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Trixy Aviation G 4-2 Maintenance Manual

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Maintenance manual

Trixy Aviation
Series
G 4-2
1
Maintenance manual G 4-2
Revision 05A – 03.05.2017
Doc. No.: TA-M-D-002-EN

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Summary of Contents for Trixy Aviation G 4-2

  • Page 1: Maintenance Manual

    Maintenance manual Trixy Aviation Series G 4-2 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 2: Gyrocopter G

    The extent and state of revision of this manual may be obtained from the index and the revision index. Maintenance for the gyrocopter G 4-2 is to be performed ONLY by an authorized persons and/or aviation workshop in accordance with the instructions and intervals given in this manual as well as the manuals for engine and propeller.
  • Page 3 REVISIONS TO THIS MANUAL Description Page Date Name Previous manual Rev. 3.0 03.05.17 R. Farrag Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 4: Table Of Contents

    The fuel system Electrical system The hydraulic brake system PERIODIC PREVENTIVE MAINTENANCE Introduction Maintenance after the first 25 hours 50 hour interval maintenance 100 hour interval maintenance 500 hour interval maintenance Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 5: Revision 05A – 03.05.2017 Doc. No.: Ta-M-D-002-En

    Recommended overhalls MAINTENANCE SERTIFICATES DAMAGE OR ACCIDENT REPORTS CERTIFICATES OF REPAIR AFTER DAMAGE MODIFICATION CERTIFICATES Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 6: General Remarks

    Please use the forms at the end of this manual to report such defects. All warranties provided by the manufacturer of the gyrocopter are void, in the event that one or more of the instructions in this manual are ignored. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 7: Certification And Registration

    All rules and regulations contained in these documents must be obeyed. The G 4-2 is constructed, manufactured and tested according to the construction regulations for ultra-light gyrocopters (BUT 2001) and Nfl II 13/09 dated 12.02.2009 and is registered under the identification number 61218 by the responsible German authority (DAeC).

  • Page 8: Description

    • Rudder and stabilizers made from CFC The series G 4-2 includes 2 models: Liberty and Princess. Liberty is an entry-level model, which is designed to basically operate with an open cabin. However, this model can be converted with an optional kit to a closed version.

  • Page 9: Side View, Top View And Front View

    1.6 Side view, top view and front view (2 models) Note: The three views are not to scale! The model Liberty Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 10 Note: The three views are not to scale! The model Princess Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 11 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 12: Components

    2 COMPONENTS 2.1 Introduction The components used in the gyrocopter series G 4-2 are illustrated and documented in this section of the maintenance manual. Bolts and nuts are to be tightened and inspected in accordance with the data provided in this manual and the tightening torque in the corresponding tables is to be used as a reference.

  • Page 13: Frame

    Cracks and damages to the frame are to be reported to the manufacturer of the gyrocopter with no delay. Note: All warranties are void in case that the instructions in this manual are not carefully followed. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 14 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 15: Rotor

    Note: All warranties are void in case that the instructions in this manual are not carefully followed. Rotor bridge for Rotor head type KK-1 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 16 Tightening torque Hexagon bolt M10x90 8.8 40 Nm Hexagon bolt M10x70 8.8 40 Nm Self-locking Hexagon nut M10 ISO 7042 Washer 10,5 DIN 125-B 25-109 Hexagon bolts 40 Nm Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 17: Rotor Head

    2.4 Rotor head (2 types) 2 Rotor head types (KK-1 and TS-1) are certified for the series G 4-2: Type KK-1 is a tilt head design. It is designed and manufactured by Trixy Aviation. It is made of high quality materials and has passed all tests required under the German rules and specifications for type certification of ultra-light gyrocopters.
  • Page 18 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 19 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 20 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 21 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 22 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 23 Self-locking Hexagon nut M6 ISO 7042 8-26 Washer 8,4 DIN 125-B 8-27 Washer 6,4 DIN 125-B 8-28 STARTER ACTUATOR 8-29 Shaft 8-30 Spring pin 6x26 DIN 1481 8-31 Spring pin 3,5x26 DIN 1481 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 24 Type TS-1 is a swash plate controlled head design. It is designed and manufactured by Trixy Aviation. It is made of high quality materials and has passed all tests required under the German rules and specifications for type certification of ultra-light gyrocopters. It is made of aircraft aluminium and stainless steel.
  • Page 25 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 26 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 27 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 28 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 29 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 30 Short cylinder head bolt with internal hexagon 10Nm 25-77 Cylinder head bolt with internal hexagon 10Nm 25-78 Cylinder head bolt with internal hexagon 10Nm 25-82 Allen screw 25-91 Allen screw 10Nm 25-92 Allen screw 25Nm Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 31: Rotor Controls

