W DOC AIRBUS | TSM A320F

Ram Air Turbine does not retract


TASK 29-22-00-810-803-A
Ram Air Turbine does not retract


1. Possible Causes
  • RAT interlock proximity switch
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 24-41-00-861-002
Energize the Aircraft Electrical Circuits from the External Power
AMM 24-41-00-862-002
De-energize the Aircraft Electrical Circuits Supplied from the External Power
AMM 29-22-00-820-005
Adjustment of the RAT Interlock Proximity Switch
AMM 29-22-00-869-006
Retraction of the Ram Air Turbine (RAT) on the Ground
AMM 29-22-51-000-011
Removal of the RAT Interlock Proximity Switch
AMM 29-22-51-400-011
Installation of the RAT Interlock Proximity Switch
3. Fault Confirmation
Subtask 29-22-00-865-054-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
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 29-22-00-860-056-B
B. Aircraft Maintenance Configuration
   (1) Open the access panel 197EB.
   (2) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
   (3) On the RAT ground control-panel (3GE):
  • Set the 28VDC switch to the ON position.
  • Set the LAMP TEST switch to the test position and make sure that all lights come on.
   (4) Retract the RAT AMM 29-22-00-869-006.
   (5) During the retraction of the RAT:
  • Obey the interlock warning light in the RAT control panel (3GE).
  • Obey the operation of the RAT.
4. Fault Isolation
Subtask 29-22-00-810-053-B
A. If the RAT starts to retract but returns to its fully extended position and the interlock warning light on the RAT control panel (3GE) comes on:
   (1) If the fault continues:
Subtask 29-22-00-860-057-B ** ON A/C NOT FOR ALL
B. Do the fault confirmation procedure as given in Para. 3. to make sure that the operation is correct.
5. Close-up
Subtask 29-22-00-860-058-B
A. Put the aircraft back to the serviceable condition.
   (1) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
   (2) Close the access panel 197EB.
[Rev.8 from Aug 2018] 2026.04.04 04:29:28 UTC