TCH.1C-27J-2-27JG
2-27
RUDDER ACTUATOR - REMOVAL AND
INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
).
2.Isolate external hydraulic power (refer to manual
3.Discharge hydraulic pressure by operating the rudder
pedals.
4.Position maintenance platform (AGE NO. 00074).
5.Open the access panel 322E.
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
20,00
Removal
AFM
2
30,00
Installation
AFM
2
40,00
Follow
Maintenance
AFM
2
20,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 220 (Min.)
Total Time Detention System:
110 (Min.)
27-20-20
2-229