N343FR
Registered owner: WELLS FARGO TRUST CO NA TRUSTEE, MD (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
8 reports on file, 2019-09-10 – 2026-06-14.
Part: BATTERY — NO TEST (ZONE 200) · airframe 22,696 hrs · 10,514 cycles
DURING SCHEDULED HEAVY CHECK EPSU TEST FOUND 10WL FAILED TEST. AIRCRAFT WAS NOT GROUNDED. REMOVED AND REPLACED 10WL EPSU BATTERY IAW AMM 33-51-38-400-002-A OPS TEST GOOD. A/C OK FOR SERVICE. AIRCRAFT WAS RETUNED TO SERVICE.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 17,210 hrs · 7,698 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING THE PRE-HANGAR CHECKS THE EPSU SYSTEM TEST GIVES THE MAINTENANCE MESSAGE: BAT/EPSU (11WL) EMER. LIGHT NEED TO BE TROUBLESHOOTED AS PER TSM 33-51-00-810-855-A REV. 97. REPLACED EPSU BATTERY (11WL) AS PER AMM 33-351-38-400-002-A REV. 97. MX ACTION IS ACCEPTABLE.
Part: SHEAR PLATE — CRACKED (FRMS 69-70) · airframe 17,210 hrs · 7,698 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEAR PLATE FR69-70 CRACKED. REQUIRES REPLACEMENT AS PER SRM 51-472-11-911-001 REV. 40. REPLACED RT SHEAR PLATE FR69-70 AS PER SRM 51-72-11-911-001 REV. 40 MX ACTION IS ACCEPTABLE.
Part: DOOR SILL — CORRODED (FRM 68) · corrosion level 2 · airframe 17,210 hrs · 7,699 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LT AFT DOOR SILL BEAM NUT PLATE HOLE AT FRAME 68 IS BEYOND ADL WITH 100% MATERIAL LOSS WHICH REQUIRES REPAIR AS PER A320 NEO SRM TASK 53-41-14-283-002 REV. 40. PERFORMED REPAIR ON LH AFT DOOR SILL BEAM AS PER A320 NEO SRM 53-41-14-300-001 REV. 40. MX ACTION IS ACCEPTABLE.
Part: DOOR SILL — CORRODED (FRM 68) · corrosion level 2 · airframe 17,210 hrs · 7,698 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON RH AFT DOOR SILL BEAM NUT PLATE HOLE AT FRAME 68 IS BEYOND ADL WITH 100% MATERIAL LOSS WHICH REQUIRES REPAIR AS PER A320 NEO SRM TASK 53-41-14-283-002 REV. 40. PERFORMED REPAIR ON RH AFT DOOR SILL BEAM AS PER A320 NEO SRM 53-41-14-300-001 REV. 40. MX ACTION IS ACCEPTABLE.
Part: SLIDE RAFT — DEFECTIVE (ZONE 200) · airframe 10,610 hrs · 4,744 cycles
DISCREPANCY: REFERENCE LP221910 ITEM 1, DOOR 1L WILL NOT STAY ARMED. CORRECTIVE ACTION: REF. N/R 124265 FOR DETAILS. R&R L1 DOOR SLIDE PACK PER AMM 25-62-44-000-007A/AMM 25-62-44-400-007A. ADJUSTED L1 DOOR GIRT FITTINGS REF. AMM 52-13-31-400-003A. OPS CHECK GOOD. PRESSURISED A/C REF. 05-53-00. T/W F9TAB1100C, DUE 12/2022.
Part: ACTUATOR — FAILED (HORIZONTAL STAB) · airframe 5,643 hrs · 2,458 cycles
DURING MX FOUND THS ONLY MOVING 1/2 DEGREE UP AND DOWN. MX IS T/S, NO ECAM FAULTS. AIRBUS IS ENGAGED. R & R THS ACTUATOR, IAW AMM 27-44-51-400-001-A. OPS CHECK GOOD.
Part: ENGINE — FAILED (NR 2) · airframe 2,889 hrs · 1,239 cycles
SUPPLEMENTAL INFORMATION, LP 1127812 ITEM 1 --- ENG 2 STALL ON CLIMB OUT, ENGINE PARAMETERS HAD N1 - ENGINE STALL 1ST THEN ENGINE FAIL - ECAM DIRECTED US TO DISCHARGE AGENT. EVEN WHEN THROTTLE IDLE - ENGINE FAIL REMAINED. CORRECTIVE ACTION LP1127812-1--REFERENCE LOG PAGE 1127818ITEM 1 FOR CORRECTIVE ACTION. CORRECTIVE ACTION LP1127818-1--THE ARTICLE IDENTIFIED ABOVE WAS REPAIRED AND/ OR INSPECTED IN ACCORDANCE WITH CURRENT FEDERAL AVIATION ADMINISTRATION (FAA) REGULATIONS AND IN RESPECT TO THE WORK ACCOMPLISHED, REPLACEMENT OF THE #2 ENGINE AND IN RESPECT TO THE WORK PERFORMED IS APPROVED FOR RETURN TO SERVICE IN AIRWORTHY CONDITION IN ACCORDANCE WITH 14CFR PART 43 PERTINENT DETAILS OF THE WORK PERFORMED ARE ON FILE AT THIS REPAIR STATION, ON WING SUPPORT UNDER WORK ORDER NR 17645, CUSTOMER WORK SCOPE REFERENCE NR SV3461702.