N659UA
Service difficulty reports · 330
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 = 'N659UA' AND registry_match = 'registration' 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.
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 = 'N659UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2004UALA00501Bulb · incorrectE&E SMOKE DETECTOR FAILS TEST. REPLACED E&E SMOKE DETECTOR. INCORRECT BULB INSTALLED. FOUND BULB ML382 INSTALLED, SHOULD BE CM382AS10.SDR 2004UALA00301Connector · looseEICAS MESSAGE, RIGHT ENGINE FUEL FILTER DISPLAYED DURING CLIMBOUT. FUEL FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. THE SWITCH WAS TESTED IN THE SHOP, AND FOUND TO BE SLIGHTLY OUT OF CALIBRATION, BUT NOT ENOUGH TO CAUSE THE EVENT. AS A RESULT OF SHOP SDR 2004UALA00415Squib · blownRT OVERWING SLIDE DOOR SQUIB BLOWN. SQUIB BLOWN IN CONJUNCTION WITH INADVERTANT SLIDE DEPLOYMENT. SQUIB REPLACED.SDR 2003UALA00978Wire · brokenEMERGENCY LIGHT INOP AT DR1 FWD CROSSAISLE. REPLACED BROKEN FEEDER CABLE. OPS CKD NORMAL.SDR 2003UALA00610Compressor · stalledABORTED TAKEOFF DUE TO NR 1 ENGINE COMPRESSOR STALL. AIRCRAFT SURGED ON TAKE OFF AT EPR ABOVE 1.25. SURGE CHECKS FOUND NO DISCREPANCY. EVENT CLASSIFIED AS A GROUP 3 SURGE DUE TO TIP CLEARANCES IN THE HPC.SDR 2002UALA01798Frame · bentFORWARD CARGO, LEFT HAND FRAME UPPER CHORD ANGLE IS BENT,STATION 500 AND STRINGER 31L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED FRAME UPPER CHORD.SDR 2002UALA01797Stringer · damagedFUSELAGE STRINGER 25L AT STATION 544 HAS A DAMAGED FASTENER HOLE DUE TO LIGHTNING STRIKE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED STRINGER WITH SPLICE.SDR 2002UALA01804Web · cracked#1 PYLON UPPER WEB AT GENERATOR CABLE FEED-THROUGH HAS 2 EA CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER.SDR 2002UALA01803Web · cracked#1 PYLON UPPER WEB AT ELECT. WIRE BUNDLE FEED-THROUGH HAS 2 EA. CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED WEB WITH REPAIR DOUBLER.SDR 2002UALA01802Web · cracked#1 ENG PYLON AFT UPPER WEB AT PNEUMATIC DUCT FEED-THROUGH IS CRACKED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER.SDR 2002UALA01801Pylon · cracked#2 PYLON STRUT UPPER TORQUE BOX WEB AT GENERATOR FEED CABLE CUT-OUT IS CRACKED IN CORNER RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER INSTALLED.SDR 2002UALA01800Stiffener · crackedLEFT HAND NOSE TUNNEL AT BODY STATION 246, LBL23, VERTICAL STIFFENER CRACKED FORWARD SIDE OF FLOOR BEAM. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPLACED STIFFENER.SDR 2002UALA01774Skin · damagedLEFT FUSELAGE SKIN STATION 544, STRINGER 25L DAMAGED AT FASTENER HOLE COMMON TO TEAR STRAP DUE TO LIGHTNING STRIKE. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND FILLERS INSTALLED.SDR 2002UALA01750Floorbeam · crackedFLOORBEAM SEAT TRACK SPLICE CRACKED AT STATION 786, LBL 10. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM WITH REPAIR SPLICES AND FILLERS.SDR 2002UALA01734Floorbeam · corrodedMAIN CABIN FLOOR BEAM T-CAP CORRODED STATION 850-854, LBL 48 TO LBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE SPLICES AND SHIMS.SDR 2002UALA01733Floorbeam · corrodedMAIN CABIN FLOOR BEAM T-CAP CORRODED STATION 850-854, RBL 48-RBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIRED ANGLE-DOUBLER AND SHIMS.SDR 2001UALA02067PackingRIGHT HYDRAULIC SYSTEM MSG AND LOW QTY LIGHT