Beechcraft Beech 95 2017 - Page 17

Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 17
Stall speed in a turn may be calculated based on V
sb
= Vs/ Cos(b) where V
sb
is stall
speed at a bank angle b.
Power-off Stall Speed at 4200lb, zero flap, Bank Angle b:
Bank angle
1/ Cos(b)
Vs indicated
Vs Calibrated
15
1.02
75
73
30
1.07
80
77
45
1.19
88
85
Power-off Stall Speed at 4200lb, full flap, Bank Angle b:
Bank angle
1/ Cos(b)
Vs indicated
Vs Calibrated
15
1.02
67
62
30
1.07
70
66
45
1.19
78
73
Maneuvering speed (Va):
This airplane is designed for normal operating limits of +4.4g and –3.0g pilot
induced loads in the clean configuration. It is limited to +2.0g and –0.0g pilot induced
loads with (any) flaps extended.
Maneuvering speed (clean) is defined as Va = 3.8 x Vs
Weight
Va KIAS
Va KCAS
4200
139
139
4000
136
136
3800
132
132
3600
129
129
Turbulence Speed
This airplane is designed to withstand vertical wind gust up to 45 feet per second.
In such gusts operating at high speed may exceed the airplanes design load factor but
operating at low speed will result in loss of control due to stall. It is recommended to
operate at Va in moderate or severe turbulence.