N827US, cancelled May 16, 2006

Service difficulty reports · 53

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 = 'N827US' AND deregistration_id = 'N827US-2006-05-16'
  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 USAAD02012Battery · inoperativeIND - SOME OF THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Mar 13, 2002 · N827US · Doug DC981 · Emergency LightingSDR USAAD02010Light · inoperativeIND - SEVERAL SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Feb 19, 2002 · N827US · Doug DC981 · Emergency LightingSDR 2001F00740Light · inoperativeIND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHTS AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMEDec 6, 2001 · N827US · Doug DC981 · Emergency LightingSDR 2001F00739Battery · dischargedIND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHTS AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMEDec 6, 2001 · N827US · Doug DC981 · Emergency LightingSDR USAAD01186Battery · dischargedIND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, TAIL CONE EMERGENCY LIGHT RECEIVER, AFT OVERWING EMERGENCY EXIT LIGHTS AND CEILING LIGHTS AT SEAT ROWS 18 TO 21 WERE DIM. THE RIGHT AFT OVERWING IDENTIFIER LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMEDec 6, 2001 · N827US · Doug DC981 · Emergency LightingSDR USAA010921Fitting · crackedPIT - FOUND FITTING CRACKED 4.5 INCHES, MAIN ENTRY DOOR UPPER HINGE FITTING BROKEN AT BASE. REPLACED WITH IDENTICAL PART NR. (M)Jun 29, 2001 · N827US · Doug DC981 · DoorsSDR USAA010808Frame · crackedPIT - FOUND FRAME CRACKED 2 INCHES, CANTED STATION 1485 AT LONGERON 3L. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M)Jun 27, 2001 · N827US · Doug DC981 · Fuselage Main, StructureSDR 2001F00000Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01103. (M)May 14, 2001 · N827US · Doug DC981 · Emergency LightingSDR USA2001F00003Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. REF USAAD01103. (M)May 14, 2001 · N827US · Doug DC981 · Emergency LightingSDR USAAD01103Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS, NACELLE SCAN, AND CEILING LIGHTS AT SEAT ROWS 7 TO 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL, NACELLE SCAN, AND CEILING EMERGENCY LIGHT BATTERIES. (M)May 14, 2001 · N827US · Doug DC981 · Emergency LightingSDR USAAD01030Battery · dischargedTPA - DURING A TEST OF THE EMERGENCY LIGHTS, ROW 25 UNDER SEAT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. A BATTERY WAS REPLACED. OPERATIONALLY CHECKED OK. (M)Feb 16, 2001 · N827US · Doug DC981 · Emergency LightingSDR USAAD00188Duct · crackedPIT-PBI - FLT 1947 - AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED A LOUD BANG FROM THE TAIL AREA, ALSO SMOKE IN THE TAIL CONE AND CABIN. NO UNUSUAL COCKPIT INDICATIONS WERE NOTED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RDec 29, 2000 · N827US · Doug DC981 · Air Distribution SystemSDR USAAD00184Bottle · dischargedMCO - THE TAILCONE SLIDE INFLATION BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE TAILCONE SLIDE ASSY. (M)Dec 1, 2000 · N827US · Doug DC981 · Escape SlideSDR USAAD00163Strut · leakingPIT-AVP - FLT 671 - AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR STRUT ASSEMBLY. (M)Oct 6, 2000 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR USAAD00159Strut · damagedBNA-PIT - FLT 548 - AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RAISED, THE NOSE GEAR LIGHT INDICATED UNSAFE AND A LOUD NOISE WAS HEARD. AT THE SAME TIME, THE AIRCRAFT DEPRESSURIZED. THE FLIGHT DECLARED AND EMERGENCY AND RETURNED TO THE FIELD TO MAKE AND UNEVENOct 6, 2000 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR USAAD00083Valve · leakingBNA-PHL - FLT 478 - DURING CLIMB-OUT, THE RIGHT HYDRAULIC SYSTEM QUANTITY WAS LOST. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. A MANUAL LANDING GEAR EXTENSION WAS REQUIRED. MAINTENANCE REPLACED THE RIGHT SPOILER CONTROL VALVE. (M)May 25, 2000 · N827US · Doug DC981 · Drag Control SystemSDR USAAD00027Seal · leakingMSP-CLT - FLT 1631 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR STRUT SEALS. (M)Feb 9, 2000 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR USAAD00004Unknown · odorMKE-PIT - FLT 1845 - AFTER ARRIVAL IN PIT, THE FLIGHT ATTENDANTS REPORTED SMELLING FUMES, THE ODOR OF FUEL AND EXHAUST DURING FLIGHT. MAINTENANCE RAN THE ENGINES AND THE APU TO CHECK FOR FUEL LEAKS. NO LEAKS WERE FOUND. THE ACM OIL LEVELS CHECKED NORMAL. BJan 15, 2000 · N827US · Doug DC981 · Air Distribution SystemSDR USAAD99176Actuator · failedPIT/TPA - FLT 1845 - WHILE CRUISING AT 35,000 FEET, THE CABIN ALTITUDE SLOWLY CLIMBED TO 10,000. AFTER CREW WAS UNABLE TO CONTROL THE CABIN ALTITUDE MANUALLY, AN EMERGENCY DESCENT WAS INITIATED AND THE AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MADec 11, 1999 · N827US · Doug DC981 · Pressure Regulator/Outflow ValveSDR USAAD99100Power Supply · failedIND - THE CEILING EMERGENCY LIGHTS ADJACENT TO THE AFT SERVICE DOOR WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY. (X)Jul 22, 1999 · N827US · Doug DC981 · Emergency LightingSDR USAA990253Frame · corrodedPIT - DURIGN C5 CHECK, FOUND 1 INCH AREA OF CORROSION ON AND AROUND FASTENER HOLE AT AFT CARGO DOOR FRAME, FORWARD STRAP FASTENER HOLE IN LINE WITH LONGERON 28R. INSTALLED STRAP ASSEMBLY PER EA NR 51730. (M)Mar 11, 1999 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA990252Frame · corrodedPIT - DURING C5 CHECK, FOUND 1 INCH AREA OF CORROSION ON AND AROUND FASTENER HOLE AT AFT CARGO DOOR FRAME, AFT STRAP FASTENER HOLE LONGERON 28R. INSTALLED STRAP ASSEMBLY PER EA NR 51730. (M)Mar 11, 1999 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA990251Skin · corrodedPIT - DURING C5 CHECK, FOUND 1 INCH LONG, 1 INCH WIDE, .011 DENT AND 1 INCH LONG, 1 INCH WIDE, .009 DEEP DENT AT RIGHT WING INBOARD FLAP, AFT SIDE, MIDDLE OF TOP CENTER SKIN PANEL. CORROSION LEVEL 1. CLEANED AND TREATED CORROSION PER SRM CHAP 51. (M)Mar 11, 1999 · N827US · Doug DC981 · Trailing Edge FlapsSDR USAAD99029Coalescer Bag · dirtyBOS-BUF - FLT 1022 - AFTER LANDING AT BUF THE FLIGHT CREW REPORTED FUMES IN THE FORWARD GALLEY AND COCKPIT 25 MINUTES AFTER TAKEOFF. SUSPECTED THE LEFT AIR CONDITIONING PACK AS THE SOURCE. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM AND REPLACED THE WATEFeb 18, 1999 · N827US · Doug DC981 · Humidity Control SystemSDR USAAD98139Sensor · malfunctionedCLT - FLT 995 - AFTER TAKEOFF FROM CLT AND GEAR RETRACTION, THE GEARS DOOR LIGHTS REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR AND RECEIVED THE SAME INDICATION. THE FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT Aug 6, 1998 · N827US · Doug DC981 · Landing Gear Door Retract SectionSDR USAAD98097Engine · failedMCO - FLT 2292 - DURING CLIMB-OUT, THERE WAS A LOUD BANG FROM THE LEFT ENGINE AND THE N1 INDICATION DECREASED. THE VIBRATION INDICATION WENT OFF SCALE ON THE HIGH SIDE. THE ENGINE THROTTLE WAS RETURNED TO IDLE, THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WMay 30, 1998 · N827US · Doug DC981 · Engine (Turbine/Turboprop)SDR USAAD97224Power Supply · inoperativePHL - EMERGENCY LIGHTS INOPERATIVE AT ROWS 27 THROUGH 30. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)Nov 24, 1997 · N827US · Doug DC981 · Emergency LightingSDR USAAD97168Bulbs · failedPIT - FL 1640 - ON APPROACH, CREW DID NOT RECEIVE THE LEFT MAIN LANDING GEAR DOWN AND LOCKED LIGHT. CREW CYCLED THE GEAR WITH SAME RESULT. CREW SUBSTITUED SIMILAR LIGHTS FROM AND FOUND THAT THE ORIGINAL LIGHT BULBS WERE BURNED OUT. FLIGHT LANDED NORMALLY ATSep 28, 1997 · N827US · Doug DC981 · Landing Gear Position and WarningSDR USAAD97108Duct · failedPIT/MDT - FLT 1672 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO FIELD. REPLACED 4 INCH RUBBER DUCT ON BOTH PACKS. (X)Jun 21, 1997 · N827US · Doug DC981 · Cabin Cooling SystemSDR USAAD97091Strut · req'd serviceFLT 441 - PIT-ORD - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR, AND NOSE STILL WOULD NOT RETRACT. RETURNED TO PIT. SERVICED NOSE STRUT WITH NITROGEN. (M)May 19, 1997 · N827US · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR USAAD97087Power Supply · failedIND - FOUND LAST ROW OF EMERGENCY TRACK LIGHTING INOPERATIVE. REPLACED POWER SUPPLY. (M)May 18, 1997 · N827US · Doug DC981 · Emergency LightingSDR USAAD96145Battery Pack · dischargedTAIL COMPARTMENT EMERGENCY LIGHTS DIM. REPLACED BOTH BATTERY PACKS IN RIGHT AFT LAVATORY. (M)Sep 27, 1996 · N827US · Doug DC981 · Emergency LightingSDR USAA950968Fitting · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND 3 INCH BY 6 INCH AREA OF CORROSION LEVEL 2 IN CUSP ANGLE AT MED FRAME LOWER ATTACH FITTING STATION 200. CORROSION TASK NR C46-53303. REMOVED CORRODED SECTION AND SPLICED NEW SECTION IN PER USAIR EA 31153. (M)Aug 24, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950988Jamb · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED FORWARD CARGO DOOR JAMB PAN