Tecnam P2008 - Page 89

P2008
Flight Manual
A40
4.6 Stall Speeds
Conditions:
- Weight 600 kg (1320 lbs)
- Throttle: idle
- No ground effect
NOTE
Altitude loss during conventional stall recovery as demonstrated during test flights is approximately 200ft with banking
under 30°.
FLAPS
KIAS
KCAS
0°
48
45
LND
40
34