Tecnam P2010 - Stall Speed

AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V5-6
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
Section 5 - Performances
STALL SPEED
2
nd
Edition, Rev. 0