W DOC AIRBUS | TSM A320F

Continuous Running of the Power Transfer Unit (PTU) After Start in Sequence of Engine 1 and Engine 2


TASK 29-23-00-810-805-A
Continuous Running of the Power Transfer Unit (PTU) After Start in Sequence of Engine 1 and Engine 2


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 29-23-00-810-802-A
Continuous Running of the Power Transfer Unit (PTU)
AMM 29-13-15-000-001
Removal of the Power Transfer Unit (PTU) Manifold of the Yellow Hydraulic System
AMM 29-13-15-400-001
Installation of the Power Transfer Unit (PTU) Manifold of the Yellow Hydraulic System
AMM 71-00-00-710-003
Engine Automatic Start
AMM 71-00-00-710-028
Engine Shutdown
3. Fault Confirmation
Subtask 29-23-00-710-058-A
A. Do this test.
   (1) Make sure that the PTU P/BSW is in the AUTO position.
   (2) Start the engine No. 1 AMM 71-00-00-710-003.
   (3) Start the engine No. 2 AMM 71-00-00-710-003.
   (4) Do a check of the PTU for continuous running.
     (a) If there is continuous running, do the subsequent steps:
       1 On the overhead panel 40VU, set the GREEN/ENG 1 PUMP P/BSW to the OFF position, and after some seconds, back to the ON position.
NOTE: The GREEN/ENG 1 PUMP is set back to its initial configuration when you set the GREEN/ENG 1 PUMP P/BSW to ON again.
       2 Do again a check for continuous running of the PTU.
   (5) Shut down the engines AMM 71-00-00-710-028.
4. Fault Isolation
Subtask 29-23-00-810-056-C
A. If after start of the engine No. 2:
   (1) The PTU starts continuous running and stops after you have switched off and on the GREEN/ENG 1 PUMP P/BSW:
   (2) If the fault continues:
Subtask 29-23-00-710-059-A
B. Do the fault confirmation procedure as given in Para. 3. to make sure that operation is correct.
[Rev.8 from Aug 2018] 2026.04.04 04:29:28 UTC