Magni Gyro M-24C Orion, Руководство по эксплуатации самолета

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M24C_AUS
M24C FLIGHT MANUAL
ISSUE B PAGE
December 2011 41
3.6 FLIGHT MANOEUVRE LIMITATIONS
- Any flight manoeuvres with constant load lower than zero g are prohibited.
- Flight at or below zero g is prohibited
- Aerobatic manoeuvres are prohibited.
Please see the APPENDIX for the flight manoeuvre limitations chart.
3.7 LOAD FACTOR LIMITATIONS
With a total aircraft weight of 500 kg, the maximum permissible acceleration load factor is equal to + 3 g.
A higher load factor will permanently deform the gyroplane’s structure.
When the gyroplane flies in a lightly loaded configuration with less than 400 kg weight, the maximum
permissible acceleration load factor is equal to + 4 g. A higher value will permanently deform the
gyroplane’s structure.
Flight configuration load factor
500 kg + 3 g
400 kg + 4 g
3.8 FLIGHT ENVELOPE
Please see the APPENDIX for the flight envelope chart.
3.9 CENTRE OF GRAVITY LIMITATIONS
In order to avoid moving the centre 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
See Appendix 4 for centre of gravity limitation data
WARNING DANGER:
- Flight without an occupant of at least 60kg in the left seat is prohibited.
- Left seat is the main pilot seat.
- Max Pilot weight is subject to MTOW limitations (See section 3.10).