W DOC AIRBUS | TSM A320F

N1 Mismatch between Engine 1 and Engine 2


TASK 73-00-00-810-873-A
N1 Mismatch between Engine 1 and Engine 2


1. Possible Causes
  • HMU-1 (4000KC1)
  • HMU-2 (4000KC2)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 72-00-00-200-026
Inspection/Check of the PS3 Line
AMM 72-00-00-220-001
Inspection of the PS3 Line Connections
AMM 72-23-00-280-002
Inspection/Check of the PS12 line
AMM 72-23-00-280-003
Inspection/Check of the PS12 Line
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 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
3. Fault Confirmation
Subtask 73-00-00-710-192-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
Subtask 73-00-00-810-123-A ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the crew observation: N1 Mismatch between Engine 1 and Engine 2
   (1) Make sure that the PO fitting on the ECU (4000KS) is clear and not clogged.
  • Do an operational test of the FADEC 1 (2) A (B) on the ground (with engine motoring) AMM 73-29-00-710-040.
   (2) After the flight crew report, if the mismatch occurs at take-off:
     (a) Do the trouble shooting procedure on the engine with the lowest N1 actual.
     (b) On this engine, do a check of the PS12 line to make sure that it is not cracked and/or broken AMM 72-23-00-280-003.
   (3) After the flight crew report, if the mismatch occurs at climb:
     (a) Do the trouble shooting procedure on the engine with the highest N1 actual.
     (b) On this engine, do a check of the PS12 line to make sure that it is not cracked and/or broken AMM 72-23-00-280-003.
   (4) Do a check of the PS3 line AMM 72-00-00-220-001.
   (5) Replace the HMU-1 (4000KC1) ( HMU-2 (4000KC2)) AMM 73-21-10-000-001 and AMM 73-21-10-400-001.
Subtask 73-00-00-810-123-B ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the crew observation: ENG 1 or 2 - Incorrect power at/after take-off (N1 mismatch):
   (1) Make sure that the PO fitting on the ECU (4000KS) is clear and not clogged.
  • Do an operational test of the FADEC 1 (2) A (B) on the ground (with engine motoring) AMM 73-29-00-710-040.
   (2) After the flight crew report, if the mismatch occurs at take-off:
     (a) Do the trouble shooting procedure on the engine with the lowest N1 actual.
     (b) On this engine, do a check of the PS12 line to make sure that it is not cracked and/or broken AMM 72-23-00-280-002.
   (3) After the flight crew report, if the mismatch occurs at climb:
     (a) Do the trouble shooting procedure on the engine with the highest N1 actual.
     (b) On this engine, do a check of the PS12 line to make sure that it is not cracked and/or broken AMM 72-23-00-280-002.
   (4) Do a check of the PS3 line AMM 72-00-00-200-026.
   (5) Replace the HMU-1 (4000KC1) ( HMU-2 (4000KC2)) AMM 73-21-10-000-002 and AMM 73-21-10-400-002.
Subtask 73-00-00-710-193-A ** ON A/C NOT FOR ALL
B. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:35:12 UTC