- Registered owner
- Bank Of Utah Owner Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 5632
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 11, 2013
- Certificate issued
- April 23, 2026
- Expires
- April 30, 2033
- Mode S code
- A8453E
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 N632AVMatched 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 N632AVMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF20260929019Sensor · abnormalFUEL F. USED / FOB DISAGREE, THE CADENSICON 19QT HAS BEEN REMOVED AND REPLACED IAW AMM 28-42-16-000/400-001-A REV 78 REV-. TORQUE APPLIED TO THE BOLT 2 42 LBF IN AND BONDING CONTACT RESISTANCE BETWEEN THE CADENSICON (1) AND THE SUPPORT BRACKET (4) 09 MILLIOSDR 2024F00187Flt Controls · trippedF/CTL FAULT IN CRUISE, AUTO FLT AP OFF IN CRUISE. IAW TSM 27-51-00-810-836-A STEP A (1) (2) (3) A-B & C OF SOLENOIDE WERE CHECKED WITHIN LIMITS. IAW AMM 27-51-00-710-001-A WTB TEST ON SFCC1 WAS PERFORMED TEST OK. ADDITIONAL ACTION SEE WO 18376426SDR ANCF2017111801Pump · inoperativeNR 1 ENGINE FAILED DURING TOUCH DOWN. DURING CRUISE, LEFT FUEL TANK PUMP 1, LOW PRESSURE AND ECAM ACTIONS ACCOMPLISHED. IAW AMM 28-21-51, THE PB401 LT FUEL PUMP 21QA WAS REPLACED.SDR ANCF2014081201Unknown · malfunctionedDURING TAKEOFF A/T FMA INDICATION WAS BLANKED WHEN AT FLX & MCT POSITION THE THRUST LEVELS WERE MOVED TO TAKEOFF & GA POSITION & NO INDICATION ON FVA WAS SHOWED EITHER, A LOW SPEED RTV WAS PERFORMED. IAW AMM 22-96-00 PB 501 AFS OPERATIONAL TEST WAS PERFORMED
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