Cessna T188C - Page 154

MODEL 188
& T188 SERIES
SERVICE
MANUAL
5
Figure
10-3.
Rudder
Assembly
10-4. RUDDER PEDAL
ASSEMBLIES.
10-6.
RUDDER.
10-5. REMOVAL AND
INSTALLATION.
10-7. REMOVAL AND
INSTALLATION. (See
a. Seat may be removed if desired. figure 10-3.)
b. Remove fuselage side access
panels from under
a. Remove fuselage access panels
from below left
left and right doors. and right doors.
c. (Refer to figure
10-1. ) Remove safety wire
and b. Remove screws
securing stinger, disconnect tail
relieve cable tension at turnbuckles (7 and 8). light wire and remove stinger.
d.
(Refer to figure 10-2.) Disconnect
cables from c. Remove
safety wire and relieve
cable tension at
rudder bar arms ( 10 and 11). turnbuckles (index 7 and 8, figure 10-1).
e. Disconnect return springs (5) from pedal arms d. Disconnect control cables at bellcrank (17).
(4). e. With rudder supported, remove bolts (index 1,
f.
Disconnect master cylinders
(6) from rudder figure
10-1) then carefully remove
rudder.
pedals (3). f. Reverse the preceding steps for reinstallation.
g. (BEGINNING WITH AIRCRAFT SERIAL 188-0318) Rig system in accordance with paragraph 10-11,
Disconnect parking brake
cable from cable bracket
safety turnbuckles and
reinstall all items removed
(19). for access.
h. (BEGINNING WITH AIRCRAFT SERIAL 18800573)
Disconnect aileron-rudder
interconnect springs (14)
10-8. REPAIR. Repair of
the rudder may be accom-
from shaft assembly (18). plished as outlined in Section 17.
i. Remove bolts securing bearing blocks (9) and
lift
pedal assemblies out of
aircraft.
10-9. CABLES AND
PULLEYS.
j. Repair or replace parts as necessary and re-
verse the preceding steps
for reinstallation. Refer
10-10. REMOVAL AND
INSTALLATION. (See
to Section 2 for lubrication requirements. Rig sys- figure 10-1.)
ter m accordance
with paragraph 10-11,
safety turn- a.
FORWARD CABLES.
buckles and reinstall all items removed for access. 1. Remove fuselage access panels from below
10-4