- Registered owner
- Wells Fargo Trust Co Na Trustee
- Location
- Columbia, MD
- Owner type
- Corporation
- Serial number
- 5360
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 21, 2012
- Certificate issued
- November 20, 2012
- Expires
- November 30, 2028
- Mode S code
- A6C6CB
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4 model are included below.
On this page
Airworthiness directives that may apply · 391
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 | 10 |
| 1998 | 22 |
| 1999 | 14 |
| 2000 | 15 |
| 2001 | 9 |
| 2002 | 15 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 10 |
| 2009 | 13 |
| 2010 | 8 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 24 |
| 2020 | 29 |
| 2021 | 17 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 558 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 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 N536AVMatched 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 N536AVMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2025111534Warning Message · illuminatedAFTER ENGINE START, AUTOFLT YAW DAMPER 1+2 ON ECAM. SUCCESSFULL RESET OPERATIONAL TEST OF THE YAW DAMPER FUNCTION WAS PERFORMED IAW AMM TASK-22-63-00-710-001-A, REV. 75 01-NOV-2025 OPERATIONAL TEST OF THE YAW DAMPER FUNCTION WAS PERFORMED SATISFACTORY. NO FAUSDR ANCF20240205002Warning Light · illuminatedDURING CLIMB THE ECAM DOOR R AFT EMER EXIT WAS SHOWED, THE DIVER TO LET WAS PERFORMED, MAINTENANCE PROCEDURE WAS PERFORMED. SENSOR MONITORING FAULT AT THE RH AFT PASSENGER COMPARTMENT EMERGENCY EXIT AND ADJUSTMENT TEST WERE ACCOMPLISHED I.A.W. TSM 52-21-00-8SDR ANCF20231704011Unknown · unknownAFTER TAKEOFF VENT EXTRACT FAULT WAS PRESENTED ON ECAM. IN ACCORDANCE WITH TSM 21-26-00-810-809-A FAILURE OF THE BLOWER FAN WAS PERFORMED, THE CONTACTOR 8HQ AND BLOWER 20HQ WERE REPLACED AND NOT HELP, THE WIRING CHECK WAS FOUND WITH BURNED AND WAS REPAIREDSDR ANCF20220725027A/C Pack · odorPILOT REPORT
23.JUL.2022 WO 16'778'322=> AFTER TAKE OFF
AFTER TAKE OFF WHEN SETTING PACK TO ON, SMELL WAS FELT AND SMOKE WAS REPORT BY FLIGHT ATENDANCE ON CABIN.
ACTIONS TAKEN
23.JUL.2022 WO 16'778'322 => I.A.W. AMM TASK 21-00-00-615-802-A REV 60, LEVEL SDR ANCF20220304012None · nonePILOT REPORT
01.MAR.2022 WO 54'372'697=> DURING CLIMB HYD G RSVR LO PRS AND THE HYD G RSVR LO LVL ECAM ACTIONS WERE COMPLETED AND PRECEED TO BAQ
ACTION TAKEN
01.MAR.2022 =>IN ACCORDANCE WITH AMM 32-31-39-04 CONF 00 REV DATE 01 FEB 2022 THE HOSE NASSY FLEXSDR ANCF20220128007None · nonePILOT REPORT
27.JAN.2022 WO 54'303'634 => AFTER LIFT OFF WHEN SELECTING LG UP, L/G GEAR NOT UPLOCKED ECAM APPEARED. ON WHEEL SD PAGE, LG WAS CONFIRMED NOT UPLOCKED. AFTER RECYCLING LG LEVER ACCORDING TO ECAM, L/G DOORS NOT CLOSED. ECAM ALSO APPEARED.
ACTIOSDR ANCF20210416010Indicator · malfunctionedDURING T/O ROLL ABOVE 100 ISIS AIRSPEED INDICATION FLASHES AND SHOW LESS SPEED THAN IN PFD. RED FLAG SHOWS ON IN THE ISIS. RTO WAS PERFORMED. LOSS OF THE AIRSPEED DATA AND THE MACH NUMBER ON THE ISIS INDICATOR TO STEP 4.A.1. WAS PERFORMED AND NO DAMAGE WERE FOSDR ANCF20200206501Proximity Sensor · malfunctioned05.FEB.2020 -> AV9839 (BOG-AXM) PILOT REPORT (WO 15703901):
AFTER TAKE OFF DURING LANDING GEAR RETRACTION APPERS ON ECAM L/G DOORS NOT CLOSED. ECAM ACTIONS WERE PERFORMED UNSUCCESFULLY.
05.FEB.2020 -> CORRECTIVE ACTION WAS PERFORMED AS FOLLOWS:
IN ACCOSDR ANCF20190828101Valve · inoperativeDURING CLIMB, TROUGHT FL 250, FLIGHT ATTENDANTS INFORMED, THAT THERE WERE NO PRESSURE IN ANY OF THE LAVATORIES AND GALLEYS. FOUND VALVE 8MP IN OPEN POSITION IAW TSM 38-31-00-810-803-A AND AMM 38-31-00-740-0001 OPNS TEST OK AS PER AMM 38-12-00-710-001-A OPNS TSDR ANCF2018010501Actuator · failedDURING TAKE OFF ROLL, THE NR 1 ENGINE COMPRESSOR VAE ON ECAM, REJECTED THE TAKE OFF BELOW 72 KTS. IAW TSM 75-30-00-810-801-A FAILURE OF THE CONTROL OF THE VBV ACTUATOR. NR 1 ENGINE AND AMM 75-31-10, PB 401, CONF 06, FUEL GEAR MOTOR AND AMM 75-31-20, PB 401SDR ANCF2017090702Duct · contaminatedAFTER ENGINE START, THERE WAS A BURNING ODOR. IAW AMM 21-52-00-200-002-A, A DETAILED VISUAL INSPECTION OF PIPE ASSEMBLEES BETWEEN THE HEAT EXCHANGEN MAIN AND THE HEATER OF RT PACK WAS ACCOMPLISHED AND FOUND TO BE CONTAMINATED.SDR ANCF2015031801Connector · faultyDURING TAXING OUT WITH THE BLOWER FAN, THE EXTRACT FAN FAULT LIGHT APPEARED TOO, IAW ESP 28-48-21. THE CONNECTOR 20HQA WAS REPLACED IAW AMM 21-26-51-000 400-001-A. THE FAN BLOWER, 20HQ, WAS REPLACED. THE OPERATIONAL TEST OF THE AEVC WAS SATISFACTORY.
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