Cessna 402C - Page 121

SECTION 5
PERFORMANCE
CONDITIONS;
Throttles - IDLE.
STALL SPEEDS
NOTE:
1. Maximum al titude loss during a
conventi
ona 1 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