TCH.1C-27J-2-27JG
2-24
RUDDER 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.Position maintenance platform (AGE NO. 00074).
4.Remove Pilot seat (refer to manual
).
5.Disable Cargo Ramp.
6.Open the access panels 211DZ, 322E, 322B and
130AD.
7.Open secondary insulation panels in left side rear
fuselage.
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
80,00
Removal
AFM
2
50,00
Installation
AFM
2
60,00
Follow
Maintenance
AFM
2
80,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 540 (Min.)
Total Time Detention System:
270 (Min.)
27-20-05
2-201