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Aquila AT01-200 Maintenance Manual

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A
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)
Doc.-No. MM-AT01-1020-110
AQUILA Aviation International GmbH
Phone:++49 33 731 707 - 0
Fax:
++49 33 731 707 - 11
e-mail: kontakt@aquila-aviation.de

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Summary of Contents for Aquila AT01-200

  • Page 1 AQUILA AT01-100 AQUILA Aviation International GmbH MAINTENANCE MANUAL MAINTENANCE MANUAL AQUILA AT01-100 (A211) AQUILA AT01-200 (A212) 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 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 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 201-207 SERVICING 12-00-00 Servicing - General...
  • Page 5 AQUILA AT01-100/200 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 24-30-00 Main Battery System - Maintenance 201-203 24-40-00 External Power - Maintenance 201-203 24-60-00 Electrical Load Distribution - Description 24-61-00 Circuit Breaker - Maintenance 201-203 24-97-00...
  • Page 6 AQUILA AT01-100/200 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 32-10-00 Main Landing Gear - Maintenance 201-202 32-20-00 Nose Landing Gear - Description 32-20-00 Nose Landing Gear - Maintenance 201-204 32-40-00 Wheels and Brakes - Description...
  • Page 7 AQUILA AT01-100/200 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages WINDOWS 56-00-00 Windows - General 56-10-00 Flight Compartment Windows - Maintenance 201-203 WINGS 57-00-00 Wings - General 57-00-00 Wings - Maintenance 201-206 57-50-00 Control Surfaces - Maintenance...
  • Page 8 AQUILA AT01-100/200 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 79-00-00 Oil - General 1-2/2 79-10-00 Oil Tank - Maintenance 201-202 79-20-00 Oil Cooler - Maintenance 201-202 79-31-00 Oil Pressure Indication - Maintenance 201-202/201 79-33-00 Oil Temperature Indication - Maintenance...
  • Page 9 AQUILA AT01-100/200 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 10 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 11 AQUILA AT01-100/200 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 12 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 13 & 2 incorporated A.06 29.02.16 Control surface ply lay-up added; repair procedures revised A.07 10.06.16 6000h check & TBOs added; battery check; wing bolts safetying A.08 09.10.18 Beringer: new axle and new wheels; Rotax: new spark plugs A.09 28.02.20 New model AT01-200...
  • Page 14 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 15 AQUILA AT01-100/200 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 16 AQUILA AT01-100/200 Introduction MAINTENANCE MANUAL Table 1 - List of Technical Publications (Cont.) Title Manual No. / Part No. Supplier Operation & Installation Manual E-1048 MT-Propeller Entwicklung GmbH Hydraulic Constant Speed Governor P-8()()-() 5.00-5” Wheels and Brakes Beringer Aero RA-002 / RF-005 User Manual...
  • Page 17 AQUILA AT01-100/200 Introduction MAINTENANCE MANUAL Table 1 - List of Technical Publications (Cont.) Title Manual No. / Part No. Supplier Kannad AF Integra DOC 09078 Kannad Aviation Enquiries Operation Manual Ref. 0146257 Orolia SAS VT-01 Transponder 01.0200.11E Garrecht Avionik GmbH...
  • Page 18 AQUILA AT01-100/200 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 19 AQUILA AT01-100/200 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 20 AQUILA AT01-100/200 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 21 AQUILA AT01-100/200 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 22 AQUILA AT01-100/200 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 23 AQUILA AT01-100/200 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* GENERAL Table of Contents 28.02.20 Introduction 28.02.20 Airworthiness Limitations 28.02.20 Time Limits / Maintenance Checks 28.02.20 Dimensions and Areas 28.02.20 Lifting & Shoring 28.02.20 Leveling and Weighing 28.02.20...
  • Page 24 AQUILA AT01-100/200 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* POWER PLANT Power Plant 28.02.20 Ignition 09.10.18 Cooling System 28.02.20 Engine Controls 28.02.20 Engine Indicating 28.02.20 Exhaust 28.02.20 28.02.20 Starting 30.04.13 Charts and Wiring Diagrams 24.10.13 * The date refers to the issue / revision date of the respective chapter.
  • Page 25 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 4 AIRWORTHINESS LIMITATIONS...
  • Page 26 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 27 EASA Major Change Approval 10045112 A.02 24.10.13 FAA validation A.03 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 Page 1 04 - RECORD OF REVISIONS 28.02.20...
  • Page 28 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 29 AQUILA AT01-100/200 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 28.02.20...
  • Page 30 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 31 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 32 / 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 33 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 5 TIME LIMITS / MAINTENANCE CHECKS...
  • Page 34 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 35 AQUILA AT01-100/200 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 36 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 37 AQUILA AT01-100/200 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 38 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 39 Nose landing gear spring 5 years package rubber elements Main landing gear struts 6000h Flexible teflon hoses 2000 h or 15 years of the brake system 1) Beringer wheel and brake system only. 4) AT01-200 only. Page 1 05-10-00 28.02.20...
  • Page 40 / 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 attaching bolts Engine shock with engine mounts overhaul...
  • Page 41 Note 3 ROTAX rubber parts 5 years / Note 3 of the engine (V-belt, hoses, carburetor parts) Spark plugs 200 h / Note 3 1) Beringer wheel and brake system only. 3) AT01-100 only. Page 3 4) AT01-200 only. 05-10-00 28.02.20...
  • Page 42 AQUILA AT01-100/200 Maintenance Checks MAINTENANCE MANUAL NOTES: Note 1: Refer to manufacturer instructions for battery replacement time limits. Note 2: Refer to latest issue of the mt-propeller Service Bulletin No. 1.-( ), and to the mt-Propeller E-124 Operation and Installation Manual.
  • Page 43 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 44 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 45 Shut down engine, set the ignition switch and the master switch to the OFF position. Remove ignition key from aircraft. 3) AT01-100 only. 4) AT01-200 only. Page 3 6) Check has to be carried out every 100 hours of operation or 12 month, whichever comes first.
  • Page 46 TCU protocol - Read out TCU via Rotax communication 76-00-00 program. Check alarm records. Rotax Heavy MM 76-00-00 3.1.1) TCU S/N:______________Hours of Operation:____________ 4) AT01-200 only. Check has to be carried out every 100 hours of operation or 12 month, whichever comes first. Page 4 05-20-00 28.02.20...
  • Page 47 AQUILA AT01-100/200 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 48 Battery BAT 2 - Check fuses of rectifier-regulator installation. 24-20-00 3) AT01-100 only. 4) AT01-200 only. Page 6 Check has to be carried out every 100 hours of operation or 12 month, whichever comes first. 05-20-00 N/VFR equipped aircraft only.
  • Page 49 Rotax Heavy MM 72-00-00 4) AT01-200 only. 6) Check has to be carried out every 100 hours of operation or 12 month, whichever comes first. 7) If more than 30% of operation hours have been flown with leaded fuel e.g.: AVGAS 100LL...
  • Page 50 Inspect safety wiring if applicable, replace as necessary. 3) AT01-100 only. 4) AT01-200 only. 6) Check has to be carried out every 100 hours of operation or 12 month, whichever comes first. Page 8 05-20-00 28.02.20...
  • Page 51 MAINTENANCE MANUAL Propeller Reference Interval Initials 100h other Engine mounts (manufactured by ROTAX and AQUILA) - R912* 12-20-00 Check mounts for deformation, cracks, corrosion, R914* 12-20-00 security and damage from heat. Check mounting bolts for SB-912-028 condition and correct torque value.
  • Page 52 AQUILA AT01-100/200 Maintenance Checks MAINTENANCE MANUAL Propeller Reference Interval Initials 100h other Spinner - Remove from aircraft and check for delamination 61-10-00 and cracks. Spinner plate - Check for cracks and fit. Blade root and hub area - Examine for oil and grease leaks.
  • Page 53 Check operation of seat adjustment mechanism and seat stops. Inspect gas spring struts for oil leakage or other damage. Seats - Check ease of movement - if required remove seats, 25-10-00 annual clean and lubricate seat rails. 4) AT01-200 only. Page 11 05-20-00 28.02.20...
  • Page 54 Check travel of control surfaces if the control stick is in the full forward /neutral/ aft, and full left /neutral/ right positions. Verify no binding or jumpy movement of the control sticks through their full range of travel. 4) AT01-200 only. Page 12 05-20-00 28.02.20...
  • Page 55 AQUILA AT01-100/200 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 56 AQUILA AT01-100/200 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 57 AQUILA AT01-100/200 Maintenance Checks MAINTENANCE MANUAL Wings, Ailerons, Flaps (Cont.) Reference Interval Initials 100h other Fuel vent lines - Check for blockage. Fuel tank drain valves - Check for correct function and leakage. Fuel tank outlet strainer - Check for damage. Clean if necessary.
  • Page 58 AQUILA AT01-100/200 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 59 AQUILA AT01-100/200 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 60 AQUILA AT01-100/200 Maintenance Checks MAINTENANCE MANUAL Nose and Main Landing Gear (Cont.) Reference Interval Initials 100h other Wheel brakes - Check pistons retraction. Check brake caliper 32-40-00 annual assembly bolt torque. Check play between brake disc and wheel clips. Change clips if play is above 0.4mm (0.016 in.)
  • Page 61 AQUILA AT01-100/200 Maintenance Checks MAINTENANCE MANUAL Electrical System / Avionics Reference Interval Initials 100h other Electrical wiring system - Check the complete electrical R912* 12-20-00 wiring system for security, damage, wear and secure fit. R914* 12-20-00 Check all cable connections for tight fit, good contact, corrosion and condition.
  • Page 62 Check throttle and propeller control levers friction lock. Foreign items - Remove any foreign items from the aircraft. 4) AT01-200 only. The aircraft is airworthy and meets the condition specified in the aircraft data sheet. All maintenance required by Service Information and Airworthiness Directives and all prescribed scheduled maintenance checks have been carried out.
  • Page 63 MAINTENANCE MANUAL 3. 6000-Hour Inspection The airframe of the type AQUILA AT01 is limited to 6.000 hours of flight time (refer to 04-00-00). An inspection program to reach an extension of replacement time can be obtained from the type certificate holder on request.
  • Page 64 AQUILA AT01-100/200 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 65 AQUILA AT01-100/200 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 66 AQUILA AT01-100/200 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 67 AQUILA AT01-100/200 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 68 AQUILA AT01-100/200 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 69 AQUILA AT01-100/200 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 55-20-00).
  • Page 70 AQUILA AT01-100/200 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 71 AQUILA AT01-100/200 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 72 AQUILA AT01-100/200 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 73 AQUILA AT01-100/200 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 74 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 75 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 Airplane Flight Manual, section 4.
  • Page 76 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 77 AQUILA AT01-100/200 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 78 AQUILA AT01-100/200 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 79 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS AND AREAS...
  • Page 80 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 81 AQUILA AT01-100/200 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 82 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 83 AQUILA AT01-100/200 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 84 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 85 AQUILA AT01-100/200 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 86 AQUILA AT01-100/200 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 87 AQUILA AT01-100/200 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 28.02.20...
  • Page 88 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 89 AQUILA AT01-100/200 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 90 AQUILA AT01-100/200 Dimensions and Areas MAINTENANCE MANUAL (Interior) Instrument Panel Firewall Aircraft Zones Figure 1 Page 2 06-20-00 28.02.20...
  • Page 91 AQUILA AT01-100/200 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 92 AQUILA AT01-100/200 Dimensions and Areas MAINTENANCE MANUAL 610AB 510AB 210BB 210AB 520AB 620AB 610BB 510BB Access / Inspection Plates Figure 1 Page 2 06-30-00 28.02.20...
  • Page 93 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 07 LIFTING AND SHORING...
  • Page 94 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 95 AQUILA AT01-100/200 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 96 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 97 AQUILA AT01-100/200 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 98 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 99 AQUILA AT01-100/200 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 100 AQUILA AT01-100/200 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 101 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 08 LEVELING AND WEIGHING...
  • Page 102 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 103 AQUILA AT01-100/200 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...
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  • Page 105 AQUILA AT01-100/200 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 106 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 107 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 108 AQUILA AT01-100/200 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 109 AQUILA AT01-100/200 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 110 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 111 AQUILA AT01-100/200 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 112 AQUILA AT01-100/200 Leveling and Weighing MAINTENANCE MANUAL Longitudinal Leveling Wedge Positioning Figure 201 Page 202 08-20-00 28.02.20...
