TCH.1C-27J-2-27JG
2-42
ELEVATOR TENSION REGULATOR -
REMOVAL AND INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Close the cargo door if open.
2.Perform ELEVATOR TRIM (normal/standby) to '0'
position.
3.Discharge hydraulic pressure and isolate hydraulic
power.
4.Disconnect electrical power from aircraft (refer to
).
5.Remove Pilot and Copilot seat refer to (refer to
6.Remove the LH (RH) ballistic protection panels from
flight compartment.
7.Remove the fwd track LH (RH) assy.
8.Open the access panels 211DZ and 130A (211GZ
and 130D).
9.Position maintenance platform (AGE NO. 00074).
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
80,00
Removal
AFM
2
60,00
Installation
AFM
2
80,00
Follow
Maintenance
AFM
2
80,00
Periodicity: AR - AS REQUIRED
27-30-05
2-338