Cessna T182 Series User Manual

MODEL 182 &T182 SERIES SERVICE MANUAL
NOTE
When inserting
screw (9) into housing (12)
Position a support stand under the
tail
locate the sprocket (5)
at the end of housing
tie-down ring to prevent tailcone from
which is farther away from the groove for dropping while working inside.
retaining
ring
(11).
b. Remove
pedestal cover (18) in
accordance with
The bearings (6 and 14)
are not pre-drilled
paragraph 9-16.
and must
be drilled on assembly.
The roll
c. Remove screws
attaching control wheel
retainer
pins (10)
are 3/32 inch
in diameter, there-
(13)
to left side of
pedestal structure
(16).
fore, requiring a 3/32
(0.094) inch drill.
d. Remove
retainer (13) and
indicator (15), using
care not to drop trim wheel (17).
f. Withbearing(6)
flushwithend ofhousing(12),
e. Disengage roller
chin (27) from sprocket
(28)
carefully drill
hearing so the drill
will emerge from
the
and trim wheel (17).
hole on
the opposite side
of housing (12).
DO NOT ENLARGE
HOLES IN HOUSING.
NOTE
g. Pres new
roll pins (10) into
pin holes.
h. Insert collar
(7), new O-ring
(13) and bearing
Removal
of the sprocket
(7) from control
(14) into opposite
end of housing 12).
wheel shaft is not recommended except
for
i.
Complete steps
and "g" for bearing
(14).
replacement
of part.
j. If a new
bearing
(16) is required,
a new
bearing
may be pressed
into the b.
Be sure force
bears
f Reverse
the preceding
steps for reinstallation.
against
the outer race
of bearing.
Rig system
in accordance
with paragrph
9-18. safety
k. Screw the threaded
rod end (15) into screw (9).
turnbuckle and reinstall all items removed for access.
l. Install
retaining
rings (11),ifthey
were re-
moved.
9-14.
CABLES AND
PULLEYS. (See
figure 9-1.)
m.
Test actuator assembly
by rotating sprocket
(5)
with fingers
while holding threaded
rod end (15). The
9-15. REMOVAL
AND INSTALLATION.
threaded rod
end should travel
in and out smoothly
a. Remove
seats, upholstery,
pedestal cover
and
with
no indication of binding.
access plates
as necessary.
Reinstall acuator assembly in
9-11. TRIM TAB FREE-PLAY
INSPECTION.
Position a support
stand under the tail
a. Place elevator
and trim tab in neutral
position
tie-down ring
to prevent tailcone from
and secure elevator
from movement.
dropping while
working inside.
b. Determine
m imum amount
of allowable free-
play
using procedures
shown in figure
9-2A.
b. Remove
travel stop blocks
(8) from control
c. Using moderate
hand pressure (up and down),
cables.
measure
free-ply at trailing edge
of trim tab.
c. Disconnect
control cables at turnbuckles(10)
d.
If trim tab freeplay
is less than maximum
al-
and at cable
ends (9).
lowable,
the system is
within prescribed
limits.
d.
Remove cable guards
and pulleys
as necessary to
e.
If trim tab free-play is more
than maximum al-
work cables
free of aircraft Disengage
roller chains
lowable. check
the following items
for looseness while
from sprocket
to ease cable removal.
moving trim tab up and down.
1. Check
push-pull tube to trim tab horn
as-
NOTE
sembly attachment for looseness.
2.
Check push-pull
tube to actuator
assembly
To ease routing
ofcables,
a length of wire
threaded rod end
attachment for
looseness
may
be attched to end
of the cable before
3. Check actuator
assembly threaded rod end
being withdrawn from aircraft Leave
for looseness
in the actuator assembly
with push-pull
wire in place,
routed through structure;
tube disconnected.
then
attach the cable being installed
and
f. If looene is apparent while checking steps e-1 pull cable into position.
and e-2, repair by installing new parts.
g. If looseness is
apparent while checking
step e-3.
e. After cable is routed
in position, install pulleys
refer
to paragraphs 9-6 through
9-10. Recheck trim
and cable guards.
Ensure cable is positioned
in pulley
tab free-play.
groove
before installing guards.
Ensure roller chains
are
positioned correctly
over sprockets.
9-12. TRIM TAB CONTROL WHEEL. (See figure f. Re-rig system in accordance with paragraph
9-1.)
9-18,
safety turnbuckle and reinstall all items re-
moved in step a".
9-13
REMOVAL AND
INSTALLATION.
a. Relieve cable tension at turnbuckle (10) 9-16. PEDESTAL COVER. (Seefigure 9-1.)
9-6 Revision 3

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)