TCH.1C-27J-2-27JG
2-35
RUDDER TRIM ELECTRICAL ACTUATOR -
REMOVAL AND INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
).
2.Isolate hydraulic power (refer to manual
3.Position maintenance platform (AGE NO. 00074).
4.Open the access panel 322E.
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
1
20,00
Removal
AFM
1
30,00
Installation
AFM
1
35,00
Follow
Maintenance
AFM
1
20,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 105 (Min.)
Total Time Detention System: 105 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00054 Kit, torque wrenches
G0001200001-001**
00074 Kit, aircraft assy platform
G0005100001
27-20-50
2-272