N265AU, cancelled Jun 20, 2003
Service difficulty reports · 51
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 = 'N265AU' AND deregistration_id = 'N265AU-2003-06-20' 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 = 'N265AU' AND deregistration_id = 'N265AU-2003-06-20' 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 USAA011351Skin · dentedCLT - FOUND SKIN DENTED 4 INCHES BY 3 INCHES, BETWEEN BS 908 TO 951 S17R AND S20R. INSTALLED DOUBLER AND TRIPLER PER EA 85513. (M)SDR USAA011350Angle · crackedCLT - FOUND DRAG ANGLE CRACKED, STATION 540, JUST ABOVE STRINGER 23L. FABRICATED PART PER T/R 53-50-03A. (M)SDR USAA011299Beam · crackedCLT - FOUND BEAM CRACKED 1.5 INCH, LOWER INTERIOR FORWARD CORNER OF FORWARD ENTRY DOOR BEAM. INSTALLED A NEW BEAM ASSY PER SRM 51-10-1 AND 51-30-2. (M)SDR USAA011304Stringer · corrodedCLT - FOUND STRINGER CRACKED 6 INCHES, STRINGER 20L STATION 777. INSTALLED STRINGER REPAIR PER SRM 53-10-3 DETAIL VII. (M)SDR USAA011300Skin · crackedCLT - FOUND SKIN CRACKS 1.5 INCH AND .250 INCH, BS 380 EQUIP COOLING EXHAUST. INSTALLED REPAIR DOUBLER PER T/R 53-30-04. (M)SDR USAA011348Strap · damagedCLT - FOUND DAMAGED TEAR STRAP 8.9 INCHES, STATION 500 STRINGER 24L TO S25L. INSTALLED DOUBLER AND TRIPLER. (M)SDR USAA011283Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 10 INCHES, STATION 1006 TO STATION 1016 BBL 0. REPAIRED PER SRM 51-30-2. (M)SDR USAA011281Structure · chafedCLT - FOUND WEAR CHAFING FROM APU BLEED DUCT .250 BY 3 INCH, STATION 1064. INSTALLED REPAIR DOUBLER PER EA 85490. (M)SDR USAA011268Door Frame · crackedCLT - FOUND DOOR FRAME CRACKED .200 INCH, FORWARD SERVICE DOOR AFT FRAME NR 3 FITTING CUT OUT. INSTALLED DOUBLER PER EA 85464. (M)SDR USAA011292Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH, RBL 45 BS 1013 FLOOR LEVEL. FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 51-10-2. (M)SDR USAA011280Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCHES BY 1 INCH, STATION 968 STRINGER 25L. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)SDR USAA011263Shear Tie · damagedCLT - FOUND SHEAR TIE WITH WORKING FASTENERS, STATION 360 ATTACH LUG, BETWEEN STRINGER 28R AND 27R. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 9A. (M)SDR USAA011267Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH BS 300 S8R. REPLACED UPPER DOOR FRAME WITH LIKE PART. (M)SDR USAA011276Seat Track · corrodedCLT - FOUND SEAT TRACK SECTION CORRODED 1 INCH BY 3 INCHES, STATION 328 TO 360 RBL 55. SPLICE IN NEW SECTION OF TRACK PER 51-10-1. (M)SDR USAA011264Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, STATION 328 S17R. REPAIR PREVIOUSLY ACCOMPLISHED PER BOEING REPAIR DRAWING 65C2757. (M)SDR USAA011286Skin · damagedCLT - FOUND SKIN WITH PREVIOUSLY INSTALLED DOUBLER 10 INCHES BY 8 INCHES, STATION 380 BETWEEN S24 AND S23. INSTALLED NEW DOUBLER PER SRM 53-30-3 FIG 1. (M)SDR USAA011309Skin · crackedCLT - FOUND SKIN CRACKED 15 INCHES BY 13 INCHES, STATION 947 S15R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 35. (M)SDR USAA011239Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, BS 706 AT S10L. NEW CLIP INSTALLED PER EO 53936227. (M)SDR