What it covers
The system which provides for rapid, complete shutoff of combustible fluids to the engine compartments during emergency procedures. Typical parts are cable, actuator, switch, lever, etc.
Service difficulty reports · 40
Reports filed under 7620, newest first.
| 1996 | 7 |
|---|---|
| 1997 | 6 |
| 1998 | 6 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 3 |
| 2006 | 1 |
| 2007 | 3 |
| 2011 | 1 |
| 2013 | 1 |
| 2017 | 1 |
| 2019 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2026 | 1 |
SDR HNAA2026012300074Engine · auto shutdownNR 2 ENGINE FAILED ON CLIMBOUT AT 91 PERCENT N1. NR 2 ENGINE WAS R & R.SDR HALA2022022200051Engine · failedATB - #2 ENGINE FAILURE OCCURRED AT 100FT AFTER TAKEOFF // PER AIRBUS RECOMMENDATION DOSSIER REFERENCE 81029165, PERFORMED INSPECTION AFTER ENGINE FAILURE PER AMM 05-51-26, NACELLE GVI PER AMM 05-34-00, AND ADDITIONAL CHECKS OF FIRE EXTINGUISHING SYSTEM PER AMSDR HALA2021080300094Sense Line · crackedATB - LEFT ENGINE COMPRESSOR STALL FOLLOWED BY ENG L SYS FAIL IN FLIGHT. // FAULT CODE 732178. PERFORMED FIM 73-21 TASK 873, FOUND P30 SENSE LINE P/N BRH17623 CRACKED. REMOVED LINE. 13971 08/04/21. INSTALLED P30 SENSE LINE PER AMM 72-00-41. PERFORMED HIGH PO
See all 40 reports