Cessna 172P - Performance - Specifications

PERFORMANCE
-
SPECIFICATIONS
SPEED:
Maximum
at
Sea
Level
96 KNOTS
Cruise, 76Vo
Powør
at 4000 Ft
95
KNOTS
CRUISE:
Recommended
lean mixture
with fuel
allowance
for
engine sta,rt,
taxi, takeoff,
ctimb
and 45 minutes
reeerve.
76Vo Power
at
4000 Ft
.
Range 960
NM
40 Gallons
Usable
Fuel
Time
9.8 HnS
76Vo Power
at 4000 Ft
F,ange 425
NM
50
GalÌons
Usable
Fuel
Time 5.0
HRS
Maximum
Range
at
10,000
Ft
. Range
495 NM
40
Gallons
Usable F''uel
Time
õ.6 HRS
Maximum
Range at 10,000
Ft
. F,ange
56õ NM
50 Gallons
Usable
Fuel
Timo
Z.g
HRS
RATE
OF
CLIMB Al
SEA
LEVEL
. 740 FPM
SER,VICE
CEILING
TAKEOFF
PER,FORMANCE:
15,000
FT
1
FLOATPLANE
MODEL
172P
Wator
Run
Total Distance
Over õO-Ft Obstacle
LANDING PER,FORMANCE:
Water
Run
Total Distanoe
Over
50-Ft
Obstacle
STALL SPEED
(KCAS):
Flaps
Up, Power Off
Flaps Down,
Power
Off
MAXIMUM
WEIGHT:
Ramp
(Dock)
Takeoff
or
Landing
STANDARD EMPTY WEIGHT:
Skyhawk Floatplane
Skyhawk II Floatplane
.
MAXIMUM
USEFUL
LOAD:
Skyhawk
Floatplane
Skyhawk
II Floatplane
.
BAGGAGE ALI,OWANCE
WING LOADING: Pounds/Sq
Ft
POWER LOADING: Pounds/HP
FUEL CAPACITY:
Total
Standard Tanks
Long Range Tanks
OIL CAPACITY
ENGINE: Avco Lycoming
160 BHP at 2700 F,PM
PILOT'S
OPEN,AIING
HANDBOOI{
SUPPLEMENT
1400 FT
2160 FT
õ90 FT
1345 FT
48
KNOTS
44 KNOTS
. 2P,27 LBs/
. 2220 LBS
1õ93 LBS
1619
LBS
. . 634 LBS
608
LBS
120 LBS
LZ.7
13.9
43
GAL.
õ4
GAL.
8
QTS
o-320-D2J
PROPELLER: Fixed Pitch, Diameter
. 80 IN.
2
30 May 198O