N585US, cancelled Sep 12, 2006
Service difficulty reports · 62
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 = 'N585US' AND deregistration_id = 'N585US-2006-09-12' 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.
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 = 'N585US' AND deregistration_id = 'N585US-2006-09-12' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA050281Door Frame · crackedPIT - FOUND DOOR WITH THREE .5 INCH CRACKS, AFT CARGO DOOR FORWARD FRAME. REMOVED AND REPLACED DOOR PER JOB CARD J3-57-52301. (M)SDR USAA040413Skin · crackedCLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D S-23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M)SDR USAA040414Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, BS 727E S23L. INSTALLED DOUBLERS PER SRM 53-00-01 FIG 229. (M)SDR USAA040232Frame · crackedFRAME CRCKED, 1 INCH LONG CRACK, STA 616 JUST BELOW STRINGER 17L. FABRICATED FILLER IAW T/R 53-62-01, 53-60-01 AND J NR 58-53503-004.SDR USAA040200Stringer · crackedSTRINGER (.2500 INCH X .1250 INCH CRACKS) CRACKED STA 908 AND STR 4R. REPLACED STRINGER SPLICE IAW SRM 51-20-02.SDR USAA040182Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED, STATION 986.5. CORROSION LEVEL 1, TASK NR C53-107-01. REPLACED INTERCOSTAL STRUCTURE BETWEEN STATION 986.5 AND 100.6 PER SRM 52-10-02. (M)SDR USAA040181Support Fitting · crackedPIT - FOUND MLG SUPPORT FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING REAR SPAR OF RIGHT WING. REPLACED RIGHT MLG SUPPORT FITTING PER EA 78221. (M)SDR USAA040179Web · crackedPIT - FOUND FLOOR WEB CRACKED 1 INCH AND 1.5 INCHES, BETWEEN STATION 559 AND 578 AT STRINGER 17L. REPLACED FLOOR WEB PER SRM 51-10-2. (M)SDR USAA040180Support Fitting · crackedPIT - FOUND MLG SUPPORT FITTING CRACKED .25 INCH LONG, LEFT MLG SUPPORT FITTING REAR SPAR OF LEFT WING. REPLACED LEFT MLG SUPPORT FITTING PER EA 78221. (M)SDR USAA040160Stringer Splice · crackedPIT - FOUND STRINGER SPLICE WITH TWO .125 INCH CRACKS, FS 907, S4R STRINGER SPLICE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)SDR USAASB03153Control Unit · malfunctionedAFTER TAKEOFF FROM TPA, CREW REPORTED UNABLE TO RETRACT FLAPS BEYOND 2 UNITS. CREW RECYCLED FLAP HANDLE AND FLAPS CIRCUIT BREAKER SEVERAL TIMES WITH NO HELP. FLIGHT RETURNED TO FIELD AT TPA WITH 2 UNITS FLAPS AND FULL SLATS. FLIGHT LANDED WITHOUT INCIDENT. SDR USAASB03033Indicator · failedCLT - FLT 953 - ON APPROACH TO CLT FROM BOS, CREW REPORTED THAT WHEN FLAPS WERE EXTENDED TO 10 UNITS, THE RIGHT TRAILING EDGE FLAP STOPPED AT 6 UNITS. CREW EXTENDED GEAR AND ATTEMPTED TO MOVE THE FLAPS TO 15 UNITS BUT FLAPS WOULD NOT MOVE. CREW DISCONTINUED SDR USAA020476Skin · crackedPIT - FOUND SKIN CRACKED 2 INCHES, STATION 727 STRINGER 24L. CUT OUT DAMAGE, NDT'D AREA, INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 201 AND TR 53-60-06. (M)SDR USAASB02185Wire · brokenEWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT 1C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEATS 2A AND C. OPERATIONAL CHECK GOOD. (M)SDR USAA020370Skin · crackedPIT - FOUND SKIN WITH TWO CRACKED .25 INCH LONG, STATION 380 BODYLINE 0 AT RIVET FASTENER. INSTALLED DOUBLER, ROUTED OUT CRACK PER TYPICAL REPAIR 53-30-07 AND EA 74918. (M)SDR USA2002F00077Wire · brokenMAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 13 ABC INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 13 ABC. OPERATIONAL CHECK NORMAL.SDR USAASB02117Solenoid · faultySYR - FLT 251 - AFTER T/O FROM SYR, COULD NOT GET THE GEAR HANDLE TO MOVE PAST THE 'OFF' POSITION. CREW DID NOT OVERRIDE THE GEAR HANDLE BECAUSE OF A FLAPPING NOISE HEARD FROM THE NLG WW. FLT RETURNED TO FIELD AT SYR AND LANDED WITHOUT FURTHER INCIDENT. AFTSDR USAA020134Bulkhead · crackedTPA - FOUND BULKHEAD WEB CRACKED TWO PLACES 2.5 INCH EACH, FS 663.75, RBL 45, W/W FORWARD BULKHEAD WEB. INSTALLED TWO DOUBLERS PER EA 94296A. (M)SDR USAA020133Skin · crackedTPA - FOUND SKIN CRACKED .25 INCH, LOWER AFT CORNER OF LOWER HINGE CUT OUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-10-12. (M)SDR USA2001F00006Panel · departedAFTER TAKEOFF, FLIGHT ENCOUNTERED COMPLETE LOSS OF SYSTEM A HYDRAULICS AND PRESSURE. LOST LG TRIANGULAR PANEL OFF TOP OF RT WING. NOSE GEAR WOULD RETRACT BUT MAIN GEAR WOULD NOT. HYDRAULIC LINE HAD BROKEN. PANEL DEPARTED AIRCRAFT AT END OF RUNWAY. CAPTAINSDR USAASB01046Indicator · failedBUF - FLT 638 - DURING DESCENT INTO BUF, CREW EXTENDED FLAPS TO 5 DEGREES AND THEN TO 10 DEGREES BUT RECEIVED A FLAP LIGHT. FLAPS WOULD NOT EXTEND BEYOND 5 DEGREES. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT LANDED AT BUF WITHOUT FURTHER INCIDENT. MAINTENSDR USAASB00352Jackscrew · wornCLT - FLT 1974 - ON DESCENT INTO CLT, FROM MBJ, CAPTAIN NOTIFIED TOWER THAT THE FLAPS WOULD NOT EXTEND BEYOND FIVE DEGREES. