- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 6153
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 17, 2014
- Certificate issued
- April 14, 2022
- Expires
- April 30, 2029
- Mode S code
- A9B27C
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 N724AVMatched 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 N724AVMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2026F00183Idg · faultedAFTER ENGINE 1 START, GEN 1 FAULT ON ECAM RESET UNSUCCESFULSDR 2026F00158Display · inoperativeLOWER ECAM WARNING DISPLAY STOPPED - AFTER PUSHBACK LOWER ECAM WARNING DISPLAY STOPPED WORKING RESET WAS PERFORMED 19:55ZSDR 2025F00221Fuel Filter · warning messageDURING GO OROUND ECAM WARNING ENG 1 FUEL FILTER CLOGSDR ANCF2019040831419Proximity Switch · dirtyAFTER TAKEOFF, DURING CLIMB PHASE, AFT CARGO DOOR MESSAGE OPEN APPEARS ON ECAM. THE INDICATION CORRESPOND WITH THE ECAM INDICATION ON DOOR PAGETHE FLIGHT RETURNED TO DEPARTURE FOR VERIFICATION THE INDICATION. DISAPPEARS DURING APPROACH. IN ACCORDANCE WITH SDR ANCF2019011101Warning System · false activationY RSRV OVERHEAT -YELLOW RSRV OVERHEAT DURING FLIGHT, THEN PTU OFF WAS COMMANDED, WE LOST YELLOW SYSTEM. CORRECTIVE ACTION: JAN 12. IN ACCORDANCE WITH TSM 29-13-00-810-802-A PARAGRAPH 3.B.(1) THE OPERATIONAL TEST YELLOW HYD SYSTEM WAS PERFORMED SATISFACTORY. HOSDR ANCF2019011001Wire Harness · abnormalJAN 10. DURING T/O RUN ECAM "BRAKES RELEASE" BEFORE 80 KTS. T/O WAS DISCONTINUED WITH BRAKE TEMP MISMATCH AND AUTO BREAK AMBAR. CORRECTIVE ACTION: IN ACCORDANCE WITH AMM TASK 32-11-43 PB 401 THE 2M HARNESS WAS REPLACED, AND BITE TEST OF THE MLG AMM TASK 32-69-SDR ANCF201812182001Static Inverter · odorATB. AVIONICS SMOKE APPEARED ON ECAM ALSO SMOKE WAS PRESENT ON COCKPIT AND CABIN RETURNED TO SKBO OVER WEIGHT LANIND WAS PERFORMED (69700 KG APROX) // STRONG CHEMICAL OR BURN ODOR IS FELT IN THE COCKPIT MAKING SLIGHTCREW UNCONSERTABLE // CORRECTIVE ACTIONS: NOSDR ANCF2016012201Hmu · malfunctionedDURING TAXI OUT, ONCE ENG 2 WASTER SWITCH WAS ELEC TO ON ENG 1. FAIL ON ECAM CAME PROCEDURE WERE DONE ENG DAMAGE WAS SUSPECTED DUE TO EN NR 1 OIL PRESS AT 0 ENG 1. FIRE PUSH BUTTON WAS PUSHED. IAW TSM 72-00-00-810-806A WAS ACCOMPLISHED STEP 3A FADEC TES WIT
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