AIRSPEED CORRECTION TABLE
(Flaps Up)
IAS
40
50 60
70
80 90
100
110
120
130
140
CAS
51
57
65
73
82
91
100
109
118
127
136
(Flaps Down)
IAS
40
50
60 70
80
90
100
CAS
49
55 63
72
81 89
98
Figure
5-1.
=Power Off=
STALLING SPEEDS
MPH = CAS
Weig�
ANGLE
OF
BAN K
1600
lbs.
Au"
CONDITION
Do
Flaps
55
57
UP
63
78
Flaps
�
49
51
56
20°
70
Flaps
48
40°
49
54
67
Figure
5-2.
5-2
Содержание 150 1968
Страница 1: ...1 RE A E MO R CES A i FLYING T A N AN fHi _ ___ _ I IDITCO JIDJEIT Jl CQ I 1968 I OWNER S MANllAL...
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