- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 3647
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 27, 2008
- Certificate issued
- March 29, 2023
- Expires
- March 31, 2030
- Mode S code
- A87F50
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 N647AVMatched 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 N647AVMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF20220608023None · nonePILOT REPORT
06.JUN.2022 WO 58'451'834=> (ENG 2 / AIR 2 BLEED LEAK DURING CRUISE, ECAM ACTIONS WERE PERFORMED)
ENG 2 / AIR 2 BLEED LEAK DURING CRUISE, ECAM ACTIONS WERE PERFORMED
ACTIONS TAKEN
06.JUN.2022 WO 58'451'834=> PERFORMED TSM TASK 36-22-00-810-8SDR ANCF20191028201Sensor · failedRTO-ENG STALL // OCT 22. DURING TAKE-OFF AFTER PUTTING THRUST LEVERS IN CLIMB A LOUD BAMG WAS HEARD AND ENG 1 STALL ON ECAM , TAKE-OFF WAS ABORTED AT 50KTS APROX. MAX BRAKE T WAS 215 // OCT 23. IN ACC TO TSM 73-00-810-865 FAULT ISOLATION 4C YROUBLESHOOTING OPESDR ANCF2019102892901Unknown · noiseRTO. SEP 29.DURING ROLLING TAKEOFF AT 30KTS THERE WAS AN STRONG NOISE ON THE LEFT SIDE OF THE AIRPLANE. ENGINES PARAMETERS WERE NORMAL TAKEOFF WAS REJECTED // CORRECTIVE ACTIONS: SEP 30. IN ACCORDANCE WITH AMM TASK 75-31-30-000-001-A,75-31-30-000-002-A, 75-31-SDR ANCF2019052201Wire Harness · burnedDURING DEBOARDING PASANGER REPORTED SMOKE ON SCREEN OF SEAT 16E AFTER VISUAL INSPECTION, A STRONG SMOKE ODOR REMAIN IN THE CABIN // CORRECRIVE ACTIONS: MAY 22. THIS REPORT IS DEFERRED IN ACCORDANCE WITH NEF I-48 CAT D LOG PAGE 22550 ITEM 2, N647AV-NEFMCC-201SDR ANCF2018012301Flap · lockedPILOT REPORT: FLAP LOCKED. AFTER T/O WAS LOCKED FLAP 1. F/CTL FLAPS LOCKED. DUE TO THE EVENT OCCURRED AT A REMOTE BASE, CURRENTLY MOVING PERSONNEL TO THE AIRPORT TO START THE TROUBLESHOOTING PROCESS.SDR ANCF2015020601Warning System · false activationREJECTED TAKEOFF ON RNWY 02 SKIPS DUE TO BRAKES SYS 2 FAULT ANNUNCIATION. THE RTO MANEUVER AT ABOUT 80 KNOTS. THIS ITEM IS DEFERRED TO DMI 667 MEL 32-42-03-2-A CAT C. MX PROCEDURE MEL WAS PERFORMED BSCU SYS 2 DEACTIVATION. IAW TASK 32-42-00-810-862 FAILURSDR ANCF2015011801Fan · malfunctionedDURING INITIAL CLIMB, WE SMELL A STRONG FUMES SITUATION, WAS IMPROVING AFTER DESELECTING THE VENTILATION SYS WHICH WAS RESTARTED SUCCESSFULLY. AFTER 2 HOURS & 30 MINUTES STRONG NOISE UNDER THE FLOOR THE AFT GALLEY APPEAR & COMING WORSE RAPIDLY & THE FUMES BESDR ANCF2015010101Controller · malfunctionedDURING DESCENT THROUGH APPROX FL 340 AN ADVISORY APPEARED ON ECAM IF CABIN ALTITUDE PASSING 8800 FT WE RECOVER MOMENTARILY IN MANUAL MODE LEAVING THE CABIN AT 6.200 WITH THE STATUS TARGET WE TRIED TO RECOVER THE AUTOMATIC CONTROLS PASSING FROM SYS 1 TO MANUAL SDR ANCF2014FA0000205Outflow Valve · inoperativeDURING INITIAL CLIMB, AIRPLANE DID NOT PRESSURIZE IAW AMM 21-26-53-000-002 AND 21-26-400-002-A, THE SKIN AIR OUTLET VALVE WAS REPLACED IAW AMM TASK 21-26-00-71 001. OPS TEST AEVC WAS PERFORMED, TEST OK.SDR ANCF2013100900171O-Ring · failedDURING CRUISE, ECM ADV ENGINE OIL QTY WAS PRESENT, ENGINE OIL QTY WENT DOWN TO 1,5 QTS, ENGINE WAS SHUTDOWN IN FLIGHT IAW AMM 79-21-1-92-2-B, SUB-TASK-79-21-1-2-58-A ITEM 4. DRAIN PLUG IN THE MAIN OIL SUPPLY FILTER AND O-RINGS WERE REPLACED, IAW AMM-71-71-3-SDR MU1Z2013022200002Support · brokenDURING MAINTENANCE CHECK, AVA HAS FOUND THE HYDRAULIC SUPPORT P/N D93570603200 COMPLETED BROKEN, AFTER AMAGE IF IT REMAINS UNDETECTED, THE TUBE ASSY P/N D2917002101100 (AIPC 29-13-03-12A ITEM 10A) AND P/N D2917000902000 (AIPC 29-13-03-15C ITEM 70C) MUST BE REPSDR ANCF2012121200140Slide · defectiveSLIDE OF 1L DOOR WAS ACCIDENTALLY ACTIVATED BY CREW MEMBERS, THE ACTIVATION WAS UNSUCCESSFUL. SLIDE WAS REMOVED, THE DAMPER PRE-CHARGE WAS RELEASED AND THE DOOR WAS FULLY OPENED AND OPERATIONALLY TESTED, THE SEAL OF THE DIAPHRAGM DAMPER WERE CHANGED, SERVICE SDR ANCF2009032200037Warning Light · illuminatedAIR TURN BACK DUE TO ECAM MESSAGE "FUEL INTERCELL TRANSFER XFR FAULT" DURING CLIMB. THIS ITEM WAS DEFERRED TO DMI NR 52. MEL 28-15-01, CAT C. IAW AMM TASK 28-15-00-810-801 INTERCELL TRANSFER SYS WAS PERFORMED TEST PASSED.
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.