N322FR
Registered owner: BANK OF UTAH 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.
16 reports on file, 2019-02-11 – 2023-09-28.
Part: TUBE — LEAKING (ZONE 400) · airframe 18,816 hrs · 8,243 cycles
REFERENCE LP 369308 HYD Y RSVR LO LVL INFLIGHT. RESERVOIR SHOWS EMPTY. OPEN.
Part: BATTERY — FAILED (ZONE 200) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260509-0020. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 10WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95. INSTALLED EPSU 10WL BATTERY IAW AMM 33-51-38-400-002-A/REV 95 PART ON: P/N: 3214-31, S/N: 909787, B/N: N322FR5042 MX ACTION IS ACCEPTABLE.
Part: BATTERY — FAILED (ZONE 200) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260509-0050. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 13WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95. INSTALLED EPSU 13WL BATTERY IAW AMM 33-51-38-400-002-A/REV 95 PART ON: P/N: 3214-31, S/N: 904163, B/N: N322FR5040. MX ACTION IS ACCEPTABLE.
Part: BATTERY — FAILED (ZONE 200) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260509-0030. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 11WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95 INSTALLED EPSU 11WL BATTERY IAW AMM 33-51-38-400-002-A/REV 95 PART ON: P/N: 3214-31, S/N: 904169, B/N: N322FR5041 MX ACTION IS ACCEPTABLE.
Part: BATTERY — FAILED (ZONE 200) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260509-0040. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING EPSU BATTERIES CAPACITY TEST, EPSU 12WL BATTERY FAILED CAPACITY TEST. REPLACEMENT IS REQUIRED IAW AMM 33-51-38-000-002-A/REV 95 AND AMM 33-51-38-400-002-A/REV 95. INSTALLED EPSU 12WL BATTERY IAW AMM 33-51-38-400-002-A/REV 95 PART ON: P/N: 3214-31, S/N: 935043, B/N: N322FR5043 MX ACTION IS ACCEPTABLE.
Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260327-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND R/H SHEAR PLATE FR69-70 CRAKED. REQUIRES REPLACEMENT AS PER A320NEO SRM 51-72-11-911-001 REV. 37. R/H SHEAR PLATE WAS REPLACED AS PER A320NEO SRM 51-72-11-911-001 REV. 37. MX ACTION IS ACCEPTABLE.
Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260330-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND L/H SHEAR PLATE FR69-70 CRAKED. REQUIRES REPLACEMENT AS PER A320NEO SRM 51-72-11-911-001 REV. 37. L/H SHEAR PLATE WAS REPLACED AS PER A320NEO SRM 51-72-11-911-001 REV. 37. MX ACTION IS ACCEPTABLE.
Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260322-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRODED AFT DOOR SILL BEAM ON LH SIDE REQUIRES REPLACEMENT AS PER A320NEO SRM 51-41-14-283-002 REV. 37. DOOR SILL INSTALLATION HAS BEEN COMPLETED AS PER A320NEO SRM 51-72-11-911-001 REV. 37. MX ACTION IS ACCEPTABLE.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260332-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND FLOOR BEAM Y765 FR67-70 CORRODED REQUIRED REPLACEMENT AS PER A320NEO SRM 51-73-00 AND 51-74-00 REV. 37. FLOOR BEAM Y765 AT FR67-70 HAS BEEN REPLACED AS PER A320NEO SRM 51-72-11-911-001 REV. 37, MX ACTION IS ACCEPTABLE.
Part: PYLON — ELONGATED (ZONE 400) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260074-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. ELONGATED HOLES ON PYLON #2 CANTILEVER FLOOR REQUIRES FUTHER EVALUATION. REF: A320 NEO SRM 54-52-12 REV. 37. PERFORMED REPAIR LAY OUT AND TRANSFER OF HOLES ON REPAIR DOUBLER AND PYLON #2 CANTILEVER FLOOR. REF: LTPR EO# A32F-54-23840-00-FINAL AND FRONTIER EA# N2-54R-37887. MX ACTION IS ACCEPTABLE.
