landing LED landing position Flap Control System Figure 17 (2) Page 25 91-00-00 24.10.13...
Page 842 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL heated pitot-static tube Pitot Heating System Figure 18 (1) EFFECTIVITY Page 26 Aircraft equipped with pitot heating system 91-00-00 24.10.13...
Page 843 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Relay NO Relay C Heater 1 Heater 2 control box for heated pitot-static tube Pitot Heating System Figure 18 (2) EFFECTIVITY Page 27 Aircraft equipped with pitot heating system 91-00-00 24.10.13...
Page 844 AQUILA AT01-100/200/300 Charts and Diagrams Charts and Diagrams MAINTENANCE MANUAL LINE 12V DC Receptacle LOAD +12V TB I1 12V Power Supply Figure 19 Page 28 91-00-00 24.10.13...
Page 845 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Headset Console Figure 20 Page 29 91-00-00 24.10.13...
Page 846 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL C36b Instruments 1 ground terminals resistive fuel module see: Fuel Indicating System Engine Monitoring System Figure 21 (1) EFFECTIVITY Page 30 Aircraft equipped with MVP-50 91-00-00 24.10.13...
Page 847 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL X M8 engine connector fuel pressure sensor oil pressure sensor oil temp. sensor outboard temp. sensor carburetor temp. sensor engine connector eng. speed sensor Engine Monitoring System Figure21 (2) EFFECTIVITY Page 31 Aircraft equipped with MVP-50 91-00-00 24.10.13...
Page 848 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL 4. Wire Routing Diagrams The wire routing diagrams listed below define the wiring of the basic electrical equipment. No. Wire routing diagram Ref. Fig. Effectivity (1) Antennas Fig. 1 300 - 306 (2) Antennas Fig.
Page 849 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP GPS antenna COM2 antenna FLARM antenna ADSB antenna marker beacon antenna XPDR antenna NAV antenna COM1 antenna Antennas - Wire Routing Figure 1 EFFECTIVITY Page 33...
Page 850 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP combined GPS/COM2 antenna GPS antenna NAV antenna COM1 antenna FLARM antenna ADSB antenna marker beacon antenna 10 XPDR antenna Antennas - Wire Routing Figure 1 EFFECTIVITY...
Page 851 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP combined GPS/COM2 antenna GPS antenna NAV antenna COM1 antenna FLARM antenna ADSB antenna marker beacon antenna 10 XPDR antenna Antennas - Wire Routing Figure 1 EFFECTIVITY...
Page 852 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Legend: GMU 44 GRS 77 GTP 59 GDC 741 GDU 620 fuselage connector G500 Garmin G500 - Wire Routing Figure 2 Page 36 91-00-00 24.10.13...
Page 853 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Legend: dome light connector, dome light connector landing light landing light NAV lights LH Pitot heat fuel sensor LH stall warning sensor fuel sensor RH 10 NAV lights RH Wings and Lights - Wire Routing...
Page 854 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Legend: alternator 1 ignition box engine connector fuselage connector trim indicator to flap actuator to trim motor wing connector head set console 10 alt. rectifier reg. unit 11 fuel pump 12 ext. power receptacle 13 alternator 2 Misc.
Page 855 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL 5. Antenna Overview The diagram below defines the position of the various antennas. Legend: ELT antenna ROD ELT antenna WHP GPS antenna COM2 antenna FLARM antenna ADSB antenna marker beacon antenna XPDR antenna...
Page 856 AQUILA AT01-100/200/300 Charts and Diagrams MAINTENANCE MANUAL Legend: ELT antenna ROD ELT antenna WHP combined GPS/COM2 antenna GPS antenna NAV antenna COM1 antenna FLARM antenna ADSB antenna marker beacon antenna XPDR antenna Antenna Overview Figure 1 EFFECTIVITY Page 40 307 - 999 91-00-00 24.10.13...

This manual is also suitable for:

At01-200 At01-100 A211 A212 A211i