XtremeAIR XA42, Flight Manual

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Airplane Flight Manual XA42
AFM-XA42-0040-002-A.01
Page 5 EASA approved Page date:
Chapter 02 24.01.2011
Maneuvers
Recommended entry speeds (IAS)
Symbol Remarks
Min. kts / km/h Max. kts / km/h
Snap roll 80 / 148 174 / 322
Tail slide 100 / 185 225 / 417
Spin V
S
Inverted spin V
S
Knife edge > 150 / 278 < 10 sec.
Inverted flight > V
S
225 / 417 < 2 min.
Particular caution must be exercised when performing maneuvers at speeds above V
A
= 174 KIAS /
322 km/h. Large or abrupt control inputs with elevator and rudder above this speed may impose
unacceptably high loads which exceed the structural capability of the aircraft.
Structure is designed for full and abrupt aileron input up to V
NE
.
For acrobatic maneuvers see chapter 4.
All maneuvers can be performed in upright and inverted flight attitude.
2.10 LOAD FACTORS
Positive load factors Negative load factors
Utility flight m
TOW
= 999 kg / 2200 lbs + 4.4g - 2g
Acrobatic flight m
TOW
= 850 kg / 1874 lbs + 10g - 10g
NOTE
CAUTION