TCH.1C-27J-2-27JG
2-17
AILERON TRIM TAB 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.Remove the Sequencer Unit (refer to manual
).
5.Remove the cover tip.
6.Remove the access 544E panel.
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
ELT
1
10,00
Removal
ELT
1
20,00
Installation
ELT
1
25,00
Follow
Maintenance
ELT
1
10,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 65 (Min.)
Total Time Detention System: 65 (Min.)
27-10-10
2-133