- Registered owner
- Umb Bank N A Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 4200
- Year built
- 2010
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 2, 2010
- Certificate issued
- March 20, 2023
- Expires
- March 31, 2030
- Mode S code
- A50321
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 N422AVMatched 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 N422AVMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2025061217Controller · faultedCAB PR 2 FAULT COME ON ECAM - IN ACCORDANCE WITH TSM 21-31-00.810-827-A CABIN PRESSURE CONTROLLER 1 AND 2 WERE REPLACED, TEST SATISFACTORY AND AMM 05-53-00-780-003-A PRESSURIZATION CHECK WAS PERFORMED SATISFACTORYSDR ANCF20232910030Adiru · fault messageLOSS OF ALTIMETER 1 DURING TAKE OFF RUN BY FAULT MSG " LOSS OF THE FCU DATA INPUT BUS ON THE ADIRU1" IN ACCORDANCE WITH TSM: 34-13-00-810-921-A THE SYSTEM TEST OF THE ADR (SYS 1) WAS PERFORMED, TEST OK. BY TSM TASK: 34-13-00-810-921-A - ASM FIG: 34-1SDR ANCF20220317014Idg · active16.MAR.2022 WO 54'378'531 => REJECTED TAKE OFF DUE TO IDG 2 OIL LO PR ON ECAM.
17.MAR.2022 WO 54'304'626 =>IN ACCORDANCE WITH AMM 24-21-51-000-040-B IDG (2) WAS REMOVED.
17.MAR.2022 WO 54'304'626 => IN ACCORDANCE WITH AMM 24-21-51-400-040E THE IDG (2) WAS INSDR ANCF20210127008Engine · failedN422AV FLIGHT 9331 CLO-BOG. DURING ENGINE NR 2 START APPEARS SPARKS OBSERVED Y GROUND PERSONNEL. CORRECTIVE ACTION: IN ACCORDANCE WITH AMM 80-11-10 PB 401, THE PNEUMATIC STARTER WAS REPLACED, AND AMM 80-11-20 PB 401 THE STARTER SHUTOFF VALVE WAS REPLACED. ESDR ANCF2018073100315Engine · power lossCRUISING AT FLIGHT LEVEL 350 FL, THE N1 OF BOTH ENGINES BEGAN TO FALL 83.4% TO A MINIMUM OF 58.5%, THEN TO 35000 FEET OF HEIGHT WAS RE-INCREASED AND THE MASTER CAUTION ALARM IS ACTIVATED FOR 5 SECONDS. PERFORMED ENGINE 1 BOROSCOPE, FOUND SATISFACTORYSDR ANCF2015082401Cradle · defectiveCHAIR 9E ENTERTAINMENT SYS WITH SMOKE. IAW AMMS 23-32-50-000-801400-801 THE HANDSET & CRADLE AT SEAT 9E WAS REPLACED. CRADLE PN RD-KA5612-13, SN ON G539284, SN OFF G349750 & HANDSET SN ON P224104 & SN OFF P035612. IAW AMMS 23-32-08-000-801400-801 THE 9E MONSDR ANCF2015080801Controller · leakingENGINE 2 FUEL LEAK BY MAST DRAIN. IAW AMM TASK 75-21-10-000 400-002 THE HPTACC WAS R & R. IAW AMM TASK 71-00-00-710 -006 MINIMUM IDE CHECK FOR LEAKS OF RT ENG WAS ACCOMPLISHED, NO FOUND LEAKS. OPERATIONAL TEST OF FADEC WITH ENG MOTORING WAS ACCOMPLISHED SATSDR ANCF2015021301Warning System · false activationDURING CRUISE OVER SPEED WARNING WAS PRESENTED DUE TO MODULATE TURBULENCE, THE CONDITION WAS PRESENTED. IAW AMM 05-51-13 PB 601 INSPECTION AFTER SLAT LIMITING SPEED EXCEEDED & AMM 05-51-13-200-001. THE MOVEMENT SURFACED FLAP SLAT WAS PERFORMED. FOUND SURFACSDR ANCF2014090501Warning Light · false activationTAKEOFF APPROXIMATELY 60KTS "LT AVIONICS" ON ECAM, TAKEOFF WAS DISCONTINUED AND RETURN TO GATE. DETAILED INSPECTION OF THE LATERAL LT AVIONICS COMPARTMENT ACCESS DOOR WAS PERFORMED IAW AMM 52-41-12-200-001-A. OPS TEST OF THE WARNING DOORS SYS WAS PERFORMSDR ANCF2010061100064Warning System · false activationPILOT REPORT: ABORTED TAKEOFF DUE TO ECAM WARNING AVIONIC DOOR OPEN. MAINTENANCE ACTION: IAW AMM TASK 52-41-13-200-001 THE AVIONICS COMPARTMENT LATERAL RIGHT AND LEFT, INSPECTION AND CHECK MAINTENANCE PROCEDURE WAS ACCOMPLISHED AND FOUND NO ABNORMAL CONDITIO
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.