N358FR

AIRBUS A320-251N · 2019 · Fixed-wing multi-engine · 2 engines · 190 seats · Valid Registration

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.

12 reports on file, 2022-07-01 – 2026-04-09.

NO TEST · 2026-04-09 Matched by certificate designator
ATA 3350

Part: BATTERY — NO TEST (ZONE 200) · airframe 20,398 hrs · 9,458 cycles

NR 3 EPSU BATTERY 10WL FWD L FAILED TEST, AIRCRAFT WAS NOT GROUNDED, SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (10WL) IAW AMM 33-51-38-000-002-A/33-51-38-400-002-A. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR F3LA202604100399
NO TEST · 2026-04-09 Matched by certificate designator
ATA 3350

Part: BATTERY — NO TEST (ZONE 200) · airframe 20,398 hrs · 9,458 cycles

EPSU BATTERY 11WL EMER L FAILED TEST, AIRCRAFT WAS NOT GROUNDED AS A RESULT OF THE SDR REPORTABLE EVENT, SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (11WL) IAW AMM 33-51-38-000-002-A/33-51-38-400-002-A. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR F3LA202604100398
OTHER · 2025-03-01 Matched by certificate designator
ATA 5320

Part: PANEL — CORRODED (ZONE 100) · airframe 17,377 hrs · 7,933 cycles

AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT THRESHOLD PANEL 261LG FOUND WITH CORROSION UPPER AND LOWER SKIN OF PANEL. REMOVAL OF CORROSION TO BE PERFORMED IAW EO-A32F-53-29845-00 FINAL. UPPER AND LOWER CORROSION REMOVED FROM PANEL 261LG IAW EO-A32F-53-29845-00 FINAL.

Source: SDR F3LA202503020194
OTHER · 2025-03-01 Matched by certificate designator
ATA 5320

Part: PANEL — CORRODED (ZONE 100) · airframe 17,377 hrs · 7,933 cycles

REFERENCE LTPR NR 5001376812-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT THRESHOLD PANEL 262LG FOUND WITH CORROSION UPPER AND LOWER SKIN OF PANEL. REMOVAL OF CORROSION TO BE PERFORMED IAW EO-A32F-53-29845-00 FINAL. UPPER AND LOWER CORROSION REMOVED FROM PANEL 262LG IAW EO-A32F-53-29845-00 FINAL.

Source: SDR F3LA202503020195
OTHER · 2025-02-25 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 17,377 hrs · 7,933 cycles

REFERENCE LTPR NR5001376477-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING DVI OF CABIN FLOOR FOUND FLOOR BEAM Y1292 AT FR12-21 CORRODED. REPLACEMENT REQUIRED AS PER SRM A320NEO 51-72-11-911-001 REV 43. FLOOR BEAM Y1292 AT FR 12-21 REPLACED AS PER A320NEO SRM 51-72-11-911-001 REV 43.

Source: SDR F3LA202502270188
OTHER · 2025-02-25 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 17,377 hrs · 7,933 cycles

REFERENCE LTPR NR5001376659-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEARPLATE FR 69-70 CRACKED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 43. R/H SHEARPLATE WAS REPLACED AS PER SRM 51-72-11 REV 43.

Source: SDR F3LA202502270192
OTHER · 2025-02-25 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 17,377 hrs · 7,933 cycles

REFERENCE LTPR NR5001376476-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING DVI OF CABIN FLOOR FOUND FLOOR RAIL-Y81 AT FR12-14 CORRODED. REPLACEMENT REQUIRED AS PER SRM 51-72-11-911-001 REV 43. FLOOR RAIL Y81 AT FR12-14 REPLACED AS PER SRM 51-72-11-911-001 REV 43.

Source: SDR F3LA202502270190
OTHER · 2025-02-25 Matched by certificate designator
ATA 5320

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 17,377 hrs · 7,933 cycles

DISCREPANCY: REFERENCE LTPR NR5001376658-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND L/H SHEARPLATE FR 69-70 CRACKED. REQUIRES REPLACEMENT AS PER SRM 51-72-11 REV 43. L/H SHEARPLATE WAS REPLACED AS PER SRM 51-72-11 REV 43.

Source: SDR F3LA202502270191
OTHER · 2025-02-25 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 17,377 hrs · 7,933 cycles

REFERENCE LTPR NR5001376656-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING DVI FOUND FLOOR BEAM Y-765 AT FR66-70 CORRODED REPLACEMENT REQUIRED AS PER SRM 51-72-11 REV 43. FLOOR BEAM Y-765 AT FR66-70 REPLACED AS PER SRM 51-72-11 REV 43.

Source: SDR F3LA202502270187
OTHER · 2025-02-25 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 17,377 hrs · 7,933 cycles

REFERENCE LTPR NR5001376475-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING DVI OF CABIN FLOOR FOUND FLOOR BEAM Y-254 AT FR12-21 CORRODED. REPLACEMENT REQUIRED AS PER A320NEO SRM 51-72-11-911-001 REV43. FLOOR BEAM Y-254 AT FR12-21 REPLACED AS PER A320NEO SRM 51-72-11-911-001 REV 43.

Source: SDR F3LA202502270186
OTHER · 2025-02-25 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 17,377 hrs · 7,933 cycles

REFERENCE LTPR NR5001376475-0050 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING DVI OF CABIN FLOOR CRACK WAS FOUND ON FWD CABIN WET AREA FLOOR BEAM-Y189 BETWEEN FR20-24. REPLACEMENT IS REQUIRED AS PER A320 SRM 51-72-911-001-REV 43. PERFORMED REPLACEMENT OF THE FLOOR BEAM-Y189 BETWEEN FR 20-24 AS PER A320NEO SRM 51-72-11-911-001 REV 43.

Source: SDR F3LA202502270189
FLUID LOSS · 2022-07-01 Matched by certificate designator
ATA 2913

Part: LINE — LEAKING (ZONE 200) · airframe 8,694 hrs · 3,839 cycles

DISCREPANCY:REFERENCE LP 277359 ITEM 1; HYD Y RSVR LO LVL Y ENG 2 PUMP LO PR Y SYS LO PR ECAM YELLOW HYD FLUID LEVEL IS NIL CORRECTIVE ACTION: PERFORMED INSPECTION OF ENG 2 PYLON FOUND SOURCE OF LEAK. REMOVED AND REPLACED PRESS ASSY P/N D2902083800000, REF AMM 29-13-49-400-812-A, SERVICED YELLOW HYD RES REF AMM 12-12-29-611-001, PERFORMED OPS TEST OF YELLOW HYD SYSTEM REF AMM 29-3-00-710-002. ALL TEST OK AT THIS TIME. NO FURTHER DEFECTS NOTED.

Source: SDR F3LA2022070500070