- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 6050
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 23, 2021
- Certificate issued
- November 1, 2021
- Expires
- November 30, 2028
- Mode S code
- AD4B05
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56 model are included below.
On this page
Airworthiness directives that may apply · 425
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1986 | 1 |
| 1990 | 6 |
| 1991 | 2 |
| 1992 | 6 |
| 1993 | 10 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 6 |
| 1997 | 14 |
| 1998 | 29 |
| 1999 | 16 |
| 2000 | 16 |
| 2001 | 13 |
| 2002 | 17 |
| 2003 | 5 |
| 2004 | 25 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 17 |
| 2008 | 11 |
| 2009 | 13 |
| 2010 | 10 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 18 |
| 2014 | 19 |
| 2015 | 25 |
| 2016 | 26 |
| 2017 | 25 |
| 2018 | 35 |
| 2019 | 25 |
| 2020 | 29 |
| 2021 | 17 |
| 2022 | 23 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 604 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
Airframe · Airbus A320-214
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB NM-13-24Air Conditioning System: Air Distribution FanSAIB NM-13-03Hydraulic Power System: Power Transfer UnitSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.Historical bulletins · 5
SAIB NE-13-33R1Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesSAIB NE-13-33Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle VanesSAIB NE-08-17R2Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-08-17R1Propulsion Technology LLC Unapproved RepairSAIB NE-08-17Propulsion Technologies International Unapproved Repair
NTSB investigations
No NTSB investigations matched to N956AVMatched 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 A320-214 aircraft
FAA incident reports
No FAA accident or incident reports matched to N956AVMatched 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 A320-214 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 ANCF20260808015Control Valve · abnormalENG 1 CTL VALVE FAULT WAS INTERMITENTE DURING CLIMB. IAW TSM75-26-00-810-802-A OPERATIONAL TEST OFF THE FADEC 1A/1B ENGINE NON MOTORING WAS PERFORMED AND AMM75-26-10-000-001/400-001 THE TBV WAS REPLECED IN ACCORDANCE WITH AMM 73-29-00-710-040-B FADEC TEST ANSDR ANCF2025100192431Proximity Sensor · failedFWD CARDO DOOR INDICATION ON ECAM IS INOP, DURING TAKE OFF AFTER WE TURNED ON BOTH PACKS AND THE WE HAD DOOR FWD CARGO INDICATION ON ECAM THE FAILURED WAS CONFIRMED ON SD BLEED PAGE NO PREZURIZATION PROBLEM WAS OBSERVED IAW AMM 52-71-12-000-002-A. THE PROXIMISDR ANCF20241021020Engine · stalledENG 1 STALL DURING FLIGHT AT 34000 FT "ENG 1" STALL FOLLOWED BY "ENG 1" FAILSDR ANCF20231205037Unknown · unknown02-DIC-2023 WO 17504734 HARD LANDING PLEASE CHECK CONDITION OF AIRCRAFT LDW WAS 59800 KGS APROX CVR AND FDR CBS WERE PULL IAW AMM 05-51-11-200-004-C, DUE REV O1 NOV 2023, INSPECTION AFTER HARD LANDING OR A HARD OVERWEIGHT LANDING FOR AIRCRAFT WITH FDIMU LOAD SDR ANCF20231209023Unknown · unknownDURING FLIGHT HYD Y RESERVOIR (RSVR) LO LVL LEAKING, IAW AMM 29-13-15-400-001-A THE PACKING 47 OF COUPLING HALF WAS REMOVED AND REPLACED AND THE COUPLING HALF WAS ADJUSTED LEAK TEST WAS PERFORMED SATISFACTORY PTU HYDRAULIC SYSTEMS NORMAL CONDITIONSDR ANCF20220531020None · nonePILOT REPORT:
27.MAY.2022 WO 58'391'564=> (CRITICAL PRIORITY) FWD CARGO DOOR ECAM IND)
DOOR FWD CARGO DOOR ECAM WAS DISPLATED AFTER TAKE OFF AND DISAPERED AFTER LANDING
ACTIONS TAKEN:
27.MAY.2022 WO 58'391'564 => THIS ITEM IS DEFERRED TO DMI W/O 58391564SDR ANCF20220511019None · nonePILOT REPORT:
07.MAY.2022 WO 54'368'555=> (DURING INITIAL CLIMB VENT AVNCS SYS FAULT COME ON ECAM, FOLLOWED)
DURING INITIAL CLIMB VENT AVNCS SYS FAULT COME ON ECAM, FOLLOWED BY VENT SKIN VALVE FAULT AND VENT BLOWER FAULT CABIN ALTITUDE CLIMBED UP TO 13000 FT
STCs that may be installed · 308
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 308 STCs