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Maintenance manual G 4-2 Revision 05A

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03.05.2017 Doc. No.: TA-M-D-002-EN

Содержание G 4-2

Страница 1: ...Maintenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 1 Maintenance manual Trixy Aviation Series G 4 2 ...

Страница 2: ...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 This manual does not substitute the education of an aviation technician or the authorization of an aviation maintenance workshop IT is to be used i...

Страница 3: ...Maintenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 3 REVISIONS TO THIS MANUAL No Description Page Date Name 01 Previous manual Rev 3 0 All 03 05 17 R Farrag ...

Страница 4: ...m 36 2 7 Propeller 41 2 8 Nose wheel and steering 45 2 9 Main gear 49 2 10 Main wheels and breaks 51 2 11 Empennage 52 2 12 Rudder controls 53 2 13 Dashboard 58 2 14 Engine 60 3 SYSTEMS 62 3 1 Introduction 62 3 2 Engine oil circuit 63 3 3 Engine coolant circuit 64 3 4 Engine ignition system 64 3 5 The fuel system 65 3 6 Electrical system 67 3 7 The hydraulic brake system 91 3 PERIODIC PREVENTIVE M...

Страница 5: ... G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 5 4 6 Recommended overhalls 99 5 MAINTENANCE SERTIFICATES 100 6 DAMAGE OR ACCIDENT REPORTS 116 7 CERTIFICATES OF REPAIR AFTER DAMAGE 120 8 MODIFICATION CERTIFICATES 124 ...

Страница 6: ...cumented by an authorized inspector DAeC as a German authority is currently overlooking these regulations and must be officially informed about annual inspections Regulations in other countries must be taken in consideration in case that the gyrocopter is registered in countries other than Germany The warranty provided by the manufacturer of the gyrocopter is only valid when maintenance is perform...

Страница 7: ...tification and Registration The statutory basis for the operation of an ultra light gyrocopter ULG is regulated in air traffic laws Details are to be obtained from associated documents 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 ...

Страница 8: ...eering via push rods Rudder steering via steel wires 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 Princess is a top model which is designed to basically operate with a closed cabin This...

Страница 9: ...Maintenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 9 Note The three views are not to scale 1 6 Side view top view and front view 2 models The model Liberty ...

Страница 10: ...Maintenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 10 Note The three views are not to scale The model Princess ...

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Страница 12: ...ction 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 In doubt the maintenance technician or the aviation workshop performing the maintenanc...

Страница 13: ...ngine mounts 2 2 Frame The frame is the structure carrying the gyrocopter and connecting all its components together It is made of a special stainless steel and welded under inert gas protection against corrosion It is tested and passed the load requirements in BUT the German specifications for type certification of ultra light gyrocopters Such high loads never occur in normal flight conditions Ho...

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Страница 15: ... manufacturer of the gyrocopter with no delay Note All warranties are void in case that the instructions in this manual are not carefully followed Warning The gyrocopter is not to be operated once cracks bends dents or any other damages are detected in the rotor system 2 3 Rotor 2 sizes Air foil NACA 8H12 Manufacturer Averso Aviation www averso info Rotor diameter 8 40 or 8 60 m Rotor circle area ...

Страница 16: ...D 002 EN 16 Pos Description Qnt Tightening torque 7 1 Hexagon bolt M10x90 8 8 4 40 Nm 7 2 Hexagon bolt M10x70 8 8 16 40 Nm 7 3 Self locking Hexagon nut M10 ISO 7042 20 7 4 Washer 10 5 DIN 125 B 36 25 109 Hexagon bolts 4 40 Nm Rotor bridge for Rotor head type TS 1 ...

Страница 17: ...efully followed Warning The gyrocopter is not to be operated once cracks bends dents or any other damages are detected in the 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 ru...

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Страница 23: ...r head bolt with internal hexagon M6x60 DIN 912 8 8 4 10 Nm 8 14 Fit bolt M6x60 10 9 3 10 Nm 8 15 Self locking Hexagon nut M8 ISO 7042 2 8 16 Self locking Hexagon nut M6 ISO 7042 9 8 17 Washer 8 4 DIN 125 B 4 8 18 Washer 6 4 DIN 125 B 9 8 19 Conical bushing 1 4 8 20 Cylinder head bolt with internal hexagon DIN 7991 M5 x10 4 8 21 Cylinder head bolt with internal hexagon M8x85 DIN 912 8 8 7 25 Nm 8 ...

