Beechcraft Beech 95 2017 - Section 2 - Limitations; Airspeed and Stall Speed Limitations

Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 16
Section 2– Limitations
Introduction to Section 2
Section 2 includes operating limitations, instrument markings, and basic placards
necessary for safe operation of the airplane, its engines, and systems. The limitations
included in this section are taken from the official operating manual in the airplane, the
shop manual, the Lycoming engine-operating manual, and other manufacturers
information sources.
The airspeeds in the airspeed limitations chart are based on airspeed calibration
data shown in section 5. This data has been gleaned from various sources within
Beechcraft documentation but may not be totally accurate.
Design Limitations
The following design speeds apply:
Speed
KIAS
KCAS
V
fe
Maximum flap extended
113
113
V
le
Maximum landing gear extended
143
143
V
mc
Minimum control speed
71
69
V
sse
Single engine safety speed
78
75
V
no
Maximum structural cruising speed (top of green arc)
161
161
V
ne
Never exceed speed (red line)
208
208
Stall Speeds
Power-off Stall speeds with zero flaps and zero bank:
Weight
Stall Speed KIAS
Stall Speed KCAS
4200
74
71
4000
72
70
3800
70
68
3600
68
66
Power-off Stall speeds with 28 flaps and zero bank:
Weight
Stall Speed KIAS
Stall Speed KCAS
4200
65
61
4000
65
60
3800
62
58
3600
61
57
Do not open pilot storm window above 126 KIAS.
Do not open passenger door in flight.