TCH.1C-27J-2-27JG
2-10
LH (RH) AILERON FUSELAGE CABLE -
REMOVAL AND INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
).
2.Remove Pilot (Copilot) seat (refer to manual
).
3.Isolate hydraulic power (refer to manual
4.Position maintenance platform (AGE NO. 00074).
5.Open the access panels 553A, 553B and 553C.
6.To gain access to LH (RH) Aileron open following
access panels 212AZ, 212BZ, 214BZ, 130AD, 130AH
and 213AZ (212EZ, 212DZ, 213BZ, 130AE and
130AG).
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
1
15,00
Removal
AFM
1
40,00
Installation
AFM
1
45,00
Follow
Maintenance
AFM
1
15,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 115 (Min.)
Total Time Detention System: 115 (Min.)
27-10-05
2-60