- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 9465
- Year built
- 2020
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 2, 2020
- Certificate issued
- March 3, 2020
- Expires
- March 31, 2030
- Mode S code
- A42323
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N366FRMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA202508270288Battery · failedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS FOUND EPSU BATTERY 10WL INOP REPLACEMENT REQUIRED IAW AMM 33-51-38-400-002-A REV. 102. REPLACED EPSU BATTERY 10WL AMM 33-51-38-400-001 CONF 00 REV 102. MX ACTION IS ACCEPTABLESDR F3LA202508190281Seat Track · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. PERFORMED REMOVAL OF CORRODED SEAT TRACK AT Y-1292 FROM FR.16 TO FR.20 IAW SRM 51-44-11 REV 45. PERFORMED INSTALLATION OF NEW SEAT TRACK AT Y1292 FROM FR.16 TO FR.20 IAW SRM 51-44-11 REV 45. MX ACTISDR F3LA202508190280Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF THE AFT CABIN FLOOR STRUCTURE A CRACK WAS FOUND ON LH SHEAR PLATE BETWEEN FR. 69 TO FR. 70. REPLACEMENT IS REQUIRED. PERFORMED REPLACEMENT OF LH SHEAR PLATE IAW SRM-51-72-11 REV SDR F3LA202508190279Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. R/H SHEAR PLATE BETWEEN FR.69-70 WAS FOUND CRACKED. PERFORMED REPLACEMENT OF R/H SHEAR PLATE BETWEEN FR. 69-70 I.A.W 51-72-11 REV 45. MX ACTION IS ACCEPTABLE.SDR F3LA2023052300062Unknown · unknownDISCREPANCY: REFERENCE LP378169 AIRCRAFT WAS GROUNDED AS A RESULT OF SDR REPORTALE EVENT. 'HYD REVR LO LVL'. REPLACE HYDRAULIC PIPE BY MACHINED PART IN PYLON FRONT SECONDARY STRUCTURE WAS COMPLIED WITH. NO LEAKS FOUND. REF PEMCO VISIT N366FR-4SDR F3LA2022111400148Actuator · leakingWHILE PERFORMING CARD 27-44-00-710-001-A FOUND THS ACTUATOR FLUID SIGHT GLASS TO BE EMPTY AND EVIDENCE OF LEAKS. RESTORED C/B'S AND PERFORMED OPS CHECK OF THS. OPS CHECK GOOD. A/C OK TO CONTINUE. AMM 27-44-51-400-001-A(J), AMM 27-41-00-730-001-A, AMM 27-44-0
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.