Service difficulty report · Wire · Airbus A330243

Difficulty date
January 6, 2020
Submitted
January 11, 2020
Operation
Air carrier
Aircraft
N973AV
Make and model
Airbus A330243
Aircraft serial
1073
Aircraft time
47,338 hours, 8,910 cycles
Engine
Rroyce RB211TRENT77
Engine time
17,777 hours, 4,165 cycles
Part
Wire
Condition
Chafed
Location
Nr 1 Engine
Stage of operation
UK
How discovered
O
Nature of condition
J
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

JAN 06 FLIGHT AV7 (MIA-BOG), PILOT REPORT WO 15953283 "ENG 1 FUEL FILTER CLOG PRESENTED ON ECAM" 1ST & CORRECTIVE ACTION JAN 06 -> IN ACCORDANCE WITH AMM TASK 73-11-41-000-802-A AND AMM 73-11-41-400-802-A WAS REMOVED AND REPLACED LP FUEL FILTER ELEMENT, FUEL AND OIL LEAK CHECK PERFORMED SATISFACTORY,

JAN 06 FLIGHT AV20 (BOG-JFK), PILOT REPORT WO 15953285 -> BEFORE TAKE OFF ENG 1 FUEL FILTER CLOG ON ECAM 1ST ACTION JAN 06 -> THIS ITEM IS PLACED ON DMI (MEL/CDL) LOGBOOK PAGE 12484 ITEM 1 N973AV-MCCCN-2020-AV0027 WO 15953285 MEL 73-30-03 PROV 1A CAT "C". 2ND ACTION JAN 07 -> IN ACCORDANCE WITH AMM TASK 73-41-00-802-A AND AMM TASK 73-11-41-400-802-A THE LP FUEL FILTER WAS REMOVED AND INSTALLED. 3RD & CORRECTIVE ACTION JAN 07 -> IN ACCORDANCE WITH AMM 73-34-11-41-000-802-A / 400-802A THE LOW PRESSURE FUEL FILTER WAS REPLACED. IN ACCORDANCE WITH AMM 73-34-11-000-803-A/400-803-A FUEL FILTER DIFERENTIAL PRESSURE SWICTH REPLACED. IAW AMM 71-00-00-860-810 IDLE CHECK PERFORMED. TEST SATISFACTORY. NO LEAK WAS FOUND.

JAN 06 FLIGHT AV249 (BOG-GRU), PILOT REPORT WO 15953407 -> BY DMI WO 15953285 BEFORE TAKE OFF ENG 1 FUEL FILTER CLOG ON ECAM. 1ST ACTION JAN 06 -> THIS ITEM IS DEFERRED TO WO DMI 15953407 IN ACCORDANCE MEL ITEM 73-30-03 PROV 1A CAT "C" MCC AUT N973AV-CNMCC-2020-AV0033 DMI LOG PAGE 16484 ITEM 2 2ST ACTION JAN 08 -> IN ACCORDANCE WITH TSM 73-21-79-810-803-A FUEL FILTER CLOGGED ON ENG 1 SUBTASK 73-21-79-810-058-A STEP C.2 A-B-C WERE ACCOMPLISHED AND THESE WERE FOUND WITHIN LIMITS. NEXT STEP REPLACE THE EEC. 3ST ACTION JAN 08 -> IN ACCORDANCE WITH AMM TASK 73-21-34-000-804 AND TASK 73-21-34-400-804-A THE EEC WAS REMOVED AND REPLACED. 4TH ACTION JAN 09 -> THE TESTS WERE PERFORMED SATISFACTORY FOR EEC CHANGE. THE ENGINE IDLE RUN UP WAS PERFORMED AND THE MESSAGE SHOWS AGAIN. 5TH & FINAL CORRECTIVE ACTION JAN 09 -> IN ACCORDANCE WITH TSM 73-21-79-810-803-A THE WIRING CHECK WAS PERFORMED, WAS FOUND A CHAFING, WAS REPAIRED IAW AMM 70-71-28-300-802-A, ENG IDLE RUN UP PERFORMED WITH SATISFACTORY RESULTS. CLOSING WO: 15953419

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