Installation of the Eye-End of the RAT Actuator

TASK 29-22-53-400-007-A
Installation of the Eye-End of the RAT Actuator

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.

MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.

WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.

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. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	SAFETY BARRIER(S)
No specific	1	WARNING NOTICE(S)
No specific	Torque wrench: range to between 5.29 and 4.74 m.daN (39.01 and 34.96 lbf.ft )
No specific	Torque wrench: range to between 8.81 and 8.13 m.daN (64.97 and 59.96 lbf.ft )

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.06LCG9)	Non Hardening Jointing Putty-Medium Temp. Area - -
(Material No.14QFB1)	Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -

C. Referenced Information

REFERENCE	DESIGNATION
TASK 29-00-00-864-001-A	Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 29-14-00-614-001-A	Depressurization of the Hydraulic Reservoirs
TASK 29-22-00-820-004-A	Adjustment of the RAT Doors
TASK 29-22-00-869-005-A	Extension of the Ram Air Turbine (RAT) on the Ground
Eye-End of the RAT Actuator

3. Job Set-up
Subtask 29-22-53-860-072-B

A. Aircraft Maintenance Configuration
(1) Make sure that the SAFETY BARRIER(S) is in position.
(2) Make sure that the WARNING NOTICE(S) is in position to tell persons not to pressurize the Blue hydraulic system.

In the cockpit on the hydraulic section 40VU of the overhead panel
On the ground service panel of the Blue hydraulic system.

(3) Make sure that the Blue hydraulic system is depressurized and put it in the maintenance configuration.
(Ref. AMM TASK 29-00-00-864-001).
(4) Make sure that the reservoir of the Blue hydraulic system is depressurized.
(Ref. AMM TASK 29-14-00-614-001).
(5) Make sure that the RAT is extended (Ref. AMM TASK 29-22-00-869-005).

Subtask 29-22-53-865-069-A

B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	HYD/RAT/CTL	2801GE	D14
** ON A/C NOT FOR ALL
49VU	HYD/RAT/CTL	2801GE	B13
** ON A/C ALL
106VU	CSM/G /EV/MAN/SPLY	6XE	B04
121VU	HYDRAULIC/RAT/SPLY/EXTN/SOL1	2803GE	P33

4. Procedure
Subtask 29-22-53-420-059-B

A. Installation of the Eye-End of the RAT Actuator
(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Apply the Non Hardening Jointing Putty-Medium Temp. Area - - (Material No.06LCG9) to the thread of the eye-end (4).
(5) Assemble the nut (3) and the locking device (2) on the eye-end (4).
(6) Install the eye-end (4) in the RAT actuator (1).
(7) Turn the eye-end (4) until the distance "Y" is the same as you recorded during the removal procedure.
(8) Tighten the nut (3) and make sure that the serrations of the locking device (2) engage correctly.
(9) TORQUE the nut (3) to between 8.81 and 8.13 m.daN (64.97 and 59.96 lbf.ft )

.
(10) Safety the nut (3) and the locking device (2) with the lockwire, 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
(11) Put the eye-end (4) in its correct position at the leg assembly (5).
(12) Install the bolt (6), the washers (7), (8) and the nut (9).
(13) TORQUE the nut (9) to between 5.29 and 4.74 m.daN (39.01 and 34.96 lbf.ft )

Subtask 29-22-53-820-052-B

B. Adjustment of the RAT Actuator
(1) Make sure that the adjustment of the RAT actuator is correct. If necessary, do the adjustment procedure of the RAT actuator (Ref. AMM TASK 29-22-00-820-004).

5. Close-up
Subtask 29-22-53-860-073-B

A. Put the aircraft back to the serviceable condition.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.04.01 00:26:28 UTC