TCH.1C-27J-2-27JG
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00074 Kit, aircraft assy platform
G0005100001
00181 Kit, flight controls rigging
pins
11G001-C052200-801
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00010 PIN, COTTER
MS24665-155
2,00
00011 NUT, SELF-LOCKING H14-3
4,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
2-25.1 REMOVAL. Proceed as follows:
A.Lock the quadrant (cockpit under floor) and rear
rudder quadrant in the vertical fin by means of
rigging pins.
B.Toggle the tension regulator at frame 7 (bulkhead
separating flight compartment from cargo
compartment).
C.Open secondary insulation panels in left side rear
fuselage.
D.Remove the two fair lead in the following way:
-Unscrew the two bolts, collect washers and
nuts, and remove the fair lead.
E.Remove the two cotter pins that fix the rudder
cable with rudder quadrant.
(Cont'd)
27-20-05
2-207