Tecnam P2010 - Stall Speed

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV5 - 6
Section 5 – Performance-
STALL SPEED
Ed. 1, Rev.0
5. STALL SPEED
Weight: 1160 kg (2557 lb)
Throttle Lever: IDLE
CG: Most Forward (19%)
No ground effect
WEIGHT
BANK
ANGLE
STALL SPEED
FLAPS 0°
FLAPS T/O
FLAPS FULL
[kg]
([lb])
[deg]
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
1160
(2557)
(FWD C.G.)
0
59
60
53
55
50
52
15
60
61
54
56
51
53
30
64
65
58
59
54
56
45
71
71
64
65
61
62
60
85
85
77
78
73
74
Altitude loss during conventional stall recovery, as demonstrated
during flight tests is approximately 350 ft with banking below 15°.
NOTE