ILLUMINATED, QTY DOWN TO 0.4, PUMPS TURNED OFF AND HYD FLUID LOSS MINIMIZED. RETURN TO FIELD OVERWEIGHT LANDING. SUPPLEMENTAL DATA UPDATE REPLACED PACKING OF CASE DRAIN FILTER DIFFERENTIAL PRESSURE INDICATOR. OPS CHSDR 2001UALA00811Cover · out of adjEMERGENCY LIGHTS REMAIN DISARMED WITH COCKPIT CONTROL SWITCH IN ARMED POSITION. SUPPLEMENTAL DATA UPDATE ADJUSTED SWITCH COVER, OPS CHECK OKAY.SDR 2001UALA00333Motor · failedBOTH PRESSURE CONTROLLERS FAILED. DESCENDED TO FL180. OPERATED NORMALLY IN MAN MODE. *S/D* 3/27/01 AT LHR, AUTO PRESS SYSTEM NR 2 WAS DEFERRED INOP. ACFT FLEW TO ORD WITH NO PRESSURIZATION FAULTS. DURING ORD-IAD LEG, FLIGHT CREW REPORTED FAILURE OF BOTH SDR 2000UALA00261Centering Cam · damagedFLAP INDICATION EICAS. DIVERTED TO MIA. *S/D* AN IMPROPERLY INSTALLED NOSE LANDING GEAR CENTERING CAM DID NOT ALLOW PROPER NOSE GEAR COMPRESSION, CAUSING CONFIGURATION WARNING LIGHTS TO APPEAR ON EICAS. REPLACED THE NOSE LANDING GEAR CENTERING CAM WITH NEWSDR 2000UALA00251Centering Cam · misinstalledAFTER TAKEOFF FLIGHT EXPERIENCED A CONFIGURATION SYSTEM WARNING HORN. WOULD NOT RESET. AIRCRAFT RETURNED TO JFK. ON FIRST APPROACH WITH FLAPS AT 30 THE FLAPS MOVED TOWARD UP, UNCOMMANDED. *S/D* NOSE GEAR STRUT WAS SERVICED WITH NEW SEALS IN JFK. CENTERINSDR 2000UALA00160Unknown · odorNR 2 ENGINE REPLACEMENT REQUIRED DUE TO OIL SMELL IN THE CABIN. LAV SMOKE DETECTOR ACTIVATED. RTF, OVERWEIGHT LANDING. ACCOMPLISHED OIL SYSTEM VACUUM AND PRESSURE CHECKS AND EXTENSIVE TEST CELL RUNS WITH NOTHING FOUND. ENGINE WAS RETURNED TO SERVICE AND HASDR 2000UALA00102Pseu · malfunctionedAIR-GND DISAGREE, NOSE AIR GND DISAGREE AND LDG GEAR MONITOR EICAS MSG''S DISPLAYED AFTER TAKEOFF. ALSO HAD AUTO THROTTLE DISCONNECT, TAIL SKID MSG, PROBE HEAT. ALL EICAS MSG''S CLEARED EXCEPT AIR-GND DISAGREE, NOSE AIR GND DISAGREE AND LDG GEAR MONITOR. DISDR 99UAL900565Battery · damagedRTF WITH MAIN BATTERY EICAS MESSAGE. *S/D* REPLACED MAIN BATTERY, CHECK NORMAL.SDR 98UAL900144Sensor · out of adjustTAKEOFF ABORTED AT 110 KNOTS. *S/D* E AND E COMPARTMENT DOOR WARNING ILLUMINATED. REPLACED AND ADJUSTED E AND E DOOR CLOSED SENSOR S201 PER MM, GROUND OPS CHECKS OK.SDR 97UAL900860Battery · dischargedEMERGENCY EXIT FLOOR LIGHTING IN RIGHT SIDE OF CABIN ROWS 21 TO 29 COMES ON INTERMITTENTLY. *S/D* THE CAUSE OF THE INTERMITTENT EEL WAS FOUND TO BE A BAD BATTERY ASSEMBLY. UAL CORRECTED THE PROBLEM BY REPLACING THE BATTERY ASSEMBLY WITH AN OVERHAULED, RECHASDR 97UAL900783Fire Card · failedRIGHT ENGINE NR 1 FIRE LOOP STATUS MESSAGE DISPLAYS CONTINUOUSLY. *S/D* PROBLEM CAUSED BY A FAULTY AUTOMATIC FAULT AND LOGIC TEST CARD (AFOLTS). REPLACED CARD, SYSTEM OPS CHECKS GOOD.SDR 96UAL900976Bleed Valve · corrodedABORTED TAKEOFF DUE TO LEFT ENGINE OVERTEMP. *S/D* THE 2.95 BLEED SOLENOID VALVES REMAINED OPEN AT HIGH POWER DUE TO INTERNAL CORROSION IN THE 2.95 BLEED VALVES. THIS LED TO THE LEFT ENGINE OVER TEMP CONDITION. THESE VALVES ARE CURRENTLY UNDERGOING AN UPGRSDR 96UAL900432Strip · inoperativeEMERGENCY EVACUATION LIGHTING STRIP AT CLOSET INOPERABLE. REPAIRED EEL STRIP.SDR 96UAL900298Bushing · failedABORTED TAKEOFF AT 70 KNOTS DUE TO BLEED VALVE EICAS MESSAGE. *S/D* A FAILED NITRONIC BUSHING CAUSED THE BLEED VALVE EICAS MESSAGE. THE LEFT HIGH PRESSURE SHUTOFF VALVE WAS REPLACED, OPERATIONS CHECK NORMAL.
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