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Aquila AT01-100 Maintenance Manual

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Download this manual See also: Pilot Operating Handbook, Operating Handbook
A
Cha/Sec/Sub
Title
TABLE OF CONTENTS
INTRODUCTION
LIST OF EFFECTIVE CHAPTERS
04
AIRWORTHINESS LIMITATIONS
04-00-00
Airworthiness Limitations - General
05
TIME LIMITS / MAINTENANCE CHECKS
05-00-00
Time Limits / Maintenance Checks - General
05-10-00
Component Time Limits
05-20-00
Scheduled Maintenance Checks
05-30-00
Daily Inspections
05-50-00
Unscheduled Maintenance Checks
06
DIMENSIONS AND AREAS
06-00-00
Dimensions and Areas - General
06-10-00
Aircraft Dimensions and Areas
06-20-00
Aircraft Zoning
06-30-00
Access/Inspection Plates
07
LIFTING AND SHORING
07-00-00
Lifting and Shoring - General
07-10-00
Jacking
08
LEVELING AND WEIGHING
08-00-00
Leveling and Weighing - General
08-10-00
Weighing
08-20-00
Leveling
09
TOWING AND TAXIING
09-00-00
Towing and Taxiing - General
09-10-00
Towing
09-20-00
Taxiing
10
PARKING, MOORING, STORAGE AND RETURN TO SERVICE
10-00-00
Parking, Mooring, Storage and Return to Service - General
10-10-00
Parking
10-11-00
Storage
10-20-00
Mooring
10-30-00
Return to Service
10-40-00
Transport
AQUILA AT01-100
MAINTENANCE MANUAL
TABLE OF CONTENTS
Table of Contents
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Page 1
TOC
29.02.16

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  • Page 1 AQUILA AT01-100 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 2 AQUILA AT01-100 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 201-206 11-30-00 Interior Placards and Markings 201-208 SERVICING 12-00-00 Servicing - General...
  • Page 3 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 24-30-00 Battery - Maintenance 24-40-00 External Power - Maintenance 201-203 24-60-00 Electrical Load Distribution - Description 24-61-00 Circuit Breaker - Maintenance 201-202 24-97-00 Electrical System Wiring - Maintenance...
  • Page 4 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 32-20-00 Nose Landing Gear - Description 32-20-00 Nose Landing Gear - Maintenance 201-203 32-40-00 Wheels and Brakes - Description 32-40-00 Wheels and Brakes - Maintenance 201-221/208...
  • Page 5 AQUILA AT01-100 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 201-205 57-50-00 Control Surfaces - Maintenance...
  • Page 6 AQUILA AT01-100 Table of Contents MAINTENANCE MANUAL TABLE OF CONTENTS (Cont.) Cha/Sec/Sub Title Pages 79-00-00 Oil - General 79-10-00 Oil Tank - Maintenance 201-202 79-20-00 Oil Cooler - Maintenance 201-202 79-31-00 Oil Pressure Indication - Maintenance 201/201 79-33-00 Oil Temperature Indication - Maintenance...
  • Page 7 AQUILA AT01-100 Record of Revisions MAINTENANCE MANUAL RECORD OF REVISIONS Date Revision Date of Date Revision Date of Number Inserted Revision Inserted Number Revision 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...
  • Page 8 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 9 AQUILA AT01-100 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 10 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 11 AQUILA AT01-100 Highlights of Revisions MAINTENANCE MANUAL HIGHLIGHTS OF REVISIONS Revision Date of Revision Date of Reason for Revision Reason for Revision Number Revision Number Revision A.01 30.04.13 Initial issue. A.02 26.08.13 SB-AT01-027 A.03 24.10.13 FAA validation (airworthiness limitations, wire routing diagrams);...
  • Page 12 AQUILA AT01-100 MAINTENANCE MANUAL...
  • Page 13 AQUILA AT01-100 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* GENERAL Table of Contents 29.02.16 Introduction 30.04.13 Airworthiness Limitations .03.15 Time Limits / Maintenance Checks 20.08.15 Dimensions and Areas 30.04.13 Lifting & Shoring 30.04.13 Leveling and Weighing 30.04.13...
  • Page 14 AQUILA AT01-100 List of Chapters MAINTENANCE MANUAL LIST OF EFFECTIVE CHAPTERS Chapter Title Date* POWER PLANT Power Plant 30.04.13 Ignition 30.04.13 Cooling System 30.04.13 Engine Controls 0.08.15 Engine Indicating 30.04.13 Exhaust 30.04.13 30.04.13 Starting 30.04.13 Charts and Wiring Diagrams 24.10.13 * The date refers to the issue / revision date of the respective chapter.
  • Page 15 AQUILA AT01-100 MAINTENANCE MANUAL CHAPTER 51 STRUCTURES...
  • Page 16 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 17: Table Of Contents

    AQUILA AT01-100 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 18 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 19: 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 20: 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 21: Composite Damage Investigation

    AQUILA AT01-100 Structures MAINTENANCE MANUAL COMPOSITE DAMAGE INVESTIGATION General This section contains maintenance information and procedures such as investigation and damage classification applicable to fiber laminate structure components. 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 22: Damage Classification 51-10-00 202

    AQUILA AT01-100 Structures MAINTENANCE MANUAL 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 23 AQUILA AT01-100 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 24 AQUILA AT01-100 MAINTENANCE MANUAL...

  • Page 25: Composite Repair

    AQUILA AT01-100 Structures MAINTENANCE MANUAL COMPOSITE REPAIR 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 26 AQUILA AT01-100 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 27 AQUILA AT01-100 Structures MAINTENANCE MANUAL 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 28 AQUILA AT01-100 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 Material Data Sheet...
  • Page 29 AQUILA AT01-100 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (1) Page 205 51-20-00 29.02.16...
  • Page 30 AQUILA AT01-100 Structures MAINTENANCE MANUAL Fuselage Ply Lay-Up Figure 202 (2) Page 206 51-20-00 29.02.16...
  • Page 31 AQUILA AT01-100 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 32 AQUILA AT01-100 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 33 AQUILA AT01-100 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 34 AQUILA AT01-100 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 35 AQUILA AT01-100 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 36 AQUILA AT01-100 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 37 AQUILA AT01-100 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 38 AQUILA AT01-100 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 39 AQUILA AT01-100 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 40 AQUILA AT01-100 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 41 (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 42 (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 43 (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 44 (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 45 (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 46 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. Pre-cure the repair at least 24 hours at 20°C (68°F) to 25°C (77°F).
  • Page 47 AQUILA AT01-100 Structures MAINTENANCE MANUAL 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 48 AQUILA AT01-100 Structures MAINTENANCE MANUAL...

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