N824BX, cancelled May 16, 2006

Service difficulty reports · 26

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 = 'N824BX' AND deregistration_id = 'N824BX-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 IXXA0200002OTransmitter · defectiveWHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND TRACED THE PROBLEJan 17, 2002 · N824BX · Doug DC871F · Hydraulic Quantity IndicatorSDR IXXA0200001OTransmitter · defectiveWHILE ENROUTE FROM JFK TO BDL, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO BDL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND TRACED THE PROBLEJan 17, 2002 · N824BX · Doug DC871F · Hydraulic Quantity IndicatorSDR 0100037OWarning System · activatedPRIOR TO ROTATION AIRCRAFT EXPERIENCED ABNORMAL EXHAUST GAS TEMPERATURE INDICATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO PARKING. NO FURTHER ABNORMALITIES OCCURRED.Jun 20, 2001 · N824BX · Doug DC871F · Engine EGT/TIT Indicating SystemSDR IXXA0100016Swivel · leakingAFTER TAKEOFF FROM TOL, THE FLIGHT CREW NOTICE A DECLINED IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATING A RUPTURED LEFT AILERON SWIVEL GLAND. MAINTENANCE REPACKED THEApr 18, 2001 · N824BX · Doug DC871F · Hydraulic System, MainSDR IXXA0000036Uplock Roller · lack of lubeEN ROUTE FROM IAH TO TOL, THE GEAR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED Oct 27, 2000 · N824BX · Doug DC871F · Landing Gear Position and WarningSDR IXXA9800078Plating · corrodedDURING ROUTINE PREFLIGHT INSPECTION, FOUND THE FUSELAGE EXTERNAL PLATING WITH CORROSION BULGE, TWO MISSING RIVET HEADS AND THREE CRACKS MIGRATING FROM ONE MISSING RIVET HEADS BETWEEN FUSELAGE STATION -21.0 TO 30.0 BETWEEN LONGERON 31 RIGHT AND 35 LEFT. THE AOct 8, 1998 · N824BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9800067Pressure Syst · malfunctionedEN ROUTE AT FLIGHT LEVEL 35.0, THE AIRCRAFT CABIN BEGAN TO CLIMB RAPIDLY, MANUAL CONTROL OF PRESSURIZATION WAS ATTEMPTED. PACK FLOWS WERE INCREASED TO 90 PERCENT CAPACITY WITH MINIMAL DECREASE IN CABIN. DESCENT INITIATED AND AT LEVEL OFF CABIN COULD BE MAINAug 25, 1998 · N824BX · Doug DC871F · Cabin Pressure Control SystemSDR IXXA980004Engine · damagedEN ROUTE FROM TOL TO ATL, DURING CRUISE THE FLIGHT ENGINEER NOTICED A MARKED DECLINE IN THE NUMBER ONE ENGINE OIL QUANTITY. THE CREW PERFORMED A PRECAUTIONARY INFLIGHT SHUTDOWN IAW COMPANY PROCEDURES, AND CONTINUED TO ATL MAKING AN UNEVENTFUL LANDING. MAINTFeb 12, 1998 · N824BX · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA96118Hpt Blade · crackedDURING PRECAUTIONARY BORESCOPE INSPECTION OF THE NR 1 ENGINE, MAINTENANCE FOUND ONE HIGH PRESSURE TURBINE BLADE TRAILING EDGE TIP CORNER MISSING. MISSING MATERIAL WAS LOCATED AT THE TRAILING EDGE TIP, DOWNWARD TO THE FIRST AIR SLOT IN AREA B, CFMI MM 72-00-00Jul 27, 1996 · N824BX · Doug DC871 · Turbine SectionSDR IXXA96117Mec · leakingCOMPRESSOR STALL ACCOMPANIED BY FLAMES EXITING THE