- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 9221
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 24, 2019
- Certificate issued
- October 24, 2019
- Expires
- October 31, 2029
- Mode S code
- A41090
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 N361FRMatched 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 N361FRMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA202606040422Flap System · malfunctionedREFERENCE LP 557839 #2 AT ABOUT 4000' MSL, UNCOMMANDED ROLL WHILE GOING FLAPS 1 TO FLAPS 2 WITH SPEED BRAKE DEPLOYED. AUTO PILOT WAS OFF. OBSERVED ON FLIGHT CONTROL. SD PAGE LEFT AIL HALF DOWN, RIGHT AIL HALF UP. FELT REDUCED ROLL AUTHORITY WHILE TURNING. AC SDR F3LA202505100233Shear Tie · crackedDISCREPANCY: REFERENCE AIRBORNE N/R 16065.0272 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT LH FUSE FR 69-70 SHEAR WEB IS CRACKED.
CORRECTIVE ACTION: REMOVED AND REPLACED L/H SHEAR WEB AT FR 69-70 IAW A320 NEO SRM 51-72-11. MX ACTION IS ACCSDR F3LA202505100232Shear Tie · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT RH FUSE FR 69-70 SHEAR WEB IS CRACKED. REMOVED AND REPLACED SHEAR WEB R/H BETWEEN FR 69-70 IAW A320 NEO SRM 51-42-11. MX ACTION IS ACCEPTABLE.SDR F3LA202505100231Seat Track · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. L1 DOOR O/B SEAT TRACK HAS CORROSION BETWEEN FR 18-20. REMOVED AND REPLACED L1 DOOR O/B SEAT TRACK IAW A320 SRM 51-72-11-911-001. MX ACTION IS ACCEPTABLE.SDR F3LA2024070800099Fitting · crackedACFT WAS REMOVED FROM SERVICE UNTIL REPAIRS MADE. REFERENCE LP352447 ITEM 1, LOST-YELLOW HYDRAULIC SYSTEM. FOUND PYLON HIGH PRESSURE FITTING CRACKED. REMOVED AND REPLACED FITTING REF.AMM 29-13-49-400-813-A. LEAK CHECK GOOD. OK TO CONTINUE.SDR F3LA2023112700216Unknown · unknownDISCERPANCY: REFERENCE LP 405902. SDR REPORTABLE EVENT. AFTER LANDING RECEIVED ECAM L/G SHOCK ABSOBER FAULT, ANTI-ICE CAPT TAT, NAV TCAS FAULTS. THESE MSGS DISAPPEARED THEN SHORTLY REAPPEARED FOLLOWED BY SMELL OF SMOKE IN COCKPIT THEN ECAM WARNING ENGINES. CORSDR F3LA2023071300091Battery · dischargedPER HEAVY CHECK T/C PERFORMED OPS TEST OF EMERGENCY LIGHTS VIA MCDU. FAULT BAT/EPSU (11WL) EMERGEN L PERFORMED T/S IAW TSM 33-51-00-810-855-A FOUND BATTERY FOR 11WL NEEDING TO BE REPLACED. REMOVED AND REPLACED BATTERY AT EPSU 11WL IAW AMM 33-51-38-000/400-002SDR F3LA2022221200172Relay · failedWHEN SETTING TRIM FOR TAKE-OFF, TRIM WHEEL KEEPS MOVING PAST DESIRED SETTING BY ITSELF. WILL MOVE FULL DOWN OR FULL UP IF NOT STOPPED MANUALLY. REMOVED AND REPLACED RELAY 36CE3 IAW AMM 20-46-50-01. OPS CHECK GOOD. A/C OK FOR SERVICE.SDR F3LA2023040100005Actuator · faultedDISCREPANCEY: REFERENCE LP 271287 WHEN SETTING TRIM FOR TAKE OFF, TRIM WHEEL KEEPS MOVING PAST DESIRED SETTING BY ITSELF WILL MOVE FULL DOWN OR FULL UP IF NOT STOPPED MANUALLY
CORRECTIVE ACTION: REFERENCE LP 271287 W/O MIA-22-1391 REMOVED THSA INSTALLED SERVSDR F3LA2021061700044Slide · no testL1 ESCAPE SLIDE FAILED EPSU TEST. THIS WAS DURING OVERNIGHT MAINTENANCE. REPLACED L1 ESCAPE SLIDE L1 IAW AMM 25-62-44-400-007-A. T/W F9TAB1763C, CAL DUE 04-2022. TEST OK.
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.