Cessna SKYCATCHER 162 - Page 7

CESSNA INTRODUCTION
MODEL 162
GARMIN G300
U.S.
PERFORMANCE - SPECIFICATIONS (Continued)
MAXIMUM WEIGHT:
Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1324 POUNDS (600.5 kg)
Takeoff. . . . . . . . . . . . . . . . . . . . . . . . . . . 1320 POUNDS (598.7 kg)
Landing . . . . . . . . . . . . . . . . . . . . . . . . . . 1320 POUNDS (598.7 kg)
STANDARD EMPTY WEIGHT. . . . . . . . . . . . 834 POUNDS (378.3 kg)
MAXIMUM USEFUL LOAD . . . . . . . . . . . . . . 490 POUNDS (220.4 kg)
BAGGAGE ALLOWANCE . . . . . . . . . . . . . . . . 50 POUNDS (22.68 kg)
WING LOADING . . . . . . . . . . . . . . . . . . . 11.0 lbs/sq. ft. (53.7 kg/sq m)
POWER LOADING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13.2 lbs/HP
FUEL CAPACITY (Usable) . . . . . . . . . . . . . . . . . 24 GALLONS (90.8 l)
OIL CAPACITY (Sump) . . . . . . . . . . . . . . . . . . . . . . 5 QUARTS (4.73 I)
ENGINE: Teledyne Continental Motors . . . . . . . . . . . . . . . . . . . O-200D
100 BHP at 2750 RPM
PROPELLER:
Fixed Pitch, Diameter . . . . . . . . . . . . . . . . . . . . 67 INCHES (1.70 m)
162PHUS-01
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