N259AU, cancelled Nov 4, 2003

Service difficulty reports · 21

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 = 'N259AU' AND deregistration_id = 'N259AU-2003-11-04'
  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 USAASB01037Apu · malfunctionedBWI- FLT 2993 - EN ROUTE FROM BOS TO FLL, AT FL350, THE APU SHUTDOWN. THE NR 2 CSD/GENERATOR WAS ALREADY ON MEL SO THE CREW DECLARED AN EMERGENCY AND BEGAN TO DIVERT TO BWI. AT FL240, THE APU WAS RESTARTED AND THE EMERGENCY WAS CANCELED. FLIGHT CONTINUED TO Feb 4, 2001 · N259AU · Boeing 737201 · Airborne Auxiliary Power Unit (APU) SystemSDR USAASB01034Pressure Switch · malfunctionedCLT - FLT 2826 - EN ROUTE FROM MCO TO BOS, THE NR 2 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED ALONG WITH HIGH OIL TEMPERATURE INDICATION ON THE CSD TEMPERATURE GAUGE. CREW DISCONNECTED THE NR 2 ENGINE CSD AND STARTED THE APU. CREW THEN RECEIVED AN APFeb 3, 2001 · N259AU · Boeing 737201 · APU Oil SystemSDR USAASB01016Proximity Switch · out of adjBWI - FLT 2679 - ON APPROACH TO BWI, THE LEADING EDGE TRANSIT LIGHT ILLUMINATED, ALONG WITH A BAD VIBRATION, DURING FLAP EXTENSION. THE NR 3 AND NR 4 LEADING EDGE SLATS WOULD NOT EXTEND. CREW DECLARED AN EMERGENCY, ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEJan 22, 2001 · N259AU · Boeing 737201 · Leading Edge Slat Position Indicating SystemSDR USAASB00267Battery Pack · faultyCLE - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK TO BE INTERMITTENTLY OPEN. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Sep 22, 2000 · N259AU · Boeing 737201 · Emergency LightingSDR USAASB00176Csd · failedCRW - FLT 2704 - EN ROUTE FROM BWI TO CLE, THE NR 1 ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED CSD AND THEN THE APU QUIT. WITH ONLY ONE POWER SOURCE REMAINING, THE FLIGHT DIVERTED TO CRW. FLIGHT LANDED WITHOUT FURTHER Jun 21, 2000 · N259AU · Boeing 737201 · AC Generation SystemSDR USAASB00175Csd · overservicedCHS - FLT 2634 - DURING CRUISE, ENROUTE FROM MCO TO BWI, THE NR 1 ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE NR 1 ENGINE CSD. A SHORT TIME LATER, THE APU HIGH OIL TEMPERATURE LIGHT ILLUMINATED RESULTING IN APU AUTO Jun 21, 2000 · N259AU · Boeing 737201 · AC Generator-AlternatorSDR USAASB00172Csd · failedLGA - FLT 2653 - CREW REPORTED THAT DURING CLIMB-OUT FROM BOS, EN ROUTE TO MCO, NUMEROUS COMPONENTS ASSOCIATED WITH THE AC BUS NR 1 FAILED OR BEAME INTERMITTENT. FOUND THE NR 1 GENERATOR FREQUENCY WAS OFF SCALE LOW. CREW STARTED THE APU AND PLACED IT ON THE Jun 18, 2000 · N259AU · Boeing 737201 · Alternator-Generator DriveSDR USAASB00053Hydraulic Line · leakingJAX - FLT 2704 - EN ROUTE FROM TPA-BWI, AT FL290, CREW CONTACTED DISPATCH VIA ACARS THAT FLT LOST SYSTEM A HYD. AT THIS TIME, IT WAS DETERMINED TO CONTINUE TO BWI. HOWEVER, ANOTHER MESSAGE WAS RECEIVED FROM ACARS STATING THAT BOTH LOW PRESSURE LIGHTS WERE ONFeb 26, 2000 · N259AU · Boeing 737201 · Hydraulic System, MainSDR USAASB99239Engine · failedCLT - FLT 8028 - DURING CLIMB-OUT FROM CLT, THE CREW ENCOUNTERED A RIGHT ENGINE VIBRATION AT ALL AIR SPEEDS ABOVE 86 PERCENT N1. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACEDOct 1, 1999 · N259AU · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAASB99193Position Ind · failedBWI - FLT 2638 - ON PREPARATION FOR LANDING AT BWI, CREW ENCOUNTERED A SPLIT FLAP INDICATION OF 1 DEGREE. FLAPS WOULD NOT EXTEND BEYOND 2 DEGREES OR RETRACT. