- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 4558
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 22, 2011
- Certificate issued
- January 21, 2011
- Expires
- January 31, 2030
- Mode S code
- AB7437
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N837VAMatched 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 GCXA20231129001Hose · leakingLOSS OF SYSTEM HYDRAULIC FLUID. REPLACED LEAKING HYDRAULIC HOSE ASSY.SDR ASAA2023021342015Plate · corrodedWHILE WORKING CUSTOMER CARD P092915 FOUND ADDITIONAL CORROSION ON THE RH AFT BULKHEAD CANTED SUPPORT AT FR33+16, Y+765, Z-1912 GROUNDED - YES. REMOVED THE DAMAGED PLATE IN FCB R/H AFT BULKHEAD CANTED AT FR33+16, Y+765, Z-1912 IAW A320 SRM 51-52-11. LOCATED, DRSDR ASAA2023021342014Plate · corrodedWHILE WORKING CUSTOMER CARD P092915 FOUND ADDITIONAL CORROSION ON THE LH AFT BULKHEAD CANTED SUPPORT AT FR33+16, Y+765, Z-1912 GROUNDED - YES. REMOVED THE DAMAGED PLATE IN FCB L/H AFT BULKHEAD CANTED AT FR33+16, Y+765, Z-1912 IAW A320 SRM 51-52-11. LOCATED, DRSDR ASAA2023010642521Door Sill · corrodedCORROSION ON R-2 SUB-THRESHOLD SUPPORT BEAM PREVIOUS REPAIR AT FRAME 67+16 TO FRAME 68, -Y 47, FLOOR LEVEL. GROUNDED - YES. FOUND NO ALLOWABLE LIMITS ON CORROSION AT R-2 DOOR SUB-THRESHOLD SUPPORT BEAM PREVIOUS REPAIR. REMOVED AND REPLACED R-2 DOOR SUB-THRESHOSDR ASAA2023010542460Door Sill · corrodedCORROSION ON L-2 DOOR SUB-THRESHOLD WEB AT FRAME 66+1-5, +Y 59-63, FLOOR LEVEL. GROUNDED - YES. DUE TO NO CORROSION OR REWORK LIMITS, REMOVED AND REPLACED L-2 DOOR SUB-THRESHOLD WEB (LOWER SILL BEAM) FR 65+ 23"- 68 + 7", STR 23L, LBL 56-65. IAW SRM 53-41-14-28SDR ASAA2023010542286Web · corrodedCORROSION ON FLOOR SUPPORT WEB AT FRAME 69+19, +Y 54, FLOOR LEVEL GROUNDED - YES. REMOVED AND REPLACED PLATE AT FR69-70, +Y54, Z-502.SDR ASAA2023010541945Support Beam · corrodedFOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL SUPPORT BEAM AROUND LAV MOUNT HOLE AT FRAME 66+6" LBL 35 BELOW FLOOR PANEL 261DF. GROUNDED - YES. NO ALLOWABLE LIMITS FOR CORROSION REMOVAL AT LONGITUDINAL BEAM HARD POINT PER A320 SRM 53-00-14-283-002 STEP 2.C SDR ASAA2022122942031Fitting · corrodedCORROSION FOUND ON R1 DOOR SCUFF PLATE SUPPORT STRUCTURE FR 17-19, Y+72, STR 23RH GROUNDED - YES. REMOVED CORROSION AT R1 DOOR SCUFF PLATE STRUCTURE FR 47-19, Y+72 STR 23R. ORIGINAL THICKNESS .120. FOUND TO BE OUT OF LIMITS. NO ALLOWABLE LIMITS. REPLACE PART. SDR ASAA2022113040985Collet · missingWHILE WORKING CUST TASK CARD 522100-02-5 FOUND RH INFLATION CABLE ASSY MISSING COLLET (CLIPS) 2 EA UNDER THE KNURLED SLIDE NUT THAT CONNECT THE MANUAL/AUTOMATIC ACTUATION CABLE TO THE RESERVOIR ACTUATION CABLE. GROUNDED - YES. REPLACED 2 EA CLIPS AND RE-ASSEMBSDR ASAA2020123033777Skin · dentedUPON WALK AROUND FOUND DENT ON LT INBOARD FLAP LOWER. GROUNDED-YES. RESOLVED ON W/O: 376466 TASKCARD: N/R-00004. ACCOMPLISHED A MAJOR REPAIR TO THE LT INBOARD FLAP LOWER SKIN, IAW A320 SRM 57-52-00-300-093. NO REINSPECT REQUIRED. NOTIFIED DARWIN; CLEARED SDR ASAA2018112627048Fan · failedELECTRICAL SMOKE SMELL THROUGHOUT AIRCRAFT CRUISE FLIGHT. GROUNDED - YES. R&R RECIR FAN FIN 15HG OPS CHECK GOOD REF AMM 21-21-51.SDR VQI2017F00022Ring · missingL1 DOOR HANDLE UNABLE TO STAY UPRIGHT. FOUND HANDLE MISSING LOCKING RING, INSTALLED A NEW RING IAW AMM 52-11-21, CHECKED GOOD, OK FOR SERVICE.SDR VQIA2017081000050Unknown · odorACRID ODOR REPORTED DURING FLT, LIKE BURNED RUBBER, IFES WERE TURNED OFF AND ODOR WENT AWAY. ODOR COMING FROM ROW 11 LT SIDE. COULD NOT DUPLICATE THE FAULT ON EXTERNAL POWER, APU POWER, APU BLEED AND PACK ON, WITH IFE ON OR OFF IAW TSM 05-50-00-81-08-31 AND
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