TCH.1C-27J-2-27JG
2-46
ELEVATOR CABLE - 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.Disable Cargo Ramp.
4.Open thermal insulation screen.
5.Remove Pilot (Copilot) seat (refer to manual
) in order to get access to LH
(RH) elevator cable.
6.To gain access to LH (RH) elevator cable, open the
access panels:
A.212AZ (212EZ).
B.212BZ (212DZ).
C.214BZ (213BZ).
D.213AZ.
E.130AH (130AE).
F.130AD (130AG).
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
60,00
Removal
AFM
2
60,00
Installation
AFM
2
80,00
Follow
Maintenance
AFM
2
60,00
27-30-05
2-355