- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 5622
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 28, 2013
- Certificate issued
- October 23, 2025
- Expires
- October 31, 2032
- Mode S code
- A72E6C
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 · 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 N562AVMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2025070320Computer · faultedVENT BLOWER FAULT AND EXTRACT FAULT. AFTER VENT AVNCS SYS FAULT. CONTINUE ON ECAM. IN ACCORDANCE WITH AMM 21-26-34-000-001-A / 400-001-A, AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC) WAS REPLACED. OPERATIONAL TEST PERFORMED AND SATISFACTORY. FAULTS CLEAR ONSDR ANCF2025061918Flight Recorder · unserviceableDURING CLIMB GREEN HYDRAULIC SYSTEM LOST ALL OIL QUANTITY. IN ACCORDANCE WITH AMM 31-33-55-400-002-A DFDR 1TU WAS REPLACED BY READING. IN ACCORDACE WIT AMM TASK 32-31-39-04 CONF 00 THE HOSE ASSEMBLY -FLEXIBLE WAS REPLACED (2765GM) OPERATIONAL TEST SATISFSDR ANCF20240506012Shock Absorber · faultedRETURNECD TO BOG DUE TO NOSE L/G SHOCK ABSORBER FSAULT AND L/G DOWNLOCKED.LANDING WEIGHT 65500 KG IAW AMM ONF 00 THE PROXIMITY SENSOR 25GA WAS REMOVED AND REPLACED AND IAW AMM 32-31-00-720-002-A THE FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION WAS PESDR ANCF20230304010Unknown · unknownPILOT REPORT
29.MAR.2023 WO 16'877'961=>OVERWEIGHT LANDING DUE TO MEDICAL EMERGENCY 69.000KG TOUCHDOWN WITH LESS THAN 360FT/MIN
ACTION TAKEN
29.MAR.2023 WO 16'877'961=> IN ACCORDANCE WITH AMM 05-51-200-004-B, FIG 05 51-11-991-03400-00-AQ (SHEET1) FLOW CHASDR ANCF20220726029Engine · not reportedPILOT REPORT
25.JUL.2022 WO 58'414'658 => DURING CRUISE ENG 2 FAIL
DURING CRUISE ENG 2 FAIL
ACTION TAKEN
NOT DEFINED YETSDR ANCF201902150501Pump · malfunctionedDURING CRUISE ECAM SHOWS A REAL FUEL LEAK ON ENG 1 // CORRECTIVE ACTION: FEB 6. DURING VISUAL INSPECTION OF THE ENG 1 WAS FOUND THE FOLLOWING DEFECTS: - THE LOWER FUEL TUBE THAT CONNECT TO HIGH PRESSURE PORT IN THE FUEL FILTER HOUSING WAS FOUND TOTALLY LOOSESDR ANCF2015010300001Landing Gear · unknownDURING TAKEOFF, EXPERIENCE LOSS OF DIRECTIONAL CONTROL VEERING TO THE RIGHT. PERFORM RTD AT LOW SPEED & RETURNED TO THE GATE. IN THE GATE THE MCDU IN PERF PAGE PROMT SHOWN 4S EO CLEAR, THE SAME AS IN ENGINE FAILURE WITH NO ECAM MESSAGE DISPLAY DURING RTO.
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