EXHAUST NOZZLE REPORTED TO THE CREW BY THE CONTROL TOWER ON LANDING ROLL AT PDX, CREW SUSPECTED THE NR 2 ENGINE. MX BORESCOPED THE NR 2 ENGINE WITH NO FINDINGS. MX FOUND THE MEC SUSPECT OF CAUSING THE STALL Jul 27, 1996 · N824BX · Doug DC871 · Fuel Control/Turbine EnginesSDR IXXA96120Control Cable · brokenON TAXI OUT AND FLIGHT CONTROL CHECKS AT ATL, AILERONS FELT STIFF WITH VERY LITTLE SPOILER PRESSURE DROP. THE AIRCRAFT RETURNED TO RAMP. MAINTENANCE INSPECTED THE FLIGHT CONTROL CABLES AND FOUND THE LEFT AILERON BUS CABLE BROKEN. MAINTENANCE REPLACED THE BRJun 26, 1996 · N824BX · Doug DC871 · Aileron Control SystemSDR IXXA9683Fire Warning · shortedEN ROUTE FROM DEN-TOL - THE NR 4 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT CAME ON INTERMITTENTLY, FOLLOWED BY A STEADY LIGHT. AFTER THREE MINUTES, THE SYSTEM WOULD NO LONGER TEST. SHORTLY THEREAFTER, THE FIRE WARNING LIGHT ILLUMINATED AND THE ENGINE WAS SHUT May 30, 1996 · N824BX · Doug DC871 · Fire DetectionSDR IXXA9605Air Distr · odorEN ROUTE BETWEEN MKE AND DEN, THE AIR CONDITIONING PACKS WERE PRODUCING A STRONG, UNIDENTIFIED ODOR. ON THE GROUND IN DEN, THE PACKS WERE OPERATIONALLY CHECKED AND FOUND NOT TO BE PRODUCING AND ODOR AT THAT TIME. A REVIEW OF THE FLIGHT SUGGESTED THAT A SMALLJan 31, 1996 · N824BX · Doug DC871 · Air Distribution SystemSDR IXXA9594Uplatch Cable · out of adjustON TAKEOFF FROM TOL TO ONT, THE CREW REPORTED AN UNSAFE GEAR AND DOOR LIGHT AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO TOL FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR LANDING GEAR SYSTEM INSPECTION AND RIG CHECK. A RIG CHECJan 3, 1996 · N824BX · Doug DC871 · Landing Gear Retraction/Extension SystemSDR IXXA9608Engine · flamed outEN ROUTE FROM TOL TO SEA, THE NR 4 ENGINE FLAMED OUT AT 35,000 FEET. TWO UNSUCCESSFUL RESTART ATTEMPTS WERE MADE. THE ENGINE WAS SECURED AND THE AIRCRAFT DIVERETED TO MSO FOR MAINTENANCE. UPON ARRIVAL IN MSO, THE FLIGHT CREW REPORTED THEY SUMPED TANKS AND RJan 2, 1996 · N824BX · Doug DC871 · Engine (Turbine/Turboprop)SDR IXXA199589Connector · deterioratedWHEN THE LANDING GEAR UPLATCH CHECK WAS PERFORMED ON DEPARTURE OUT OF TOL, THE GEAR DOOR WARNING LIGHT REMAINED ON. THE AIRCRAFT ELECTED TO RETURN TO TOL FOR MAINTENANCE. TOL MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE ELECTRICAL CONNECTOR FOROct 21, 1995 · N824BX · Doug DC871 · Landing Gear Position and WarningSDR IXXA199587Flap Fitting · brokenAT MSP, IT WAS DISCOVERED THAT THE STATION 98 OUTBOARD FLAP BASE FITTING ON LEFT INBOARD FLAP SECTION HAD EXPERIENCED A TYPICAL FAILURE DUE TO A CRACK THAT ORIGINATED IN THE UPPER FLAP VANE ATTACH BOLT HOLE. THE OPPOSING BASE FITTING AT THAT STATION HAD RECIEOct 13, 1995 · N824BX · Doug DC871 · Trailing Edge FlapsSDR IXXA199585Uplatch Switch · failedON DEPARTURE OUT OF BOS, THE LANDING GEAR FAILED THE UPLATCH CHECK. THE LANDING GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULT, WITH