    2.5 Rotor controls The rotor control system is designed and manufactured of high quality materials by Trixy Aviation. It passed all tests required under the German rules and specifications for type certification of ultra-light gyrocopters. The bolts, bushings and axes are of special design and must not be replaced by standard parts.
  • Page 32 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 33 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 34 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 35 Washer 8,4 DIN 125-B 9-13 Adjusting washer DIN 988 - 8 x 14 x 1 9-14 Conical bush 2 9-15 Washer 6,4 DIN 125-B 9-16 Adjusting washer M8x50 10.9 25 Nm Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 36: Prerotator System

    2.6 Pre-rotator system The pre-rotator system is designed and manufactured of high quality materials by Trixy Aviation. The belt must be periodically sprayed with silicon spray. Exchanging the clutch belt requires removing the propeller from the mounting flange (pulley). The main pre-rotator gear in the rotor head and the Bendix-gear in the pre-rotator system must be greased with neutral grease in all scheduled maintenance works.
  • Page 37 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 38 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 39 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 40 10 Nm 10-40 Wuerth Linsenschraube mit Scheibe 10 Nm 10-41 Kurze Zylinderschraube mit Innensechskant 10 Nm 10-42 Sechskantmutter 10-43 Federscheibe 10-47 Zylinderschraube mit Innensechskant 10 Nm 10-34 Passschraube 10 Nm Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 41: Propeller

    500 h To be exchanged: 1000 h Type 4: EXCALIBUR Manufacturer: E-Props www. e-props.fr No. of blades: Diameter: 1720 mm Blade material: Adjustment: Ground adjustable. To be exchanged: 800 h Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 42 Cracks and damages in the propeller are to be reported to the manufacturer of the gyrocopter with no delay. Note: All warranties are void in case that the instructions in this manual are not carefully followed. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 43 Type 1: Ground adjustable propeller. Contact DUC or Trixy Aviation for more details. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 44 Type 2: In flight adjustable propeller. Contact Neuform or Trixy Aviation for more details. Pos. Description Qnt. Tightening Torque Cylinder head bolt with internal hexagon M8x125 11-1 25 Nm DIN 912 11-2 Self-locking Hexagon nut M8 ISO 7042 11-3 toothed washer 8,4...

  • Page 45: Nose Wheel And Steering

    2.8 Nose wheel and steering The nose wheel suspension and ist structure are designed and manufactured by Trixy Aviation of high quality materials. It passed all load tests required by the German rules and specifications for the certification of ultra-light gyrocopters. However, continuous stress during taxiing, take-offs and landings on rough terrain may cause damage to the nose wheel structure.
  • Page 46 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 47 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 48 12-4 Split pin 3,2x32 DIN 94 12-5 Washer 17 DIN 125-B 12-6 Tower nut M16 DIN 979 12-7 Washer 8,4 DIN 125-B 12-8 Self-locking Hexagon nut M8 ISO 7042 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 49: Main Gear

    Note: All warranties are void in case that the instructions in this manual are not carefully followed. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 50 Cylinder head screw with internal hexagon 13-3 10 Nm M6x40 DIN 912 13-4 Washer 8,4 DIN 125-B 13-5 Self-locking Hexagon nut M8 ISO 7042 13-6 Washer 6,4 DIN 125-B Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 51 The main wheels and the brakes are high quality products of Beringer Aero SA. The brake hydraulic system is designed and manufactured by Trixy Aviation. Use original parts only from the manufacturer to insure flight safety. See also main gear in the previous chapter and brake system in further in this manual.

  • Page 52: Empennage

    Pos. Description Qnt. Tightening Torque 15-1 Internal hexagon bolts with flange M6x16 10 Nm 15-2 Big Washer 6,4 DIN 9021 15-3 Internal hexagon bolts with flange M5x16 6 Nm Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 53: Rudder Controls

    2.12 Rudder controls The rudder and ist control system is designed and manufactured by Trixy Aviation. The rudder is made of CFC in sandwich construction under vacuum. It is controlled by bowden wires along with the nose wheel. The rudder control system is to be overhauled:...
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  • Page 55 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 56 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 57 16-7 Internal hexagon bolts with flange M6x16 10 Nm 16-8 Pin 6x15 16-9 Cotter pin 1,6x12 DIN 94 16-10 Internal hexagon bolts with flange M6x30 10 Nm 16-11 Bush Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 58: Dashboard

    7. Main switch 8. Mag 1 (ignition circuit switch 1) 9. Mag 2 (ignition circuit switch 2) 10. Auxiliary fuel pump (optional in type G 4-2 R with Rotax 912 ULS) 11. Avionics Switch 12. Landing light switch (optional) 13. Navigation light switch (optional) 14.
  • Page 59 20. ELT remote control (optional) 21. Booster reset switch (Rotax 914 UL engine only) 22. Booster warning lights (Rotax 914 UL engine only) 23. Controller for constant speed propeller (optional) Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 60: Engine

    50° C / max. 130° C Oil temperature: Fuel quality: EN228 Super (min ROZ 95) or EN228 Super plus (min ROZ 95) Alternative fuel (*): AVGAS 100 LL (ASTM D910) Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 61 (last valid edition) by workshops and persons, who are authorized by Rotax. Note: All warranties are void in case that the instructions in this manual are not carefully followed. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 62: Systems

    3 SYSTEMS 3.1 Introduction The systems of the gyrocopters G 4-2 are described and illustrated in this chapter of the maintenance manual. Construction drawings and material lists are not included in this manual. It is considered that authorized persons and/or authorized aircraft repair and maintenance workshops are to perform maintenance on the gyrocopter.

