Tecnam P2010 2015 - 5. Stall Speed

AFMS N"D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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5. STALL SPEED
Weight: 1160 kg (2SS7 lb)
Throttle Lever: IDLE
CG: Most Forward (19%)
No ground effect
BANK
WEIGHT
ANGLE
[kg]
[deg]
([lb])
0
1160
15
(2557)
30
IFWDC.G.)
45
60
STALL SPEED
Ft.APs o·
FIAPST/O
FIAPS Full
KIAS KCAS KIAS
KCAS KIAS KCAS
S9 60 S3
SS
so
S2
60
61
S4 S6 Sl
S3
64
6S
S8 S9 S4
S6
71 71
64 6S 61
62
8S
8S
77
78 73 74
Altitude loss during conventional stall recovery, as demonstrated
durmgjlight tests is approximately 350 ft with banking below 15°.
Section 5 - Performance
STALL SPEED
Ed. 2, Rev.O