N829US, cancelled Sep 24, 2003

Service difficulty reports · 30

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 = 'N829US' AND deregistration_id = 'N829US-2003-09-24'
  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 ASOA03307Cam · out of rigFLT 4140 - DURING GROUND INSPECTION IN DFW, THE MAIN PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE AND DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE RIGGED THE MAIN PASSENGER DOOR UPPER CAM MECHANISM. OPERATIONAL AND WARNING CHECKS GOOD. AIRCRAFT OK FOR SJul 13, 2003 · N829US · Doug DC982 · Passenger/Crew DoorsSDR USAAD01163Battery · dischargedPHL - THE LOW LEVEL EMERGENCY LIGHTS IN THE FIRST CLASS SECTION OF THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Sep 22, 2001 · N829US · Doug DC982 · Emergency LightingSDR USAAD01141Battery · inoperativeBOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Jul 30, 2001 · N829US · Doug DC982 · Emergency LightingSDR USAAD01128Power Supply · dischargedCLT - THE CEILING EMERGENCY LIGHTS A SEAT ROWS 20 THROUGH 24 ILLUMINATE WITH THE POWER SHUTOFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)Jun 14, 2001 · N829US · Doug DC982 · Emergency LightingSDR USAA010684Attach Angle · crackedPIT - FOUND PYLON ATTACH ANGLE CRACKED .25 INCH, LOWER PYLON ATTACH ANGLE STATION 1463 CANTED. STOP DRILLED CRACK PER TYPICAL REPAIR 54-10-06A. (M)Jun 5, 2001 · N829US · Doug DC982 · Fuselage Structure (General)SDR USAA010685Attach Angle · crackedPIT - FOUND ATTACH ANGLE CRACKED .75 INCH, RIGHT UPPER PYLON ATTACH ANGLE CANTED STATION 1464. STOP DRILLED CRACK PER TYPICAL REPAIR 54-10-06A. (M)Jun 5, 2001 · N829US · Doug DC982 · Fuselage Main, Attach FittingsSDR USAAD01118Battery · inoperativeMCO - THE LOW LEVEL LIGHT AT SEAT 25D DID NOT TEST. MAINTENANCE REPLACED THE BATTERY. (M)May 30, 2001 · N829US · Doug DC982 · Emergency LightingSDR USAAD01111Water Heater · malfunctionedPHL-IND - FLT 1787 - DURING DESCENT, AN ELECTRICAL BURNING SMELL WAS DETECTED IN THE LAVATORY AREA. THE AFT LAVATORY WATER HEATER CIRCUIT BREAKER WAS PULL BUT THE SMELL CONTINUED. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTEMay 20, 2001 · N829US · Doug DC982 · Wash Water SystemSDR USAAD01018Battery · dischargedTPA - THE LOW LEVEL EMERGENCY LIGHT AS SEAT ROW 25 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Feb 4, 2001 · N829US · Doug DC982 · Emergency LightingSDR USAA001736Longeron · crackedPIT - FOUND LONGERON CRACKED .5 INCH, LONGERON 4L AT INTERSECTION OF FRAME 160. SPLICED IN LONGERON SECTION PER SRM 53-02. (M)Oct 13, 2000 · N829US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA001738Longeron · crackedPIT - Q-3, LONGERON CRACKED .25 INCH AT LONGERON 2L INTERSECTION OF FRAME 160. SPLICED IN LONGERON SECTION PER SRM 53-02 FIG 18. (X)Oct 13, 2000 · N829US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA001737Longeron · crackedPIT - Q-3, LONGERON CRACKED .25 INCH AT LONGERON 3L AT INTERSECTION OF FRAME 160. SPLICED IN LONGERON SECTION PER SRM 53-02. (X)Oct 13, 2000 · N829US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA001735Angle · crackedPIT - Q-3, REPAIR ANGLE CRACKED, 1.75 INCHES IN RADIUS OF REPAIR ANGLE AT BS 1474, RIGHT VERTICAL STABILIZER. SPLICED IN NEW SECTION AND INSTALLED REPAIR ANGLES (DOUBLERS) PER EA 15895 AND SRM 53-05 FIG 23A. (X)Oct 13, 2000 · N829US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAAD00093Battery · dischargedPHL - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 24 ILLUMINATED AND COULD NOT BE EXTINGUISHED. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Jun 14, 2000 · N829US · Doug DC982 · Emergency LightingSDR USAAD00029Strut · lack of lubeLGA - BUF - FLT 2240 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE STRUT, JACKED THE NOSE OF THE AIRCRAFT AND PERFORMED A NOSE GEAR RETRACTION AND EXTENSION CHEFeb 16, 2000 · N829US · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR USAAD99099Relay · failedPIT/MSY - FLT 474 - AFTER TAKEOFF IT WAS NOTED THERE WERE NO CABIN LIGHTS OR LAVATORY LIGHTS. THE TOILETS DID NOT FLUSH, THE NR 4 TR INDICATED ZERO, AND THE BATTERY CHARGER WAS INOPERATIVE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAIJul 19, 1999 · N829US · Doug DC982 · AC Power Distribution SystemSDR