Page 64
025-00-16C M16C FLIGHT MANUAL, Issue G
02 March 2016
AT LIMIT STOP OF PRE-ROTATION LEVER
6. ENGINE r.p.m. - Gently increase the engine speed ( 5 , 2 ) until reaching 200 r.p.m. of the
rotor (standard pre-rotation).
WARNING DANGER:
The minimum rotor pre-rotation value is 150 r.p.m. It is strictly forbidden to proceed with
takeoff operations if the rotor r.p.m. is inferior to this minimum value.
NOTE:
Under identical conditions of power, the length of the takeoff run depends on the rotor r.p.m.
reached during pre-rotation. The maximum speed of the pre-rotation system is 280 r.p.m. The
life of the pre-rotation system and its inspection frequency depend on the average rotor
r.p.m. applied during the pre-rotation operation.
WARNING DANGER:
If it is not possible to reach the minimum rotor r.p.m. during pre-rotation, stop the operation
and return to the parking area.
7. BRAKES (6)- release.
8. RELEASE PRE-ROTATION LEVER - once the rotor turns at 200 r.p.m., quickly release the
pre-rotation lever (3).
WARNING DANGER:
It is strictly forbidden to operate the pre-rotation lever (3) apart from the pre-rotation
procedure.
Summary of Contents for M-16 C
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Page 79: ...Page 79 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 Fig 5 1 Operation Limits...
Page 90: ...Page 90 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 APPENDICES...
Page 91: ...Page 91 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 APPENDIX 1 CG DATA...
Page 94: ...Page 94 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 APPENDIX 2 PERFORMANCE DATA...
Page 96: ...Page 96 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 APPENDIX 3 HEIGHT VELOCITY DIAGRAM...
Page 98: ...Page 98 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 APPENDIX 4 MANOEUVRE LIMITATIONS...
Page 100: ...Page 100 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 APPENDIX 5 ENGINE PARAMETERS...
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Page 103: ...Page 103 025 00 16C M16C FLIGHT MANUAL Issue G 02 March 2016 APPENDIX 6 VOLTMETER DEVICE...
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