ALONG BOTTOM EDGE BETWEEN PAN AND FUSELAGE SKIN CORROSION REF C51-53300. REMOVED LOWER SECTION OF DOOR JAMB AND SPLICED IN NEW SECTION PER SRM 53-05 FIGAug 23, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950969Frame · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND 3 AREAS 2 INCHES BY 3 INCHES OF LEVEL 2 CORROSION AFT SIDE OF FRAME AT STATION 1250 FROM LONGERON 28L TO 28R. CORROSION TASK NR C57-53300. CLEANED CORRODED SECTION AND INSTALLED DOUBLERS PER SRM 53-03 FIG 2A. (M)Aug 23, 1995 · N827US · Doug DC981 · Fuselage Main, FrameSDR USAA950984Longeron · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH BY 20 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED AT LONGERON 28L, STATION 1211 TO 1231 CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M)Aug 18, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950967Longeron · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 29R AT STATION 1297 CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M)Aug 18, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950966Longeron · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 28R AT STATION 1287. CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M)Aug 18, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950986Beltframe · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED IN BELTFRAME BETWEEN LONGERON 28R AND 28L BELTFRAME 180. CORROSION TASK NR C45-53300. REMOVED SECTION OF BELTFRAME AND SPLICED IN NEW SECTION PER SRM 53-03 FIG 2A. (M)Aug 16, 1995 · N827US · Doug DC981 · Fuselage Main, FrameSDR USAA950983Angle · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK LEFT SIDE STATION 1463, DRAG ANGLE. INSTALLED FILLER AND DOUBLER PER SRM 53-05 FIG 23. (M)Aug 16, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950982Cusp Membrane · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND 12 INCH CRACK IN CUSP MEMBRANE STATION 1231, LONGERON 18L. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 96. (M)Aug 16, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950981Longeron · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND 5 CRACKS .125 INCH TO .375 INCH LONG, BELTFRAME 256 TO 408 IN LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M)Aug 16, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950987Track · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND CORROSION 1 INCH BY 6 INCHES LEFT INBOARD SEAT TRACK MOUNT HOLES AT STATION 1205. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M)Aug 14, 1995 · N827US · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR USAA950985Angle · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND 2 INCH BY 29 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED RIGHT LAV T-CUSP ANGLE FROM STATION 1309 TO 1338 LONGERON 18R. CORROSION TASK NR C58-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05 FIG 25. (M)Aug 12, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950970Doubler · corrodedPIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION 2 INCHES BY 35 INCHES STATION 1338, JACK PAD DOUBLER AFT CARGO AREA. CORROSION TASK NR C57-53300. REPLACED DOUBLER, CUT OUT DAMAGED AREA AND SPLICED IN NEW SECTION PER USAIR TYPICAL REPAIR 53-30-10. Aug 11, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950980Longeron · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND 6 CRACKS APPROXIMATELY .125 INCH TO .25 INCH IN LONGERON 17L AT BELTFRAME 237, 275, 295, 332, 370 AND 389. SPLICED IN NEW SECTION OF LONGERON BETWEEN STATION 237 TO 408 PER SRM 53-02 FIG 2. (M)Aug 10, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950979Longeron · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK LONGERON 4L AT STATION 160. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M)Aug 10, 1995 · N827US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA950978Jamb · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK UPPER FORWARD CORNER OF MED JAMB. INSTALLED INTERNAL AND EXTERNAL DOUBLER PER SRM 53-05 FIG 2B. (M)Aug 10, 1995 · N827US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950649Pump · inoperativeMCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE FJun 29, 1995 · N827US · Doug DC981 · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZW813Rtn Line Filter · inoperativeMCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE FJun 29, 1995 · N827US · Doug DC981 · Hydraulic Filter, Main
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