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N411AV

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Airbus A320-214 · CFM International CFM56-5B4 series

Open in FAA registry

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Registered owner
Aircol 9
Location
Wilmington, DE
Owner type
Corporation
Serial number
4011
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 4, 2009
Certificate issued
March 29, 2019
Expires
March 31, 2029
Mode S code
A4D7EB
Airbus A320-214Airframe model · 182 seats · 2 engines · 160 registeredTCDS A28NMAirframe · Airbus A320-214Engine modelCFM International CFM56-5B4 series

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
See all 558 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 1
SAIB NE-08-17R2Turbine Section - Propulsion Technology LLC Unapproved RepairIssued Mar 7, 2011

NTSB investigations · 1

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

NTSB DCA25WA049IncidentClass 5 · ForeignBogota, ColombiaNov 16, 2024 · No damage

FAA incident reports

No FAA accident or incident reports matched to N411AVMatched 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 · 5

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

SDR ANCF2025081222Filter · cloggedENG 2 FUEL FILTER CLOG AFTER T/O ON ECAM. FROM TSM 73-00-00-810-976-A STEP 4.A (A) (B) THE FUEL FILTER ELEMENT WAS REMOVED AND REPLACED IAW AMM 73-11-10-000-004-A/400-004-A. AND IDLE CHECK WAS PERFORMED WITHOUT LEAKS IAW AMM 71-00-00-710-006.Aug 11, 2025 · N411AV · Airbus A320214 · Fuel Controlling SystemSDR ANCF2018020601Computer · malfunctionedHIGH VIBRATION ON INITIAL CLIMB, LT & RT AILERON FAULTS ON ECAM. DURING TAKEOFF ROLL THE VIBRATION WAS FELT ON THE NOSE GEAR. LT AND RT NWA WERE REPLACED IAW AMM 27-93-34, PB 401, ELAC 2CE1 WAS REPLACED IAW AMM 27-93-00-710A. OPS TESTED SATISFACTORY.Feb 6, 2018 · N411AV · Airbus A320214 · Flight Control SystemSDR ANCF2015061201Fan · malfunctionedELECTRICAL SHORT CIRCUIT SMELL WAS FELT BEFORE TAKEOFF AT GND, RETURN WAS DONE. IAW AMM 21-26-51 PB 401 THE BLOWER FAN WAS REPLACED IAW ESPM 20-46-10 THE CB 1HQ AVNCS VENT BLOWER FAN WAS REPLACED & IAW ESPM 20-44-11 THE CONNECTOR 20 HQA WAS REPLACED. IAW AMMJun 12, 2015 · N411AV · Airbus A320214 · Air Distribution FanSDR ANCF2013071900162Control Unit · malfunctionedWHEN SELECTING THE L/G DOWN AND FLAPS 3, ECAM WARNING BRAKES NORMAL BRAKE SYS FAULT CAME ON AFTER APPLYING THE LANDING DISTANCE PROCEDURE, WE DECIDED TO COME BACK TO DEPARTURE. THE ANTI-SKID N/W STRG SW WAS RESET SUCCESSFULLY IAW AMM 32-43-34-000-001A AND 32-Jul 19, 2013 · N411AV · Airbus A320214 · Landing Gear Retraction/Extension SystemSDR ANCF2011052900090Unknown · malfunctionedAFTER T/O THRUST WAS APPLIED AT 50 PERCENT POWER SET, POWER DROP TO 21.1 PERCENT ON RIGHT ENGINE, AIRCRAFT TURN TO THE RIGHT, REJECTED T/O WAS EXCECUTED. IAW TSM 77-00-00-810-852, OPERATIONAL TEST OF THE FADEC ON GROUND WITH ENGINE NON-MOTORING PERFORMED, IAWOct 14, 2011 · N411AV · Airbus A320232 · Engine Indicating 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