Cessna T182 Series User Manual

MODEL
182 & T182 SERIES
SERVICE MANUAL
MODELS
182,
F182
AND
T182
GROSS WEIGHT
(Takeoff
and Landing)
(182
& F182 thru 1980) .. . . ....
... ......
2950 lb.
(T182
& 182 1981
& ON) ...................
3100 lb.
FUEL CAPACITY
Standard Wing (Total)
...............
.... 61 gal. THRU 1978
Standard
Wing (Usable).
....................
56 gal. THRU
1978
Long-Range
(Total) ......................
80 gal.
THRU 1978
Long-Range (Usable). ..................
. 75
gal. THRU 1978
Wet Wing (Total).
.......................
92 gal. 1979 &
ON
Wet Wing (Usable) .......................
88 gal. 1979 & ON
OIL CAPACITY
Without
External Oil
Filter (182 &
F182). ............
12 qts.
With External Oil
Filter (182 &
F182) ..............
13 qts.
Without External Oil Filter
(T182). ...............
8 qts.
With External Oil Filter (T182)
.................
9 qts.
ENGINE MODEL
(182 & F182) .................
CONTINENTAL
0-470 Series
ENGINE MODEL (T182)
......................
LYCOMING
0-540 Series
PROPELLER (Constant Speed) ................... 82" McCAULEY
MAIN
WHEEL TIRES .......................
6.00 x 6, 6-Ply
rating
Pressure ...................
....... 42
psi
NOSE
WHEEL TIRE.......................
5.00 x 5, 6-Ply
rating
Pressure
...........................
49
psi
NOSE
GEAR STRUT PRESSURE (Strut Extended)
........... 55 psi
to 60 psi
WHEEL ALIGNMENT
Camber .. .....
.. . . . ... . . . . . ....
... 5
°
to 7°
Toe-In ...........................
. 0" to. 06"
AILERON TRAVEL
Up ..... .... . ..
. . . ... . . . . .
20
° ±
2
°
Down . . . . . . .
. . . . . . . . . . . . . . .
.. 15
° ±
2
°
WING FLAP TRAVEL ........... ......... . 0° to 40
°
+1° -2° THRU 1981
0° ±
0 ° t o 3 8 ° +0 ° - 1 °
1982 & ON
RUDDER TRAVEL
(Measured Parallel
to Water Line)
Right . . . .
. . . . . . .
. . . . . . . .
. . . . . . ..
. 24
°
+0 -1
Left . . .
. . . . . . . .
. . . . . . .
. . . . . . . .
... 24 +0 -1
RUDDER TRAVEL
(Measured Perpendicular
to Hinge Line)
Right ...........................
. 27° 13' +0 -1
Left
.............................
27°
13' +0 -1
ELEVATOR TRAVEL (Relative to Stabilizer)
Up (182 &
F182). .......................
26
°
± 1° THRU
1980
Up (182
& T182). .......................
28
°
± 1
°
1981
& ON
Down (182
& F182). ......................
17
°
± 1
°
THRU
1980
Down
(182& T182). ......................
21
°
± 1
°
1981
& ON
ELEVATOR TRIM TAB TRAVEL
Up
(182 & F182).
.......................
25
°
± 2°
THRU
1980
Up (182& T182) .........................
24
°
± 2
°
1981 & ON
Down (182, F182
& T182) .
.................
15
°
± 1
°
PRINCIPAL
DIMINSIONS
Wing Span ........... ... . ........... 432.00"
Tail Span. ................... ........ 140. 00"
Lenght
(182 & F182) ......................
337.47"
Length (T182) ..... ...
. . ... . .. .. .......
338. 97"
Fin Height ......... .. ... ....... ... . 109.68"
Track Width ............. . ........... 109.25"
BATTERY LOCATION
......................
Aft of Baggage Compartment
Measured with strobe lights installed.
Measured
with
aircraft empty.
(Maximum with
nose gear depressed
and
flashing beacon
installed
on fin. )
Figure 1-1. Aircraft Specifications
1-2

Cessna T182 Series Specifications

General

Engine Type	Lycoming IO-540-AB1A5
Horsepower	230 hp
Seating Capacity	4
Service Ceiling	18, 100 feet
Takeoff Distance	1, 600 feet
Landing Distance	1, 350 ft
Type	Single-engine
Max Takeoff Weight	3, 100 lb
Wingspan	36 ft
Length	29 ft
Height	9 feet 3 inches
Fuel Capacity	92 US gal (348 L)