Cessna T188C - Page 17

MODEL
188
& T188
SERIES
SERVICE
MANUAL
GROSS WEIGHT
(Restricted
Category
- AgTruck
beginning
with 1974)
. .
. 4200
lb.
(Restricted
Category
- AgTruck
thru
1973 and
A188B AgWagon)
4000
lb.
(Restricted
Category
- AgWagon
230)............
3800 b.
(Normal
Category
- AgWagon
230
and
300) ....
. .
3300
b.
(Restricted
Category
-
AgHusky
turbo)
.....
. .
4400
b.
MAXIMUM
OPERATING
ALTITUDE
(Certified).
.........
12,
500
ft.
FUEL CAPACITY
Metal
Tank (Total)
Not installed
on
18802746 and
subsequent
. .37
gal.
(Usable)
. .
. . .
.. .
.. .
. .
. . .
. ...
36.5 gal.
Rubberized
Cell
(Total)
..................
....
56 gal.
(Usable)
. . .
. .
. . .
. .
. .
. . .
. .
. 54
gal.
Rubberized
Cell
(Total)
.................
.
54 gal.
(Usable)
..............
.... 52 gal.*
OIL
CAPACITY
Without
External
Filter
. . .
.. .
.. .
. . .
. . .
. . .
12 qt
With
External
Filter
......
.............
. 13
qt
ENGINE MODEL
188
(Refer
to Section
11 for
Engine Data)
..............
CONTINENTAL
0-470 SERIES
A188 (Refer
to Section
11A
for Engine
Data)
.........
CONTINENTAL
10-520
SERIES
T188C
(Refer to
Section 11B
for Engine
Data)
...
CONTINENTAL
TS1O-520
SERIES
PROPELLER
230 HP (Fixed-Pitch,
Two-Blade)
.............
90"
McCAULEY
230 HP (Constant-Speed,
Two-Blade)
.............
88" McCAULEY
230
HP & 300
HP (Constant-Speed,
Two-Blade)
........
86" McCAULEY
300 HP (Constant-Speed,
Two-Blade)
............
82" McCAULEY
300
HP (Constant-Speed,
Two-Blade)
...
.........
80" McCAULEY
300
HP (Constant-Speed,
Three-Blade)
...........
80" McCAULEY
310
HP (Constant-Speed,
Three-Blade)
..
........
80"
McCAULEY
MAIN WHEEL TIRES
Standard
. ...............
8.00-6,
6-Ply Rating
Pressure . . .
.. .. ......
. ...
.. . 35 psi
Optional
.
....
.
. . .... . . .... . . .
. 8.50-10,
6-Ply Rating
Pressure
.....
.........
........
25
psi
Optional
. ..
...........
. .22
x 8.00-8,
6-Ply
Rating
Pressure . .
.. . . ...
. ...... . . ...
35 psi
TAIL WHEEL TIRE
Standard .....
.................
. 2.80-8,
4-Ply Rating
Pressure
. . ..
. ..
.....
..
60-70
psi
Optional .
. . . . .
. . . . . .
. . . . . .
..
3.50-10,
4-Ply Rating
Pressure
. . ... ..
.. ... ...
.. .
50-60 psi
WHEEL ALIGNMENT
Camber ...
....................
.. 2
°
to
4
°
Toe
In (Total
Both Wheels)
...
......
.. .. .....
0"
to . 12"
AILERON
TRAVEL (Measured
from
Droop Position)
Up ...........................
18°±1
°
Down .
. ....................
.......
.
10°±1
°
Droop Position
......
.
.....
. .......
3±0°30'
Down from
0
WING
FLAP
TRAVEL
(Thru
188-0293)
. . .
. . .
. . . .
. . . .
. ....
.
0
°
.
10, 20,
28°± 2
°
(188-0294
Thru
18800832)
.
......
......
0
°
, 10
°
, 20
°
± 1
(Beginning
18800833)
.........
0,
5, 10,
20-,
±1-
RUDDER TRAVEL
Right
.. ...
...................
24,
+0° -1
°
Left
. . .
. . . . .
. ..
..
. 24
°
, +0
°
-1
°
ELEVATOR TRAVEL
U p .. . . . . . . . . . . . . . . . . . . . .. .. . 2 6
°
1
°
Down .
..... ..
.. . .. . .
... 21
°
±
1'
ELEVATOR TRIM TAB TRAVEL
U p . . . .
. . . . . . . .
. . . . . . . . .
. . . . 12 ±
1
Down
......
.
. .. .
27
°
1
°
Figure
1-1.
Aircraft
Specifications
(Sheet
1 of 2)
1-2