N332FR
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.
6 reports on file, 2018-10-23 – 2024-05-27.
Part: WIRE HARNESS — DAMAGED (SLIDE) · airframe 18,815 hrs · 8,356 cycles
AC WAS ON R.O.N. FOR THIS ISSUE. REFERENCE NR 131972 AND 131973 FAULT FOUND DURING EPSU TEST. "ESCAPE SLIDE LT/EPSU (12WL) EMER R. REPAIRED WIRING FOR CONECTOR 60WL
Part: SLIDE RAFT — FAILED (ZONE 200) · airframe 18,815 hrs · 8,356 cycles
DISCREPANCY: AC WAS ON R.O.N. FOR THIS ISSUE. REFERENCE LP315992 ITEM 2, EPSU TEST FAULTED (10WL FWD L) REMOVED AND REPLACED R1 DOOR SLIDE REF. AMM 25-62-44-000-803-A/400-803-A. T/W: F9TAB11302C, DD: 08/24. OPS CHECK GOOD./END/
Part: SHEAR PLATE — CORRODED (FRMS 66-70) · corrosion level 2 · airframe 18,245 hrs · 8,085 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX.L/H CABIN FLOOR AFT-ENTRANCE AREA- L/H LATERAL SHEAR PLATE FR66 AND FR70 HAVE CORROSION AND CRACK DOT 870-011. L/H CABIN AFT FLOOR ENTRANCE AREA LATERAL SHEAR PLATE FR66 TO FR70 REMOVED AND REPLACED IAW A320 SRM 51-72-11-911-001 A320 SRM 51-44-11 AND AMM 320 34-55-11-000-001-A. MX ACTION IS ACCEPTABLE.
Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,245 hrs · 8,085 cycles
REFERENCE AIRBORNE/PEMCO N/R 15088.0288 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. R/H CABIN FLOOR AFT-ENTRANCE AREA- R/H LATERAL SHEAR PLATE FR66 AND FR70 HAVE CORROSION AND CRACK. R/H CABIN AFT FLOOR ENTRANCE AREA LATERAL SHEAR PLATE FR66 TO FR70 REMOVED AND REPLACED IAW A320 SRM 51-72-11-911-001 A320 SRM 51-44-11 AND AMM 320 34-55-11-000-001-A. MX ACTION IS ACCEPTABLE.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 8,486 hrs · 3,684 cycles
DISCREPANCY: EPSU TEST FAILED. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY (11WL). OPS OK. REF. AMM 33-51-38-400-002-A.
Part: PROBE — BLOCKED (PITOT/STATIC SYS) · airframe 562 hrs · 242 cycles
RTO AT 80 TO 100 KTS. FIRST OFFICER AIRSPEED INDICATOR INOP. WEIGHT WAS 150.4 POSSIBLE AUTO BRAKE ISSUE. COULD NOT DISENGAGE AUTOBRAKES AFTER DECEL LIGHT CAME OFF. AC WAS GROUNDED. PER TSM 34-13-81-810-824-A PERFORMED INSPECTION OF THE PITOT PROBE (9DAZ) IAW AMM 34-11-15-200-001. FOUND AND CLEAR BLOCKAGE ON PROBE. PERFORMED OPS OF NORMAL BRAKING SYSTEM IAW AMM 32-42-00-710-001-A. OPS CHECK GOOD NO FURTHER DEFECTS NOTED.