N286AU, cancelled Aug 1, 2002

Service difficulty reports · 34

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 = 'N286AU' AND deregistration_id = 'N286AU-2002-08-01'
  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 USAASB01044Relief Valve · obstructedTPA - FLT 2850 - ON CLIMB-OUT FROM PBI, EN ROUTE TO BOS, THE AIRCRAFT WOULD NOT PRESSURIZE. DECISION WAS MADE TO DIVERT TO TPA. WHEN AIRCRAFT HIT THE GROUND AND LANDED AT TPA, AIRCRAFT PRESSURIZED NORMALLY. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND INSUFeb 9, 2001 · N286AU · Boeing 7372B7 · Cabin Pressure Control SystemSDR USAASB00265Acm · leakingBWI - FLT 2704 - ON DESCENT INTO BWI, FROM TPA, FUMES OF SULFUR/RUBBER SMELL WAS NOTICED THROUGH OUT THE CABIN. ODOR WAS STRONGEST IN SEAT ROWS 13 TO 17 AND WAS MOST NOTICEABLE WHEN ENGINE ANTI-ICE WAS SELECTED. SMELL DISSIPATED WHEN ENGINE ANTI-ICE WAS TURNSep 20, 2000 · N286AU · Boeing 7372B7 · Cabin Cooling SystemSDR USAA001351Stringer · corrodedTPA - FOUND STRINGER CORRODED 2 INCHES, STATION 986.5, STRINGER 27 LEFT. INSTALLED NEW SECTION OF STRINGER PER SRM 53-10-3 FIG 1. (M)Aug 25, 2000 · N286AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAASB99297Pressure Switch · failedBWI - FLT 2740 - ON DESCENT INTO BWI, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW SHUTDOWN THE NR 1 ENGINE AT 6,000 FT PER HANDBOOK PROCEDURES. FLIGHT LANDED AT BWI WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME Dec 18, 1999 · N286AU · Boeing 7372B7 · Engine Starting SystemSDR USAASB99272Gcu · malfunctionedTPA - FLT 2674 - FLIGHT LOST THE NR 1 TRANSFER BUS AND ALL INSTRUMENTS ON BOTH SIDES DURING ROTATION. CREW RESET THE NR 1 TRANSFER BUS CIRCUIT BREAKER WHICH BROUGHT BACK ALL INSTRUMENTS EXCEPT THE MACH AIRSPEED INDICATION. FLIGHT RETURNED TO FIELD AT TPA ANDNov 17, 1999 · N286AU · Boeing 7372B7 · DC Generating SystemSDR USAA991073Skin · crackedTPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN SKIN L-2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNER. INSTALLED DOUBLER PER REPAIR DOCUMENT 53-30-3 FIG 34 AND TR 53-30-10 REV A. (M)Oct 11, 1999 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA991072Skin · crackedTPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN SKIN R-2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNER. INSTALLED DOUBLER PER REPAIR DOCUMENT 53-30-3 FIG 33. (M)Oct 11, 1999 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980661Skin · crackedTPA - DURING A CX-5 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN FORWARD SERVICE DOOR UPPER HINGE CUTOUT AFT UPPER CORNER DOOR SKIN. INSTALLED DOUBLER PER TR 52-40-03A. (M)Dec 29, 1998 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB98189Fan · failedJAX - FLT 2606 - EN ROUTE FLL/BWI, CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. CREW SECURED THE GASPER FAN AND RIGHT PACK. THE SMOKE APPEARED TO ABATE. FLIGHT DIVERTED TO JAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE GASPER FAN CIRCUIT BJul 22, 1998 · N286AU · Boeing 7372B7 · Air Distribution FanSDR USAASB97241Oil Press Trans · failedCLT (FL 1223) AT FL 350 APPROXIMATELY 70 MILES NORTH OF CLT, THE NR 1 ENGINE OIL PRESSURE WENT TO ZERO. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO CLT. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. (20 MINUTES SINGLE ENSep 8, 1997 · N286AU · Boeing 7372B7 · Engine Oil PressureSDR USAA970158Angle · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT LOWER FASTENER HOLE OF FRAME INNER CHORD ANGLE BS 616 FRAME, WL 203. INSTALLED CHORD ANGLE REPAIR, REPAIRED PER EA 42310. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA970157Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1.25 INCH STATION 970 STRINGER 27L. REPLACED STRINGER SECTION, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 1. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA970156Floorbeam · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH BY .5 INCH CORRODED AREA WL 208.1 LBL 7 INCH BS 312 FLOORBEAM. INSTALLED REPAIR STRAPS, REPAIRED PER TR 5310-01A. CORROSION TASK NR C53-107-01, CORROSION LEVEL 1. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA970155Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 709 WL 203.5 LONGITUDINAL FLOORBEAM WEB. CUTOUT DAMAGE, INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-2. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA970154Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK RBL 25, .5 INCH CRACK LBL 25, .5 INCH CRACK LBL 45, .5 INCH CRACK RBL 45 BS 520, WL 207.75 FLOORBEAM. STOP DRILLED, INSTALLED DOUBLER, REPAIRED PER EA 42309. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA970153Frame · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT LOWER FASTENER HOLE OF FRAME INNER CHORD BS 616 RT WL 203. REPAIRED CHORD ANGLE, REPAIRED PER EA 42310. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA970152Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND GOUGE .5 INCH DIAMETER STATION 440 STRINGER 21R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA970151Skin · dentedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND DENT 1 INCH BY 2 INCH STATION 937 ABOVE STRINGER 20L, SKIN. INSTALLED DOUBLER, REPAIRED PER EA 42374. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA970150Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 668 LBL 24 INCH WL 205 FLOORBEAM WEB. INSTALLED DOUBLER, REPAIRED PER EA 42333. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA970149Floorbeam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK LBL 24.5 STATION 676 FLOORBEAM. INSTALLED CHANNEL, REPAIRED PER EO 5791G632. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA970148Skin · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT AFT END OF FORWARD AIRSTAIR HANEL CUTOUT SKIN BS 375 BETWEEN STRINGER 21-22L. INSTALLED EXT REPAIR DOUBLER, REPAIRED PER 53-30-03. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA970147Skin · dentedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH BY .75 INCH BY .020 DEEP DENT STRINGER 20R BS 312 SKIN. CUTOUT DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA970146Stringer · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 6 INCHES AT STATION 887 STRINGER 25R. INSTALLED DOUBLER (REPLACED DAMAGED SECTION), REPAIRED PER SRM 53-10-3. CORROSION TASK NR, C53-208-01, CORROSION LEVEL 1. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA970145Skin · lightning strikeINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND LIGHTNING STRIKE BS 203 BELOW STRINGER 19R SKIN. CUT OUT DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA970144Floorbeam · corrodedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 14 INCHES STATION 328 LBL 51 TO LBL 27 FLOORBEAM UPPER CHORD. REPLACED T-CAP, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 1. (M)Apr 22, 1997 · N286AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAASB97027Hyd Hose · leakingATL - FL 628 - FLIGHT DIVERTED TO ATL, DUE TO LOSS OF SYSTEM 'A' HYDRAULIC QUANTITY. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AFTER TURNING OFF RUNWAY, MAINTENANCE MET AND TOWED THE AIRCRAFT TO THE GATE. MAINTENANCE REPLACED Jan 24, 1997 · N286AU · Boeing 7372B7 · Hydraulic System, MainSDR USAASB97013Wire · brokenCMH - MAINTENANCE FOUND A SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING INOP IN THE AFT SECTION OF THE CABIN. MAINTENANCE REPAIRED A BROKEN WIRE AT THE FLOOR TRACK LIGHTING IN THE AFT SECTION OF THE CABIN. OPS CHECK GOOD. (M)Jan 14, 1997 · N286AU · Boeing 7372B7 · Light System WiringSDR USAASB96227Power Supply · inoperativeFOUND FORWARD CEILING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK. (M)Nov 12, 1996 · N286AU · Boeing 7372B7 · Emergency LightingSDR USAASB96190Battery Pack · dischargedSYR - MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHT INOP IN THE FORWARD CABIN. MAINTENANCE REPLACED THE BATTERY PACK AT THE FORWARD OVERHEAD CABIN. OPS CHECK GOOD. (M)Aug 3, 1996 · N286AU · Boeing 7372B7 · Emergency LightingSDR USAASB96132Downlocksensor · failedMCO - FL 1145 - ON DESCENT INTO MCO, LANDING GEAR WAS LOWERED,NOSE GEAR RED LIGHT FLICKERED ON. CAPTAIN WENT THROUGH MANUAL GEAREXTENSION PROCEDURE. NOSE GEAR SHOWED DOWN AND LOCKED IN VIEW FINDER.EMERGENCY EQUIPMENT WAS CALLED OUT. ABOUT FOUR MINUTES FROM Jul 17, 1996 · N286AU · Boeing 7372B7 · Landing Gear Position and WarningSDR USAASB96130Retract Mech · lack of lubePIT - FLT 1589 - DURING APPROACH TO PIT AND LANDING GEAR LOWERED, NOSE GEAR RED LIGHT STAYED ON. CREW RECYCLED GEAR, BUT NOSE GEAR RED LIGHT STILL SHOWED RED FOR APPROXIMATELY 20 SECONDS, THEN TURNED GREEN. FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT. MAIJul 16, 1996 · N286AU · Boeing 7372B7 · Landing Gear Retraction/Extension SystemSDR USAASB96120Downlock Sensor · out of adjustCLT - FLT 1126 - ON GEAR EXTENSION, NOSE GEAR RED LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR WITH NO HELP. GEAR VISUAL CHECK INDICATED GEAR WAS DOWN. RED LIGHT FINALLY WENT OUT AND GREEN LIGHT ILLUMINATED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTEJul 5, 1996 · N286AU · Boeing 7372B7 · Landing Gear Position and WarningSDR USAASB96098Lamp · burned outRSW - FLT 989 - ON APPROACH INTO RSW AT GEAR EXTENSION, CAPTAIN FAILED TO GET NOSE GEAR LIGHT. CAPTAIN DID A GO-AROUND AND RELAMPED NOSE GEAR DOWNLIGHT. GEAR WAS CYCLED WITH NORMAL GEAR INDICATION. RELAMPED NOSE GEAR LIGHT. (X)Jun 10, 1996 · N286AU · Boeing 7372B7 · Landing Gear Position and WarningSDR USAA951046Mode Cntl Pnl · failedPHL - FLT NR 0117 - CLIMBING OUT FROM LGA EN ROUTE TO MCO WITH ALT ALERTING AND 'A' CHANNEL AUTOPILOT ON MEL, AIRCRAFT WOULD NOT HOLD ALTITUDE OR RESPOND TO CHANGES WITHOUT USING ALT SEL. MAINTENANCE REPLACED THE AUTOPILOT MODE CONTROL PANEL. BITE CHECKED ANSep 27, 1995 · N286AU · Boeing 7372B7 · Autopilot System
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