Страница 24: ...tructions in this manual are not carefully followed Warning The gyrocopter is not to be operated once cracks bends dents or any other damages are detected in the rotor head 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 certi...

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Страница 30: ...linder head bolt with internal hexagon 4 10Nm 25 39 Short cylinder head bolt with internal hexagon 8 5Nm 25 40 Washer 8 25 41 Self locking Hexagon nut M10 ISO 7042 8 25 43 Fit bolt 2 25Nm 25 52 Fit bolt 2 25Nm 25 53 Cylinder head bolt with internal hexagon 4 10Nm 25 57 Safety ring 1 25 58 Allen screw 2 5Nm 25 63 Safety ring 1 25 64 Safety ring 1 25 110 Cylinder head bolt with internal hexagon 2 25...

Страница 31: ...y Note All warranties are void in case that the instructions in this manual are not carefully followed Warning The gyrocopter is not to be operated once cracks bends dents or any other damages are detected in the rotor control system 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 rul...

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Страница 35: ...justing washer M6x55 10 9 2 10 Nm 9 5 Self locking Hexagon nut M8 ISO 7042 2 9 6 Self locking Hexagon nut M6 ISO 7042 2 9 7 Washer 8 4 DIN 125 B 4 9 8 Conical bush 1 4 9 9 Fit bolt M8x50 10 9 2 25 Nm 9 10 Fit bolt M8x35 10 9 4 25 Nm 9 11 Self locking Hexagon nut M8 ISO 7042 6 9 12 Washer 8 4 DIN 125 B 4 9 13 Adjusting washer DIN 988 8 x 14 x 1 8 9 14 Conical bush 2 8 9 15 Washer 6 4 DIN 125 B 4 9 ...

Страница 36: ...ual are not carefully followed Warning The gyrocopter is not to be operated once cracks bends dents or any other damages are detected in the pre rotator system Removing and installing the propeller is to be performed by authorized persons only 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...

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Страница 40: ...380 1 25 Nm 10 13 Big Washer 8 4 DIN 9021 1 10 14 Big Washer 6 4 DIN 9021 2 10 15 Wuerth M5x12 4 10 Nm 10 16 Wuerth M5x16 2 10 Nm 10 17 Self locking Hexagon nut M8 ISO 7042 3 10 18 Cylinder head bolt with internal hexagon 2 10 Nm 10 19 Cylinder head screw with internal hexagon 1 10 Nm 10 20 Big Washer 6 4 DIN 9021 1 10 21 Washer 6 4 DIN 125 B 1 10 22 Cylinder head bolt with internal hexagon 3 25 N...

Страница 41: ...form www neuform composites de No of blades 3 Diameter 1700 mm Blade material CFC Adjustment In flight adjustable To be overhauled 500 h To be exchanged 1000 h Type 3 TXL3 V 70 R2 Manufacturer Neuform www neuform composites de No of blades 3 Diameter 1720 mm Blade material CFC Adjustment In flight adjustable To be overhauled 500 h To be exchanged 1000 h Type 4 EXCALIBUR Manufacturer E Props www e ...

Страница 42: ...d by the manufacturer of the propeller 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 Warning The gyrocopter is not to be operated once cracks or other damages are detected in the propeller Removing and installing the propeller is to be pe...

Страница 43: ...Maintenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 43 Type 1 Ground adjustable propeller Contact DUC or Trixy Aviation for more details ...

Страница 44: ...ription Qnt Tightening Torque 11 1 Cylinder head bolt with internal hexagon M8x125 DIN 912 6 25 Nm 11 2 Self locking Hexagon nut M8 ISO 7042 6 11 3 toothed washer 8 4 6 11 4 Washer 8 4 DIN 125 B 6 11 5 Indexing pin ø10x20 DIN 6325 LK75 3 11 6 Cylinder head bolt with internal hexagon M8x70 DIN 912 6 11 7 Washer 8 4 DIN 125 B 12 11 8 Self locking Hexagon nut M8 ISO 7042 6 ...

