43.51 lbf.ft).
(23)
TORQUE the union nut (30) to between 2.9 and 3.2 m.daN (21.38 and
23.59 lbf.ft).
(24)
TORQUE the nut (46) to between 4.74 and 5.29 m.daN (34.95 and 39.01 lbf.ft).
NOTE : An axial gap of 1.32 mm (0.0519 in.) to 1.82 mm (0.0716 in.)
____ between the forked mounting (43) and the washers (41) is permitted.
Subtask 29-22-53-790-052
C. Leak Test of the Hydraulic Connections
(1)
Remove the container from below the hydraulic connections.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Pressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-002).
(4)
Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
(5)
Examine the hydraulic connections of the ejection jack and make sure that there are no leaks.
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(6)
Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003). Subtask 29-22-53-820-053
D.
Adjustment of the RAT Doors
(1)
Do the adjustment procedure of the RAT doors (Ref. TASK 29-22-00-820-004).
(2)
If you can not adjust the doors correctly, do the adjustment procedure of the RAT actuator (Ref. TASK 29-22-00-820-004).
Subtask 29-22-53-869-052
E. Retract the RAT (Ref. TASK 29-22-00-869-006). Subtask 29-22-53-710-060
F. Do an operational test of the automatic deployment of the RAT (Ref. TASK 29-22-00-710-006).
5. Close-up
________ Subtask 29-22-53-410-059
A. Close Access
(1)
Put the protective cover (2) in the correct installation position over the deployment solenoids (Ref. Fig. 402/TASK 29-22-53-991-011) .
(a)
Tighten the screws (1) in the quick release fasteners (3).
(b)
Install the screw (5) in the protective cover (2).
(2)
Install the access panels 147BB, 147CB.
(3)
Close the main gear main door (Ref. TASK 32-12-00-010-001).
(4)
Close the access door 195BB. Subtask 29-22-53-942-056
B.
Put the aircraft back to the serviceable condition.
(1)
Remove the access platform(s).
(2)
Remove the safety barrier.
(3)
Remove the warning notice(s).
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INTENTIONALLY BLANK
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29-22-53Page 426
1 1 Config-1 Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-061, 101-105, 201-203,
TASK 29-22-53-000-007 Removal of the Eye End of the RAT Ejection Jack (2454GE) WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU
_______
EXTEND/RETRACT THE RAT.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice(s)
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B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-22-00-869-001 Extension of the Ram Air Turbine (RAT) on the Ground 29-22-53-991-008 Fig. 404
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