- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 7727
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 6, 2017
- Certificate issued
- December 7, 2020
- Expires
- December 31, 2027
- Mode S code
- A35283
Airbus A320-251NTCDS A28NMAirframe · Airbus A320-251NTCDS E00089ENEngine · CFM International LEAP-1A26
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 99
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2017 | 3 |
|---|---|
| 2018 | 11 |
| 2019 | 15 |
| 2020 | 20 |
| 2021 | 12 |
| 2022 | 17 |
| 2023 | 15 |
| 2024 | 14 |
| 2025 | 24 |
| 2026 | 20 |
See all 151 ADs
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Airbus A320-251N
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565NTSB investigations
No NTSB investigations matched to N313FRMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A320-251N aircraft
FAA incident reports
No FAA accident or incident reports matched to N313FRMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A320-251N aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA2023071900099Door Sill · corrodedDISCREPANCY: 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 SDR F3LA2023071900098Shear Plate · crackedDISCREPANCY: 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 SHEASDR F3LA2023071900097Shear Plate · crackedDISCREPANCY: 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 SHEARSDR F3LA2022052400042Diaphragm · puncturedDISCREPANCEY: 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-SDR F3LA2021090200064Line · leakingHYD 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-ASDR F3LA2020123100057Power Supply · failedDISCREPANCY: 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.SDR F3LA2018110500477Tube · leakingDISCREPANCY: 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.
STCs that may be installed · 149
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Airbus A320-251N
STC ST12434ACReplacement of the wing fuel tank access panel gasketSTC ST02714CHModify the aircraft interior to match standard passenger configurationsSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.