USAA011238Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, BS 663, S10L. NEW CLIP INSTALLED PER EO 53936227. (M)SDR USAA011307Frame · dentedCLT - FOUND FRAME DENTED 1 INCH BY 1 INCH, AFT CARGO STATION 767 ABOVE STRINGER 24R. INSTALLED DOUBLER AT STATION 767 PER SRM 51-40-3. (M)SDR USAA011303Seat Track · corrodedCLT - FOUND FLOOR TRACK CORRODED 1 INCH BY 1 INCH, AFT CARGO STATION 806 S26R. INSTALLED REPAIR TIE DOWN FLOOR SUPPORT PER SRM 53-10-5 FIG 11. (M)SDR USAA011282Beam · corrodedCLT - FOUND BEAM CORRODED, AFT CARGO STATION 797 S26R. REPLACED STRAP 65-47957-11 SRM 51-10-01. (M)SDR USAA011306Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 847 JUST ABOVE STRINGER 26R. INSTALLED DOUBLER. (M)SDR USAA011302Shear Tie · crackedCLT - FOUND SHEAR TIE CRACKED .5 INCH, AT STRINGER 25R TO FRAME AT STATION 947.5. REPLACE TIE CLIP. (M)SDR USAA011279Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 4 INCHES, STATION 663 BL 0. INSTALLED WEB, SPLICE ANGLE REPAIR. (M)SDR USAA011285Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED AT CLIP NUT HOLES 2 INCHES BY 60 INCHES, BS 986, LBL 6 TO RBL 54, WL 207. INSTALLED NEW T-CAP. (M)SDR USAA011284Intercostal · corrodedCLT - FOUND BEAM INTERCOSTAL CORRODED 2 INCHES BY 26 INCHES, BS 990-1016 LBL 6 TO LBL 16. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-3. (M)SDR USAA011289Floorbeam · corrodedCLT - FOUND BEAM CORRODED 2 INCHES BY 33 INCHES, BS 1016 BBL 0 LBL 33. INSTALLED T-CAP PER T/R 53-60-02. (M)SDR USAA011290Floorbeam · corrodedCLT - FOUND BEAM/CHANNEL/WEB CORRODED 5 INCHES, BS 1014-1019 BBL 0 LBL 6. INSTALLED T-CAP. (M)SDR USAA011261Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 4 FEET BY 2 INCHES, STATION 328, BL 0 RIGHT TO SERVICE DOOR. FABRICATED AND INSTALLED T-CAP. (M)SDR USAA011291Skin · dentedCLT - FOUND SKIN DENTED 1 INCH, BS 280 STRINGER 24R. REMOVED DAMAGE, INSTALLED REPAIR PER SRM 53-30-3. (M)SDR USAASB01109Power Supply · inoperativeBWI - THE OUTSIDE AND AFT EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)SDR USAASB01094Power Supply · failedBOS - PILOT REPORTED THAT THE AFT LEFT AND AFT RIGHT EMERGENCY ESCAPE SLIDE LIGHTS WERE INOPERATAIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK (P/N 61-0478-9). OPS CHECK GOOD. (M)SDR USAA010295Stringer · crackedTPA - FOUND STRINGER CRACKED 1.25 INCH, STRINGER 27, STATION BS 947. INSTALLED PART PER SRM 53-10-3 FIG 1. (M)SDR USAASB00359Transmitter · malfunctionedBOS - FLT 2610 - WHILE SELECTING FLAPS 5 ON APPROACH AT MHT, THE FLAPS JAMMED BETWEEN THE 2 AND 5 POSITION. DUE TO THE SHORT RUNWAYS AT MHT, CREW DECIDED TO DIVERT TO BOS. DURING FINAL APPROACH TO BOS, CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHSDR USAASB00198Adc · failedTPA - FLT 2674 - ON CLIMB-OUT, NR 2 MACH METER OFF FLAG DISPLAYED, NR 2 ALTIMETER STANDBY FLAG APPEARED, TCAS BECAME INOPERATIVE, ALT REPORTING ON THE XSPONDER BECAME INOP, NR 2 V-SPEED SHOWED A DESCENT DURING CLIMB. CREW UNABLE TO PULL ANY CB'S ON PANEL TO RSDR USAASB99281Power Supply · failedCLE - MAINTENANCE FOUND BOTH AFT DOOR EXTERIOR EMERGENCY LIGHTS AND INTERIOR LOWER EXIT SIGN LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 