  • Page 113 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 09 TOWING AND TAXIING...
  • Page 114 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 115 AQUILA AT01-100/200 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 116 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 117 AQUILA AT01-100/200 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 118 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 119 AQUILA AT01-100/200 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 120 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 121 AQUILA AT01-100/200 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 122 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 123 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE...
  • Page 124 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 125 AQUILA AT01-100/200 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 126 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 127 AQUILA AT01-100/200 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 128 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 129 AQUILA AT01-100/200 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 130 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 131 AQUILA AT01-100/200 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 132 AQUILA AT01-100/200 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 133 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 134 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 135 AQUILA AT01-100/200 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 136 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 137 AQUILA AT01-100/200 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 138 AQUILA AT01-100/200 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 139 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 11 PLACARDS AND MARKINGS...
  • Page 140 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 141 AQUILA AT01-100/200 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...
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  • Page 143 AQUILA AT01-100/200 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 144 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 145 AQUILA AT01-100/200 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 146 AQUILA AT01-100/200 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 147 AQUILA AT01-100/200 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. Detail- Exterior Placards and Markings Figure 201 (1) Page 203 11-20-00 28.02.20...
  • Page 148 AQUILA AT01-100/200 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 149 AQUILA AT01-100/200 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 28.02.20...
  • Page 150 AQUILA AT01-100/200 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 151 AQUILA AT01-100/200 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 28.02.20...
  • Page 152 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 153 AQUILA AT01-100/200 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 154 AQUILA AT01-100/200 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. Interior Placards and Markings Figure 201 (1)
  • Page 155 AQUILA AT01-100/200 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 156 AQUILA AT01-100/200 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 157 AQUILA AT01-100/200 Placards and Markings MAINTENANCE MANUAL Note: Placards illustrated are not to scale. KRAFTSTOFF FUEL AUSFLIEGBAR USABLE 109,6 LITER 109.6 LTR Detail- 28.9 GAL TANKWECHSEL SWITCH TANKS ALLE 60 MIN EVERY 60 MIN VORNEHMEN PARKBREMSE PARKING BRAKE Detail- ZIEHEN EIN...
  • Page 158 Weitere Betriebsgrenzen stehen im Flughandbuch. Interior Placards and Markings Figure 201 (5) 1) Aircraft equipped with analog engine instruments only. 2) Aircraft equipped with Aspen avionics only. AT01-200 only. Aircraft equipped with pitot heating system only. Page 206 Aircraft equipped with non-(E)TSO’d GPS-receiver only.
  • Page 159 COM/NAV 1 Detail- COM/NAV 2 Detail- VORSICHT CAUTION Elektrische Hauptkraft- Electric Main Fuel Pump Detail- stoffpumpe BAT2 for Flight BAT2 im Flug for Parking am Boden Interior Placards and Markings Figure 201 (6) 3) AT01-200 only. Page 207 11-30-00 28.02.20...
  • Page 160 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 161 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 12 SERVICING...
  • Page 162 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 163 AQUILA AT01-100/200 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 164 AQUILA AT01-100/200 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 165 AQUILA AT01-100/200 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 166 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 167 29.0 Unusable Fuel 10,4 Fuel Specification The following fuel is approved for use in the AQUILA AT01-100/200. The minimum RON should be 95. EN 228 Super (Premium) EN 228 Super plus (Premium plus) AVGAS 100 LL (Grade ASTM-D910, blue color)
  • Page 168 AQUILA AT01-100/200 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 169 (AT01-100) / at the base of the gascolator close to the electrical fuel pumps (AT01-200). The drain is accessible from outside the nose section. The center of the fuel drains can be pushed inward with the fuel sampler to inspect for water and contamination.
  • Page 170 Fueling (1) Move aircraft to a designated fuel loading / fuel unloading area. (2) Make sure that the ALT1/BAT and ALT2/BAT2 (AT01-200) switches are in the OFF position. (3) Ground aircraft and filling device as described above. (4) Position a fire extinguisher near to the fuel tank to be serviced.
  • Page 171 The oil filler cap of the oil tank is located on the right side of the engine behind cylinder no. 3 (AT01-100) / on the left side of the engine behind cylinder no. 4 (AT01-200). It is accessible by opening the oil access plate on the upper cowling. The oil filler cap has a dipstick with min - max markings to check oil level.
  • Page 172 AQUILA AT01-100/200 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 173 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) / right (AT01-200) inside of the lower cowling. To increase its effectiveness, the filter element should be treated with filter oil.
  • Page 174 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 175 AQUILA AT01-100/200 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 176 AQUILA AT01-100/200 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 177 AQUILA AT01-100/200 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 178 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 179 AQUILA AT01-100/200 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.
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  • Page 181 AQUILA AT01-100/200 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 182 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 183 AQUILA AT01-100/200 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 184 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 185 AQUILA AT01-100/200 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 186 AQUILA AT01-100/200 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 187 AQUILA AT01-100/200 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 188 AQUILA AT01-100/200 Servicing MAINTENANCE MANUAL Lubrication Chart Figure 301 (1) Page 302 12-22-00 28.02.20...
  • Page 189 AQUILA AT01-100/200 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 190 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 191 AQUILA AT01-100/200 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 192 AQUILA AT01-100/200 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 193 AQUILA AT01-100/200 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 194 AQUILA AT01-100/200 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 195 AQUILA AT01-100/200 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 196 AQUILA AT01-100/200 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 197 AQUILA AT01-100/200 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.
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  • Page 199 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 20 STANDARD PRACTICES - AIRFRAME...
  • Page 200 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 201 AQUILA AT01-100/200 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...
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  • Page 203 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 204 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 205 AQUILA AT01-100/200 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 206 AQUILA AT01-100/200 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 207 AQUILA AT01-100/200 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 208 AQUILA AT01-100/200 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 209 AQUILA AT01-100/200 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 210 AQUILA AT01-100/200 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 211 AQUILA AT01-100/200 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 212 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 213 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 21 VENTILATION AND HEATING...
  • Page 214 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 215 AQUILA AT01-100/200 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 216 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 217 AQUILA AT01-100/200 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.
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  • Page 219 AQUILA AT01-100/200 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 220 AQUILA AT01-100/200 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 221 AQUILA AT01-100/200 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 222 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 223 AQUILA AT01-100/200 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 224 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 225 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 23 COMMUNICATIONS...
  • Page 226 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 227 AQUILA AT01-100/200 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 228 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 229 AQUILA AT01-100/200 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 230 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 231 AQUILA AT01-100/200 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 232 AQUILA AT01-100/200 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 233 AQUILA AT01-100/200 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 234 AQUILA AT01-100/200 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 235 AQUILA AT01-100/200 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 236 AQUILA AT01-100/200 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 237 AQUILA AT01-100/200 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 238 AQUILA AT01-100/200 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 239 AQUILA AT01-100/200 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 240 AQUILA AT01-100/200 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 241 AQUILA AT01-100/200 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 242 AQUILA AT01-100/200 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 243 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER...
  • Page 244 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 245 AQUILA AT01-100/200 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 ............24-20-00 Introduction 24-20-00 Description and Operation 24-20-00 ALTERNATOR SYSTEM - MAINTENANCE ..........24-20-00...
  • Page 246 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Effectivity 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 General 24-97-00 Splicing...
  • Page 247 AQUILA AT01-100/200 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 248 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 249 AQUILA AT01-100/200 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 250 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL TROUBLE POSSIBLE CAUSE REMEDY 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 251 AQUILA AT01-100/200 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 252 AQUILA AT01-100/200 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 253 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL warning light “ALT 1” circuit breaker “Warning Lights” external alternator 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 254 AQUILA AT01-100/200 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 “Annunciator” Main “Main...
  • Page 255 AQUILA AT01-100/200 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 Night-VFR or Rotax 914 equipped aircraft). Refer to the appropriate ROTAX publications for maintenance procedures on the internal alternator.
  • Page 256 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL Detail- External Alternator Installation Figure 201 Page 202 24-20-00 28.02.20...
  • Page 257 AQUILA AT01-100/200 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 61-10-00). (7) Remove alternator drive belt. Install Alternator Drive Belt (1) Install alternator drive belt around drive pulley.
  • Page 258 AQUILA AT01-100/200 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 28.02.20...
  • Page 259 AQUILA AT01-100/200 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 204 Aircraft equipped with Rotax 914F engine 24-20-00...
  • Page 260 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL 5. BAT 2 Battery Removal/Installation (Ref. Fig. 202) Remove BAT 2 Battery (1) Ensure electrical power to aircraft is OFF. (2) Remove engine cowling (refer to 71-10-00). (3) Disconnect main battery (refer to 24-30-00).
  • Page 261 AQUILA AT01-100/200 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 262 AQUILA AT01-100/200 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 28.02.20...
  • Page 263 AQUILA AT01-100/200 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 264 AQUILA AT01-100/200 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 265 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL 4. Battery Condition Check For Night-VFR equipped aircraft or aircraft equipped with Rotax 914F 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 266 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 267 AQUILA AT01-100/200 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 268 AQUILA AT01-100/200 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 24-40-00 Aircraft equipped with an external power receptacle...
  • Page 269 AQUILA AT01-100/200 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.
