- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 6209
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 3, 2014
- Certificate issued
- April 28, 2022
- Expires
- April 30, 2029
- Mode S code
- A9C158
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4/3 model are included below.
On this page
Airworthiness directives that may apply · 381
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 | 9 |
| 1998 | 20 |
| 1999 | 14 |
| 2000 | 13 |
| 2001 | 8 |
| 2002 | 12 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 9 |
| 2009 | 13 |
| 2010 | 7 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 23 |
| 2020 | 29 |
| 2021 | 16 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 545 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 CFM56-5B4/3 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 N728AVMatched 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 N728AVMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2025F00220Gyro · faultedNAV ADR 1 FAULT ON ECAM DURING TAKE OFF (REJECTED TAKE OFF) AT SPEED OF 90 KTSSDR 2025F00207Start Valve · failedENG 2 START VALVE FAULT . START VALVE NOT OPENSDR 2025F00099Sensor · activeGPWS ACTIVATED DURING APP RWY 2G PEI.SDR ASMF202403260099Computer · inoperativeF/CTL ELACT PITCH FAULT AND F/CTL ALTN LAW DURING GO AROUND WE HAD F/CTL ELACT PITCH FAULT AND F/CTL ALTN LAW GO AROUND WAS PERFORMED AT CUC.SDR 2023FA0000402Computer · warning messageAFTER T/O ALT LAW PROT LOST ON ECAM (FLT CONTROL). AS PER AMM 27-93-34-000-001 ELAC 2 WAS REMOVED. IN ACCORDANCE WITH AMM 27-93-34-400-001-A WAS INSTALLED OPERATIONAL TEST AND LAND CAT III CAPABILITY SATISFACTORYSDR 2023F00203Uplock · defectiveDURING TAKEOFF ROLL ¨UNLOCKED¨INDICATION ON NOSE GEAR AT 120KTS AFTER GEAR RETRACTION L/G NOT UPLOKED ON ECAM, ECAM ACTION WERE PERFORMED SATISTACTORILY // IAW TO AMM 32-31-21-400-001-A AND 32-31-21-720-050-A OF THE NLG UPLOCK ASSEMBLY WAS REPLACED AND TEST SDR ANCF20211013004None · none10.OCT.2021=> PIREP WO 16487931: DURING TO LEFT EMERGENCY EXIT (AFT) WAS PRESENTED ON ECAM TAKE OFF WAS REJECTED.
PREVIOUS REPORTS INITIALLY CONSIDERED EXTERNAL EVENTS:
08.OCT.2021=> FL 8550AV PIREP WO 16487907: L DOOR EXIT OPEN APPEAR ON ECAM DURING APPROASDR ANCF201910280201Electrical Box · odorSMOKE. OCT 2. IFE SYS ROWS 7.8,9,10 ABC IN MIDDLE OF FLIGHT SHUTTED DOWN WITH MODERATE BURNED SMELL IFE GENERAL SYS DISCONNECTED // CORRECTIVE ACTIONS: OCT 2. SYST RESETED IFE REMAINS DISCONNECTED ON SEAT SEAT ROW 9ABC, ROW SEAT 7,8 AND 10 OPERSATED AND CHECK SDR ANCF2019082301Sensor · abnormalAGO 23. DURING INITIAL CLIMB A YAW MOVEMENT WAS FELT AFTER THIS HAPPENDS WE NOTICED AN OSCILLATION ON ENG #1 THIS ENGINE WAS REDUCED TO IDLE AND INCREASED AGAIN TO CL THRUST IN ORDER TO OBSERVE BEHAVIOR BUT THE OSCILLATION CONTINUES. FINALLY WE REDUCED AGAIN ASDR ANCF2019F00095Windshield · crackedRIGHT WINDSHIELD CRACKING DURING FLIGHT + CLAMP. RIGHT WINDSHIELD MUST BE REPLACED. AIRCRAFT RETURNS FROM FLIGHT TO BOG BY WINDOW SIDE CAPTAIN WITH CRACK ANTI ICE R WINDSHIELD.SDR ANCF2018012802Controller · failedDURING INITIAL CLIMB, THE ECAM MASTER CAUITON F/CTL R AIL FAULT, 5 MINUTES LATER, F/CTL AIL SERVO FAULT. IAW AMM 27-14-51, PB 401. THE AILERON SERVO CONTROL WAS REPLACED .SDR ANCF2015032701Autothrottle Sys · out of adjustECAM MSG CAME UP AFTER STARTING ENG 1, MSG SHOWN ON ECAM AUTO FLIGHT, AUTO THROTTLE OFF CORRECTIVE ACTION. IAW AMM TASK 22-30-00 PB 501 CONF 00 AMM TASK 34-10-00-860-004-A IT WAS PERFORMED. ADJUSTED & TESTED AUTO THROTTLE SYS 1 & 2. FUNCTIONAL & OPERATIONALSDR ANCF2015021102Relay · failedDURING APPROACH ECAM, LANDING GEAR NOT DOWN LOCK. THIS ITEM IS DEFERRED TO DMI 19
MEL 32-31-00 CAT B. IAW AMM 32-31-00-040-803 DEACTIVATION OF THE LG RETRACTING SYS WAS ACCOMPLISHED. IAW TSM 32-31-00-810-808 THE STEP 3 B & STEP 4 A 4 FAUL INSOLATION WERE AC
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