USAAD99050Hose · rupturedDCA-BUF - FLT 8005 - DURING CLIMB POWER SETTINGS THE TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED BUT WOULD EXTINGUISH DURING CRUISE POWER. THE AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLEX COUPLING DOWNSTREAM OF THE RIGApr 2, 1999 · N829US · Doug DC982 · Air Distribution SystemSDR USAA990084Web · crackedPIT - DURING C2 CHECK, FOUND 1 INCH CRACK ON VERTICAL WEB AT CENTER OF DOOR ADJACENT TO DOOR OPERATING MECHANISM BETWEEN BEAM 4 AND 5 INNER DOOR HINGE, BOX AFT INTERCOSTAL. INSTALLED DOUBLER P/N SR09520001-3 PER SRM 52-05 FIG 4-5. (M)Feb 12, 1999 · N829US · Doug DC982 · Passenger/Crew DoorsSDR USAAD98168Generator · failedMCO-PIT - FLT 843 - EN ROUTE THE LEFT ENGINE GENERATOR POWER DROPPED OFF LINE, AND THE APU WAS ON MEL. THE AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE GENERATOR. (M)Oct 1, 1998 · N829US · Doug DC982 · AC Generator-AlternatorSDR USAAD98130Fuse · brokenTPA - FLT 1622 - DURING CRUISE, THE LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED WITH THE QTY INDICATING 4 QTS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE LANDING WEIGHT WAS 132,000 LBS. MAINTENANCE REPLACED THE UPPER HYDRAULIC FUSJul 31, 1998 · N829US · Doug DC982 · Hydraulic System, MainSDR USAAD98091Battery · dischargedTHE PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES. (M)May 15, 1998 · N829US · Doug DC982 · Emergency LightingSDR USAAD97103Clamp · looseBDL/CLT - FLT 1053 - AT 1,000 FEET AFTER TAKEOFF, 'TAIL COMPARTMENT TEMP HI' LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH HP BLEED SELECTED OFF AND POWER REDUCED. REPEATED FROM PREVIOUS WRITE-UP. RETURNED TO FIELD. REPOSITIONED AND SECURED LOOSE CLAMP AT LEFTJun 17, 1997 · N829US · Doug DC982 · Pneumatic Distribution SystemSDR USAAD97102Gasket · failedBDL/CLT - FLT 1053 - AFTER TAKEOFF AT 600 FEET, 'TAIL COMPARTMENT TEMP HI' LIGHT ILLUMINATED. LIGHT WENT OUT WITH HP BLEEDS SELECTED OFF AND POWER REDUCED. RETURNED TO FIELD. REPLACED HI TEMP SENSOR GASKET, RAN ENGINES, NO OBVIOUS LEAKS NOTED. (X)Jun 17, 1997 · N829US · Doug DC982 · Pneumatic Distribution SystemSDR USAAD97086Engine · failedFLT 463 - CLT-IAH - AFTER CLIMB THROUGH 19,000 FEET, CREW HEARD A LOUD BANG, AND LEFT ENGINE PARAMETERS BEGAN TO DROP. RETURNED TO CLT. REPLACED LEFT ENGINE. (M)May 18, 1997 · N829US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAAD97064Transmitter · failedFLIGHT 1438 - BOS-FLL - LEFT OIL PRESSURE LOW LIGHT CAME ON IN FLIGHT. OIL PRESSURE GAUGE INDICATED 34 PSI. OIL TEMP, QTY, AND ALL OTHER ENGINE INDICATIONS NORMAL. DIVERTED TO CLT. REPLACED OIL PRESSURE RELIEF VALVE AND OIL PRESSURE TRANSMITTER. (M)Apr 2, 1997 · N829US · Doug DC982 · Engine Oil PressureSDR USAAD97054Mechanism · not latchedFLT 2198 - ROC-PHL - AIRCRAFT FAILED TO PRESSURIZE ON TAKEOFF. RETURNED TO FIELD. L2 DOOR BAYONET WAS NOT IN PROPER POSITION. OPENED AND CLOSED DOOR. NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. (M)Mar 10, 1997 · N829US · Doug DC982 · Passenger/Crew DoorsSDR USAAD96173Batteries · dischargedFORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK. (M)Nov 28, 1996 · N829US · Doug DC982 · Emergency LightingSDR USAA960508Beltframe · corrodedPIT - DURING Q-2/C-5 CHECK, FOUND .5 INCH BY 4 INCH CORRODED AREA,STATION 1322 LONGERON 30 BELTFRAME. SPLICED IN NEW BELTFRAME PER SRM53-14-3, CORROSION TASK NR C57-53300. CORROSION LEVEL 1.(M)Jul 16, 1996 · N829US · Doug DC982 · Fuselage Main, FrameSDR USAAD96068Pressurization · malfunctionedRIC/CLT - FLT 761 - CABIN ALTITUDE CONTROLLER FAILED TO MAINTAIN ALTITUDE AND CLIMBED AT A HIGH RATE ABOVE 10,000 FEET. DESCENDED TO 8,000 FEET. PERFORMED BITE CHECK ON NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NO FAULTS FOUND. RAN NR 1 AND NR 2 PACKS, OPSJun 1, 1996 · N829US · Doug DC982 · Cabin Pressure Control SystemSDR USAA950526Cargo Net · out of positionBOS - FLIGHT 0120 - WHILE ON ROTATION, THE CREW FELT A BUMP THEN NOTICED THE FORWARD CARGO DOOR LIGHT ILLUMINATED. THE CAPTAIN DECIDED TO RETURN TO BOS. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PRESSURIZED THE AIRCRAFT AND CHECKED FOR LEAKS. NONE WERE FMay 23, 1995 · N829US · Doug DC982 · Cargo Compartments
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