N817US, cancelled May 21, 2004

Service difficulty reports · 39

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 = 'N817US' AND deregistration_id = 'N817US-2004-05-21'
  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 USAAD01191Odor · detectedORD - PIT - FLT 1194 - THERE WAS A STRONG RUBBER SMELL IN THE AIRCRAFT DURING TAKEOFF. THE SMELL DISAPPEARED SHORTLY AFTER GEAR RETRACTION. MAINTENANCE NOTICED A SLIGHT TIRE RUBBER SMELL IN THE MAIN WHEEL WELLS. THE CONDITION OF THE MAIN WHEEL WELLS AND TIRDec 16, 2001 · N817US · Doug DC982 · Air Distribution SystemSDR 2002F00000Battery · dischargedIND - THE MAIN ENTRY EMERGENCY LIGHT AND THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY EMERGENCY LIGHT ASSEMBLY AND THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M)Dec 12, 2001 · N817US · Doug DC982 · Emergency LightingSDR USAAD01189Light · inoperativeIND - THE MAIN ENTRY EMERGENCY LIGHT AND THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY EMERGENCY LIGHT ASSEMBLY AND THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M)Dec 12, 2001 · N817US · Doug DC982 · Emergency LightingSDR USAAD01187Receiver · inoperativePIT - THE CATWALK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT RECEIVER. (M)Dec 8, 2001 · N817US · Doug DC982 · Emergency LightingSDR USAAD00133Fuel Control · leakingFLL-PIT - FLT 1821 - FUEL SMELL IN PASSENGER CABIN AND COCKPIT. MAINTENANCE REPLACED THE APU FUEL CONTROL UNIT. (M)Aug 16, 2000 · N817US · Doug DC982 · APU Engine Fuel and ControlSDR USAAD00131Unknown · odorCLT-BOS - FLT 506 - 45 MINUTES AFTER TAKEOFF, THE SMELL OF JET FUEL WAS VERY STRONG. SMELL LASTED 15 MINUTES. MAINTENANCE RAN THE ENGINES, CHECKED THE AIR CONDITIONING COMPONENTS AND THE AIR CYCLE UNITS. THE WING AND WING PANELS WERE INSPECTED FOR SEEPAGE AAug 14, 2000 · N817US · Doug DC982 · Air Distribution SystemSDR USAA000298Skin · crackedPIT - FOUND TWO SKIN CRACKS BOTH .125 INCH LONG, AT STATION 1380 BETWEEN LONGERON 14R AND 15R. CUT OUT DAMAGED, INSTALLED FILLERS AND DOUBLERS PER SRM 53-04 FIG 18 SHT 1 PAGE 98A. (M)Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA000299Longeron · crackedPIT - FOUND LONGERON 1 INCH CRACK, STATION 160 LONGERON 4L. CUT OUT DAMAGED SECTION, INSTALLED NEW AND SPLICED PER SRM 53-02 FIG 18. (M)Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA000300Longeron · crackedPIT - FOUND 2 INCH CRACK, STATION 160 LONGERON 2L. CUT OUT DAMAGED SECTION. INSTALLED NEW AND SPLICED PER SRM 53-02 FIG 18. (M)Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA000301Floorbeam · corrodedPIT - FOUND CORROSION, 1 INCH BY 20 INCHES, FLOORBEAM UPPER CHORD, STATION 1309. CUT OUT CORRODED SECTION. INSTALLED NEW AND SPLICED PER EA 54092. CORROSION LEVEL 1. (M)Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Floor BeamSDR USAA000302Longeron · crackedPIT - FOUND 1.5 INCH CRACK AT STATION 160, LONGERON 3L. CUT OUT DAMAGED SECTION, INSTALLED NEW AND SPLICED PER SRM 53-02, FIG 18. (M)Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA000303Longeron · crackedPIT - FOUND 1 INCH CRACK AT STATION 160 LONGERON NR 1. CUT OUT DAMAGED SECTION, INSTALLED NEW AND SPLICED PER SRM 53-02, FIG 18. (M)Feb 9, 2000 · N817US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAAD99012Battery · dischargedBUF - THE OVERHEAD EMERGENCY LIGHT AT SEAT ROW 30 AND BETWEEN THE AFT LAVATORIES WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Jan 18, 1999 · N817US · Doug DC982 · Emergency LightingSDR USAAD98141Engine · malfunctionedPIT - FLT 365 - EN ROUTE BUF-CLT - CREW NOTED A RISE IN THE LEFT ENGINE OIL TEMPERATURE, EXCEEDING 165 DEGREES. THE ENGINE STARTED TO VIBRATE. CREW SECURED THE ENGINE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ENGAug 9, 1998 · N817US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAAD98135Filter · cloggedPIT-TPA - FLT 219 - THE RIGHT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED DURING CRUISE. AFTER ABNORMAL PROCEDURES FAILED TO EXTINGUISH THE LIGHT THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO CLT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLAAug 5, 1998 · N817US · Doug DC982 · Turbine Engine Oil SystemSDR USAAD97180Retract Mech · malfunctionedPHL - FLT 531 - AFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. CREW CYCLED THE GEAR. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED A GEAR SWING AND COULD NOT DUPLICATE THE FAULT. THE GEAR WAS LUBED AS A PRECAUTION. (X)Oct 15, 1997 · N817US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAAD97045Downlock Ind · failedFLT 1192 - PIT-BDL - WHEN GEAR WAS EXTENDED AT BDL, NOSEGEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATED. CYCLED GEAR AND LIGHT STILL DID NOT ILLUMINATE. DID TOWER FLYBY, AND LANDED NORMALLY AT BDL. RELAMPED DOWN AND LOCKED INDICATOR. (M)Feb 24, 1997 · N817US · Doug DC982 · Landing Gear Position and WarningSDR USAAD96128Engine · failedFLT 984 - CLT-ORF - AFTER TAKEOFF, THE NR 2 OIL FILTER CLOGGING LIGHT ILLUMINATED. AT IDLE POWER, THE LIGHT REMAINED ILLUMINATED, ACCOMPANIED BY RISING OIL TEMPERATURE AND REDUCED FUEL FLOW. SHUT DOWN NR 2 ENGINE, AND RETURNED TO FIELD. 19 MINUTES SINGLE ENGSep 15, 1996 · N817US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAAD96124Comp Blades · fod damageFLT 1224 - ATL-PIT - LEFT ENGINE COMPRESSOR STALLS ON CLIMB-OUT FROM ATL. RETURNED TO FIELD. NO ENGINE SHUTDOWN. FOUND FOD DAMAGE TO 7TH STAGE COMPRESSOR BLADES. REPLACED ENGINE. (M)Sep 2, 1996 · N817US · Doug DC982 · Turbine Engine Compressor SectionSDR USAAD96104Temp Sensors · failedFLT NR 1665 - PIT-FLL - 'TAIL COMPT TEMP HIGH' LIGHT ILLUMINATED DURING CLIMB. RETURNED TO FIELD. REPLACED WIRING BETWEEN TAIL COMPARTMENT TEMPERATURE SENSORS AND AFT PRESSURE BULKHEAD. (M)Jul 14, 1996 · N817US · Doug DC982 · Overheat DetectionSDR USAAD96100Battery Pack · dischargedFIRST CLASS FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK. (M)Jul 9, 1996 · N817US · Doug DC982 · Emergency LightingSDR USAAD96085Circuit Breaker · failedFLT 765 - CLT-MSY - ON CLIMB, WHEEL WELL OVERHEAT CIRCUIT BREAKER POPPED. RETURNED TO FIELD. REPLACED CIRCUIT BREAKER. (M)Jun 24, 1996 · N817US · Doug DC982 · Overheat DetectionSDR USAAD96073Cooling Screen · dirtyFLT 985 - BDL-TPA - WITH RIGHT GENERATOR ON MEL AND APU RUNNING FOR ELECTRICAL POWER, GOT APU OIL TEMP HI CAUTION LIGHT AT FL 350. DESCENDED TO FL 250, AND LIGHT WENT OUT. FLIGHT DIVERTED TO CLT DUE TO FUEL AND WEATHER CONSIDERATIONS AT NEW ALTITUDE. FOUND Jun 8, 1996 · N817US · Doug DC982 · AC Generator-AlternatorSDR USAA951244Frame · corrodedPIT - DURNG Q1/C6 INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA PREVIOUSLY REWORKED BELT FRAME, STA 1250, BETWEEN LONGERON 28R AND LONGERON 29R. CORROSION TASK REF C57-53300, LEVEL 1. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-14, FIGURE 5.Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, FrameSDR USAA951243Fitting · corrodedPIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, STA 180 - STA 200, RT SIDE BELOW FORWARD SERVICE DOOR IN FITTINGS AND CUSP ANGLE. CORROSION TASK NR C46-53305. SPLICED IN NEW SECTION OF CUSP AND FITTINGS PER SRM 53-03-5, CONF. J060Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951242Longeron · corrodedPIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LONGERON 28L SPLICE AT STA 228. CORROSION TASK NR C51-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14. (X)Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA951241Support Rail · corrodedPIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LT AND RT FLOOR SUPPORT RAILS, STA 218 - STA 541, FORWARD