  • Page 63: Engine Oil Circuit

    The pilot in command must insure correct oil pressure and oil temperature above 50 °C before applying full power. The maximum allowed oil temperature is 130 °C. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 64: Engine Coolant Circuit

    The circuit must be check for leaks. All hoses must be in good conditions 3.4 Engine ignition circuits More information about the ignition circuits are found in Rotax manual. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 65: The Fuel System

    914 by an electrical pump fixed on the fire wall in a lower level than the tank. Both G 4-2 may be optionally equipped with an electric auxiliary fuel pump, which is then fixed on the lower part of the fire wall.
  • Page 66 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 67 It can, however, optionally be equipped with an auxiliary fuel pump and/or a back-up battery system. The Types G 4-2 RT, G 4-2 TI and G 4-2 TIS are equipped with 2 electrical fuel pumps, a back-up battery and a battery management system (BMS) in the standard configuration.
  • Page 68 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
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  • Page 91: The Hydraulic Brake System

    However, los of fluid may mean leaks in the system. This must be fixed to avoid brake failure. It is recommended to exchange the hydraulic fluid in the system every 500 h. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 92 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 93 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

  • Page 94: Periodic Preventive Maintenance

    3.1 Introduction This chapter explains the periodic preventive maintenance required and highly recommended to insure flight safety. Trixy Aviation Insists on professional and timely maintenance. The information in this chapter for maintenance intervals must be adhered to; otherwise all manufacturer warranties are void.

  • Page 95: Maintenance After The First 25 Hours

    26. Inspect the rudder and its control system for function 27. Adjust the rudder control Bowden if needed 28. Inspect the attachment of the canopy to the cabin and the locks Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 96 27. Inspect landing light 28. Inspect defroster fan for function 29. Inspect navigation lights and strobe (if installed) 30. Inspect ELT for function (if installed) Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 97 13. Inspect electric auxiliary fuel pump function (if installed) 14. Inspect cabin heating system for function (if installed) 15. Inspect oil cooler and clean thoroughly 16. Inspect coolant heat exchanger assembly and clean thoroughly Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 98 26. Disassemble the main wheels and inspect the brake pads 27. Exchange the hydraulic fluid in the system and insure the system is properly vented. 28. Inspect fuel tanks (exchange after 2000 h), exchange fuel filters Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 99 1500 hours Frame Inspection hours Frame Exchange 2000 hours DUC-Propeller Overhaul hours DUC-Propeller Exchange hours Neuform-Propeller Overhaul hours Neuform-Propeller Exchange 1000 hours Hydraulic fluid Exchange hours Engine Exchange 2000 hours Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 100 Note: All warranties are void in case that the instructions in this manual are not carefully followed. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 101 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 102 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 103 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 104 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 105 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 106 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 107 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 108 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 109 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 110 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 111 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 112 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 113 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 114 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 115 Gyrocopter in accordance with the instructions in this manual. Remarks: The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 116 Location: ______________ Datum: __________________ Signature: Please send this report to: and to: DAeC Trixy Aviation GmbH Hermann-Blenk-Strasse 28 Eschbuehel 10 F D-38108 Braunschweig A-6850 Dornbirn Germany Austria Telefax: +49 531 23540-66 info@trixyaviation.com Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 117 Location: ______________ Datum: __________________ Signature: Please send this report to: and to: DAeC Trixy Aviation GmbH Hermann-Blenk-Strasse 28 Eschbuehel 10 F D-38108 Braunschweig A-6850 Dornbirn Germany Austria Telefax: +49 531 23540-66 info@trixyaviation.com Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 118 Location: ______________ Datum: __________________ Signature: Please send this report to: and to: DAeC Trixy Aviation GmbH Hermann-Blenk-Strasse 28 Eschbuehel 10 F D-38108 Braunschweig A-6850 Dornbirn Germany Austria Telefax: +49 531 23540-66 info@trixyaviation.com Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 119 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 120 The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 121 The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 122 The gyrocopter is airworthy and is returned to service. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 123 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 124 ________ of the manual. The gyrocopter is airworthy and was returned to cervice. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 125 ________ of the manual. The gyrocopter is airworthy and was returned to cervice. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 126 ________ of the manual. The gyrocopter is airworthy and was returned to cervice. Name of authorized person: ________________________ Signature: Date of certificate: ____________________ Stamp (if available): Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 127 Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...
  • Page 128 The content of this manual, (including text, pictures and drawings) is not to copy without the written permission of Trixy Aviation GmbH. Maintenance manual G 4-2 Revision 05A – 03.05.2017 Doc. No.: TA-M-D-002-EN...

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