P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
42
4.4 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 100ft with banking
under 30°.
0 °
30 °
45 °
60 °
FLAP
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
0°
44
52
47
54
52
58
62
65
15°
42
50
45
52
50
56
59
63
35°
39
38
42
50
46
53
55
60
LATERAL BANK