TCH.1C-27J-2-27JG
2-54
LH (RH) ELEVATOR ACTUATOR - REMOVAL
AND INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
).
2.Discharge hydraulic system pressure before removing
any hydraulic component.
3.Discharge hydraulic pressure from three elevator
hydraulic accumulators ( two hydraulic accumulators
of the system No 1 and the hydraulic accumulator of
the system No 2).
4.Put in the flight compartment a warning target :
A.DO NOT MOVE THE CONTROL COLUMN.
B.DO NOT OPEN RAMP AND CARGO.
C.DO NOT SUPPLY THE HYDRAULIC SYSTEM.
5.Isolate hydraulic power (refer to manual
6.Disable Ramp & Cargo system.
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Removal
AFM
1
20,00
Installation
AFM
1
25,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 45 (Min.)
Total Time Detention System: 45 (Min.)
27-30-25
2-426