Part: PYLON — ELONGATED (ZONE 400) · airframe 18,790 hrs · 8,234 cycles
REFERENCE NR 5001260074-0040. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. ELONGATED HOLES ON PYLON #1 CANTILEVER FLOOR REQUIRES FUTHER EVALUATION. REF: A320 NEO SRM 54-52-12 REV. 37. PERFORMED REPAIR LAY OUT AND TRANSFER OF HOLES ON REPAIR DOUBLER AND PYLON #2 CANTILEVER FLOOR. REF: LTPR EO# A32F-54-23819-00-FINAL AND FRONTIER EA# N2-54R-37886 MX ACTION IS ACCEPTABLE.
Earlier reports · 2019–2022 · 5 reports
2022
Part: ELT — FAILED (ZONE 200) · airframe 16,328 hrs · 7,186 cycles
AFT FIXED ELT 110MX FAILED OPERATIONAL CHECK AMM 25-65-00-710-001 REF TASK CARD 256535-02-1. REMOVED AND REPLACED FIXED ELT IAW AMM 25-65-35-000-001-A AND 25-65-35-400-001-A. OPS CHECKS GOOD IAW AMM 25-65-00-740-001-A. COMPLIED WITH EA# N2-25R-37366 IN INSTALLING NEW FIXED ELT. T/W SN F9TAB2197C CAL 07/23.//END//
2021
Part: PIPE — LEAKING · airframe 12,629 hrs · 5,528 cycles
LP178842 ITEM 1 DISCREPENCY -- HYD GREEN SYSTEM LOSS OF FLUID IN FLIGHT --- CORRECTIVE ACTION -- FOUND L/H ENG HYD PRESSURE LINE LEAKING JUST ABOVE FAN COWL UNDER PANEL 413AL. REMOVED AND REPLACED HYD LINE IAW AMM 20-21-12-911-001-A SERVICED GREEN SYS AMM 12-12-229-611-001-A PERFORMED OPS / LEAK CKECK W/ ENGINE RUN AMM 29-11-0-710-001-A OPS/LEAK CHECK GOOD . PUT LANDING GEAR SYS BACK TO NORMAL AFTER FREE FALL AMM 32-00-00860-003-A.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 12,099 hrs · 5,283 cycles
GREEN HYDRAULIC SYSTEM FAILURE AND MANUAL GEAR EXTENSION. DURING THE T/S FOUND HYD LINE #1 ENGINE PYLON CRACKED. SVCD GREEN HYD PER REF AMM 12-12-29-611-301-A. R/R ENG 1 PYLON HYD LINE PER AMM 29-11-49-04, LK & OPS CK OK. C/W AMM 32-00-00-860-003-A TO PUT LG SYS BACK TO NORMAL MODE AFTER FREE FALL EXTENSION.
Part: LINE — LEAKING (HYD PUMP) · airframe 10,347 hrs · 4,464 cycles
HYD G RSVR LO LEVEL HYD G ENGINE 1 PUMP LO PR HYD G SYS LO PR. FOUND HYD LINE PART NR D2902083800000 LEAKING IN FORWARD PYLON NR 1 ENGINE. CORRECTIVE ACTION: REPLACED HYD LINE, PER AMM 29-00-00-910-0014-A. LEAK CHECK C/W NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.
2019
Part: ACTUATOR — FAILED (SLAT SYSTEM) · airframe 4,589 hrs · 1,908 cycles
FLIGHT CONTROL SLATS FAULT ECAM SLATS AT ZERO, FLAPS WORK. THE PREVIOUS 2 FLIGHTS ALSO HAD THE SAME ECAM. REMOVED AND REPLACED TYPE A SLAT ACTUATOR ASSEMBLY, OPS AND RIG CHECKS GOOD, REFERENCE AMM 27-84-48 PB401 LEFT WING #11 SLAT TRACK 6041CM.