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  • Page 271 AQUILA AT01-100/200 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.
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  • Page 273 AQUILA AT01-100/200 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 274 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL Table 201: Circuit Breaker Current Ratings (Cont.) Current Rating Circuit Breaker Effectivity 7.5A (8A) Aspen EFD1000 NAV/GPS 1 & 2 GTN 650 G500 Autopilot ( GMC507 & s ervos) Elevator Trim from S/N 327...
  • Page 275 AQUILA AT01-100/200 Electrical Power MAINTENANCE MANUAL Table 201: Circuit Breaker Current Ratings (Cont.) Current Rating Circuit Breaker Effectivity Avionic Blower Traffic Monitor TRX 1500, TRX 2000 Blind Encoder ACK-A30 Audio PM 501, PM 500EX NAV/GPS1 SL30, CDI1 NAV/GPS2 SL30, CDI2 GPS Map 495, GPS Map 496, Aera 5XX ADAHRS1 &...
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  • Page 277 AQUILA AT01-100/200 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.
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  • Page 279 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 25 EQUIPMENT / FURNISHINGS...
  • Page 280 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 281 AQUILA AT01-100/200 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 282 AQUILA AT01-100/200 Equipment / Furnishings MAINTENANCE MANUAL Page 02 25 - TOC 15.09.09...
  • Page 283 AQUILA AT01-100/200 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.
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  • Page 285 AQUILA AT01-100/200 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 286 AQUILA AT01-100/200 Equipment / Furnishings MAINTENANCE MANUAL Detail- Seat Installation Figure 201 Page 202 25-10-00 28.02.20...
  • Page 287 AQUILA AT01-100/200 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 288 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 289 AQUILA AT01-100/200 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.
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  • Page 291 AQUILA AT01-100/200 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". 2. Panels, Coverings and Carpets Removal and Installation Panels are typically attached to the aircraft fuselage structure with small screws.
  • Page 292 AQUILA AT01-100/200 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 293 AQUILA AT01-100/200 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 294 AQUILA AT01-100/200 Equipment / Furnishings MAINTENANCE MANUAL...
  • Page 295 AQUILA AT01-100/200 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 296 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 297 AQUILA AT01-100/200 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 298 AQUILA AT01-100/200 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 299 AQUILA AT01-100/200 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 300 AQUILA AT01-100/200 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 301 AQUILA AT01-100/200 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 302 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 303 AQUILA AT01-100/200 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 304 AQUILA AT01-100/200 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 305 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 27 FLIGHT CONTROLS...
  • Page 306 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 307 AQUILA AT01-100/200 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 308 AQUILA AT01-100/200 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 309 AQUILA AT01-100/200 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 310 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 311 AQUILA AT01-100/200 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 312 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL pushrod 4 pushrod 3 pushrod 2 pushrod 1 Aileron Control System Design and Function Figure 1 Page 2 27-10-00 30.04.13...
  • Page 313 AQUILA AT01-100/200 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 314 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL left side shown (right side analogous) Detail- Detail- Component Installation Figure 201 Page 202 27-10-00 30.04.13...
  • Page 315 AQUILA AT01-100/200 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. (3) Perform aileron control system inspection/check (refer to “Inspection/Check” below). (4) Install access plate 210 AB (refer to 06-30-00).
  • Page 316 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL left side shown (right side analogous) Detail- Detail- Component Installation Figure 202 Page 204 27-10-00 30.04.13...
  • Page 317 AQUILA AT01-100/200 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 318 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL Detail- left side shown (right side analogous) Detail- Aileron Bellcrank Installation Figure 203 Page 206 27-10-00 30.04.13...
  • Page 319 AQUILA AT01-100/200 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 320 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 321 AQUILA AT01-100/200 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 322 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL Rudder Control Design And Function Figure 1 Page 2 27-20-00 30.04.13...
  • Page 323 AQUILA AT01-100/200 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 324 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL Detail- Rudder Control Installation Figure 201 Page 202 27-20-00 30.04.13...
  • Page 325 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL (2) Reinstall lower half of middle bearing block. (3) Reconnect steering tubes to rudder bars. (4) Reconnect master cylinders to the rudder pedal assembly. (5) Reconnect control cables to rudder control actuator arms and re-rig system (refer to “Adjustment/Test“...
  • Page 326 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL Detail- Rudder Pedal / Master Cylinder Installation Figure 202 Page 204 27-20-00 30.04.13...
  • Page 327 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL (3) Verify rudder can be moved smoothly through full travel. No grinding is audible. (4) Check rudder for correct travel using an inclinometer, if necessary perform rudder control system adjustment/test (refer to “Adjustment/Test” below).
  • Page 328 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 329 AQUILA AT01-100/200 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 330 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL pushrod 2 pushrod 1 Elevator Control System Design And Function Figure 1 Page 2 27-30-00 30.04.13...
  • Page 331 AQUILA AT01-100/200 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 332 AQUILA AT01-100/200 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 30.04.13...
  • Page 333 AQUILA AT01-100/200 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 334 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL Fuselage structure omitted for clarity. Detail- Detail- Component Installation Figure 202 Page 204 27-30-00 30.04.13...
  • Page 335 AQUILA AT01-100/200 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 336 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 337 AQUILA AT01-100/200 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 338 AQUILA AT01-100/200 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 30.04.13...
  • Page 339 AQUILA AT01-100/200 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 340 AQUILA AT01-100/200 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 30.04.13...
  • Page 341 AQUILA AT01-100/200 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 342 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL flap actuator torque tube Flap Control System Design and Function Figure 1 Page 2 27-50-00 30.04.13...
  • Page 343 AQUILA AT01-100/200 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 344 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL Detail- Fuselage structure omitted for clarity. Flap Control System Installation Figure 201 Page 202 27-50-00 30.04.13...
  • Page 345 AQUILA AT01-100/200 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 346 AQUILA AT01-100/200 Flight Controls MAINTENANCE MANUAL Detail- Wing structure omitted for clarity. Flap Control System Installation Figure 201 Page 204 27-50-00 30.04.13...
  • Page 347 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 GmbH 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 348 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 349 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 28 FUEL...
  • Page 350 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 351 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity FUEL - GENERAL .....................28-00-00 Rotax 912S Introduction 28-00-00 Rotax 912S General Description 28-00-00 Rotax 912S FUEL - GENERAL .....................28-00-00 Rotax 914F Introduction 28-00-00 Rotax 914F General Description...
  • Page 352 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Chapter Section Title Subject Page Effectivity FUEL FLOW INDICATION - MAINTENANCE ..........28-45-00 Fuel flow ind. General 28-45-00 Fuel flow ind. Fuel Flow Transducer Removal/Installation 28-45-00 Fuel flow ind. Fuel Flow Differential Module Removal/Installation 28-45-00 Fuel flow ind.
  • Page 353 AQUILA AT01-100/200 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 354 AQUILA AT01-100/200 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 355 AQUILA AT01-100/200 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 356 AQUILA AT01-100/200 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 357 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 358 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 359 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL FUEL DISTRIBUTION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! 1. General The fuel distribution system consists primarily of the fuel selector / shut-off valve, electrical fuel pump(s), fuel filter, fuel lines and the AUX fuel pump switch.
  • Page 360 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL Notes: Fuel system components Detail- in left wing analogous. Fuselage structure omitted fuel return line for clarity. fuel line Fuel Selector / Shut-Off Valve Installation Figure 201 Page 202 28-20-00 28.02.20...
  • Page 361 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL fuel return line fuel line 2 Nm 17.7 in.lbs Detail- Fuel Level Sensor / Fuel Tank Outlet Strainer Installation Figure 202 Page 203 28-20-00 28.02.20...
  • Page 362 AQUILA AT01-100/200 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 28.02.20...
  • Page 363 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL KS_Syst_Loc_R914.iso check valve main fuel pump from fuel selector / shut-off valve check valve aux. fuel pump 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 28.02.20...
  • Page 364 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL 2. Fuel Selector / Shut-Off Valve Removal/Installation Remove Fuel Selector / Shut-Off Valve (1) Ensure electrical power to aircraft is OFF. (2) Disconnect battery (refer to 24-30-00). (3) Drain fuel from fuel system completely using the wing fuel tank drains and the drain at the electrical fuel pump (Rotax 912) / gascolator (Rotax 914).
  • Page 365 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL 4. Electrical Fuel Pump Removal/Installation (Rotax 914F only) Remove Electrical Fuel Pump (1) Ensure electrical power to aircraft is OFF. (2) Close fuel selector / shut-off valve. (3) Disconnect battery (refer to 24-30-00). (4) Drain fuel from system with drainer at bottom of gascolator.
  • Page 366 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL (11) Secure cap / bowl using locking wire. (12) Reconnect battery (refer to 24-30-00). (13) Perform operational check of the fuel distribution system. (14) Inspect system for any signs of fuel leakage. (15) Install all items removed for access.
  • Page 367 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! 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 368 AQUILA AT01-100/200 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 369 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL Fuel Quantity Indicating System Calibration NOTE: A calibration module is necessary to perform the steps described below. The calibration module is installed at the back of the fuel quantity indicator. For further information on fuel tank calibration or if no calibration module is installed refer to SI-AT01-018, latest revision.
  • Page 370 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 371 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! 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 372 AQUILA AT01-100/200 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 373 AQUILA AT01-100/200 MAINTENANCE MANUAL Select “Fuel Quantity 2/R”, “Calibrate”, “Flight” and repeat step (7) for the RH wing fuel tank. (9) Add 13,7 liters (3.62 gallons) of fuel to each wing fuel tank. (10) Wait approx. 30 seconds. Then gently shake wing to assure fuel quantity sensors settle in their final position.
  • Page 374 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 375 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL FUEL QUANTITY INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! 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 376 AQUILA AT01-100/200 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 24-30-00). (3) Remove glare shield (refer to 31-10-00). (4) Disconnect electrical connectors from back of module.
  • Page 377 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 12-11-00).
  • Page 378 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 379 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL FUEL PRESSURE INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! 1. General Fuel pressure indication is included in the engine monitoring system. Fuel pressure is measured by a pressure transducer electrically connected to the engine data converter (EDC).
  • Page 380 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 381 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL FUEL FLOW INDICATION - MAINTENANCE WARNING: PERFORM ALL FUEL SYSTEM MAINTENANCE IN ACCORDANCE WITH SAFETY PRECAUTIONS CONTAINED IN 12-11-00! 1. General Fuel flow is measured by two FT-60 fuel flow trancducers: One installed in the fuel supply line, the other one in the return line.
  • Page 382 AQUILA AT01-100/200 Fuel MAINTENANCE MANUAL (8) Reconnect battery (refer to 24-30-00). (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 383 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 31 INDICATING / RECORDING SYSTEMS...
  • Page 384 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 385: Table Of Contents

