POH / AFM
AQUILA AT01-100C
Section 5
PERFORMANCE
Document Nr.:
Issue:
Supersedes Issue:
Date:
Page:
FM-AT01-1010-103
A.02
28.05.2013
15.10.2013
5 - 4
5.2.2
Stall Speeds
Stall speeds were determined in the following configuration:
-
Forward center of gravity (CG) limit: 16.8 in (427 mm) behind the Ref. Datum
-
Takeoff weight 1653 lb. (750 kg)
-
Engine idle
Flap
Position
Bank Angle
0°
30°
45°
60°
KCAS
KIAS
KIAS
KIAS
KIAS
UP
52
49
51
55
> 64
T/O
48
45
47
51
> 60
LDG
43
39
42
47
> 57
Tab.: 5.2.2 Stall Speeds [kts]
NOTE
Stalling speed with bank angle should be considered as for reference purposes only.
Slight differences in how the aircraft stalls can lead to discrepancies. The greater the angle of
bank and flap deflection, the greater the discrepancies.