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES. FLIGHT LANDED WITHAug 5, 1999 · N259AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR USAASB99182Hinge · failedBWI - FLT 2622 - DURING CLIMB-OUT FROM BWI, CREW REPORTED A LOUD UNBEARABLE SQUEAL COMING FROM THE MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTJul 24, 1999 · N259AU · Boeing 737201 · Passenger/Crew DoorsSDR USAASB98166Oven · overheatedPGV - FLT 1077 - AT FL 350 EN ROUTE TO JAX FROM LGA, THE FORWARD GALLEY OVEN CAUGHT FIRE. THE FLIGHT ATTENDANT USED A FIRE EXTINGUISHER AND PUT OUT THE FIRE. THIRTY MINUTES LATER THE FIRE RESTARTED AND SMOKE ENTERED THE COCKPIT. CAPTAIN DECLARED AN EMERGENCJul 2, 1998 · N259AU · Boeing 737201 · Buffet/GalleysSDR USAASB98128Clamp · looseCLT - FLT 338 - FLIGHT DEPARTED CLT AND RIGHT PACK ON MEL. SHORTLY AFTER LIFTOFF, THE LEFT WING BODY OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND BLOWING HOT AMay 30, 1998 · N259AU · Boeing 737201 · Pneumatic Distribution SystemSDR USAA980105Skin · crackedINT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK ON EXTERNAL FUSELAGE SKIN AT FORWARD RT SERVICE DOOR LOWER HINGE CUTOUT FORWARD EDGE SKIN. REMOVED SECTION OF SKIN AND INSTALLED REPAIR DOUBLER. REPAIRED PER SB 737-53-1074 FIG 3 AND SRM 5Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980104Frame · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION BS 787 BETWEEN STRINGER 26R AND STRINGER 27R. CUTOUT CORRODED AREA AND INSTALLED REPAIR SKIN ATTACH ANGLE, REPAIRED PER SRM 53-10-4 FIG 7. CORROSION TASK NR C53-208-01, CORROSION LEVEFeb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980103Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 12 INCH SECTION OF CORROSION STRINGER 27L, BS 967 AND BS 987 STRINGERS. CUTOUT STRINGER, FABRICATED REPAIR SECTIONS AND SPLICED AND INSTALLED ON A/C BS 947 PLUS 10 INCHES TO BS 1016, REPAIRED PER SRM 5Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980102Frame · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORROSION BS 286, STRINGER 28L FRAME WEB. CUTOUT CORRODED SECTION OF FRAME WEB AND INSTALLED NEW SECTION, REPAIRED PER SRM 51-40-02. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980101Stringer · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK IN STRINGER, S18R BS 333. SPLICED STRINGER 65-45800-189, REPAIRED PER EA 43633. (M)Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980100Stringer · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 15 LT AT STATION 1138, STRINGER. REPLACED SECTION OF STRINGER AND SPLICED TOGETHER, REPAIRED PER SRM 53-10-7. (M)Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB97269Light · inoperativeCMH - FOUND EMERGENCY LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPAIRED THE EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.Sep 26, 1997 · N259AU · Boeing 737201 · Emergency LightingSDR USAASB96255Light · failedBWI - FLT 404 - CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE SEAT 9C IS INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. (M)Dec 7, 1996 · N259AU · Boeing 737201 · Emergency Lighting
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