    AQUILA AT01-100/200 Indicating / Recording MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity INDICATING / RECORDING SYSTEMS - GENERAL........31-00-00 AT01-100A Introduction 31-00-00 AT01-100A General Description 31-00-00 AT01-100A INDICATING / RECORDING SYSTEMS - GENERAL........31-00-00 AT01-100B Introduction 31-00-00 AT01-100B...
  • Page 386 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 387: 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 388 AQUILA AT01-100/200 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 389: 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 390 AQUILA AT01-100/200 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 391: 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 392 Autopilot control panel (optional) COM/NAV Ignition switch Transponder ALT1 / BAT switch Engine monitoring system ALT2 / BAT2 switch (AT01-200 only) AUX fuel pump switch Circuit breaker panel Avionic master switch Fresh air ventilator NAV light switch Carburetor heat control...

  • Page 393: Instrument Panel - Maintenance

    AQUILA AT01-100/200 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 394 AQUILA AT01-100/200 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 395 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 32 LANDING GEAR...
  • Page 396 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 397 AQUILA AT01-100/200 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 398 AQUILA AT01-100/200 MAINTENANCE MANUAL TABLE OF CONTENTS - CONTINUED Chapter Section Title Subject Page Effectivity Main Gear Wheel Disassembly/Assembly 32-40-00 Cleveland/Grove Nose Gear Wheel Removal/Installation 32-40-00 Cleveland/Grove Nose Gear Wheel Disassembly/Assembly 32-40-00 Cleveland/Grove Brake Master Cylinder Removal/Installation 32-40-00 Cleveland/Grove Brake Caliper Removal/Installation...

  • Page 399: Landing Gear - General

    AQUILA AT01-100/200 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 400 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 401: Main Landing Gear - Description

    AQUILA AT01-100/200 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 402 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 403: Main Landing Gear - Maintenance

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL MAIN LANDING GEAR - MAINTENANCE 1. Main Gear Leg Removal/Installation WARNING: CONTACT WITH HYDRAULIC FLUID CAN CAUSE SKIN IRRITATIONS. CAUTION: EXCESSIVE HYDRAULIC FLUID WILL ATTACK THE SURFACE OF VARIOUS MATERIALS. READ AND ADHERE TO ALL MANUFACTURER’S INSTRUCTIONS.
  • Page 404 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL Detail- UHMW-insert UHMW-insert UHMW-insert UHMW-insert Main Gear Leg Installation Figure 201 Page 202 32-10-00 09.10.18...

