Tecnam P92-JS - STALL SPEED

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
5-5
P92-JS
S E C T I O N 5
PERFORMANCE
STALL SPEED (Approved data)
CONDITIONS: - weight 550 kg
- engine idle
- no ground effect
LATERAL BANKING
0°
30°
45°
60°
FLAPS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
0°
44
43
47
46
52
51
63
61
15°
42
41
45
44
50
49
60
58
38°
40
39
42
41
47
46
56
55
CONDITIONS: - weight 600 kg
- engine idle
- no ground effect
LATERAL BANKING
0°
30°
45°
60°
FLAPS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
0°
46
45
49
48
54
53
66
64
15°
44
43
47
46
52
51
63
61
38°
41
40
44
43
49
48
58
56
NOTE
Altitude loss during conventional stall recovery as demonstrated
during test flights is approximately 100 ft with banking under 30°.