CESSNA SECTION 1
MODEL 172R GENERAL
PERFORMANCE-SPECIFICATIONS
(Continued)
WING LOADING: Lbs/Sq Ft . . . . . . . . . . . . . . . . . . . . . . . . . 14.1
POWER LOADING: Lbs/HP . . . . . . . . . . . . . . . . . . . . . . . . . 15.3
FUEL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 56 GAL
OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 QTS
ENGINE: Textron Lycoming . . . . . . . . . . . . . . . . . . . . IO-360-L2A
160 BHP at 2400 RPM
PROPELLER: Fixed Pitch, Diameter . . . . . . . . . . . . . . . . . 75 IN.
* NOTE
Speed performance is shown for an airplane equipped with
optional speed fairings which increase the speeds by
approximately 2 knots. There is a corresponding difference
in range, while all other performance figures are unchanged
when speed fairings are installed.
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 the Cessna Aircraft Company
under carefully documented conditions and will vary with
individual airplanes and numerous other factors affecting flight
performance
Feb 28/00 iii/(iv blank)
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