Cessna 172SPHUSR05 Pilot Operating Handbook page 21

CESSNA
MODEL 1 72S
WING LOADING: Lbs/Sq Ft . . . . . . . . . . . . . . . . . . . . . . . . .
POWER LOADING Lbs/HP . . . . . . . . . . . . . . . . . . . . . . . . .
FUEL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OIL CAPACITY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ENGINE: Textron Lycoming . . . . . . . . . . . . . . . . . . . . IO-360-L2A
1 80 BHP at 2700 RPM
PROPELLER: Fi x ed Pi t ch, Di a meter
Speed performance i s shown for an ai r pl a ne equi p ped wi t h
speed fai r ings whi c h increase the speeds by approximatel y
2 knots. There i s a corresponding di f ference i n range, while
all other performance figures are unchanged when speed
fai r ings are installed.
The above performance figures are based on ai r plane wei g hts at
2550 pounds, standard atmospheric condi t ions, level, hard-surfaced
dry runways and no wind. They are cal c ulated val u es deri v ed from
flight tests conducted by The Cessna Ai r craft Company under
careful l y documented condi t i o ns and will vary wi t h indi v i d ual
ai r planes and numerous factors affecting flight performance.
Revision 4
R MANCE·SPECIFICATI NS
(Continued)
NOTE
*
PERFORMANCE­
SPECIFICATIONS
1 4.7
1 4.2
56 GAL
8 QTS
76 IN.
v