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025-00-16C M16C FLIGHT MANUAL, Issue G
02 March 2016
5.7 LOAD FACTOR LIMITATIONS
Considering a flight configuration of 500 kg, the maximum value of normal bearable acceleration is equal to
+ 3 g. A higher value will permanently deform the gyroplane's structure.
Flight configuration load factor
500 kg + 3 g
5.8 HEIGHT-VELOCITY ENVELOPE
Please see the APPENDIX 3 for the height-velocity chart.
5.9 C OF G LIMITATIONS
In order to avoid shifting of the center of gravity beyond the front and rear limits, the gyroplane's loading
limits are as follows:
- Minimum pilot weight 60 kg
- Maximum pilot weight 120 kg
- Maximum passenger weight 120 kg
Also see APPENDIX 1
WARNING DANGER:
Flying without pilot in the front sear is prohibited.
NOTE:
Keep in mind that the weight of either, the passenger or fuel, do not influence significantly
the variation of the center of gravity, as they remain in center of gravity position.
5.10 LOAD LIMITATIONS
Maximum weight allowed during takeoff 500 kg
Maximum weight allowed during landing 500 kg
5.11 FLIGHT LIMITS
Flight restricted to VMC.
Summary of Contents for M-16 C
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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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