N591EL, cancelled Feb 10, 2024

Service difficulty reports · 17

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ANCF2015042601Acm · seizedDURING 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 Apr 26, 2015 · N591EL · Airbus A318111 · Cabin Cooling SystemSDR ANCF2013080700163Unknown · vibrationHIGH 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 AAug 7, 2013 · N591EL · Airbus A318111 · Fuselage Main, StructureSDR ANCF2013040100153Connector · looseDOOR 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 OFApr 1, 2013 · N591EL · Airbus A318111 · Door System WiringSDR ANCF2012101600133Unknown · odorLOW 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 PERFOROct 16, 2012 · N591EL · Airbus A318111 · Air Distribution SystemSDR ANCF2012031300115Sdac · damagedDURING 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 ACCORDANCEMar 22, 2012 · N591EL · Airbus A318111 · Central WarningSDR ANCF2012013000111Computer · faultyREJECTED 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.Jan 30, 2012 · N591EL · Airbus A318111 · Flight Control SystemSDR ANCF2012012300108Warning System · false activationGEN 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 Jan 23, 2012 · N591EL · Airbus A318111 · AC Generator-AlternatorSDR MU1Z2011020200007Radome · damagedDURING 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 ARDec 10, 2011 · N591EL · Airbus A318111 · Aerodynamic FairingsSDR EE4Y20110031Stop Fitting · wornLOWER FUSELAGE FWD CARGO COMPARTMENT DOOR CUT OUT LOWER JAM, STOP FITTING WITH WEAR AT FR 26RH.Jan 15, 2011 · N591EL · Airbus A318111 · Fuselage Main, StructureSDR EE4Y20110030Stop Fitting · wornLOWER FUSELAGE AFT CARGO COMPARTMENT DOOR CUT OUT LOWER JAM, FOUND STOP FITTING WITH WEAR AT FR59 RT.Jan 15, 2011 · N591EL · Airbus A318111 · Fuselage Main, StructureSDR EE4Y20110010Skin · damagedUPPER FUSELAGE FWD PAX/ CREW DOOR RT UPPER CORNERS CUTOUT EXTERNAL SURFACE WITH MARKS.Jan 10, 2011 · N591EL · Airbus A318111 · Fuselage Main, Plate/SkinSDR EE4Y20110009Seal · wornNR 2 ENGINE CORE NOZZLE INNER AND OUTER PYLON SEAL WITH WEAR.Jan 10, 2011 · N591EL · Airbus A318111 · Nacelle/Pylon, Main FrameSDR EE4Y20110008Support Angle · crackedRT WING T/E CAVITY, HYD LINE WITH SUPPORT ANGLE CRACKED AT STA 3250.Jan 10, 2011 · N591EL · Airbus A318111 · Wing Miscellaneous StructureSDR EE4Y20110007Inlet · crackedAPU 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.Jan 9, 2011 · N591EL · Airbus A318111 · APU Exhaust SystemSDR EE4Y20110003Housing · delaminatedAIR CONDITIONING BAY, RT PLENUM'S HSG WITH FIBERGLASS DAMAGE (DELAMINATED & BROKEN). THE HOUSING DAMAGE AREA REQUIRES A MAJOR REPAIR.Jan 7, 2011 · N591EL · Airbus A318111 · Cabin Cooling SystemSDR EE4Y20110002Skin · crackedENGINE 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.Jan 5, 2011 · N591EL · Airbus A318111 · Nacelle/Pylon, Plate/SkinSDR EE4Y20110001Panel · delaminatedVERTICAL 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 INDIJan 5, 2011 · N591EL · Airbus A318111 · Rudder, Plate/Skin
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