- Registered owner
- Wells Fargo Trust Co Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 6411
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 29, 2015
- Certificate issued
- January 28, 2015
- Expires
- January 31, 2028
- Mode S code
- A9F29E
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 · 2
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 N740AVMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF20251215038Outflow Valve · faultedVENT SKIN VALVE FAULT AT 4500 FT PROCEDURE DONE AND UNSUCCWAFUL RETURNED TO VUP. IAW AMM 21-26-00-040-002-A STEP 4.A.7.10 POSITION OF THE SKIN AIR OULET VALVE WAS VERIFY TO 45° AFTER DEACTIVATION. WAS FOUND WITH AMBAR XX ON ECAM. SUBSCUENTLY THE SKIN AIR OUSDR ANCF2025120637Wheel · vibrationSTRONG AND CONTINIOUS NOISE ON NOSE GEAR COMPARTMENT, DURING THE INITIAL CLIMB THROUGHT 12.000FT A STRONG AND CONTINIOUS NOISE WAS HEARD AND FELT IN THE NOSE GEAR COMPARTMENT. RETURNED TO THE AIRPORT OF ORIGIN. I.A.W TSM 32-20-00-840-802-A STEP B(5), PERFORMESDR ANCF20231309024Unknown · unknown13. SEP.2023 WO 17554013 DURING FLIGHT WE HAD EMERGENCY ELECTRICAL CONFIG - ELEC GEN 1 & 2 FAULT WE ARE CURRENTLY IDENTIFYING THE FAULTSDR ANCF2022011406None · none13.JAN.2022 PILOT REPORT - WO 54'324'316=> ENGINE NUMBER TWO DIFFERENCE OF APPROXIMATELY 11 PERCENT OF N1
DURING THE INITIAL CLIMB THE ENGINE NUMBER TWO HAD DIFFERENCE OF APPROXIMATELY 11 PERCENT OF N1 WITH ENGINE ONE, EVEN SHOWING THE BLUE ARC OF DIFFERENCESDR ANCF20211125001None · none23-NOV.21 PILOT REPORT WO 16538464 => DURING CLIMB PASSING FL270 AND ABOUT 20 MINUTES AFTER DEPARTURE THE FOB INDICATION STARTED TO DECREAS RAPIDLY. THE ADVISOTY OF FUEL UMBALANCED CAME UP AND THEN FUEL AUTO TRANSFER FAULT WAS TIGGERED BY THE ECM. THE DECSDR ANCF20210115007Skin · damagedN740AV FLIGHT 8598 PSO-BOG DURING WALK AROUND AT BOG, EVIDENCE OF DAMAGES BY FOD WERE FOUND ON RT THS AND RT ELEVATOR, IAW AMM 05-51-14-200-803-A. INSPECTION OF THE AIRCRAFT AFTER A BIRD STRIKE AND/OR FOD WAS PERFORMED. EVIDENCE OF DAMAGE BY FOD (STONE-ROCK-SDR ANCF2019022801Fan · abnormalFEB 28. DURING CRUISE STRONG NOISE IN THE RADOME THE RADAR WAS TURNED OFF THEN STRONG BURNED SMELL IN COCKPIT. CORRECTIVE ACTIONS: MAR 1. IAW-AMM 05-50-00-810-831-A ITEM 4 BLOWER, EXTRACT FAN, STACTIC INVETER AND RADAR RECEIVER TRANSCEIVER WERE INSPECTED AND WSDR ANCF2018012701Wheel · vibrationSTRONG VIBRATION AFTER LIFT OFF, IAW AMM 32-41-11 PB 401 THE BOTH NOSE WHEELS WERE REPLACED.SDR ANCF2017090101Warning Message · false activationDURING TAKE OFF ROLL, ECAM FOR THE AVIONICS DOOR ILLUMINATED TWICE AT LOW SPEED. PERFORMED TSM 52-41-00-810-804-A, DISSAGREE BETWEEN ECAM SYSTEM DISPLAY PAGE INDICATION AND THE CLOSED AND LOCK WAS PERFORMED AND TEST SATISFACTORY.SDR ANCF2015032702Control Unit · malfunctionedWHEEL NW STRG FAULT ON ECAM. IAW AMM 32-42-34-000-001A THE BSCU, FIN 10GG, WAS REMOVED.
IAW AMM 32-42-34-400-001A THE BSCU WAS INSTALLED. PERFORMED TEST OF THE BSCU AMM 32-46-00-740-001.
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