Cessna 172P Pilot's Operating Handbook And Flight Manual page 4

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