CESSNA INTRODUCTION
MODEL 172S
NAV
III
PERFORMANCE-SPECIFICATIONS (Continued)
STANDARD EMPTY
WEIGHT
..............
.
MAXIMUM USEFUL LOAD
.................
.
BAGGAGE ALLOWANCE
..................
.
WING LOADING: Lbs/Sq Ft
POWER LOADING Lbs/HP
FUEL
CAPACITY
........................
.
OIL CAPACITY
............................
.
ENGINE: Textron Lycoming
...................
.
180
BHP
at 2700
RPM
PROPELLER: Fixed Pitch, Diameter
NOTE
1663 POUNDSI
895 POUNDS
120 POUNDS
14.7
14.2
56
GALLONSI
8 QUARTS
IO-360-L2A
761NCHESI
•
Speed performance
is
shown for
an
airplane
equipped with 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
airplane weights
at
2550 pounds, 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.
I 172SPHAUS-01
U.S.
v