W DOC AIRBUS | TSM A320F

Thrust Reverser Deployed Position Set with No Reverse Indication on Engine 2



1. Possible Causes
· HCU-THRUST REV (4101KS)
2 Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
Ref. AMM 78-30-00-440-012 Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after
Ground Maintenance
Ref. AMM 78-30-00-440-013 Activation of the Thrust Reverser System for Flight
Ref. AMM 78-31-00-710-041 Operational Test of the Thrust Reverser System with the CFDS
Ref. AMM 78-31-51-000-010 Removal of the Thrust Reverser Hydraulic Control Unit
Ref. AMM 78-31-51-400-010 Installation of the Thrust Reverser Hydraulic Control Unit
Ref. AMM 78-32-00-860-010 Manual Extension of the Thrust Reverser Translating Sleeves
Ref. AMM 78-32-00-860-011 Manual Retraction of the Thrust Reverser Translating Sleeves
3. Fault Confirmation
Subtask 78-30-00-710-080-A
A. Test
Not applicable.
4. Fault Isolation
Subtask 78-30-00-810-065-A
A. If the fault symptom is identified by the crew observation: T/R REV-deployed position set, no reverse
indication on engine 2:
· make sure that the thrust reverser lockout pins are not in their de-activation positions Ref.
AMM 78-30-00-440-013 .
(1) If the fault continues:
· make sure that the HCU lock lever is in the unlock position Ref. AMM 78-30-00-440-012 .
(2) If the fault continues:
· make sure that the translating sleeves move freely Ref. AMM 78-32-00-860-010 and Ref.
AMM 78-32-00-860-011 .
(3) If the fault continues:
· replace the HCU-THRUST REV (4101KS) Ref. AMM 78-31-51-000-010 and Ref.
AMM 78-31-51-400-010 .
Subtask 78-30-00-710-081-A
B. Do the operational test of the thrust reverser system with the CFDS (through FADEC 2A and 1B menus)
Ref. AMM 78-31-00-710-041 . [Rev.6 from Feb 2017] 2026.04.04 04:38:06 UTC