# N591EL: 2004 Airbus A318, registration cancelled 2024-02-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 10, 2024 - Status when cancelled: Sale reported, canceled - Airframe: [Airbus A318](https://openairdocs.org/model/airbus-a318) (registry code 3940022) - Engine: [CFM International CFM56-5B8/P series](https://openairdocs.org/engine/cfm-international-cfm56-5b8-p-series) (registry code 13022) - Serial number: 2333 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 19, 2011 - Last registry action: May 12, 2023 - Mode S code: A7A18D - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.7532° N, 80.2345° W: Placed by OpenAirDocs at the center of ZIP code 33145, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N591EL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=591EL - Page: https://openairdocs.org/deregistered/N591EL-2024-02-10 From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Airbus A318: https://openairdocs.org/model/airbus-a318.md ## Service difficulty reports (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ANCF2015042601](https://openairdocs.org/sdr/ANCF2015042601), Apr 26, 2015: ACM. SEIZED. DURING INITIAL CLIMB AFTER TAKEOFF PROX AT 3500 FT THE FLIGHT ATTENDANT CALLED TO THE COCKPIT & INFORMED SMELL & SMOKE IN THE CABIN. THE CREW PERFORMED THE SMOK - [SDR ANCF2013080700163](https://openairdocs.org/sdr/ANCF2013080700163), Aug 7, 2013: UNKNOWN. VIBRATION. HIGH VIBRATION DURING CLIMBING AT 25,000 FT AND 27,000 FT, IAW TSM 53-35-00-810-801. A VIBRATION AND/OR NOSE FELT AND TSM 05-50-00-810-801-A IDENTIFICATION OF T - [SDR ANCF2013040100153](https://openairdocs.org/sdr/ANCF2013040100153), Apr 1, 2013: CONNECTOR. LOOSE. DOOR FWD CARGO INDICATION DURING CLIMB -- IN ACCORDANCE WITH AMM 52-71-00-200-001- A VISUAL INSPECTION ON THE FWD CARGO SENSOR CONNECTOR LOOSE. THIS ITEM IS DEF - [SDR ANCF2012101600133](https://openairdocs.org/sdr/ANCF2012101600133), Oct 16, 2012: UNKNOWN. ODOR. LOW SPEED REJECTED TAKEOFF DUE TO RUBBER SMELL IN THE CABIN. IN ACCORDANCE WITH TSM 26-15-00-810-804-A CHECK BY ODOURS AND MIST IN THE CABIN, NON EXTERNAL OIL O - [SDR ANCF2012031300115](https://openairdocs.org/sdr/ANCF2012031300115), Mar 22, 2012: SDAC. DAMAGED. DURING TAKEOFF ROLL CONFIG PARK ON WAS PRESENTED ON ECAM WITH PARK BRAKE IN OFF POSITION. TAKEOFF WAS ABORTED A SECOND ATTEMPT WAS PERFORMED AND CONTINOUS REPET - [SDR ANCF2012013000111](https://openairdocs.org/sdr/ANCF2012013000111), Jan 30, 2012: COMPUTER. FAULTY. REJECTED TAKE OFF DUE TO AILERON SERVO FAULT, IAW AMM 27-93-24-000/400-001A THE ELAC 2 WAS REPLACED TEST ON GROUND SATISFACTORY IAW AMM 27-93-00-710-001-A AND 2 - [SDR ANCF2012012300108](https://openairdocs.org/sdr/ANCF2012012300108), Jan 23, 2012: WARNING SYSTEM. FALSE ACTIVATION. GEN 1 FAULT DURING TAKEOFF ROLL, TAKEOFF THRUST WAS APPLIED AND THE FAULT CAME ON AT ABOUT 60-70 KTS, REJECTED TAKEOFF WAS DONE. IN ACCORDANCE WITH AMM 24-21-00 - [SDR MU1Z2011020200007](https://openairdocs.org/sdr/MU1Z2011020200007), Dec 10, 2011: RADOME. DAMAGED. DURING DESCENT STRONG HIT WAS FELT IN THE RADOME ZONE, WITH VISUAL CONFIRMATION OF BIRD STRIKE AFTER PARKING (RADOME BROKEN) THE MEASURES OF THE DAMAGE ARE THE - [SDR EE4Y20110031](https://openairdocs.org/sdr/EE4Y20110031), Jan 15, 2011: STOP FITTING. WORN. LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUT OUT LOWER JAM, STOP FITTING WITH WEAR AT FR 26RH. - [SDR EE4Y20110030](https://openairdocs.org/sdr/EE4Y20110030), Jan 15, 2011: STOP FITTING. WORN. LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR CUT OUT LOWER JAM, FOUND STOP FITTING WITH WEAR AT FR59 RT. - [SDR EE4Y20110010](https://openairdocs.org/sdr/EE4Y20110010), Jan 10, 2011: SKIN. DAMAGED. UPPER FUSELAGE FWD PAX/ CREW DOOR RT UPPER CORNERS CUTOUT EXTERNAL SURFACE WITH MARKS. - [SDR EE4Y20110009](https://openairdocs.org/sdr/EE4Y20110009), Jan 10, 2011: SEAL. WORN. NR 2 ENGINE CORE NOZZLE INNER AND OUTER PYLON SEAL WITH WEAR. - [SDR EE4Y20110008](https://openairdocs.org/sdr/EE4Y20110008), Jan 10, 2011: SUPPORT ANGLE. CRACKED. RT WING T/E CAVITY, HYD LINE WITH SUPPORT ANGLE CRACKED AT STA 3250. - [SDR EE4Y20110007](https://openairdocs.org/sdr/EE4Y20110007), Jan 9, 2011: INLET. CRACKED. APU MUFFLER-EXHAUST, DUCT INLET AND TUBE ASSY-FELT METAL WITH DENTS, CRACKS AND PUNCTURE. NOTE: INLET AND FELT METAL DENTS, CRACKS AND PUNCTURE REQUIRE MAJOR RE - [SDR EE4Y20110003](https://openairdocs.org/sdr/EE4Y20110003), Jan 7, 2011: HOUSING. DELAMINATED. AIR CONDITIONING BAY, RT PLENUM'S HSG WITH FIBERGLASS DAMAGE (DELAMINATED & BROKEN). THE HOUSING DAMAGE AREA REQUIRES A MAJOR REPAIR. - [SDR EE4Y20110002](https://openairdocs.org/sdr/EE4Y20110002), Jan 5, 2011: SKIN. CRACKED. ENGINE NR 1 & NR 2, ENGINE PYLON, PRECOOLER FAIRING SKIN WITH CRACKS (ID ACCESS PANEL NR 413DL & NR 423DL). THE SKIN CRACKS REQUIRE A MAJOR REPAIR. - [SDR EE4Y20110001](https://openairdocs.org/sdr/EE4Y20110001), Jan 5, 2011: PANEL. DELAMINATED. VERTICAL STABILIZER, RUDDER PN: D5547100300000, SN: TS-3706, LT AND RT SIDE PANEL WITH FLUID INDICATION (WATER INGRESS) IAW THERMOGRAPHY INSP AROUND HOISTING PO --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.