- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 8300
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 31, 2018
- Certificate issued
- July 31, 2018
- Expires
- July 31, 2028
- Mode S code
- AA8A8A
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 N779AVMatched 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 N779AVMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF20240606014Controller · faultedVENT AVNCS SYS FAULT REPLACED THE AEVC(10HQ) REF AMM 21-26-34-000-001 AND AMM 21-26-34-100-001 AND PERFORMED OPERATIONAL TEST IAW AMM 21-26-51-710-051-A AEVC ON: P/N 87292325V07 S/N 1161 UNIT LOANED BY AMERICAN AIRLINESSDR RJEF20240603001Avionics Unit · faultedDURING TAKEOFF FOLLOWING MESSAGE APPEARS: "VENT BLOWER/EXTRACT FAULT". THIS GENERATED A PRESSURIZATION FAILURE. REPLACED THE AEVC(10HQ) REF AMM 21-26-34-000-001 AND AMM 21-26-34-100-001 AND PERFORMED OPS TEST IAW AMM 21-26-51-710-051-A ALL OK.SDR RJEF20221402001None · noneENG 1 CTL VALVE FAULT // IN REFERENCE TO TSM 75-33-00-810-811-A THE RESISTANCE AND INSULATION CHECK ON THE EEC A ELECTRICAL HARNESS CONECTOR
P8A WAS FOUND.
SOCKETS J AND -D (LOWERCASE) (BETWEEN 21 AND 39 OHMS) = 34.9 OHMS
SOCKETS -V (LOWERCASE) AND -B (LOWESDR RJEF20220302001None · noneENG 1 FIRE 3 TIMES HIGH TEMP NACELLE ADV TO 300° ENG 1. AS PER TSM 77-21-00-810-837-A RV 59 PERFORMED INSP OF ENG #1 CORE ZONE AND THE ONLY TUBE LOOSE WAS FOUND TRANSIENT BLEED VLV AIR TUBE AND HARNESS FIN 45DVC1 WAS FOUND DAMAGED DUE HIGH TEMP 779-TSR-2022-0
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.