CARGO, CORROSION TASK NR C51-5330. INSTALLED SPLICE REPAIR PER USAIR TYPICAL REPAIR 53-20-09A. (X)Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951240Skin · crackedPIT - DURING Q1/C6 INSPECTION, FOUND 4.75 INCH CRACK JUST OUTBOARD OF NR 7 SLAT TRACK CUT-OUT LEADING EDGE SKIN. INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 57-06A, FIGURE 1, AND USAIR EA NR 31672. (X)Nov 22, 1995 · N817US · Doug DC982 · Wing, Plate/SkinSDR USAA951239Longeron · corrosionPIT - DURING Q1/C6 INSPECTION, FOUND .50 INCH BY 9 INCH AREA OF LEVEL 1 CORROSION RESULT FROM UNIQUE EVENT, BROKEN WATER LINE. CORROSION TASK NR C57-53300. LONGERON 28L FROM STA 1315 - STA 1332. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14 AND USAIR EA NR 31Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA951238Skin · crackedPIT - DURING Q1/C6 INSPECTION, FOUND CRACK APPROXIMATELY 1 INCH LONG IN SECOND LAYER OF SKIN IN UPPER FORWARD CORNER OF M.E.D. IN FUSELAGE SKIN (X-RAY INSPECTION) SSI 53-11-015. CUT OUT CRACK AND INSTALLED FILLER AND DOUBLERS PER SRM 53-05, FIGURE 25A. (X)Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA951237Skin · crackedPIT - DURING Q1/C6 INSPECTION, FOUND .020 INCH CRACK IN LIGHTNING STRIKE AREA OF FUSELAGE EXTERIOR SKIN AT STA 380, LONGERON 6L AND LONGERON 7L. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 53-30-11. (X)Nov 22, 1995 · N817US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA951236Clip · corrodedPIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STA 1060 BETWEEN LONGERON 29R AND LONGERON 30R SKIN CLIP. CORROSION TASK NR C57-53300. SPLICED IN SECTION OF SKIN CLIP PER SRM 53-03, FIGURE 3. (X)Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951234Membrane · crackedPIT - DURING A Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN CUSP MEMBRANE WEB STATION 1032 OUTBOARD OF RT SEAT TRACK. ACCOMPLISHED SPLICE REPAIR PER USAIR EA NR 315530A. (M)Nov 22, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951212Frame · crackedPIT - DURING Q-1/C-6 INSPECTION, FOUND .5 INCH CRACK AT CANTED FRAME 1485 AT LONGERON 7L. STOPPED DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-14-4 FIG 3. (M)Nov 14, 1995 · N817US · Doug DC982 · Fuselage Main, FrameSDR USAA951211Skin · crackedPIT - DURING Q-1/C-6 INSPECTION, FOUND 1.09375 INCH CRACK AT STATION 821 AND LONGERON 17R IN EXTERIOR SKIN. CUTOUT DAMAGED AREA AND INSTALLED FILLER AND 6.5 INCH BY 8.5 INCH INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW H. (M)Nov 14, 1995 · N817US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA951210Clip · crackedPIT - DURING Q-1/C-6 INSPECTION, FOUND 1 INCH CRACK IN FRAME TO FUSELAGE CLIP AFT SIDE OF BS 1437 AT LONGERON 1. SPLICED IN NEW CLIP PER SRM 53-03 FIG 6. (M)Nov 14, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951209Cusp Membrane · crackedPIT - DURING Q-1/C-6 INSPECTION, FOUND .25 INCH CRACK RIGHT SIDE CABIN STATION 984 AND 1003 AT LONGERON 18 CUSP LINE MEMBRANE. MANUFACTURED CUSP MEMBRANE AND INSTALLED PER SRM 53-05 FIG 97. (M)Nov 14, 1995 · N817US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA950006Clamp · leakingMCO - FLT 2382 - AFTER DEPARTING MCO, CREW RECEIVED AND OVERHEAT INDICATION IN THE TAIL SECTION. THE CREW FOLLOWED EMERGENCY PROCEDURES TO ISOLATE THE PROBLEM. THE LT PACK WAS SHUTDOWN, BUT THE CABIN PRESSURE COULD NOT BE MAINTAINED ON THE RIGHT PACK. THE CJan 4, 1995 · N817US · Doug DC982 · Cabin Cooling SystemSDR USAA950009Lines · looseCLT - FLT 1133 - A VIBRATION WAS REPORTED IN THE FLOOR OF THE ACFT AND AFT JUMPSEAT AREA. THE CREW DECIDED TO DIVERT TO CLT. FOUND SENSE LINES TO LT AUGMENTATION VALVE AND PILOT PRESSURE REGULATORS LOOSE. TIGHTENED LINES. (W)Jan 1, 1995 · N817US · Doug DC982 · Cabin Pressure Control System
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