  • Page 405: Nose Landing Gear - Description

    AQUILA AT01-100/200 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 406 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 407: Nose Landing Gear - Maintenance

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL NOSE LANDING GEAR - MAINTENANCE 1. Nose Gear Leg Removal/Installation (Ref. Fig. 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 408 AQUILA AT01-100/200 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 09.10.18...
  • Page 409 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL Secured with safety wire. Detail- Damper Assy and Nose Wheel Fork Installation Figure 202 Page 203 32-20-00 09.10.18...
  • Page 410 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL Detail- Damper Assembly Figure 203 Page 204 32-20-00 09.10.18...

  • Page 411: Wheels And Brakes - Description

    AQUILA AT01-100/200 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 Beringer Aero maintenance manual for 5.00-5”...
  • Page 412 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 413: Wheels And Brakes - Maintenance

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL WHEELS AND BRAKES - MAINTENANCE 1. Main Gear Wheel Removal/Installation (Ref. Fig. 201) Remove a Main Gear Wheel (1) Jack aircraft or appropriate main gear wheel (refer to 07-00-00). (2) Remove screws securing wheel fairing and remove wheel fairing.
  • Page 414 AQUILA AT01-100/200 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 09.10.18...
  • Page 415 AQUILA AT01-100/200 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 416 AQUILA AT01-100/200 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 417 AQUILA AT01-100/200 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 09.10.18...
  • Page 418 AQUILA AT01-100/200 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 419 AQUILA AT01-100/200 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 420 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL (2) Remove valve cap and deflate tire completely. Then remove valve core. (3) Break tire beads away from wheel flanges by applying pressure by hand or using a wood or plastic tool as close to the tire bead as possible. Tire lubricant may be used to help. Repeat operation every 90°...
  • Page 421 AQUILA AT01-100/200 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 422 AQUILA AT01-100/200 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 09.10.18...
  • Page 423 AQUILA AT01-100/200 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 09.10.18...

  • Page 424: Wheel Assembly Maintenance

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL tightening order of wheel assembly screws CAUTION: TAKE CARE TO ENSURE O-RING IS IN PLACE. (12) 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.
  • Page 425 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL max. play clip screw clip inner wheel half brake disk CAUTION: DO NOT REUSE A BALL BEARING THAT HAS ALREADY BEEN MOUNTED, EVEN IF IN NEW CONDITION. Removal of Clips and Clip Screws (main wheels only) (1) Remove screws and clips if they are out of tolerance.
  • Page 426 AQUILA AT01-100/200 Landing Gear Landing Gear MAINTENANCE MANUAL (3) Apply air pressure to dry internal threads. CAUTION: OILY SOLVENT OR OILY AIR PRESSURE MUST NOT BE USED ON INTERNAL THREAD BECAUSE THREADLOCKER WILL NOT PROPERLY LOCK THE SCREWS. Inspection (1) Visually inspect wheel flanges (and central spacer) for scratches, cracks, nicks, corrosion, or other damage.

  • Page 427: Brake Master Cylinder Removal/Installation

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL CAUTION: DO NOT USE A HAMMER TO PRESS BEARING, IT WILL DAMAGE BALLS AND CAUSE FAILURE OF BALL BEARING. (3) Install new circlips after cooling down period. Check that circlips are in place. CAUTION: CIRCLIPS MAINTAIN BALL BEARINGS, IF CIRCLIPS ARE NOT IN PLACE BEARING CAN SLIDE OUT AND CAUSE BLOCKING OF THE WHEEL.
  • Page 428 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL pedal shaft master brake cylinder Detail- pilot’s left pedal assembly Master Brake Cylinder Installation Figure 204 EFFECTIVITY Page 216 Aircraft equipped with Beringer wheel/brake system 32-40-00 09.10.18...
  • Page 429 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL On Aircraft Pads Change (1) Remove main gear wheel from main gear strut (refer to “Main Gear Wheel Removal” above). (2) Remove the 3 caliper assembly screws. NOTE: Do not remove the caliper back plate from the axle.

  • Page 430: Brake Pad Replacement

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL CAUTION: WHEN THE BRAKES ARE RELEASED YOU MUST BE ABLE TO TURN THE WHEEL EASILY BY HAND. (11) Condition brake pads (refer to “Brake System Conditioning” below). brake pad assemblies back plate brake disc 25 Nm 220 in.lbs...

  • Page 431: Brake Disc Replacement

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL 7. Brake Disc Replacement The minimum allowable brake disc thickness is 3.8 mm (0.15 in.). Maximum coning allowed is 0.3 mm (0.012 in.). The maximum values for grooves and bumps are 0.2 mm (0.008 in.).

  • Page 432: Brake System Conditioning

    AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL 9. Brake System Conditioning When new brake pads have been installed, it is important to condition them properly to obtain the service life designed into them. Rated brake torque value is reached only after a full conditioning of brake pads and disc.
  • Page 433 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL WARNING: CONTACT WITH HYDRAULIC FLUID CAN CAUSE SKIN IRRITATIONS. CAUTION: EXCESSIVE HYDRAULIC FLUID WILL ATTACK THE SURFACE OF VARIOUS MATERIALS. READ AND ADHERE TO ALL MANUFACTURERS INSTRUCTIONS. PROVIDE A SUITABLE COLLECTING VESSEL FOR HYDRAULIC FLUID.
  • Page 434 AQUILA AT01-100/200 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 222 Aircraft equipped with Beringer wheel/brake system 32-40-00 09.10.18...
  • Page 435 AQUILA AT01-100/200 Landing Gear MAINTENANCE MANUAL NOTE: Causes for replacement of caliper casing are: - Signs of deep corrosion. - Anodizing color removed on more than 15% of external surface. - Heavy nicks. - Anodizing removed on internal piston bore.
  • Page 436 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 437: Brake Assembly Maintenance

    AQUILA AT01-100/200 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 438 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 439: Wheels And Brakes - Maintenance

    AQUILA AT01-100/200 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 440 AQUILA AT01-100/200 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 09.10.18...

  • Page 441: Nose Gear Wheel Removal/Installation

    AQUILA AT01-100/200 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 442 AQUILA AT01-100/200 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 09.10.18...

  • Page 443: Brake Master Cylinder Removal/Installation

    AQUILA AT01-100/200 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 444 AQUILA AT01-100/200 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 09.10.18...

  • Page 445: Brake Disc Removal/Installation

    AQUILA AT01-100/200 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 446: Brake System Bleeding

    AQUILA AT01-100/200 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 447 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 33 LIGHTS...
  • Page 448 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 449 AQUILA AT01-100/200 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 450 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 451: Lights - General

    AQUILA AT01-100/200 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 452 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 453: Interior Lights - Maintenance

    AQUILA AT01-100/200 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 454: Cockpit Light Removal/Installation

    AQUILA AT01-100/200 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 455: Exterior Lights - Maintenance

    Galactica (from S/N AT01-327 or SI-AT01-018, annex 19) LED navigation/position/anti-collision lights and a Hella 90mm module halogen (AT01-100) / Whelen Parmetheus PAR-36 Plus LED (AT01-200) landing light. The maintenance of exterior lights is limited to the removal and installation of components and light bulb replacement (halogen light only).

  • Page 456: Navigation/Position/Anti-Collision Light

    AQUILA AT01-100/200 Lights MAINTENANCE MANUAL 3. Navigation/Position/Anti-Collision Light Removal/Installation/Check Remove 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. (3) Disconnect wires at connector.
  • Page 457 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 34 NAVIGATION...
  • Page 458 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 459 AQUILA AT01-100/200 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 460 AQUILA AT01-100/200 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 461: Navigation - General

    AQUILA AT01-100/200 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 462 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 463: Pitot/Static System - Description

    AQUILA AT01-100/200 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 464 AQUILA AT01-100/200 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 28.02.20...

  • Page 465: Pitot/Static System - Maintenance

    AQUILA AT01-100/200 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 466: P/S Heat Control Box Removal/Installation (Optional)

    AQUILA AT01-100/200 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 467 AQUILA AT01-100/200 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 28.02.20...

  • Page 468: Inspection/Check

    AQUILA AT01-100/200 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 469: Stall Warning System - Description

    AQUILA AT01-100/200 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 470 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 471: Stall Warning System - Maintenance

    AQUILA AT01-100/200 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 472 AQUILA AT01-100/200 Navigation MAINTENANCE MANUAL...

