5-5 STALL SPEEDS
Conditions:
C.G
..................................................................................................Forward
Power
................................................................................................... IDLE
Bank Angle
..........................................................................................Noted
Example:
Weight
..................................................................................... 7255 pounds
Flaps
..........................................................................................................0°
Bank Angle
..............................................................................................30°
C.G
..................................................................................................Forward
Stall Speed: 65 KIAS / 82 KCAS
WEIGHT
BANK
ANGLE
(DEG.)
STALL SPEEDS
FLAPS 0° FLAPS 10° FLAPS 20° FLAPS 35°
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
7255
LB
0 61 77 51 66 48 61 46 60
30 65 82 55 70 51 66 49 64
45 73 91 61 78 57 73 55 71
60 86 108 72 92 68 87 65 85
6690
LB
0 59 74 49 63 46 59 44 58
30 63 79 52 67 49 63 47 62
45 70 87 58 75 55 70 53 69
60 83 104 69 89 65 83 62 81
6000
LB
0 55 70 46 60 44 56 42 55
30 59 74 50 64 47 60 45 58
45 66 83 55 71 52 66 50 65
60 78 98 65 84 62 79 59 77
5000
LB
0 51 64 42 54 40 51 38 50
30 54 68 45 58 43 55 41 53
45 60 76 50 65 47 61 45 59
60 71 90 60 77 56 72 54 70
Table 5-5 – Stall Speeds
NOTES:
• Maximum altitude loss during wings level stall is approximately 500 ft.
• KIAS values are approximate and may not be accurate at stall.
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