Core Exhaust Nozzle Type Discrepancy on Engine 1
TASK 73-20-00-810-977-A
Core Exhaust Nozzle Type Discrepancy on Engine 1
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 73-20-00-710-324-A ** ON A/C NOT FOR ALL
Subtask 73-20-00-810-279-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:35:32 UTC
Core Exhaust Nozzle Type Discrepancy on Engine 1
1. Possible Causes
- J14 Identification connector
- ECU [4000KS]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| 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 73-21-60-740-005 | Entry of the Core Chevron Nozzle Status Through MCDU |
| AMM 73-21-90-000-002 | Removal of the Engine Identification Connector |
| AMM 73-21-90-400-002 | Installation of the Engine Identification Connector |
| AMM 73-21-90-860-001 | Programming of the Identification Plug (Push-Pull Design) for SAC engines |
| AMM 73-29-00-710-040 | Operational Test of the FADEC on the ground (with Engine Motoring) |
Subtask 73-20-00-710-324-A ** ON A/C NOT FOR ALL
A. Test
(1) Do the operational test of the FADEC on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation(1) Do the operational test of the FADEC on the ground (with engine non motoring) AMM 73-29-00-710-040.
Subtask 73-20-00-810-279-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J14WRONG, ECU ENTRY:
Subtask 73-20-00-710-325-A ** ON A/C NOT FOR ALL - Visually verify the nozzle configuration:
NOTE: There are two configuration of core exhaust nozzle.
- Standard nozzle configuration is identified by a smooth conical exit surface
- Core chevron nozzle configuration is identified by 8 chevrons (triangular) around the circumference of the exit surface (SB RA32078-118).
(1) If a standard nozzle configuration is physically installed: - Standard nozzle configuration is identified by a smooth conical exit surface
- Core chevron nozzle configuration is identified by 8 chevrons (triangular) around the circumference of the exit surface (SB RA32078-118).
- On the left or right MCDU, get access to the ENGINE MAIN MENU screen.
- Push the line key (3L) adjacent to the LRU IDENT REPORT:
- Replace the J14 Identification connector AMM 73-21-90-000-002 and AMM 73-21-90-400-002 or Do Re-programming of the Identification Connector (Push-pull design only) to a standard nozzle configuration AMM 73-21-90-860-001.
- Do a configuration change of the Core Chevron Nozzle status on LRU IDENT REPORT AMM 73-21-60-740-005.
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
- On the left or right MCDU, get access to the ENGINE MAIN MENU screen.
- Push the line key (3L) agjacent to the LRU IDENT REPORT:
- Replace the J14 Identification connector AMM 73-21-90-000-002 and AMM 73-21-90-400-002 or Do Re-programming of the Identification Connector (Push-pull design only) to a core chevron nozzle configuration AMM 73-21-90-860-001.
- Do a configuration change of the Core Chevron Nozzle status on LRU IDENT REPORT AMM 73-21-60-740-005.
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
B. Do the test given in Para. 3.A.