Cessna T182 Series User Manual

MODEL 182 & T182 SERIES SERVICE MANUAL
7-4. TROUBLE SHOOTING (Cont).
TROUBLE PROBABLE CAUSE REMEDY
INCORRECT
FLAP TRAVEL. Incorrect
rigging. Refer to paragraph
7-18.
7-5. FLAP MOTOR
AND TRANSMISSION ASSEMBLY.
d. Remove remaining items by removing bolt
(28).
Use care
not to drop parts
into tunnel area.
7-6. REMOVAL
AND INSTALLATION.
(See
e. Reverse
the preceding steps
for reinstallation.
figure
7-2.)
Do not overtighten bolt (28) causing lever
(14) to bind.
a.
Run flaps to full
DOWN position.
Rig system
in accordance
with paragraphs
7-18 and
b.
Disconnect
battery
ground
cable and
insulate
7-19.
terminal
as a safety
precaution.
c.
Remove access
plates
beneath flap
motor and
7-10. DRIVE
PULLEYS.
(See
figure 7-2.)
transmission
assembly
in right wing.
7-11. REMOVAL AND INSTALLATION.
NOTE a. Remove access plate adjacent to drive pulley
(13) in right wing.
Flap motor
(9), transmission
(7), hinge as-
b. Unzip or remove
headliner as necessary
for ac-
sembly
(10), and actuating tube (5) are re-
cess to turnbuckles (index 4, figure 7-1),
remove
moved from the aircraft
as a unit. On
air-
safety wire and loosen
turnbuckles.
craft
equipped with long range
fuel tanks, it
c. Remove bolt
(19) securing flap push-pull
rod (14)
may be
easier to detach
motor and trans-
to drive pulley
(13) and lower
RIGHT flap
gently.
mission
assembly from
other components
d. Remove
bolt (20) securing
actuating
tube (5) to
before
removing from wing.
drive pulley (13)
and lower LEFT flap
gently. Retain
bushing.
d.
Remove bolt (20)
securing actuating
tube (5)
to e.
Remove cable locks
(12) securing
control cables
drive pulley (13).
to drive
pulley (13). Tag cables
for reference on re-
e. Screw
actuating
tube
(5) in toward
transmission
installation.
(7) as far
as possible by hand.
f. Remove bolt
(11) attaching drive pulley
(13) to
f. Remove
bolt (1)
securing flap
motor
hinge (10)
wing
structure.
to
wing. Retain
brass washer
between
hinge and
wing
g. Using care,
remove
drive pulley
through access
structure
for use
on reinstallation.
opening,
being
careful not
to drop bushing.
Retain
g. Disconnect motor
electrical leads at quick-dis-
brass washer
between drive pulley
and wing structure
connects.
for
use on reinstallation.
Tape
open ends
of drive
h. Disconnect
wiring at limit switches (23 and 26).
pulley after removal to protect bearings.
i. Carefully
work
assembly
from wing through
ac-
h. To
remove left
wing drive
pulley, use
this same
cess
opening.
procedure
omitting
step "d".
j. Reverse
preceding
steps
for reinstallation.
If
i.
Reverse the
preceding
steps for reinstallation.
hinge
assembly (10) was
removed from
the transmis-
Rig system
in accordance
with paragraph
7-18, safety
sion (7)
for any reason,
ensure
that short
end of
turnbuckles
and
reinstall all
items removed
for ac-
hinge is
reinstalled
toward
the top.
cess.
k.
Use Loctite grade CV
adhesive on threads
of set-
screw
(6) and collar
(24) whenever actuating
tube (5)
7-12. REPAIR.
Repair
is limited to replacement
of
is removed.
Torque setscrew
to
40 inch-pounds.
bearings.
Cracked,
bent or excessively
worn
drive
1. Complete
operational
check
as outlined
in para-
pulleys
must be
replaced.
Lubricate bearings
as out-
graph
7-3 and rerig
system
in accordance
with para-
lined in Section
2.
graph 7-18 and 7-19.
7-13. FLAPS. (See figure 7-4.)
7-7. REPAIR
Repair consists
of replacement
of
motor,
transmission,
actuating tube and associated
7-14.
REMOVAL AND INSTALLATION.
hardware.
Bearings
in hinge
assembly
may
also
be
a. Run
flaps
to
full DOWN
position.
replaced.
Lubricate
as outlined
in
Section
2.
b. Remove
access
plates
(1) from
top leading
edge
of flap.
7-8.
FLAP CONTROL
LEVER
(See
figure
7-3.)
c. Disconnect
push-pull
rod (6)
at flap
bracket
(7).
d.
Remove bolts (5) at
each flap track. As
flap is
7-9.
REMOVAL AND
INSTALLATION.
removed
from wing, all
washers, rollers
and bush-
a. Remove
follow-up
control torque
tube (17)
from
ings will
fall free.
Retain these
for reinstallation.
switch
mounting arm
(24).
e.
Reverse the
preceding
steps for reinstallation.
b. Remove
flap
operating
switches
(23 and
25) from
If
push-pull
rod
(6) adjustment
is not disturbed,
re-
switch
mounting
arm
(24).
DO
NOT disconnect
elec-
rigging
of system
should
not be
necessary.
Check
trical
wiring
at switches.
flap travel
and
rig in accordance
with paragraph
7-18,
c.
Remove
knob
(15)
from
control
lever
(14).
if necessary.
7-4

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)