- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 4567
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 12, 2011
- Certificate issued
- March 4, 2022
- Expires
- March 31, 2029
- Mode S code
- A740FF
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4 model are included below.
On this page
Airworthiness directives that may apply · 391
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 5 |
|---|---|
| 1991 | 1 |
| 1992 | 6 |
| 1993 | 10 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 10 |
| 1998 | 22 |
| 1999 | 14 |
| 2000 | 15 |
| 2001 | 9 |
| 2002 | 15 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 8 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 24 |
| 2020 | 29 |
| 2021 | 17 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 558 ADs
Information bulletins that may apply · 8
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.Engine · CFM International CFM56-5B4 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-12-29Engine Fuel Distribution CFM56-5B LPTACC Fuel ManifoldHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N567AVMatched 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 N567AVMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2026FA0000514Proximity Sensor · faultedAFT CARGO DOOR OPEN ECAM INDICATION DURING INITIAL CLIMB AFT CARGO DOR OPEN ECAM INDICATION LIMITATING CLIMB TO 10.000 FT, SYSTEM NOT PRESURIZING CORRECTLY. PERFORMED OPS TEST OF ACFT PRESSURIZATION FOR LEAKS IAW AMM 05-583-00-780-001-A01, NO LEAKS NOTED AFT SDR 2026FA0000486Controller · faultedDURING CLIMB AIR ENG BLEED 1+2 FAULT. IAW AMM 36-11-42-04 CONF 00 THE BLEED AIR PRECOLLER RH ENG WAS REMOVED AND REPLACED, IAW AMM 36-11-53-04 CONF 00 THE OVERPRESSURE VALVE 5HA2 WAS R & R. IAW AMM 36-11-55-04 CONF 00 THE BLEED PRESSURE REGULATOR VALVE CONTSDR ANCF2026010523041Sensor · faultedNLG STEERING FAULT DURING FLIGHT - FOLLOWING TSM 32-51-00-810-812-A REV. 75 WAS PERFORMED CHECK AND CLEANING IN THE ELECTRICAL CONNECTOR OF STEERING FEEDBACK MONITOR SENSOR (4GC) AND
ELECTRICAL CONNECTOR OF STEERING FEEDBACK CONTROL CHANNEL (3GC) IAW ESPM 20SDR ANCF20210812002Outflow Valve · faultedDURING TAKE OFF ROLL VENT AVIONICS SYSTEM FAULT APPEARS ON ECAM. AIRCRAFT DIDNT PRESSURIZE DURING FLIGHT. MASK WERE USED AND INMEDIATE RETURN WAS REQUIRED. IN ACCORDANCE WITH TSM 21-26-00-810-804A / AMM 21-26-53-000-002/400-001-A01 THE SKIN AIR OUTLET VALVE 2SDR ANCF20210107005Connector · dirtyPILOT REPORT (WO 16107549) AFTER BIRD STRIKE DURING FINAL APP RED UNLK LEFT MAIN LANDING GEAR CAME ON AFTER GO AROUND L/G LGCIU 1 FAULT APPEAR ON ECAM. CORRECTIVE ACTION: INSPECTION OF THE AIRCRAFT AFTER BIRD STRIKE WAS PERFORMED AND SENSOR 15GA WAS FOUND UNPSDR ANCF2019030701Warning System · false activationMAR 7. DURING TAKE OFF ROLL DOOR L AVIONICS APPEAR ON ECAM. CORRECTIVE ACTIONS: MAR 7. DURING TAKE OFF ROLL DOOR L AVIONICS APPEAR ON ECAM IN ACCORDANCE WITH MEL THIS ITEM IS DEFERRED TO DMI MEL 52-70-01 CAT C DUE DATE 17 MAR 2019 ITEM 4 AUTHORIZED MCC CNMCC-2SDR ANCF2015081601A/C Pack · faultedAIR PACK 1 & 2 FAULT DURING TAKEOFF ROLL, BETWEEN 40 & 60 KNTS, DISCONTINUED TAKEOFF. IAW TSM TASK 21-61-00-810-807-A PACK 1 & PACK 2 INOPERATIVE & AMM TASK 21-61-00-710-001 OPERATIONAL TEST OF PACK TEMP CONTROL SYS WERE ACCOMPLISHED WITH BOTH PACKS OPERATINGSDR ANCF2015061901Engine · bird ingestionDURING TAKEOFF ROLL BIRD STRIKE & INGESTION ON ENG N 1 OCCURRED. LOUD NOISE WAS HEARD, SMOKE & FIRE WAS OBSERVED FROM CONTROL TOWER. CURRENTLY VISUAL & BORESCOPE INSPECTION ARE ACCOMPLISHED IN ORDER TO IDENTIFY THE MAGNITUDE OF DAMAGES.SDR ANCF2015032302Starter · malfunctionedDURING ONE ENG TAXI DEPARTURE 3 ENG START. ECAM WARNING WAS PRESENTED IN THE LAST ENG START. THERE WAS NO INDICATION OF N1 & N 2 ROTATION ON ENG 2. IAW AMM 80-11-10 PB 401 CONF 06. THE RT STARTER MOTOR WAS REPLACED, TESTED OK.SDR ANCF2011052900082Warning Light · illuminatedREJECTED TAKEOFF, DURING TAKEOFF ECAM MESSAGE, THIS MESSAGE (THRUST MESSAGE) APPEARS ON THE ECAM AP REJECTED WAS BELOW 100 KNOTS, MESSAGE "ENGINE THRUST NO SET". IAW AMM TASK 22-96-00-710-001 THE OPS TEST AUTOPILOT SYS WAS PERFORMED, TEST SATISFACTORY. (PFSDR ANCF2011040400075Director · malfunctionedDURING CLIMB ECAM FWD CRG DET, AFT CRG DET ECAM WAS PERFORMED FWD ISOL VALVE WAS SELECTED OFF AND AS STATUS REMAINS AS INOPERATIVE SYSTEM. CIDS 2 PRESENT IN MAINTENANCE STATUS. SMOKE IN MAINTENANCE STATUS IS PRESENT. IN ACCORDANCE WITH AMM 26-17-00-810-823
STCs that may be installed · 301
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 301 STCs