CESSNA PERFORMANCE-
MODEL 182T SPECIFICATIONS
PERFORMANCE-SPECIFICATIONS
(Continued)
STANDARD EMPTY WEIGHT: . . . . . . . . . . . . . . . . . . . 1918 LBS
MAXIMUM USEFUL LOAD: . . . . . . . . . . . . . . . . . . . . . 1192 LBS
BAGGAGE ALLOWANCE: . . . . . . . . . . . . . . . . . . . . . . . 200 LBS
WING LOADING: Lbs/Sq Ft . . . . . . . . . . . . . . . . . . . . . . . . . 17.8
POWER LOADING: Lbs/HP . . . . . . . . . . . . . . . . . . . . . . . . . 13.5
FUEL CAPACITY: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92 GAL
OIL CAPACITY: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 QTS
ENGINE: Textron Lycoming . . . . . . . . . . . . . . . . . . IO-540-AB1A5
230 BHP at 2400 RPM
PROPELLER: Diameter - 3-Blade . . . . . . . . . . . . . . . . . . . 79 IN.
NOTE
The above performance figures are based on the indicated
weights, standard atmospheric conditions, level, hard-surfaced dry
runways and no wind. They are calculated values derived from flight
tests conducted by The Cessna Aircraft Company under carefully
documented conditions and will vary with individual airplanes and
numerous factors affecting flight performance.
Apr 30/01 v
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