  • Page 473: Attitude And Direction - Maintenance

    AQUILA AT01-100/200 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 474: Attitude Indicator Removal/Installation

    AQUILA AT01-100/200 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 475 AQUILA AT01-100/200 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 476 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 477: 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 478: Efd Battery Replacement

    AQUILA AT01-100/200 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 479: Configuration Module (Cm) Removal/Installation

    AQUILA AT01-100/200 Navigation MAINTENANCE MANUAL (4) Feed circular connector down through ½ inch hole in aircraft skin and mount RSM (vent hole faces aft) with four 8-32 non-ferrous screws. Tighten to 1,4-1,7 Nm (12-15 in.lbs). NOTE: It is critical that the screws are non-ferrous to avoid compass errors.
  • Page 480 AQUILA AT01-100/200 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 481 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 482 AQUILA AT01-100/200 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 28.02.20...
  • Page 483 AQUILA AT01-100/200 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 484: Inspection/Check

    AQUILA AT01-100/200 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 485: 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 486: Inspection/Check

    AQUILA AT01-100/200 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 487: 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 488: Inspection/Check

    AQUILA AT01-100/200 Navigation MAINTENANCE MANUAL lf G3X LRUs are removed and reinstalled or if any work has been done on the aircraft that could affect the system wiring, antenna cables, or any interconnected equipment, the checkout and return to service procedures in section 8 of the G3X Touch EFIS Part 23 AML STC Maintenance Manual have to be completed.

  • Page 489: 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 490: Inspection/Check

    AQUILA AT01-100/200 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 491: 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 492 AQUILA AT01-100/200 Navigation MAINTENANCE MANUAL Operation of the SAI 340 / KI 300 is not permitted unless an inspection as described in this section has been completed within the preceding 12 calendar months. See the following table for necessary tests or checks and the specific intervals for the SAI 340 / KI 300:...

  • Page 493: Independent Position Determining - Maintenance

    AQUILA AT01-100/200 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 navigation management system (NMS).
  • Page 494 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 495: Independent Position Determining - Maintenance

    AQUILA AT01-100/200 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 496 AQUILA AT01-100/200 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 28.02.20...

  • Page 497: Gps Antenna Removal/Installation

    AQUILA AT01-100/200 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 498 AQUILA AT01-100/200 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 28.02.20...

  • Page 499: Dependent Positioning Determining - Maintenance

    AQUILA AT01-100/200 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 500: Transponder Removal/Installation

    AQUILA AT01-100/200 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 501: Inspection/Check

    AQUILA AT01-100/200 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 502 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 503 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 51 STRUCTURES...
  • Page 504 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 505 AQUILA AT01-100/200 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 506 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 507: 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 508: Structure Classes

    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 509: Composite Damage Investigation

    AQUILA AT01-100/200 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 510: Damage Classification

    AQUILA AT01-100/200 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 511 AQUILA AT01-100/200 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 512 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 513: Composite Repair

    AQUILA AT01-100/200 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 514: Approved Materials

    AQUILA AT01-100/200 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 515: Tools, Equipment And Material

    AQUILA AT01-100/200 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 516: Material Data Sheet

    AQUILA AT01-100/200 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 517 AQUILA AT01-100/200 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (1) Page 205 51-20-00 29.02.16...
  • Page 518 AQUILA AT01-100/200 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (2) Page 206 51-20-00 29.02.16...
  • Page 519 AQUILA AT01-100/200 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 520 AQUILA AT01-100/200 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 521 AQUILA AT01-100/200 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 522 AQUILA AT01-100/200 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 523 AQUILA AT01-100/200 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 524 AQUILA AT01-100/200 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 525 AQUILA AT01-100/200 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 526 AQUILA AT01-100/200 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 527 AQUILA AT01-100/200 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 528 AQUILA AT01-100/200 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 529: Repair Of Sandwich Components

    (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 530 (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 531 (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 532 (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 533 (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 534: Repair Of Monolithic Components

    (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 535: Exterior Finish

    AQUILA AT01-100/200 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 536 AQUILA AT01-100/200 Structures MAINTENANCE MANUAL...
  • Page 537 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 52 DOORS...
  • Page 538 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 539 AQUILA AT01-100/200 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 540 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 541: Doors - General

    AQUILA AT01-100/200 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 542 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 543: Canopy - Maintenance

    AQUILA AT01-100/200 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 544 AQUILA AT01-100/200 Doors MAINTENANCE MANUAL Detail- Canopy Latching Mechanism Figure 201 (1) Page 202 52-10-00 30.04.13...
  • Page 545 AQUILA AT01-100/200 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 546 AQUILA AT01-100/200 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 547: Baggage Door - Maintenance

    AQUILA AT01-100/200 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 548 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 549 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 53 FUSELAGE...
  • Page 550 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 551 AQUILA AT01-100/200 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 552 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 553 AQUILA AT01-100/200 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 554 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 555 AQUILA AT01-100/200 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 556 AQUILA AT01-100/200 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 557 AQUILA AT01-100/200 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 558 AQUILA AT01-100/200 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 559 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 560 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 561 AQUILA AT01-100/200 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 562 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 563 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 55 STABILIZERS...
  • Page 564 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 565 AQUILA AT01-100/200 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 566 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 567: Stabilizers - General

    AQUILA AT01-100/200 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 568 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 569: Horizontal Stabilizer - Maintenance

    AQUILA AT01-100/200 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 570 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 571: Elevator - Maintenance

    AQUILA AT01-100/200 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 572 AQUILA AT01-100/200 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 573 AQUILA AT01-100/200 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 574 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 575: Vertical Stabilizer - Maintenance

    AQUILA AT01-100/200 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 576 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 577: Rudder - Maintenance

    AQUILA AT01-100/200 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 578 AQUILA AT01-100/200 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 579 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 56 WINDOWS...
  • Page 580 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 581 AQUILA AT01-100/200 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 582 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 583 AQUILA AT01-100/200 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 584 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 585 AQUILA AT01-100/200 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 586 AQUILA AT01-100/200 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 587 AQUILA AT01-100/200 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 588 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 589 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 57 WINGS...
  • Page 590 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 591 AQUILA AT01-100/200 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 592 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 593: Wings - General

    AQUILA AT01-100/200 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 594 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 595: 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 596 AQUILA AT01-100/200 Wings MAINTENANCE MANUAL wing spar root ribs wing fuel tank Detail- Wing Structure Figure 201 Page 202 57-00-00 10.06.16...
  • Page 597 AQUILA AT01-100/200 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 598 AQUILA AT01-100/200 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 599 AQUILA AT01-100/200 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 600: Wing Attachment Bolt Removal/Installation

    AQUILA AT01-100/200 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 601: Control Surfaces - Maintenance

    AQUILA AT01-100/200 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 602 AQUILA AT01-100/200 Wings MAINTENANCE MANUAL Detail- Detail- Flap/Aileron Structure Figure 201 Page 202 57-50-00 10.06.16...

  • Page 603: Adjustment - Control Surface Balancing

    AQUILA AT01-100/200 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 604 AQUILA AT01-100/200 Wings MAINTENANCE MANUAL wing Detail- right flap Flap Installation Figure 202 Page 204 57-50-00 10.06.16...
  • Page 605 AQUILA AT01-100/200 Wings MAINTENANCE MANUAL Detail- Aileron Installation Figure 203 Page 205 57-50-00 10.06.16...
  • Page 606 AQUILA AT01-100/200 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 607 AQUILA AT01-100/200 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 608 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 609 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 61 PROPELLER...
  • Page 610 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 611 AQUILA AT01-100/200 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 612 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 613: Propeller - General

    AQUILA AT01-100/200 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) variable pitch, two blade wood-composite propeller.
  • Page 614 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 615: Propeller - Troubleshooting

    AQUILA AT01-100/200 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 616: Troubleshooting

    AQUILA AT01-100/200 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 617 AQUILA AT01-100/200 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 618 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 619: Propeller Assembly - Maintenance

    AQUILA AT01-100/200 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) 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 620: Propeller Removal/Installation

    The dome is mounted to the bulkhead by means of screws. 4. Propeller Removal/Installation Remove Propeller (1) Ensure ALT1/BAT, ALT2/BAT2 (AT01-200 only) and ignition switches are OFF and the throttle is closed. (2) Remove upper engine cowling (refer to 71-10-00).

  • Page 621: Inspection/Check

    AQUILA AT01-100/200 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 622 AQUILA AT01-100/200 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 623: Propeller Control - Maintenance

    AQUILA AT01-100/200 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 624 AQUILA AT01-100/200 Propeller MAINTENANCE MANUAL gasket governor 20-24 Nm 180-220 in.lbs Governor Installation Figure 201 Page 202 61-20-00 28.02.20...

