- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 6167
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 14, 2014
- Certificate issued
- March 8, 2023
- Expires
- March 31, 2030
- Mode S code
- A9AEC5
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B7 model are included below.
On this page
Airworthiness directives that may apply · 275
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 2 |
|---|---|
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 4 |
| 2001 | 5 |
| 2002 | 5 |
| 2003 | 2 |
| 2004 | 20 |
| 2005 | 14 |
| 2006 | 13 |
| 2007 | 14 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 7 |
| 2011 | 11 |
| 2012 | 10 |
| 2013 | 14 |
| 2014 | 18 |
| 2015 | 22 |
| 2016 | 23 |
| 2017 | 23 |
| 2018 | 31 |
| 2019 | 21 |
| 2020 | 29 |
| 2021 | 18 |
| 2022 | 21 |
| 2023 | 19 |
| 2024 | 14 |
| 2025 | 21 |
| 2026 | 16 |
See all 422 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Airbus A319-115
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 CFM56-5B7 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 N723AVMatched 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 A319-115 aircraft
FAA incident reports
No FAA accident or incident reports matched to N723AVMatched 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 A319-115 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF20231203027Fan · burnedDURING CRUISE BURNING SMEEL COMING OUT OF THE BRAKE PEDALS AND VIBRATIONS FELT BETWEEN GALLEY AND COCKPIT. DURING INSPECTION OF THE AICRAFT WAS FOUND THE EXTRACT FAN BURN, AND IN ACORDANCE WWITH 21-26-51-000-001-A / 400-001-A THE EXTRACT FAN 18HQ WAS REPLACEDSDR ANCF20220920040Thermocouple · crackedPILOT REPORT
17.SEP.2022 WO 16'655'282=> ENG 2 EGT OVER LIMIT COME ON DURING INITIAL CLB. ECAM ACTIONS WERE PERFORMED. ENG 2 WAS SHUTDOWN
ACTIONS TAKEN
18.SEP.2022 WO 16'655'282=> IN ACCORDANCE WITH AMM TASK 77-21-10-200-002-A THE INSPECTION OF THE THERSDR ANCF20211223002None · nonePILOT REPORT - WO16'582'204
20.DEC.2021 => (URGENT PRIORITY) AFT CARGO DOOR INDICATION OPEN/CLOSED INTERMITTENT. AFT CARGO DOOR INDICATION OPEN/CLOSED INTERMITTENT
CORRECTIVE ACTION
20.DEC.2021=> THIS REPORT IS DEFERRED IAW MEL 52-70-01-3 LEVEL "C" 723-TSSDR ANCF2019102301Sensor · abnormalATB - IFSD / OCT 23. CLIMBING THROUGH 16000 FT THE ENGINE 2 N1 HAD A DECREASE IN POWER FROM 89.1% TO 54% THEN SLOW REGAINED ITS POWER AGAIN THROUGHT 17000FT IT PRESENTED THE SAME BEHAVOIR PASSING 13000 IN DESENTT THE ECAM SHOW ENG 2 FAIL AND THEN WE PROCEED ASSDR ANCF2015030803Control Unit · malfunctionedFUEL AUTO FEED FAULT, IAW TSM 28-21-00-810-823 DUE FUEL ON BOARD DISAGREE IN THE REPORT
P5376714-2. THIS FAULT WAS PRESENTED BECAUSE THE FUEL NOT WAS USED IN THE CORRECT SEQUENCE & WARNING IS RESET IMMEDIATELY WHEN THE FUEL DISTRIBUTION CONDITIONS NO LONGER ESDR ANCF2015030804Ignition Sys · faultedENGINE 1 IGN A FAULT. IAW TSM 74-00-00-810-801A FAILURE OF THE IGN SYS ENG 1 WAS ACCOMPLISHED. AMM 74-00-00-710-043 OPERATIONAL TEST OF THE IGN SYS A & B ENG 1 WAS PERFORMED, TESTED SUCCESSFUL.
STCs that may be installed · 215
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.