# Service difficulty reports: N591EL, cancelled Feb 10, 2024 A list on [N591EL, cancelled Feb 10, 2024](https://openairdocs.org/deregistered/N591EL-2024-02-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ANCF2015042601](https://openairdocs.org/sdr/ANCF2015042601.md): Acm · seized · Apr 26, 2015 · N591EL · Airbus A318111 · Cabin Cooling System > 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 SMOKE PROCEDURE & RETURNED TO DEPARTURE AIRPORT. AFTER LANDING AIR PACK 1 OVHT APPEARED ON ECAM. IAW - [SDR ANCF2013080700163](https://openairdocs.org/sdr/ANCF2013080700163.md): Unknown · vibration · Aug 7, 2013 · N591EL · Airbus A318111 · Fuselage Main, Structure > 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 THE CAUSE OF IN-FLIGHT AIRFRAME VIBRATIONS AND/OR NOISES WERE PERFORMED, VIBRATION REPORTING SHEET A - [SDR ANCF2013040100153](https://openairdocs.org/sdr/ANCF2013040100153.md): Connector · loose · Apr 1, 2013 · N591EL · Airbus A318111 · Door System Wiring > 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 DEFERRED TO DMI #262 IN ACCORDANCE WITH MEL 52-70-01-3 CAT "C". IAW AMM 52-71-12-400-001-A ADJUST OF - [SDR ANCF2012101600133](https://openairdocs.org/sdr/ANCF2012101600133.md): Unknown · odor · Oct 16, 2012 · N591EL · Airbus A318111 · Air Distribution System > 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 OR FUEL LEAKS WERE FOUND. THE FUMES IN THE CABIN/ OIL SMOKE AT THE APU EXAUST CHECK MUST BE PERFOR - [SDR ANCF2012031300115](https://openairdocs.org/sdr/ANCF2012031300115.md): Sdac · damaged · Mar 22, 2012 · N591EL · Airbus A318111 · Central Warning > 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 REPETITIVE CHIME WAS HEARD WITHOUT ANY ECAM ANNUNCIATION, TAKEOFF WAS ABORTED ONCE AGAIN. IN ACCORDANCE - [SDR ANCF2012013000111](https://openairdocs.org/sdr/ANCF2012013000111.md): Computer · faulty · Jan 30, 2012 · N591EL · Airbus A318111 · Flight Control System > 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 22-97-710-001-A. - [SDR ANCF2012012300108](https://openairdocs.org/sdr/ANCF2012012300108.md): Warning System · false activation · Jan 23, 2012 · N591EL · Airbus A318111 · AC Generator-Alternator > 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 PB 601 INTEGRATED DRIVE GENERATOR SYSTEM CHECK WAS PERFORMED OK. IN ACCORDANCE WITH AMM 32-40-00 - [SDR MU1Z2011020200007](https://openairdocs.org/sdr/MU1Z2011020200007.md): Radome · damaged · Dec 10, 2011 · N591EL · Airbus A318111 · Aerodynamic Fairings > 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 FOLLOWING: LENGTH: 190 MM, WIDE: 130 MM, DEPTH: 5 MM. DENT DAMAGE (BIRD STRIKE) IN THE BULKHEAD AR - [SDR EE4Y20110031](https://openairdocs.org/sdr/EE4Y20110031.md): Stop Fitting · worn · Jan 15, 2011 · N591EL · Airbus A318111 · Fuselage Main, Structure > LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUT OUT LOWER JAM, STOP FITTING WITH WEAR AT FR 26RH. - [SDR EE4Y20110030](https://openairdocs.org/sdr/EE4Y20110030.md): Stop Fitting · worn · Jan 15, 2011 · N591EL · Airbus A318111 · Fuselage Main, Structure > 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.md): Skin · damaged · Jan 10, 2011 · N591EL · Airbus A318111 · Fuselage Main, Plate/Skin > UPPER FUSELAGE FWD PAX/ CREW DOOR RT UPPER CORNERS CUTOUT EXTERNAL SURFACE WITH MARKS. - [SDR EE4Y20110009](https://openairdocs.org/sdr/EE4Y20110009.md): Seal · worn · Jan 10, 2011 · N591EL · Airbus A318111 · Nacelle/Pylon, Main Frame > NR 2 ENGINE CORE NOZZLE INNER AND OUTER PYLON SEAL WITH WEAR. - [SDR EE4Y20110008](https://openairdocs.org/sdr/EE4Y20110008.md): Support Angle · cracked · Jan 10, 2011 · N591EL · Airbus A318111 · Wing Miscellaneous Structure > RT WING T/E CAVITY, HYD LINE WITH SUPPORT ANGLE CRACKED AT STA 3250. - [SDR EE4Y20110007](https://openairdocs.org/sdr/EE4Y20110007.md): Inlet · cracked · Jan 9, 2011 · N591EL · Airbus A318111 · APU Exhaust System > 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 REPAIR. - [SDR EE4Y20110003](https://openairdocs.org/sdr/EE4Y20110003.md): Housing · delaminated · Jan 7, 2011 · N591EL · Airbus A318111 · Cabin Cooling System > 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.md): Skin · cracked · Jan 5, 2011 · N591EL · Airbus A318111 · Nacelle/Pylon, Plate/Skin > 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.md): Panel · delaminated · Jan 5, 2011 · N591EL · Airbus A318111 · Rudder, Plate/Skin > VERTICAL STABILIZER, RUDDER PN: D5547100300000, SN: TS-3706, LT AND RT SIDE PANEL WITH FLUID INDICATION (WATER INGRESS) IAW THERMOGRAPHY INSP AROUND HOISTING POINTS. LT SIDE PANEL FLUID INDICATION COMMON TO HOISTING POINT NR 1 & 3 AND RT SIDE PANEL FLUID INDI ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N591EL' AND deregistration_id = 'N591EL-2024-02-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N591EL-2024-02-10/reports --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.