W DOC AIRBUS | AMM A320F

Servicing of the Ram Air Turbine (RAT)


TASK 12-13-29-600-001-A
Servicing of the Ram Air Turbine (RAT)


FIN: 2GE
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
No specific
Torque wrench: range to between 12.5 and 9.2 lbf.ft (1.69 and 1.25 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03ABB1)
Synthetic base Lubricating Oil-Turbine Engine Low Temp. -
(Material No.14QFB1)
Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
195EB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
PACKING
AIPC 29-22-51-01-050
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 29-10-00-864-003-A
Depressurize the Blue Hydraulic System
TASK 29-22-00-869-005-A
Extension of the Ram Air Turbine (RAT) on the Ground
TASK 29-22-00-869-006-A
Retraction of the Ram Air Turbine (RAT) on the Ground
3. Job Set-up
Subtask 12-13-29-860-050-A
A. Aircraft Maintenance Configuration
   (1) Depressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-864-003).
   (2) Extend the Ram Air Turbine (RAT) (Ref. AMM TASK 29-22-00-869-005).
   (3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
   (4) Put the WARNING NOTICE(S) 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.
Subtask 12-13-29-010-050-A
B. Get Access
   (1) Open the access door 195EB.
Subtask 12-13-29-865-050-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GED14
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GEB13
** ON A/C ALL
106VUCSM/G /EV/MAN/SPLY6XEB04
121VUHYDRAULIC/RAT/SPLY/EXTN/SOL12803GEP33
4. Procedure
Subtask 12-13-29-612-050-A
A. Oil Replenishing of the Lower RAT Gearbox
   (1) Remove and discard the lockwire from the oil fill plug (1).
   (2) Remove the oil fill plug (1).
   (3) Fill the RAT gearbox with Synthetic base Lubricating Oil-Turbine Engine Low Temp. - (Material No.03ABB1) , until it spills from the fill port.
   (4) Clean the oil fill plug (1) with a clean lint-free cloth Textile-Lint free Cotton - (Material No.14SBA1) .
   (5) If necessary install a new AIPC 29-22-51-01-050 PACKING (2) on the fill plug (1).
   (6) Install the fill plug (1) in the lower gearbox (3).
   (7) TORQUE the fill plug (1) to between 12.5 and 9.2 lbf.ft (1.69 and 1.25 m.daN )
T.
   (8) Safety the oil fill plug (1) with the lockwire 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
5. Close-up
Subtask 12-13-29-865-051-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GED14
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GEB13
** ON A/C ALL
106VUCSM/G /EV/MAN/SPLY6XEB04
121VUHYDRAULIC/RAT/SPLY/EXTN/SOL12803GEP33
Subtask 12-13-29-410-050-A
Subtask 12-13-29-860-051-A
C. Put the aircraft back to its initial configuration.
   (1) Retract the RAT (Ref. AMM TASK 29-22-00-869-006).
   (2) Remove the SAFETY BARRIER(S).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.03.31 22:55:16 UTC