CESSNA INTRODUCTION
MODEL T182T NAV III
GFC 700 AFCS
U.S.
PERFORMANCE - SPECIFICATIONS (Continued)
MAXIMUM WEIGHT:
Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3112 POUNDS
Takeoff. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3100 POUNDS
Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2950 POUNDS
STANDARD EMPTY WEIGHT. . . . . . . . . . . . . . . . . . . . 2029 POUNDS
MAXIMUM USEFUL LOAD . . . . . . . . . . . . . . . . . . . . . . 1083 POUNDS
BAGGAGE ALLOWANCE . . . . . . . . . . . . . . . . . . . . . . . . 200 POUNDS
WING LOADING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17.8 lbs/sq. ft.
POWER LOADING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13.2 lbs/HP
FUEL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92 GAL
OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 QUARTS
ENGINE: Textron Lycoming. . . . . . . . . . . . . . . . . . . . . . TIO-540-AK1A
235 BHP at 2400 RPM
PROPELLER: 3-Bladed, Constant Speed, Diameter. . . . . . 79 INCHES
* Speed performance and range are shown for an airplane
equipped with the standard wheel and brake fairings. These
fairings increase the speeds approximately 3 knots over an
airplane without the fairings.
The above performance figures are based on the indicated weights,
standard atmospheric conditions, level, hard-surface dry runways and
no wind. They are calculated values derived from flight tests conducted
by Cessna Aircraft Company under carefully documented conditions
and will vary with individual airplanes and numerous factors affecting
flight performance.
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