Cessna 172P - Performance Specifications; Maximum Weight; Engine

PERFORMANCE-
SPECIFICATIONS
7õ7o Powet
at 8000
Ft
50
ea,llons
Usable Fuål
761o
Powet
at
8000
Ft
62
Glallons Usoblo Fuel
Maximum
Range at 10,000
Ft
40
Gallous
Ueable
FueI
Maximum
Range at 10,000
Ft
50 Gallons
Usable Fuel
Maximum
Ilange
at
10,000
Ft
62
Clellons
Usable
FueI
N,ATE OF CLIMB AT
SEA
LEVEL
SERVICE
CEILING
TAKEOFF
PER,FOH,MANCE:
Ground Roll
Total
Distance
Over 50-F t
Obstacle
I,ANDING PER,FOR,MANCE
¡
Ground Roll
Total Distanco
Over õ0-Ft
Obst¿cle
STALL
SPEED
(KCAS):
Flaps
Up, Power
Off
Flaps Down, Power
Pff
MAXIMUM WEIGHT:
Remp
raÈeãttorLandinj::::
STANDARD
EMPTY
WEIGHT:
Skyhawk
Skyhawk
II
MAXIMUM USEFUL I,OAD:
Skyhowk
Range
58ó NM
Timo
õ.0 HRS
Range
Time
Rango
Tlmo
Range
Time
F,ange
.tï.
.
::::
CESSNA
MODEL 172P
PERFORMANCE
-
SPECIFICATIONS
SPEED:
Maximum
at Soa Level
.1Zg KNOTS
Cruis
0 Ft
.120 KNOTS
CRUISE:
mixture
with fuel allowancefor
engine
cllmb
and 45
minutes reserve.
767o
Power
at 8000
Ft
Range
440 NM
40
Clallons Usable Fuel
Timõ
g.B
HRg
75õ NM
6.4 HRS
õSO NM
õ.8
HRÉI
680 NM
7.4 HRS
875
NM
9.4 HRS
.7OO FPM
.13,000 FT
.890 FT
.1825
FT
.540
FT
.1280
FT
.51 KNOTS
.46 KNOTS
Skyhawk
II
BAGGAGEALLOWAÑCb' :
:
WÍNG
LOADING:
Pounds/Sq
Ft
PO1üER
LOADIÑG: Pounds/HP
FUEL CAPACITY: Total
Standard
Tanks
Long Range Tanks
Integral
Tanks
OTL CAPACITY
ENGINE:
Avco Lycoming
160 BHP
ôt 2700 RPM
PROPELLER: Fixed Pitch, Diameter
.
.2407
LBS
.
.2400
LBS
1414
LBS
1440
LBS
.993
LBS
.967
LBS
.120 LBS
.13.8
.15.0
.43 GAL.
.õ4 GAL.
.88 GAL.
.8
QTS
.o-320-DAJ
. .75IN.
Tho ebovo
porlor:mrnoe
llgureg
Brs brsed on the lndlcet¿d welghte, stenda.rd
oboepherlo
oondltloae,
level
hs¡d-surlsoo
dql¡
rutrw&ya, o¡rd
no wlnd. They s¡e o¡lcul¿ted
v¡lue¡
derlved tron flþht teets oonductod
by the Cee¡¡¿ Airorelt Company under ca,refully
doorño[3ed oondltlone ¡,nd
will
vor¡l
wlth
l¡dlvldu¡l
alrplanee
¡nd
numerous
l¡¡to¡¡
afleotlng
lllght
pedoturnoe,
lt
30 May 1980