Registered owner
Aircol 16
Owner type
Corporation
Serial number
4284
Year built
2010
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 20, 2010
Certificate issued
June 4, 2024
Expires
June 30, 2031
Mode S code
A2DCEB

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.

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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.

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.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N284AVMatched 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 Industrie A320-214 aircraft

FAA incident reports

No FAA accident or incident reports matched to N284AVMatched 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 Industrie A320-214 aircraft

Service difficulty reports · 6

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR ANCF20232910028Fuel Filter · abnormalDURING CLIMB ENG 2 FUEL FILTER CLOG ON ECAM IN ACCORDANCE WITH AMM 73-11-10-000-004-A AND 73-11-10-400-004-A THE FUEL FILTER ELEMENT WAS REMOVED AND REPLACED TEST OK AND OPERATIONAL TEST SATISFACTORY FOR LEAKS. THE FAULT CONTINUES PRESENT. SEE WORKORDER 17Oct 26, 2023 · N284AV · Airbus A320214 · Aircraft Fuel SystemSDR ANCF20210113006Skin · damagedN284AV FLIGHT AV8598 PSO-BOG. DURING WALKAROUND 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-ROOct 28, 2020 · N284AV · Airbus A320214 · Elevator, Plate/SkinSDR ANCF2015032201Splice · unknownTHE COCKPIT DOOR LOCKING KEYPAD INOPERATIVE. IAW AMM52-51-12 PB 401 THE BOTTOM STRIKE 30MQ WAS R & R, NO HELP. PENDIENT CONNECT SPLICE C PN NSA936830-20 IAW AMM 32-01-12 PB 401. THE STRIKE, 30HR, WAS REPLACED IAW ESPM 20-43-13. THE SPLICE VS7117 PIN C WAS RMar 22, 2015 · N284AV · Airbus A320214 · Door System WiringSDR ANCF2015031101Engine · fodREJECTED TAKEOFF DUE TO FOD ENG 1. ENG 1 IS IN REMOVAL & INSTALLATION PROCESS. BORESCOPE INSPECTION IS DONE ON ENG REMOVED & WILL BE SEND TO MANUFACTURER SHOP FOR INVESTIGATION.Mar 11, 2015 · N284AV · Airbus A320214 · Engine (Turbine/Turboprop)SDR ANCF2014112901Warning System · activatedDURING DESCENT LGCIU NR 2 CAME ON ECAM. IAW AMM 32-69-00-00-740--001-A BITE THE LGCIU WAS ACCOMPLISHED. TESTED SATISFACTORY.Nov 29, 2014 · N284AV · Airbus A320214 · Landing Gear Position and WarningSDR ANCF2013190900168Unknown · odorDURING INITIAL CLIMB STRONG BURNED SMELT WAS FELT ON THE COCKPIT NOT POSIBLE SOURCE WAS DETECTED, AIR CONDIONING OR ELECTRIC, AFTER INITIAL CLIMB OUT SMELLED APPARENTLY DISSAPEAR, NOT VISIBLE SMOKE OF ANY KIND WAS DETECTED DURING THE WHOLE OPERATION BUT SMOKE Sep 17, 2013 · N284AV · Airbus A320214 · Air Distribution System

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