Страница 45: ...arefully followed 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 whee...

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Страница 48: ...rque 12 1 Cylinder head screw with internal hexagon M10x135 DIN 912 1 40 Nm 12 2 Self locking Hexagon nut M10 ISO 7042 1 12 3 Washer 10 5 DIN 125 B 2 12 4 Split pin 3 2x32 DIN 94 1 12 5 Washer 17 DIN 125 B 1 12 6 Tower nut M16 DIN 979 1 12 7 Washer 8 4 DIN 125 B 1 12 8 Self locking Hexagon nut M8 ISO 7042 1 ...

Страница 49: ...r of the gyrocopter with no delay Note All warranties are void in case that the instructions in this manual are not carefully followed 2 9 Main gear The main gear suspension is designed and manufactured by Trixy Aviation of GFC and CFC in sandwich construction under vacuum It passed all load tests required by the German rules and specifications for the certification of ultra light gyrocopters Howe...

Страница 50: ...e 13 1 Cylinder head screw with internal hexagon M8x90 DIN 912 4 25 Nm 13 2 Cylinder head screw with internal hexagon M6x45 DIN 912 6 10 Nm 13 3 Cylinder head screw with internal hexagon M6x40 DIN 912 10 10 Nm 13 4 Washer 8 4 DIN 125 B 8 13 5 Self locking Hexagon nut M8 ISO 7042 4 13 6 Washer 6 4 DIN 125 B 16 ...

Страница 51: ... warranties are void in case that the instructions in this manual are not carefully followed 2 10 Main wheels and brakes 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 syste...

Страница 52: ...oad tests required by the German rules and specifications for the certification of ultra light gyrocopters It is mounted on the tail of the frame by screws in 7 spots It is also designed to carry the rudder see the following chapter Pos Description Qnt Tightening Torque 15 1 Internal hexagon bolts with flange M6x16 10 10 Nm 15 2 Big Washer 6 4 DIN 9021 10 15 3 Internal hexagon bolts with flange M5...

Страница 53: ...ety Repairs may only be carried out by persons who are authorized by the manufacturer Note All warranties are void in case that the instructions in this manual are not carefully followed 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...

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Страница 57: ... 2 Fit bolt M6x30 10 9 6 10 Nm 16 3 Self locking Hexagon nut M6 ISO 7042 8 16 4 Washer 6 4 DIN 125 B 17 16 5 Special Aluminum nut M16x1 5 4 5 15 Nm 16 6 Cotter pin 4x40 DIN 94 4 16 7 Internal hexagon bolts with flange M6x16 4 10 Nm 16 8 Pin 6x15 2 16 9 Cotter pin 1 6x12 DIN 94 2 16 10 Internal hexagon bolts with flange M6x30 1 10 Nm 16 11 Bush 1 ...

Страница 58: ...ional 6 Circuit breakers 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 Heating fan switch optional with cabin heating 15 Defroster Fan Switch optional with cabin heating 16 Engine start switch 17 GEN altern...

Страница 59: ...rcuit breakers 7 Master switch 8 Mag 1 switch ignition circuit switch 1 9 Mag 2 switch ignition circuit switch 2 10 Auxiliary fuel Pump switch optional with Rotax 912 ULS engine 11 Avionic master switch optional 12 Landing Lt switch 13 Nav Lt switch optional navigation and strobe light 14 Heating fan switch optional with cabin heating 15 Ventilation fan switch 16 Engine start switch 17 Gen alterna...

Страница 60: ... 914 UL Max Power 115 HP 5800 U min Continuous power 100 HP 5500 U min Max Permitted RPM 5800 Max Continuous RPM 5800 U min Cylinder head temperature max 135 C Oil temperature min 50 C max 130 C Fuel quality EN228 Super min ROZ 95 or EN228 Super plus min ROZ 95 Alternative fuel AVGAS 100 LL ASTM D910 Oil type SAE 10W 40 API SG or higher Example Shell Advance VSX4 To be overhauled 2000 h Trixy 912 ...

