MAXIMUM-RATE-OF-CLIMB DATA
2200 Pounds Gross Weight - Flaps Retracted
ALTITUDE
FEET		 TEMPERATURE
°F.		 IAS
MPH		 RATE OF CLIMB
FT./MIN.		 FUEL USED
FROM SEA LEVEL
GALLONS
S.L.
2500
4500
6500
8500
10500		59°
50°
43°
36°
28°
21		91
89
88
87
86
85		660
550
460
370
280
200		1.0
1.8
2.7
3.7
4.9
6.5
NOTES: 1. Full throttle climb, mixture leaned above 5000 feet to
smooth engine operation.
2. Fuel used includes taxi and warm up allowance.
3. Power loss attributable to the presence of humidity can
be as high as 7%, this represents approximately 100 FPM
loss in climb rate at sea level.