TCH.1C-27J-2-27JG
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00052 PIN, COTTER
MS24665-153
AR
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
2-13.1 REMOVAL. Remove elevator drum and bracket,
proceed as follows:
A.Remove aileron drum and bracket assembly as
follows:
-Disconnect cable control tension nuts from
quadrant.
-Remove nuts, flat washers, and bolts.
-Position ground strap out of the way, then lift
drum and bracket assembly from airplane
frame.
2-13.2 INSTALLATION. Proceed as follows:
A.Attach drum and bracket assembly with ground
strap to air frame with bolts, flat washers, and nuts.
B.Attach servo motor cables to quadrant.
FOLLOW ON MAINTENANCE:
1.Restore hydraulic power system (refer to manual
2.Connect electrical power to aircraft (refer to manual
3.Close the access panels 553A, 553B and 553C.
4.Remove maintenance platform (AGE NO. 00074).
5.Perform the adjustment:
27-10-05
2-88