THE LANDING GEAR LEVER IN THE UPLATCH CHECK POSITION, THE UNSAFE LIGHT WAS ILLUMINATED WITH NO APPARENT GEAR EXTENSION. INSOct 10, 1995 · N824BX · Doug DC871 · Landing Gear Position and WarningSDR IXXA199579Uplock Switch · bent pinORD/PDX - ON TAKEOFF, CREW REPORTED WITH LANDING GEAR HANDLE UP, LANDING GEAR UNSAFE LIGHT REMAINED ON. CREW RECYCLED GEAR HANDLE AND IT OPERATED NORMALLY. ON APPROACH TO PDX, GEAR EXTENDED NORMALLY. CREW DID OPS CK AND RETRACTED GEAR. WITH GEAR HANDLE UP, Sep 22, 1995 · N824BX · Doug DC871 · Landing Gear Position and WarningSDR IXXA199576Connector · contaminatedON TAKEOFF OUT OF ONT, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. CYCLING THE LANDING GEAR EXTINGUISHED THE DOOR WARNING LIGHT. IN TOL, TROUBLESHOOTING REVEALED A HIGH RESISTANCE IN THE LEFT MLG DOOR UPLATCH SWITCH CIRCUIT CAUSED BY A CONTAMINSep 15, 1995 · N824BX · Doug DC871 · Landing Gear Position and WarningSDR IXXA199524Oil Cap · unlockedOKC - ON DEPARTURE, FLIGHT CREW NOTICED THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO OKC FOR MAINTENANCE. SOME OIL QUANTITY WAS RETAINED, AND MINIMUM WINDMILLING OIL PRESSURE WAS MAINTAINMar 31, 1995 · N824BX · Doug DC871 · Turbine Engine Oil SystemSDR IXXA9542Skin · crackedDURING ROUTINE C-CHECK INSPECTION, EXTERNAL PLATING OF THE RIGHT WING EXHIBITED FOUR CRACKS. THE DAMAGE WAS AT WS XRS 74.8 BETWEEN STR 9 THROUGH STR 12. REPAIR OF THE AREA WAS ACCOMPLISHED BY CUTTING OUT THE CRACKS, INSTALLING FILLERS FOR THE REMOVED MATERIAFeb 17, 1995 · N824BX · Doug DC871 · Wing, Plate/SkinSDR IXXA9541Belt Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, STA 1120 BELT FRAME WAS FOUND CORRODED. DAMAGE WAS LIMITED TO ONE AREA JUST INBOARD OF LONGERON 35 RT AND APPROXIMATELY 1 INCH IN DIAMETER. THE DAMAGE WAS REPAIRED BY CUT-OUT, INSTALLING A FILLER, AND INSTALLING AN EXTERNALFeb 14, 1995 · N824BX · Doug DC871 · Fuselage Main, FrameSDR IXXA9540Belt Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND AT STA 1020 BELT FRAME. TWO AREAS, ONE AT LONGERON 34.5 RT AND ONE AT 34.5 LT, WERE 1 INCH BY 1 INCH AREAS. CORROSION REMOVAL WENT BEYOND SRM LIMITS. REPAIR OF THE BELT FRAME IAW DRAWING HSE27Feb 14, 1995 · N824BX · Doug DC871 · Fuselage Main, FrameSDR IXXA9538Drag Angle · crackedDURING ROUTINE C-CHECK INSPECTION, A 2.200 INCH CRACK WAS FOUND IN THE NR 2 PYLON, INBOARD DRAG ANGLE. AFTER EVALUATION BY DOUGLAS AND FAA DER APPROVAL, THE AIRCRAFT WAS RETURNED TO SERVICE WITH FOLLOW-UP INSPECTIONS REQUIRED AT C-CHECK AND REPLACEMENT REQUIRFeb 12, 1995 · N824BX · Doug DC871 · Nacelle/Pylon StructureSDR IXXA9539Hinge Fitting · crackedDURING ROUTINE C-CHECK, THE LEFT OUTBOARD FLAP, INBOARD FLAP BASE HINGE FITTING WAS CRACKED IN HALF ON THE OUTBOARD HALF. THE FITTING WAS REPLACED IAW DOUGLAS SB 27-249 AND THE AIRCRAFT MM. (X)Feb 2, 1995 · N824BX · Doug DC871 · Trailing Edge Flaps
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