Serial number
4001
Year built
2009
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 18, 2009
Certificate issued
March 29, 2019
Expires
March 31, 2029
Mode S code
A4B06C
Registered owner
Aircol 8
Owner type
Corporation

From the FAA registry file of October 20, 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. Not a compliance determination.

1990In forceSuperseded2026
ADs by the year they took effect: 558 ADs
19905
19911
19926
199310
199410
19954
19965
199710
199822
199914
200015
20019
200215
20033
200423
200520
200613
200716
200810
200913
20108
201112
201212
201317
201418
201523
201625
201724
201831
201924
202029
202117
202222
202319
202415
202521
202617
See all 558 ADs

Information bulletins that may apply · 8

Advisory, not mandatory. Matched the same way as ADs.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N401AVMatched by N-number and event date. 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 N401AVMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A320-214 aircraft

Service difficulty reports · 6

Reports filed since July 20, 2001, when this mark’s previous registration was cancelled.

SDR ANCF20220817030Check Valve · unserviceablePILOT REPORT 13.AUG.2022 WO 16741973=> WHEEL N/W STRG FAULT APPEARED DURING CLIMB WHEEL N/W STRG FAULT APPEARED DURING CLIMB LANDING WEIGTH 65800KGS ACTIONS TAKEN 13.AUG.2022 WO 16741973=> IAW TSM: 32-51-00-810-826-A STEP A WATER WAS FOUND IN ELECTRICALAug 13, 2022 · N401AV · Airbus A320214 · Landing Gear SystemSDR ANCF20210105003None · nonePILOT REPORT 01.JAN.2022 WO 16469431 => ENG 2 FUEL FILTER CLOGGED ACTION TAKEN 01.JAN.2022=> IN ACCORDANCE WITH AMM 73-11-10 PB 401 FUEL FILTER ELEMENT WAS REPLACEDJan 1, 2022 · N401AV · Airbus A320214 · Engine Fuel DistributionSDR ANCF2016042501Outflow Valve · malfunctionedDURING CLIMB AFTER 9.300 FT & AFTER PACK 2 ON ADY 00 CABIN PRESS SYS WAS PRESENTED, OUTLET VLV REMAINED OPEN ALL TIME. IAW TSM 21-26-00-810-819-A THE SKIN TEMP SENSOR 28HQ, SMOKE DETECTOR 1WA WERE REPLACED & THE AVIONICS EQUIPMENT VENTILATION CONTROLLER WAS TApr 25, 2016 · N401AV · Airbus A320214 · Pressure Regulator/Outflow ValveSDR ANCF2014011000181Unknown · malfunctionedDUE TO ENG THRUST ASYMMETRY TAKEOFF WAS DISCONTINUED. IAW AMM 73-29-00-410-040A THE TEST ENG FADEC 1 TO 2 WAS PERFORM, NO FAIL. THE TEST FADES WAS ACCOMPLISHED.Feb 24, 2014 · N401AV · Airbus A320214 · Fuel Controlling SystemSDR ANCF2013041200156Slide · unwanted deploySLIDE DOOR 1L WAS ACTIVATED ACCIDENTALLY BY THE FLIGHT CREW BEFORE PUSHBACK, THE SLIDE DID NOT DEPLOY CORRECTLY DUE TO THE GATE WAS CONNECTED. IAW AMM 52-10-00-610-001A REPLACEMENT OF THE DIAPHRAGMAN IN THE PERCUSSION MECHANISM OF THE DOOR DAMPER ACTUATOR WASApr 13, 2013 · N401AV · Airbus A320214 · Escape SlideSDR ANCF2013031300152Engine · slowDURING TAKE OFF, WHEN THRUST LEVERS WERE ADVANCED BETWEEN FLEX AND TOGA, ECAM WARNING SHOWED ENGINES THRUST LEVERS NOT SET, ENGINES DID NOT SPOOL UP RAPIDLY AS EXPECTED IN A NORMAL TAKEOFF, DECIDED TO ABORT TAKEOFF. GROUND RETURN WAS PERFORMED AND PERFORMEDMar 13, 2013 · N401AV · Airbus A320214 · Engine (Turbine/Turboprop)

Earlier aircraft with this N-number · 1

This aircraft carried N401AV before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.