- Registered owner
- Wells Fargo Trust Co Na Trustee
- Location
- Columbia, MD
- Owner type
- Corporation
- Serial number
- 5477
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 12, 2013
- Certificate issued
- February 11, 2013
- Expires
- February 28, 2029
- Mode S code
- A5DB2F
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 N477AVMatched 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 N477AVMatched 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
Reports on N477AV not matched to an aircraft · 1
They name N477AV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF202602264006Switch · abnormalHYD Y RSR LO LV - IAW AMM 29-13-41-000/400-004-A, REV 76, THE LOW LEVEL SWITCH OF THE YELLOW HYDRAULIC RESERVOIR WAS REPLACED, TEST SATISFACTORY WITH ENGINE RUN-UP AMM 71-00-00-710-003-B REV.SDR ANCF20250609616Indication Sys · faultedENG HIGH VIB AT T/O AFTER THUSH LEVERS IDLE FAULT IND DISAPPEAR. THIS REPORT ITEM IS DEFERREED IAW DMI/MEL 77-00-02-3 ITEM CAT "C". REV 62 01-APR-2025 MCCAUTH. 477-TSR-2025-06-036 IAW TSM 77-00-00-810-867-A STEP 3A OPERATIONAL TEST EVMU WAS SATISFACTORY TSDR ANCF20250502012Engine · bird ingestionBIRD STRIKE DURING TAKE OFF ENGINE RH - IN ACCORDANCE WITH TSM TASK 72-00-00-810-819-A AND AMM TASK 72-00-00-200-006-A BOROSCOPE PORTS S2,S4,S5,S7,S8, S20 HIGH TURBINE AND CUMBUSITON CHAMBER AT 3 O CLOCK AND COMBUSTION CHAMBER AT 6 O CLOCK WERE OPEN - IN ACCORSDR ANCF20230205013Windshield · crackedBIRD STRIKE DURING CLB L. OULET WINDSHIELD CRACKED. THE WINDSHIELD WAS REMOVED AND REPLACED, I.A.W AMM 56-11-11-000-001-A AND AMM 56-11-11-400-001-A UNTIL AMM SUBTASK 56-11-11-420-055-A REV 63 DATE 01-FEB-2023. INSTALLATION OF THE WINDSHIELD WAS ACCOMPLISHESDR 2014FA0000309Ecu · malfunctionedDURING CLIMB, AN INTERMITTENT AND CONTINUOUS FAULT WAS PRESENTED, NR 1 ENGINE THRUST REVERSE UNLOCKED. THE FAULT FLASHED AND DISAPPEARED CONTINUOUSLY. ENGINE CONTROL UNIT WAS REMOVED AND A NEW ECU WAS INSTALLED IAW AMM 73-21-60, PB 401, SUBTASK 23-21-60-800
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