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TCH.1C-27J-2-27JG
2-14
LH (RH) AILERON CABIN CABLE - REMOVAL
AND INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
manual 
TCH.1C-27J-2-00GV
).
2.Isolate hydraulic power (refer to manual
TCH.1C-27J-2-00GV
) .
3.Open the access panels to gain access to LH (RH)
Aileron Cabin Cable 212AZ, 212BZ, 214BZ, 130AH,
130AD and 213AZ (212EZ, 212DZ, 213BZ, 130AE
and 130AG).
4.Remove Pilot (Copilot) seat in order to get access to
LH (RH) Aileron Cabin Cable (refer to manual
TCH.1C-27J-2-25JG
)
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
30,00
Removal
AFM
1
30,00
Installation
AFM
1
35,00
Follow
Maintenance
AFM
2
30,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 185 (Min.)
Total Time Detention System: 125 (Min.)
27-10-05
2-93