W DOC AIRBUS | TSM A320F

Stall of the Engine 1 or 2


TASK 80-00-00-810-833-A
Stall of the Engine 1 or 2


1. Possible Causes
  • tail wind conditions and/or high altitude airport
  • N2 SNSR
  • PS3
  • VSV
  • T25
  • HMU-1 [4000KC1]
  • HMU-2 [4000KC2]
  • ECU [4000KS]
  • fuel pump
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 36-11-00-810-813-A
Loss of Automatic Electrical Closure for the Bleed Pressure Regulator Valve on Engine 1
TSM TASK 36-11-00-810-814-A
Loss of Automatic Electrical Closure for the Bleed Pressure Regulator Valve on Engine 2
TSM TASK 36-11-00-810-829-A
Loss of the Non-Return Function and Temperature Limitation Function of the Bleed Pressure-Regulator Valve of the Engine 1
TSM TASK 36-11-00-810-830-A
Loss of the Non-Return Function and Temperature Limitation Function of the Bleed Pressure-Regulator Valve of the Engine 2
TSM TASK 70-00-00-810-801-A
Engine Failure(s)
AMM 71-00-00-710-006
Minimum Idle Check
AMM 72-00-00-200-003
Procedure After the Engine has Exceeded the Operational Limits
AMM 72-00-00-200-008
Inspection/Check After the Engine has Exceeded the Operational Limits
AMM 72-32-00-200-001
Inspection/Check of the HPC Front Stator Assembly
AMM 72-32-00-210-002
Inspection/Check of the HPC Front Stator Assembly
AMM 73-11-10-000-001
Removal of the Fuel Pump and Filter Assembly
AMM 73-11-10-000-003
Removal of the Fuel Pump and Filter Assembly
AMM 73-11-10-400-001
Installation of the Fuel Pump and Filter Assembly
AMM 73-11-10-400-003
Installation of the Fuel Pump and Filter Assembly
AMM 73-21-10-000-001
Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-000-002
Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-001
Installation of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-002
Installation of the Hydromechanical Unit (HMU)
AMM 73-21-60-000-001
Removal of the Electronic Control Unit (ECU)
AMM 73-21-60-400-001
Installation of the Electronic Control Unit (ECU)
AMM 73-21-60-740-001
Read the CLASS 3 REPORT
AMM 73-21-60-740-007
Correct Time Limited Faults (Non Asterisked) of the Engine Scheduled Maintenance Report
AMM 73-21-60-740-026
Read the CLASS 3 REPORT
AMM 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
3. Fault Confirmation
Subtask 80-00-00-710-117-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not applicable, the confirmation can cause damage to the engine.
4. Fault Isolation
Subtask 80-00-00-810-192-A ** ON A/C NOT FOR ALL
A. If the following failure message is displayed in the post-flight report:
   (1) PRESS REG-V 4001HA1 OR 10HA1 is displayed:
   (2) PRESS REG-V 4001HA2 OR 10HA2 is displayed:
Subtask 80-00-00-810-094-A ** ON A/C NOT FOR ALL
B. This warning is set if a stall condition is detected by the ECU before the engine N2 speed reaches 58 per cent.
This warning may be caused by tail wind conditions and/or high altitude airport.
   (1) If this was the case, an engine restart attempt should be carried out in automatic mode.
  • if an engine restart attempt was successful, no additional maintenance action is required.
   (2) If trouble duplicates:
  • do not interrupt the start sequence and leave the ECU authority for 2 additional start attempts (follow ECAM procedure).
   (3) Consider pointing A/C into the wind for engine start if possible.
If above conditions do not apply:
     (a) Look for failure messages including the following words in FADEC test results and FADEC scheduled maintenance report AMM 73-21-60-740-007: N2 SNSR , PS3 , VSV , T25 .
       1 If any of those messages is present:
       2 If no message is found:
   (4) Do a detailed visual inspection of the VSV control linkage AMM 72-32-00-200-001 and look for any broken or loose components:
  • repair or replace as required.
   (5) If nothing is found:
   (6) If trouble repeats:
   (7) If nothing is found:
Subtask 80-00-00-810-094-C ** ON A/C NOT FOR ALL
B. This warning is set if a stall condition is detected by the ECU before the engine N2 speed reaches 58 per cent.
This warning may be caused by tail wind conditions and/or high altitude airport.
   (1) If this was the case, an engine restart attempt should be carried out in automatic mode.
  • if an engine restart attempt was successful, no additional maintenance action is required.
   (2) If trouble duplicates:
  • do not interrupt the start sequence and leave the ECU authority for 2 additional start attempts (follow ECAM procedure).
   (3) Consider different A/C heading for engine start if possible.
If above conditions do not apply:
     (a) Look for failure messages including the following words in FADEC test results and class 3 report AMM 73-21-60-740-026 : N2 SNSR , PS3 , VSV , T25 .
       1 If any of those messages is present:
       2 If no message is found:
   (4) Do a detailed visual inspection of the HPC Front Stator Assembly AMM 72-32-00-210-002 and look for any broken or loose components:
  • repair or replace as required.
   (5) If nothing is found:
   (6) If nothing is found:
   (7) If trouble repeats:
   (8) If nothing is found:
Subtask 80-00-00-810-094-D ** ON A/C NOT FOR ALL
B. This warning is set if a stall condition is detected by the ECU before the engine N2 speed reaches 58 per cent.
This warning may be caused by tail wind conditions and/or high altitude airport.
   (1) If this was the case, an engine restart attempt should be carried out in automatic mode.
  • if an engine restart attempt was successful, no additional maintenance action is required.
   (2) If trouble duplicates:
  • do not interrupt the start sequence and leave the ECU authority for 2 additional start attempts (follow ECAM procedure).
   (3) Consider pointing A/C into the wind for engine start if possible.
If above conditions do not apply:
     (a) Look for failure messages including the following words in FADEC test results and FADEC scheduled maintenance report AMM 73-21-60-740-007 and class 3 report AMM 73-21-60-740-001: N2 SNSR , PS3 , VSV , T25 .
       1 If any of those messages is present:
       2 If no message is found:
   (4) Do a detailed visual inspection of the VSV control linkage AMM 72-32-00-200-001 and look for any broken or loose components:
  • repair or replace as required.
   (5) If nothing is found:
   (6) If nothing is found:
   (7) If trouble repeats:
   (8) If nothing is found:
Subtask 80-00-00-710-118-A ** ON A/C NOT FOR ALL
C. Do a minimum idle check to make sure that all engine instruments give the correct indication AMM 71-00-00-710-006.
[Rev.8 from Aug 2018] 2026.04.04 04:38:37 UTC