- Registered owner
- Umb Bank N A Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 2857
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 17, 2008
- Certificate issued
- December 20, 2018
- Expires
- December 31, 2028
- Mode S code
- AD2F24
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B5/P model are included below.
On this page
Airworthiness directives that may apply · 295
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 | 3 |
| 1999 | 5 |
| 2000 | 15 |
| 2001 | 9 |
| 2002 | 14 |
| 2003 | 3 |
| 2004 | 21 |
| 2005 | 14 |
| 2006 | 13 |
| 2007 | 14 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 7 |
| 2011 | 11 |
| 2012 | 10 |
| 2013 | 15 |
| 2014 | 18 |
| 2015 | 19 |
| 2016 | 23 |
| 2017 | 21 |
| 2018 | 27 |
| 2019 | 21 |
| 2020 | 26 |
| 2021 | 18 |
| 2022 | 21 |
| 2023 | 19 |
| 2024 | 12 |
| 2025 | 22 |
| 2026 | 15 |
See all 441 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Airbus A319-112
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 CFM56-5B5/P 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 N949FRMatched 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 A319-112 aircraft
FAA incident reports
No FAA accident or incident reports matched to N949FRMatched 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 A319-112 aircraft
Service difficulty reports · 46
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA20200203005Line · crackedHYD GREEN RSVR LOW LEVEL. R&R #1 ENGINE HYDRAULIC LINE PER AMM 20-33-11-911-001A, IPC 29-11-06 FIGURE 02E ITEM 220. OPS AND LEAK CHECK OK ON ALL SYSTEMS, NO LEAKS NOTED. SEE LP 1182557 ITEM 3 FOR ADDITIONAL INFORMATION. PERFORMED OPS TASK 32-00-00-481-003A DUSDR F3LA201911060137Hinge Fitting · wornDISCREPANCY: REFERENCE PEMCO N/R: 2650N343 LH MLG DOOR AFT KEEL BEAM HINGE FITTING FWD LUG WORN
CORRECTIVE ACTION: REPAIRED L/H MLG DOOR AFT KEEL BEAM, HINGE FITTING LUG PER AIRBUS REPAIR R533 70508 ISSUE B, AREA REQ RE-INSPECTION
WITH A THRESHOLD OF 8500FC SDR F3LA201911060136Fitting · crackedDISCREPANCY: REFERENCE PEMCO N/R: 2650N341 RH FR16 UPPER DOUBLE JOGGLE AREA AFT LOWER HOLE (BL SHOWS CRACK INDICATION IN THE INBD
LAYER AT 9 OCLOCK POS. VIEWED FROM THE EXTERIOR
CORRECTIVE ACTION: REPAIRED R/H FR16 DOUBLE JOGGLE UPPER CORNER HOLE "B" IAW AIR
See all 46 reportsSTCs that may be installed · 219
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 219 STCs