  • Page 625: Inspection/Check

    AQUILA AT01-100/200 Propeller MAINTENANCE MANUAL (5) Adjust governor (refer to “Adjustment/Test” below). (6) Install upper engine cowling (refer to 71-10-00). (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 71-10-00).
  • Page 626 AQUILA AT01-100/200 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 627 AQUILA AT01-100/200 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. Slowly move propeller lever forward. If popeller speed is max. 2385 rpm with propeller lever in full forward position governor adjustment is finished.
  • Page 628 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 629 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 71 POWER PLANT...
  • Page 630 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 631 AQUILA AT01-100/200 Power Plant MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity POWER PLANT - GENERAL ................71-00-00 Rotax 912S Introduction 71-00-00 Rotax 912S General Description 71-00-00 Rotax 912S POWER PLANT - GENERAL ................71-00-00 Rotax 914F Introduction 71-00-00...
  • Page 632 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 633: Power Plant - General

    AQUILA AT01-100/200 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 634 AQUILA AT01-100/200 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 635: Power Plant - General

    AQUILA AT01-100/200 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 636 AQUILA AT01-100/200 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 637: Power Plant - Troubleshooting

    AQUILA AT01-100/200 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 638 AQUILA AT01-100/200 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 639 AQUILA AT01-100/200 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 640 AQUILA AT01-100/200 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 641: Power Plant - Maintenance

    (16) Disconnect electrical cables to engine, alternator and sensors at connector or suitable place. (17) Remove wiring harness and bonding cables from engine. (18) Lift engine just enough to relief weight from engine mounts. (19) Remove nuts, washers, and bolts securing engine to AQUILA engine mount. (20) Remove engine from aircraft. Page 201 71-00-00 28.02.20...

  • Page 642: Engine Cleaning

    Reinstall all tubes, hoses, control cables and wiring as previously installed (including heat, abrasion and fire protection and supports / attachments). (1) Hoist engine into alignment with AQUILA engine mount attach points. (2) Assemble engine shock mounts. (3) Install engine mount bolts, washers, and nuts (refer to 71-20-00).

  • Page 643: Cowling - Maintenance

    AQUILA AT01-100/200 Power Plant MAINTENANCE MANUAL COWLING - MAINTENANCE 1. General The engine cowling is made from laminated fiberglass 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 644 AQUILA AT01-100/200 Power Plant MAINTENANCE MANUAL (5) Rotax 912: Install flexible air hose to induction air filter casing and secure using clamp. Rotax 914: Fasten induction air filter casing to lower cowl with Camloc quick-release fasteners. (6) Put upper cowl in position and secure to lower cowl and fuselage with Camloc quick-release fasteners.

  • Page 645: 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 646 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 647: Air Induction System - Maintenance

    AQUILA AT01-100/200 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 648 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 649: Air Induction System - Maintenance

    AQUILA AT01-100/200 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 650 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 651 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 74 IGNITION SYSTEM...
  • Page 652 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 653 AQUILA AT01-100/200 Ignition System MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page IGNITION SYSTEM - GENERAL ..............74-00-00 Introduction 74-00-00 General Description 74-00-00 IGNITION SYSTEM - MAINTENANCE............74-00-00 General 74-00-00 SMD-Electronic Module Removal/Installation 74-00-00 Double Ignition Coil Assembly Removal/Installation 74-00-00...
  • Page 654 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 655: Ignition System - General

    AQUILA AT01-100/200 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 656 AQUILA AT01-100/200 Ignition System MAINTENANCE MANUAL IGNITION SYSTEM ignition circuit A ignition circuit B Ignition System Electrical Schematic Figure 1 Page 2 74-00-00 09.10.18...

  • Page 657: Ignition System - Maintenance

    AQUILA AT01-100/200 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 658: Spark Plug Removal/Installation

    AQUILA AT01-100/200 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 24-30-00). (6) Install engine cowling (refer to 71-10-00). 4. Spark Plug Removal/Installation Remove Spark Plug (1) Remove engine cowling (refer to 71-10-00).
  • Page 659 AQUILA AT01-100/200 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 660 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 661 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 75 COOLING SYSTEM...
  • Page 662 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 663 AQUILA AT01-100/200 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 664 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 665: Cooling System - General

    AQUILA AT01-100/200 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 666 AQUILA AT01-100/200 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 667: Cooling System - Maintenance

    AQUILA AT01-100/200 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 668: Expansion Tank Removal/Installation

    AQUILA AT01-100/200 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) Install engine cowling (refer to 71-10-00).
  • Page 669 AQUILA AT01-100/200 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 28.02.20...
  • Page 670 AQUILA AT01-100/200 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 28.02.20...
  • Page 671 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 76 ENGINE CONTROLS...
  • Page 672 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 673 AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectifity ENGINE CONTROLS - GENERAL ............76-00-00 Introduction 76-00-00 General Description 76-00-00 ENGINE CONTROLS - MAINTENANCE ..........76-00-00 General 76-00-00 Control Quadrant Disassembly/Assembly 76-00-00 Throttle Control Cable Removal/Installation...
  • Page 674 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 675: Engine Controls - General

    AQUILA AT01-100/200 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 676 AQUILA AT01-100/200 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 677: Engine Controls - Maintenance

    AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL ENGINE CONTROLS - MAINTENANCE 1. General For propeller speed control adjustment/test procedures, refer to 61-20-00. For carburetor heat control adjustment/test procedures, refer to 71-60-00. 2. Control Quadrant Disassembly/Assembly For control quadrant disassembly/assembly, refer to figure 201.
  • Page 678 AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL rear stop adjusting bolts Detail- Control Quadrant Assembly Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 912S engine 76-00-00 28.02.20...
  • Page 679 AQUILA AT01-100/200 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 28.02.20...

  • Page 680: Governor Control Cable Removal/Installation

    AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL 4. Governor Control Cable Removal/Installation Remove Governor Control Cable (1) Remove engine cowling (refer to 71-10-00). (2) Remove access panels 211 FT, 211 FB, 211 EC (refer to 25-12-00) in the cabin. (3) Disconnect governor control cable from governor control arm.
  • Page 681 AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL Detail- Detail- Choke Control Assembly Figure 202 Page 204 76-00-00 28.02.20...

  • Page 682: Throttle Control Adjustment/Test

    AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL 6. Throttle Control Adjustment/Test Idle Speed Adjustment 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 683: Turbo Charger Control

    AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL Throttle Inspection/Check (1) Check proper Bowden cable routing to prevent influence to carburetor actuation caused by any movement of engine or other controls, thus possibly falsifying precise idle speed setting and synchronization. (2) Inspect the throttle control cable attachment to carburetors throttle control arm and to the control quadrant.
  • Page 684 AQUILA AT01-100/200 Engine Controls MAINTENANCE MANUAL Remove Wastegate Servo Motor Ensure electrical power is OFF. (2) Disconnect battery (refer to 24-30-00). (3) Remove access panel 211AB (refer to 25-12-00) from front cockpit floor. (4) Remove wastegate control cable from servo motor (refer to “...
  • Page 685 AQUILA AT01-100/200 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 686 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 687 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 77 ENGINE INDICATING...
  • Page 688 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 689 AQUILA AT01-100/200 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...........77-10-00 Analog General 77-10-00 Analog Tachometer Removal/Installation 77-10-00 Analog Manifold Pressure Gauge Removal/Installation...
  • Page 690 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 691: Engine Indicating - General

    AQUILA AT01-100/200 Engine Indicating MAINTENANCE MANUAL ENGINE INDICATING - GENERAL 1. Introduction This chapter describes those systems and components which indicate engine operation. Refer to 28-00-00 for further information on fuel pressure, fuel quantity and fuel flow measuring systems. Refer to 79-00-00 for further information on oil pressure and oil temperature measuring systems.
  • Page 692 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 693: Power Indication - Maintenance

    AQUILA AT01-100/200 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 694 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 695: Power Indication - Maintenance

    AQUILA AT01-100/200 Engine Indicating MAINTENANCE MANUAL POWER INDICATION - MAINTENANCE 1. General Propeller speed indication is included in the Garmin G3X Touch system. Propeller/engine speed is measured by a sensor mounted on the internal alternator casing at the rear end of the engine and electrically connected to the GEA 24 engine interface at the back of the instrument panel.
  • Page 696 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 697: Power Indication - Maintenance

    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 Transducer Removal/Installation Remove Manifold Pressure Transducer (1) Ensure electrical power to aircraft is OFF.
  • Page 698 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 699: Temperature Indication - Maintenance

    AQUILA AT01-100/200 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 700 AQUILA AT01-100/200 Engine Indicating MAINTENANCE MANUAL 4. Carburetor Temperature Sensor Removal/Installation (optional) Remove Carburetor Temperature Sensor (1) Ensure electrical power to aircraft is OFF. (2) Remove engine cowling (refer to 71-10-00). (3) Disconnect battery (refer to 24-30-00). (4) Disconnect electrical lead to sensor.

