N338FR
Registered owner: UMB BANK NA TRUSTEE, UT (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.
7 reports on file, 2022-06-30 – 2024-03-08.
Part: SUPPORT — CORRODED (FRMS 16-20) · corrosion level 2 · airframe 17,610 hrs · 7,802 cycles
REFERENCE LTPR NR 5001304676-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRODED CENTER SILL SHAPE ON LH SIDE FWD CABIN BETWEEN FR16-20, NO ALLOWABLE DAMAGE LIMIT FOUND ON SRM. REPLACEMENT IS REQUIRED AS PER A320 NEO SRM 51-72-11 REV. 39, REPLACED SILL SHAPE ON LH SIDE FWD CABIN BETWEEN FR16-20 AS PER A320 NEO SRM 51-72-11 REV. 39.
Part: SEAT TRACK — CORRODED (FRMS 12-21) · corrosion level 2 · airframe 17,610 hrs · 7,802 cycles
REFERENCE LTPR NR 5001304700-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRODED RAIL Y254 ON FWD CABIN BETWEEN FR 12-21 REPLACEMENT REQUIRED AS PER A320 NEO SRM 51-72-11 REV 39. REPLACED RAIL Y254 BETWEEN FR12-21 AS PER A320 NEO SRM 51-72-11 REV. 39.
Part: SHEAR PLATE — CRACKED (FRMS 69-70) · airframe 17,610 hrs · 7,802 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. RH SHEAR PLATE WITH CRACK BETWEEN FRAMES 69-70 REQUIRES REPLACEMENT AS PER A320 NEO SRM 51-72-11-911-001 REV 39. PERFORMED REPLACEMENT OF RH PLATE BETWEEN FRAMES 69-70 AS PER A320 NEO SRM 51-72-11-911-001 REV. 39 MX ACTION IS ACCEPTABLE.
Part: SHEAR PLATE — CRACKED (FRMS 69-70) · airframe 17,610 hrs · 7,802 cycles
AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. LH SHEAR PLATE WITH CRACK BETWEEN FRAMES 69-70 REQUIRES REPLACEMENT AS PER A320 NEO SRM 51-72-11-911-001 REV 39 PERFORMED REPLACEMENT OF LH PLATE BETWEEN FRAMES 69-70 AS PER A320 NEO SRM 51-72-11-911-001 REV. 39 MX ACTION IS ACCEPTABLE.
Part: DOOR SILL — CORRODED (FRM 68) · corrosion level 2 · airframe 17,610 hrs · 7,802 cycles
REFERENCE LTPR NR 5001304768-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LH AFT DOOR SILL BEAM NUT PLATE AT FRAME 68 REQUIRES REPAIR AS PER A320 NEO SRM 53-41-14-300-001 REV. 39 REPAIRED LH AFT DOOR SILL BEAM AS PER A320 NEO SRM 53-41-14-300-001 REV 39 MX ACTION IS ACCEPTABLE.
Part: CABIN AIR SYS — CONTAMINATED · airframe 13,464 hrs · 5,953 cycles
STRONG ODOR OF DEICE FLUID IN COCKPIT AND CABIN. PERFORMED IDENTIFICATION CAUSE FOR CABIN ODOR IAW TSM 05-50-00-810-831-A SUBTASK 05-50-00-810-085-E, TYPE 8 CAUSED BY DE-ICING FLUID INGESTION. PERFORMED LEVEL A DECONTAMINATION IAW AMM 21-00-00-615-802-A REF 214905-2. AC OK FOR SERVICE. NR 1 & 2 ENGS RAN FOR ODOR IAW AMM 71-00-00-860-827-A, AMM 71-00-00-860-829-A. RUN CHECK GOOD. NO DEFECTS NOTED NOTED AT THIS TIME. AC OK FOR SERVICE.
Part: CYLINDER — LEAKING (ZONE 800) · airframe 11,886 hrs · 5,257 cycles
DISCREPANCY: REFERENCE LP253472 ITEM 3: L2 DOOR ASSIST/DAMPER LEAKING. CORRECTIVE ACTION: REMOVED AND REPLACED L2 DOOR DAMPER/CYLINDER PER AMM 52-13-14-400-001-B