61-0478-9) AND POWER SUPPLY. OPERATIONAL CHECK GOOD. (X)SDR USAASB99280Battery · dischargedALB - MAINTENANCE FOUND THE COCKPIT EMERGENCY EXIT SIGN INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (X)SDR USAASB99154Connector · brokenBWI - FL2700 - FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT INCIDENT DUE TO THE NR 2 ENGINE FUEL HEAT VALVE OPEN LIGHT FLICKERING AND THE NR 2 ENGINE OIL TEMPERATURE RISING SLIGHTLY HIGHER THAN THE NR 1 ENGINE INTO THE YELLOW RANGE. NO ENGINE SHUT DOWN OSDR USAA990483Stringer · corrodedTPA - DURING CX-4 CHECK, FOUND 8 INCHES OF STRINGER WEB CORRODED AT STRINGER 27R AT STATION 967 THROUGH 975. REPLACED STRINGER PER SRM 53-00-03. (M)SDR USAASB98325Control Panel · malfunctionedPIT - FL2053 - FLIGHT DIVERTED TO PIT DUE TO THE LEFT WING TO BODY OVERHEAT LIGHT CONTINUOUSLY FLICKERING FLIGHT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE LEFT WING TO BODY OVERHEAT DETECTION LOOP. NO DEFECTS NOTEDSDR USAASB97244Battery Pack · dischargedPIT - EMERGENCY LIGHTS (AISLE) FROM SEATS 7-13 WORK INTERMITTENTLY. MTC REPLACED EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK OK. REF: OPERATOR CONTROL NR 97ZZZX4225. (X)SDR 97ZZZX4225Battery Charger · inoperativePIT - EMERGENCY LIGHTS (AISLE) FROM SEATS 7-13 WORK INTERMITTENTLY. MTC REPLACED EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK OK. REF: OPERATOR CONTROL NR USAASB97244.SDR USAA970271Frame · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 616, LBL 63, WL 201.5 FRAME. INSTALLED FILLER AND DOUBLER ON ANGLE, REPAIRED PER EA 42969. (M)SDR USAA970270Skin · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN OUTER SKIN AT LOWER HINGE CUTOUT AFT ENTRY DOOR. INSTALLED EXT SKIN REPAIR, REPAIRED PER SERM 53-30-3 (FIG 34) AND EA 42994. (M)SDR USAA970269Bulkhead · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 CRACKS 1.5 INCH, .75 INCH AND 1.5 INCH. THE 1.5 INCH CRACK RBL 4.75 WL 201, .75 INCH CRACK LBL 4.75 WL 98, 1.5 INCH CRACK RBL 4.75 WL 198 178 BULKHEAD. INSTALLED DOUBLER AND STOP DRILLED PER TR 53-10-11. (M)SDR USAA960806Stringer · corrodedROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 13 INCHES OF CORROSION, STRINGER 27 LEFT, BETWEEN STATION 1003 AND 1016. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR USAASB96114Strap · out of positionPIT - FLT 1279 - WHILE CLIMBING THROUGH 8,000/9,000 FEET, FLIGHT ATTENDANT ADVISED CAPTAIN OF A NOISE FROM THE REAR OF THE AIRCRAFT. AFTER LEVELLING OFF AT 11,000 FEET, DISCOVERED THE SAFETY RESTRAINING STRAP WAS CAUGHT IN THE 2L DOOR. THERE WAS NO DOOR WARNSDR USAASB96057Flap Indicator · failedCLT - FLT 1632 - AFTER TAKEOFF, CREW RECEIVED FLAP ASYMMETRY LIGHT UPON RETRACTION OF FLAPS. NO UNCOMMANDED ROLL WAS EXPERIENCED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAP INDICATOR. (M)SDR USAA951003Oil Press Xmittr · failedBUF - FLT NR 1063 - ON CLIMB-OUT FROM BUF, NR 2 ENGINE OIL PRESSURE INDICATION DROPPED TO 15 PSI. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO BUF WHERE LANDING WAS WITHOUT INCIDENT. SET WAS 11 MINUTES. MAINTENANCE REPLACED THE NR 2 ENGINE OIL PRESSURE
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