Cessna 1969-1976 172 Series Service Manual page 8

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GROSSWEIGHT 23001b NOTE
FUEL CAPACITY
Standard Wing (Total)
. . . . . . . . . . . . . . . . . . . .
42 gal. These specifications are
LOng-mnge Wing (Total)
. . . . . . . . . . . . . . . . . .
52 gal. and F172-Series aircraft,
Long-Range Wing (Usable).
. . . . . . . . . . . . . . . . .
48 gal. except as indicated.
(Without External Filter)
. . . . . . . . . . . . . . . . . .
8 qt
(With External Filter).
. . . . . . . . . . . . . . . . . . .
9 qt
Standard Wing (Usable)
. . . . . . . . . . . . . . . . . . .
38 gal.
applicable to both Model 172
OIL CAPACITY
ENGINE MODEL
172-Series(Refer to Section 11 f o r Engine Data)
. . . . . . . .
LYCOMING 0-320 S e r i e s
F172-Series (Refer to Section 11A thru 1971 Models).
. . . . .
CONTINENTAL 0-300 S e r i e s
F17P-Series (Refer t o Section 11 Beginning with 1972 Models).
.
LYCOMING-0-320 S e r i e s
PROPELLER (Fixed Pitch)
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76" MCCAULEY
MAIN WHEEL TIRES
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6.00
x 6, 4-Ply Rating
P r e s s u r e (Thru 1970 Models)
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24 p s i
P r e s s u r e (Beginning with 1971 Models)
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29 p s i
NOSE WHEEL TIRE (Standard)
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5.00 x 5, 4-Ply Rating
P r e s s u r e (Thru 1970 Models)
. . . . . . . . . . . . . . . .
26 p s i
P r e s s u r e (Beginning with 1971 Models)
. . . . . . . . . . . .
31 p s i
NOSE WHEEL TIRE (172-Series Only, Optional)
. . . . . . . . . .
6.00 x 6, 4-Ply Rating
P r e s s u r e
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26 p s i
C a m b e r .
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3" t o 5"
Toe-In
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0" to .06"
Camber
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2" to 4"
Toe-In
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0" to .18"
u p . .
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2 0 " * 1 "
D o w n . .
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1 5 " * l 0
(Thru 1972 Models).
. . . . . . . . . . . . . . . . . . . .
0" to 40"
*
2 "
(Beginning with 1973 Modelsb
. . . . . . . . . . . . . . . .
0" to 40°, +Oo - 2 O
Right
. . . . . . . . . . . . . . . . . . . . . . . . . . .
16' 10'*1"
Left
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16' 10' *lo
Right
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17' 44'*1"
Left
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17' 44'51'
U p . .
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28", + 1 " - 0 "
Down
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23", + I "
-
0 "
U p . .
. . . . . . . . . . . . . . . . . . . . . . . . . .
? B o , + 1 " - 0 "
Down
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13", + l o
-
0"
Wing Span (Conventional Wing Tip)
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Wing Span (Conical-Camber Wing Tip)
. . . . . . . . . . . .
35' 10"
Wing Span (Conical-Camber With Strobe Lights)
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Tail Span
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11'
Length
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26' 11"
Flashing Beacon Installed on Fin
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8'
-
9 1/2"
Track Width (Thru 1970 Models)
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7' 2"
Track Width (Beginning with 1971 Models).
8'
-
3 1/2"
BATTERY LOCATION.
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Firewall
NOSE GEAR STRUT PRESSURE (Strut Extended).
. . . . . . . . .
45 p s i
WHEEL ALIGNMENT (Flat Spring Struts)
WHEEL ALIGNMENT (Tublar Spring Struts
*
(Tubular Gear is non-adjustable)
AILERON TRAVEL
WING FLAP TRAVEL
RUDDER TRAVEL (Measured parallel to water line)
RUDDER TRAVEL (Measured perpendicular to hinge line)
E LEVATOR TRAVEL
E LE VATOR TRIM TAB TRAVEL
PRINCIPAL DIMENSIONS
36' 2"
36'
Fin Height (Maximum with Nose Gear Depressed and
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*
No provisions are made for aligning wheels on tubular g e a r aircraft.
The tolerances provided
are
to be used only f o r checking existing
wheel alignment.
Figure 1-1. Aircraft Specifications
1-2 Change 2