Cessna 402C Pilot Operating Handbook page 121

SECTION 5
PERFORMANCE
CONDITIONS;
Throttles - IDLE.
STALL SPEEDS
NOTE:
1.
Maximum al titude loss during a
conventi ona1 stall is approx i-
mately 600 feet.
2. Maximum nose down pi tch atti tude
and altitude loss during recovery
from an engine inoperative stall
is approximately 10 degrees below
the horizon and 300 feet, respec-
tively.
ANGLE OF BANK
WEIGHT
Pounds Configuration
0° 20° 40° 60°
Flaps
Gear
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
6850
0°
Up
80 78 83 80 93
89 115 110
15°
Down
78 76
81 78 90 87
III
107
45°
Down
71
6B
74
71
82
78 103 97
6500
0°
Up
78 76
81 78 90
86 112 107
15° Down
76 74
78 76 87
84 108 104
45°
Down 69 67
71
69 80
76 100 94
6000
0°
Up
74 73
76 75 87
83 108 103
15°
Down
73
71
75 73 83
81 104 100
45°
Down 64 64 68 66
77 73 96 90
5000
0°
Up
67 66
69 68 78
76 98 94
15°
Down
66 65 69 67 76
74 74 92
45° Down
59 58
61
60 69
67 88 83
Fi 9uro 5-8
1 November 1979