Страница 61: ... damages are detected in the engine DO not attempt to take off with a rough running engine Always ensure that max Power is available before flight Note All warranties are void in case that the instructions in this manual are not carefully followed Oil type SAE 10W 40 API SG or higher Example Shell Advance VSX4 To be overhauled 1500 h Trixy 912 TIS Max Power 150 HP 5800 U min Continuous power 140 H...

Страница 62: ...manual are not carefully followed 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 Such author...

Страница 63: ...awing The pilot in command must inspect the oil quantity prior to every flight 1 Switch both ignition circuits off 2 Open the cover of the oil container 4 3 Rotate the propeller counter clock wise 8 10 full rotations 4 Check the oil level in the container between the middle and the upper limit of the dip stick The pilot in command must insure correct oil pressure and oil temperature above 50 C bef...

Страница 64: ...rting the engine The coolant reservoir 1 must be completely full up to the cover 3 The expansion container 4 must show coolant level between the marks MIN and MAX The heat exchanger 2 must be clean 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 ...

Страница 65: ...Excessive fuel is lead back to the tank via return line which connects to the tank on its upper side A vent line is also connected to the upper side of the tank An auxiliary tank is optionally built in the left side of the gyrocopter It is identical with the standard tank In such a case both tanks are connected together through the fuel supply line Fuel is supplied from both tanks equally via a T ...

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Страница 67: ...lass Cockpit NESIS warns the pilot in the event that the voltage drops under 12 V The screen of the glass cockpit switches off at 10 V but the data in processed until the circuit voltage drops down to 6 5 V The battery will not be recharged once the voltage drops down to 8 V or lower and it must be exchanged Authorized personnel must examine the battery and the battery charging controller in every...

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Страница 91: ...els via hydraulic hoses which is lead inside the main gear strut An optional brake lever may be installed on the left side of the co pilot and in such a case it is mechanically connect to the main brake lever in the front part of the cabin The fluid reservoir is in sight of the pilot and must be inspected by the pilot in command before flight It must contain fluid up to 50 of its volume Use DOT 4 ...

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Страница 94: ... 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 Contact Trixy Aviation with any questions which might arise or for more information whenever needed The maintenance works described in this manual are compulsory work...

Страница 95: ... rotor control system for cracks bends and defects 12 Inspect the torque of the bolts in the rotor control system 13 Inspect the pre rotation system for function and defects 14 Apply silicon spray on pre rotator clutch belt and pulleys 15 Inspect the hydraulic brake system on function and leaks 16 Add hydraulic fluid Dot 4 if needed 17 Inspect the nose wheel construction for bends cracks and damag...

Страница 96: ...r pedal 13 Inspect and lubricate re rotation gear and bendix gear 14 Apply silicon spray on pre rotator clutch belt and pulleys 15 Inspect the hydraulic brake system on function and leaks 16 Add hydraulic fluid Dot 4 if needed 17 Inspect the nose wheel construction for cracks and damages 18 Inspect the air pressure in the nose wheel 2 5 bar 38 psi 19 Inspect the main wheels for defects 20 Inspect ...

Страница 97: ...ect the steering system of the nose wheel 6 Inspect torque and tighten the nuts of the main wheels if needed 7 Inspect torque and tighten the main wheel bolts x6 if needed 8 Inspect tires for thread and damage exchange if needed 9 Inspect the attachment of the cabin on the frame 10 Inspect the attachment of the fire wall on the frame 11 Inspect fuel system for leaks 12 Inspect battery and charging...

Страница 98: ...rake pad and exchange if needed 13 Assemble the rotor head and attach it to the mast 14 Attach the rotor to the rotor head and secure it 15 Detach disassemble the thoroughly inspect the propeller 16 Exchange worn blades or any defective parts use origin parts 17 Assemble all parts balance and adjust the propeller 18 Disassemble the pre rotation system and inspect all parts 19 Exchange the angular ...

