- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 8135
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 20, 2018
- Certificate issued
- May 5, 2020
- Expires
- May 31, 2027
- Mode S code
- A3904C
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 N329FRMatched 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 N329FRMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA202602100360None · noneSEVERE TURBULENCE, FL370,.78 MACH/CLEAN CONFIG. AIRSPEED VARIATIONS +/- 30 KIAS, UNCOMMANDED BANK 15-20 DEGREE, UNCOMMANDED PITCH OSCILLATIONS +/- 7 DEGREES. AIRCRAFT WAS GROUNDED AS A RESULT. AS PER DECODED VALUES FROM DFDR NO LIMITS WERE EXCEEDED. NO INSP SDR F3LA2024010400000Power Supply · failedDURING HEAVY CHECK, EPSU TEST YIELDS FAULT "335138 EPSU (10WL) FWD L". NOTE: THIS DID NOT CAUSE A FLIGHT DELAY. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) 10WL FOLLOWING AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. BITE TEST, INTERFACE ANSDR F3LA2023120100223Shear Tie · crackedREFERENCE NR 5001278796-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. RH SHEAR PLATE FOUND WITH CRACK BETWEEN FR69-70 REQUIRES REPLACEMENT AS PER S320 NEO SRM 51-72-11 REV. 38. REPLACED RH SHEAR PLATE BETWEEN FR69-70 AS PER S320 NEO SRM 5SDR F3LA2023120100222Beam · corrodedREFERENCE NR 5001278731-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND SIGN OF CORROSION ON BEAM Y765 FR67-68 REPLACEMENT REQUIRED AS PER A320 NEO SRM 53-41-14-283-009 REV. 38. REPLACED BEAM Y765 FR67-68 AS PER A320SDR F3LA2023120100221Floorbeam · corrodedREFERENCE NR 5001278789-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON FLOOR BEAM Y1162.5 BETWEEN FRAMES 68-69 REQUIRES REPLACEMENT AS PER A320 NEO SRM 53-41-11-283-009 REV. 38. REPLACED FLOOR BEAM Y1162.5 BETWEEN FRAMES 68-69 SDR F3LA2023120100220Door Sill · corrodedREFERENCE NR 5001278745-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRDED LH AFT DOOR SILL SHAPE BETWEEN FRAMES 66-68 REQUIRES REPLACEMENT AS PER A320 NEO SRM 51-72-11-911-001 REV. 30. REPLACED LH AFT DOOR SILL SHAPE BETWEEN FR66-68 ASDR F3LA2023120100219Door Seal · corrodedDISCREPANCY: REFERENCE NR 5001278732-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LH DOOR SILL BEAM NUT PLATE HOLE ALONG FRAME 68 REQUIRES REPAIR AS PER A320 NEO SRM TASK 53-41-15-300-001 REV. 38. REPAIRED LH DOOR SILL BEAM SDR F3LA201908010058Control Handle · failedLANDING GEAR LGCIU 1 & 2 FAULTS, PERFORMED LANDING GEAR GRAVITY EXTENSION PROCEDURES. REMOVED AND REPLACED RELAY (62GA) PERFORMED GEAR SWING NO FAULTS NOTED. REMOVED AND RE[PLACED LANDING GEAR CONTROL LEVER, OPS CHECKS AND LANDING GEAR SWING GOOD IAW 32SDR F3LA2018061100353Unknown · odorODOR OF ELECTRICAL BURNING COMING FROM THE AIR VENTS AT ROW 31 DURING CRUISE. MAINTENANCE INSPECTED THE AIRFRAME & CABIN FOR ODORS IAW AMM 05-50-00-810-831A. INTERIOR CABIN FWD & AFT CARGO BAYS, AVIONICS BAYS, ENGINE RUN WITH NEGATIVE RESULTS. CREW NOTED NO
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.