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MX TSDR USAASB00314Flap · malfunctionedBWI - FLT 2046 - ON APPROACH TO DCA, FROM MCI, THE TRAILING EDGE FLAPS STOPPED AT 8-10 DEGREES WITH NEEDLES SPLIT ON INDICATOR. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO BWI. FLIGHT LANDED AT 5 DEGREES TRAILING EDGE FLAPS AND WITHOUT SDR USAASB00243Warning Light · illuminatedPIT - FLT 1624 - ON CLIMB-OUT FROM PIT, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED AS LEADING EDGE SLATS AND FLAPS DID NOT FULLY RETRACT. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFORSDR USAASB00256Battery Pack · dischargedRDU - WHILE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LEFT OVERHEAD EXIT LIGHTS, THE OVERWING DOOR EXIT LIGHTS, THE SEAT MOUNTED EXIT LIGHT AT OVERWING DOOR ROW AND ONE BULLNOSE EMERGENCY LIGHT OVER SEAT ROW 14, RIGHT SIDE, WOULD NOT HOLD CHARGE AFTSDR USAASB00185Control Panel · failedPHL - FLT 637 - EN ROUTE FROM BOS-PHL, AT FL280, THE CABIN PRESSURE BEGAN TO SLOWLY CREEP UP TO 10,000 FEET. THE ALTITUDE WARNING HORN SOUNDED AND THE CREW BEGAN AN IMMEDIATE DESCENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED. FLIGHT CONTISDR USAA000888Frame · wornCLT - FOUND FRAME WORN 3 INCHES WEAR AREA CAUSED BY APU DUCT CLAMP, STATION 1040. REPAIRED PER EA 67421/SRM 53-00-03. (M)SDR USAA000878Angle · crackedCLT - FOUND CHORD ANGLE CRACKED 4 INCHES, STATION 1138, STRINGER 5R INSIDE UPPER STRAP CHORD ANGLE. FABRICATED REPAIR AND INSTALLED PER SRM 53-00-01 FIG 221. (M)SDR USAA000868Frame · crackedCLT - FOUND FRAME CRACKED .5 INCHES, STATION 480, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M)SDR USAA000869Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 440, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M)SDR USAA000870Frame · crackedCLT - FOUND FRAME CRACKED .5 INCHES, STATION 500A, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000871Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 400, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000858Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 400, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER SRM 53-10-14A. (M)SDR USAA000859Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 440, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000861Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 727D, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000862Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 747, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000863Frame · crackedCLT - FOUND FRAME CRACKED, STATION 747 STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000864Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 787, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000865Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 827, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000866Frame · crackedCLT - FOUND FRAME .5 INCH CRACKED, STATION 827, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000867Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 867, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000860Frame · crackedCLT - FOUND FRAME CRACKED .5 INCHES, STATION 480, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)SDR USAA000848Door Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR JAMB FRAME UPPER FORWARD DOOR STOP FITTING. REMOVED AND REPLACED PART PER BOEING DWG 65-55878. (M)SDR USAA000815Bulkhead · crackedCLT - FOUND TWO CRACKS IN BULKHEAD .25 INCH AND .75 INCH, WL 201, LBL 5. FABRICATED AND INSTALLED REPAIR PART PER TR 53-10-08 FIG 209. (M)SDR USAA000814Angle · crackedCLT - FOUND ANGLE CRACKED 1 INCH, LOWER FORWARD WING TO BS 540 ABOVE RT RAM AIR DUCT. INSTALLED DOUBLER PER TR 53-50-03. (M)SDR USAA000884Channel · crackedCLT - FOUND U-CHANNEL CRACKED .375 INCH, STRINGER 18A SHAFT LEFT W/W PLUS 727. REPLACED STRINGER 18A SHELF. (M)SDR USAA000885Frame · corrodedCLT - FOUND 1 INCH CORROSION, STATION 807 BETWEEN STRINER 23R-24R. FABRICATED REPLACEMENT STIFFENER PER DWG 69-38178. CORROSION LEVEL 1, TASK NR C53-202-01. (M)SDR USAA000883Support Bracket · crackedCLT - FOUND DOOR SUPPORT CRACKED 2 INCHES, LOWER CORNER AT FORWARD DOOR SUPPORT. INSTALLED DOUBLER PER SRM 51-70-11. (M)SDR USAA000882Drag Brace · crackedCLT - FOUND DRAG BRACE ANGLE CRACKED .5 INCH, BS 536, STRINGER 21L. INSTALLED FABRICATED SUPPORT ANGLE SECTION PER TR 53-50-03. (M)SDR USAA000887Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH IN FRAME AT INBOARD RIVET HOLE, STATION 787, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED REPAIR DOUBLER PER TR 53-10-14A. (M)
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