  • Page 701: Carburetor Temperature Sensor Removal/Installation

    AQUILA AT01-100/200 Engine Indicating MAINTENANCE MANUAL TEMPERATURE INDICATION - MAINTENANCE 1. General Cylinder head temperature indication is included in the MVP-50 engine monitoring system / G3X Touch system. Temperature is measured by a type K thermocouple electrically connected to the engine data converter (MVP-50) / GEA 24 engine interface (G3X).
  • Page 702 AQUILA AT01-100/200 Engine Indicating MAINTENANCE MANUAL Install Carburetor Temperature Sensor (1) Install sensor head and new copper sealing washer. Secure with Loctite (medium strength). CAUTION: TIGHTEN THE SENSOR HEAD CAREFULLY TO AVOID STRIPPING THE THREAD. (2) Connect electrical connector to sensor.

  • Page 703: Engine Monitoring System - Maintenance

    AQUILA AT01-100/200 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 transducers and - the wiring and extension cables.

  • Page 704: 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 705 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 78 EXHAUST...
  • Page 706 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 707 AQUILA AT01-100/200 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 ............78-00-00 Rotax 912S General 78-00-00 Rotax 912S Exhaust System Removal/Installation 78-00-00 Rotax 912S...
  • Page 708 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 709: Exhaust System - General

    AQUILA AT01-100/200 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 710 AQUILA AT01-100/200 Cooling System MAINTENANCE MANUAL...

  • Page 711: Exhaust System - Maintenance

    AQUILA AT01-100/200 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 712: Main Muffler Inspection/Check

    AQUILA AT01-100/200 Exhaust MAINTENANCE MANUAL 3. Main Muffler Inspection/Check WARNING: FAILURE TO INSPECT THE MAIN MUFFLER FOR LEAKS COULD RESULT IN CARBON MONOXIDE ENTERING THE CABIN AREA, LEADING TO SERIOUS INJURY OR DEATH. For main muffler inspection/check time intervals refer to 05-10-00.
  • Page 713 AQUILA AT01-100/200 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 engine 78-00-00 28.02.20...
  • Page 714 AQUILA AT01-100/200 Exhaust MAINTENANCE MANUAL Detail- heat shroud support bracket main muffler Detail- tail pipe Detail- Heat Shroud / Tail Pipe Installation Figure 202 EFFECTIVITY Page 204 Aircraft equipped with Rotax 912S engine 78-00-00 28.02.20...

  • Page 715: Exhaust System - Maintenance

    AQUILA AT01-100/200 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 716 AQUILA AT01-100/200 Exhaust MAINTENANCE MANUAL Install Tail Pipe (1) Slide exhaust bend on socket of main muffler. (2) Align exhaust bend to support bracket on engine mount and secure with clamp. (3) Apply heat resistant anti seize paste (e.g. Loctite LB 8150) to ball joint.
  • Page 717 AQUILA AT01-100/200 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 78-00-00 28.02.20...
  • Page 718 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 719 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 79...
  • Page 720 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 721 AQUILA AT01-100/200 MAINTENANCE MANUAL TABLE OF CONTENTS Chapter Section Title Subject Page Effectivity OIL - GENERAL ....................79-00-00 Rotax 912S Introduction 79-00-00 Rotax 912S General Description 79-00-00 Rotax 912S OIL - GENERAL ....................79-00-00 Rotax 914F Introduction 79-00-00 Rotax 914F General Description...
  • Page 722 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 723: Oil - General

    AQUILA AT01-100/200 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 724 AQUILA AT01-100/200 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 725: Oil - General

    AQUILA AT01-100/200 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 726 AQUILA AT01-100/200 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 727: Oil Tank - Maintenance

    AQUILA AT01-100/200 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 728 AQUILA AT01-100/200 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 28.02.20...

  • Page 729: Oil Cooler - Maintenance

    AQUILA AT01-100/200 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) or in the lower right part of the lower engine cowling below / behind the turbocharger and behind an air duct (Rotax 914F).
  • Page 730 AQUILA AT01-100/200 MAINTENANCE MANUAL Detail- heat protection sleeve rubbing 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 28.02.20...
  • Page 731 AQUILA AT01-100/200 MAINTENANCE MANUAL Detail- Detail- Oil Cooler Installation Figure 201 EFFECTIVITY Page 202 Aircraft equipped with Rotax 914F engine 79-20-00 28.02.20...
  • Page 732 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 733: Oil Pressure Indication - Maintenance

    AQUILA AT01-100/200 MAINTENANCE MANUAL OIL PRESSURE INDICATION - MAINTENANCE 1. General The oil pressure indicating system consists of an oil pressure transducer, 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 734 AQUILA AT01-100/200 MAINTENANCE MANUAL Install Oil Pressure Transducer (1) Install new gasket and transducer to engine. Torque to 15 Nm (135 in.lbs). (2) Connect electrical connector to transducer. (3) Reconnect battery (refer to 24-30-00). (4) Install engine cowling (refer to 71-10-00).

  • Page 735: Oil Pressure Indication - Maintenance

    AQUILA AT01-100/200 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 transducer electrically connected to the engine data converter (EDC). Engine oil pressure is measured on the right side of the oil pump casing.
  • Page 736 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 737: Oil Temperature Indication - Maintenance

    AQUILA AT01-100/200 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 738 AQUILA AT01-100/200 MAINTENANCE MANUAL...

  • Page 739: Oil Temperature Indication - Maintenance

    AQUILA AT01-100/200 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). Engine oil temperature is measured in the oil filter / oil pump area.
  • Page 740 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 741 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 80 STARTING...
  • Page 742 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 743 AQUILA AT01-100/200 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................80-11-00 General 80-11-00 Starter Removal/Installation 80-11-00 Page 1 80 - TOC 30.04.13...
  • Page 744 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 745 AQUILA AT01-100/200 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 746 AQUILA AT01-100/200 Cooling System MAINTENANCE MANUAL...
  • Page 747 AQUILA AT01-100/200 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 748 AQUILA AT01-100/200 Cooling System MAINTENANCE MANUAL...
  • Page 749 AQUILA AT01-100/200 MAINTENANCE MANUAL CHAPTER 91 CHARTS AND DIAGRAMS...
  • Page 750 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 751 AQUILA AT01-100/200 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 752 AQUILA AT01-100/200 MAINTENANCE MANUAL...
  • Page 753 AQUILA AT01-100/200 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 754 AQUILA AT01-100/200 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 755 AQUILA AT01-100/200 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 756 AQUILA AT01-100/200 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 757 AQUILA AT01-100/200 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 758 AQUILA AT01-100/200 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 759 AQUILA AT01-100/200 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 760 AQUILA AT01-100/200 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 761 AQUILA AT01-100/200 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 762 AQUILA AT01-100/200 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 763 AQUILA AT01-100/200 Charts and Diagrams MAINTENANCE MANUAL Circuit Breakers and Switches Figure 7 (2) Page 11 91-00-00 24.10.13...
  • Page 764 AQUILA AT01-100/200 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 765 AQUILA AT01-100/200 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 766 AQUILA AT01-100/200 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 767 AQUILA AT01-100/200 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 768 AQUILA AT01-100/200 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 769 AQUILA AT01-100/200 Charts and Diagrams MAINTENANCE MANUAL landing light NAV light RH Lights Figure 12 (2) Page 17 91-00-00 24.10.13...
  • Page 770 AQUILA AT01-100/200 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 771 AQUILA AT01-100/200 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 772 AQUILA AT01-100/200 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 773 AQUILA AT01-100/200 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 774 AQUILA AT01-100/200 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 775 AQUILA AT01-100/200 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 776 AQUILA AT01-100/200 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 777 AQUILA AT01-100/200 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 778 AQUILA AT01-100/200 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 779 AQUILA AT01-100/200 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 780 AQUILA AT01-100/200 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 781 AQUILA AT01-100/200 Charts and Diagrams MAINTENANCE MANUAL Headset Console Figure 20 Page 29 91-00-00 24.10.13...
  • Page 782 AQUILA AT01-100/200 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 783 AQUILA AT01-100/200 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 784 AQUILA AT01-100/200 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 785 AQUILA AT01-100/200 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 786 AQUILA AT01-100/200 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 787 AQUILA AT01-100/200 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 788 AQUILA AT01-100/200 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 789 AQUILA AT01-100/200 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 790 AQUILA AT01-100/200 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 791 AQUILA AT01-100/200 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 792 AQUILA AT01-100/200 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...

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