N313FR
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.
7 reports on file, 2018-11-01 – 2023-07-01.
Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 18,997 hrs · 8,352 cycles
DISCREPANCY: REFERENCE NR 5001248674-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. LH SHEAR PLATE WITH CRACK BETWEEN FRAME 68-70 REQUIRES REPLACEMENT AS PER A320 NEO SRM 51-72-11 REV 36 CORRECTIVE ACTION: PERFORMED REPLACEMENT OF LH SHEAR PLATE BETWEEN FR68-70 AS PER A320 NEO SRM 51-72-11 REV 36. MX ACTION IS ACCEPTABLE./END/
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 18,997 hrs · 8,352 cycles
DISCREPANCY: REFERENCE NR 5001248673-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. LH AFT DOOR SILL NUT HOLE CORRODED AT FR 68 REPAIR REQUIRED AS PER A320 NEO SRM 53-41-14-300-001 REV 36 CORRECTIVE ACTION: PERFORMED INSTALLTION OF REPAIR ANGLE AND FILLER ON LH AFT PAX DOOR SILL FR68 PER A320 NEO SRM 53-41-14-300-001 REV 36. MX ACTION IS ACCEPTABLE./END/
Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 18,997 hrs · 8,352 cycles
DISCREPANCY: REFERENCE NR 5001248675-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. RH SHEAR PLATE WITH CRACK BETWEEN FRAME 68-70 REQUIRES REPLACEMENT AS PER A320 NEO SRM 51-72-11 REV 36 CORRECTIVE ACTION: PERFORMED REPLACEMENT OF RH SHEAR PLATE BETWEEN FR68-70 AS PER A320 NEO SRM 51-72-11 REV 36. MX ACTION IS ACCEPTABLE./END/
Part: DIAPHRAGM — PUNCTURED (ZONE 800) · airframe 15,344 hrs · 6,741 cycles
DISCREPANCEY: REFERENCE LP 198808 R2 DOOR ASSIST DAMPER CYLINDER DIAPHRAM PUNCTURED ( WILL NOT TAKE CHARGE) CORRECTIVE ACTION: REFERENCE LP 198808 REMOVED AND REPLACED CYCLINDER DOOR DAMPER IAW AMM 52-13-14-400-001-B. TORQUE WRENCH S/N DRK88196 CAL DUE 9-22-2022
Part: LINE — LEAKING (HYD SYSTEM) · airframe 13,009 hrs · 5,661 cycles
HYD Y RSVR LO LVL IN FLIGHT. REPLACED ENG PYLON PRESS LINE IN FWD PYLON, P/N D2902083400000 LEAK CHECK GOOD AMM 29-13-49-400-842-A
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 11,043 hrs · 4,731 cycles
DISCREPANCY: AFT EMERGENCY EXIT SIGNS NOT ILLUMINATED. CORRECTIVE ACTION: R & R EPSU, IAW AMM 33-51-38-000/400-001-A. OPERATIONS CHECK GOOD, AC OK TO CONTINUE.
Part: TUBE — LEAKING (ENGINE FUEL) · airframe 4,442 hrs · 1,837 cycles
DISCREPANCY: REFERENCE LP1122030 ITEM 2. ENGINE #2 LEAKING FUEL AT PS LINE CONNECTING AT FUEL PUMP AND FROM BRAIDING ON PB3 LINE. CORRECTIVE ACTION: R & R GASKET FOR PS LINE AND R & R FUEL LINE PB3 TO HEAT EXCHANGER IAW AMM 73-11-05 PB401 AND 79-21-25 PB401. T/W F9TAB2957C DUE 9/19, F9TAB1763C DUE 8/19. SEE LOGPAGE 112031 ITEM 1 FOR LEAK CHECK./END/