Textron 172R180HP, Pilot Operating Handbook

Page: 7 / 396

CESSNA
MODEL 172A (180 HP)
PERFORMANCE­
SPECIFICATIONS
PERFORMANCE-SPECIFICATIONS
(Continued)
WING LOADING: Lbs/Sq Ft . . . . . . . . . . . . . . . . . . . . . . . . . 14.7
POWER LOADING Lbs/HP . . . . . . . . . . . . . . . . . . . . . . . . . 14.2
FUEL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 56 GAL
OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 QTS
ENGINE: Avco Lycoming . . . . . . . . . . . . . . . . . . . . . . IO-360-l2A
180 BHP at 2700 RPM
PROPELLER: Fixed Pitch, Diameter . . . . . . . . . . . . . . . . . 76 IN.I
The above performance figures are based on airplane weights at
2550 pounds, 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.
Oct 4/01
V