Страница 99: ...r angular gear Exchange 500 hours Pre rotator Bendex gear Exchange 500 hours Rotor Overhaul 500 hours Rotor Exchange 1500 hours Rotor head Overhaul 500 hours Rotor head Exchange 1500 hours Frame Inspection 500 hours Frame Exchange 2000 hours DUC Propeller Overhaul 500 hours DUC Propeller Exchange 800 hours Neuform Propeller Overhaul 500 hours Neuform Propeller Exchange 1000 hours Hydraulic fluid E...

Страница 100: ...tructions in this manual Engine and propeller are to be maintained by authorized workshops and authorized persons by the respective manufacturer All maintenance works are to be documented in the following certificates in this chapter of the manual The certificates must be signed by the authorized person who performed the maintenance works with date and stamp if available Records of engine maintena...

Страница 101: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 102: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 103: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 104: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 105: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 106: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 107: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 108: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 109: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 110: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 111: ..._ Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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 ____________________ Sta...

Страница 112: ...Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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...

Страница 113: ...Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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...

Страница 114: ...Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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...

Страница 115: ...Hour meter ______________ Date of maintenance Start ______________ End _______________ I certify herewith that the maintenance works are successfully performed on this 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...

Страница 116: ... ___________ Gyrocopter ____________ Description of the damage Description of the damage course of events Person established this record Name _____________________________________ Address _____________________________________ _____________________________________ _____________________________________ Tel Fax _________________ __________________ Location ______________ Datum __________________ Sign...

Страница 117: ...yrocopter ____________ Description of the damage Description of the damage course of events Person established this record Name _____________________________________ Address _____________________________________ _____________________________________ _____________________________________ Tel Fax _________________ __________________ Location ______________ Datum __________________ Signature Please s...

Страница 118: ...yrocopter ____________ Description of the damage Description of the damage course of events Person established this record Name _____________________________________ Address _____________________________________ _____________________________________ _____________________________________ Tel Fax _________________ __________________ Location ______________ Datum __________________ Signature Please s...

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Страница 120: ..._____________ Damage reported on __________________ Total hours Gyrocopter ____________ Engine _____________ Date of repair works Start ______________ End _______________ Description of repairs I herewith certify that this gyrocopter was repaired using original spare parts under the instructions and with the permission of the manufacturer The gyrocopter is airworthy and is returned to service Name...

Страница 121: ..._____________ Damage reported on __________________ Total hours Gyrocopter ____________ Engine _____________ Date of repair works Start ______________ End _______________ Description of repairs I herewith certify that this gyrocopter was repaired using original spare parts under the instructions and with the permission of the manufacturer The gyrocopter is airworthy and is returned to service Name...

Страница 122: ..._____________ Damage reported on __________________ Total hours Gyrocopter ____________ Engine _____________ Date of repair works Start ______________ End _______________ Description of repairs I herewith certify that this gyrocopter was repaired using original spare parts under the instructions and with the permission of the manufacturer The gyrocopter is airworthy and is returned to service Name...

Страница 123: ...Maintenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 123 ...

Страница 124: ...___ End _______________ I certify herewith that the modification made to this gyrocopter was made after consulting the manufacturer and obtaining the needed permissions Modification I have weighed the gyrocopter after the modification according to the method described in the flight and operation manual and I have issued a weight and balance report which is documented in the flight and operation ma...

Страница 125: ...___ End _______________ I certify herewith that the modification made to this gyrocopter was made after consulting the manufacturer and obtaining the needed permissions Modification I have weighed the gyrocopter after the modification according to the method described in the flight and operation manual and I have issued a weight and balance report which is documented in the flight and operation ma...

Страница 126: ...___ End _______________ I certify herewith that the modification made to this gyrocopter was made after consulting the manufacturer and obtaining the needed permissions Modification I have weighed the gyrocopter after the modification according to the method described in the flight and operation manual and I have issued a weight and balance report which is documented in the flight and operation ma...

Страница 127: ...Maintenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 127 ...

Страница 128: ...intenance manual G 4 2 Revision 05A 03 05 2017 Doc No TA M D 002 EN 128 The content of this manual including text pictures and drawings is not to copy without the written permission of Trixy Aviation GmbH ...

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Trixy Aviation G 4-2, Руководство по обслуживанию

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