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DATE
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24 July 2019
B
209-00-24C
M24C PLUS FLIGHT MANUAL
27
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.
3.7 LOAD FACTOR LIMITATIONS
With a total aircraft weight of 535 kg, the maximum permissible acceleration load factor is equal to
+3 g. A higher load factor will permanently deform the gyroplane 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 structure.
3.8 FLIGHT ENVELOPE
The height-velocity diagram shows the height and speed limits. The area delimited by the curve
on the graph shows the conditions where a safe landing is not possible in case of an engine
failure.
Aircraft weight [kg]
Maximum load factor [g]
400
+4
535
+3