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.

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)Oct 23, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA011350Angle · crackedCLT - FOUND DRAG ANGLE CRACKED, STATION 540, JUST ABOVE STRINGER 23L. FABRICATED PART PER T/R 53-50-03A. (M)Oct 12, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Oct 10, 2001 · N265AU · Boeing 737201 · Passenger/Crew DoorsSDR USAA011304Stringer · corrodedCLT - FOUND STRINGER CRACKED 6 INCHES, STRINGER 20L STATION 777. INSTALLED STRINGER REPAIR PER SRM 53-10-3 DETAIL VII. (M)Oct 4, 2001 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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)Oct 3, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA011348Strap · damagedCLT - FOUND DAMAGED TEAR STRAP 8.9 INCHES, STATION 500 STRINGER 24L TO S25L. INSTALLED DOUBLER AND TRIPLER. (M)Oct 2, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011283Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 10 INCHES, STATION 1006 TO STATION 1016 BBL 0. REPAIRED PER SRM 51-30-2. (M)Sep 30, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011281Structure · chafedCLT - FOUND WEAR CHAFING FROM APU BLEED DUCT .250 BY 3 INCH, STATION 1064. INSTALLED REPAIR DOUBLER PER EA 85490. (M)Sep 28, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Sep 25, 2001 · N265AU · Boeing 737201 · Fuselage Main, StructureSDR 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)Sep 25, 2001 · N265AU · Boeing 737201 · Fuselage Structure (General)SDR USAA011280Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCHES BY 1 INCH, STATION 968 STRINGER 25L. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)Sep 24, 2001 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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)Sep 22, 2001 · N265AU · Boeing 737201 · Fuselage Main, StructureSDR USAA011267Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH BS 300 S8R. REPLACED UPPER DOOR FRAME WITH LIKE PART. (M)Sep 20, 2001 · N265AU · Boeing 737201 · Fuselage Main, FrameSDR 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)Sep 20, 2001 · N265AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA011264Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, STATION 328 S17R. REPAIR PREVIOUSLY ACCOMPLISHED PER BOEING REPAIR DRAWING 65C2757. (M)Sep 19, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR 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)Sep 19, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR 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)Sep 18, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA011239Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, BS 706 AT S10L. NEW CLIP INSTALLED PER EO 53936227. (M)Sep 14, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011238Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, BS 663, S10L. NEW CLIP INSTALLED PER EO 53936227. (M)Sep 14, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Sep 13, 2001 · N265AU · Boeing 737201 · Fuselage Main, FrameSDR 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)Sep 13, 2001 · N265AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA011282Beam · corrodedCLT - FOUND BEAM CORRODED, AFT CARGO STATION 797 S26R. REPLACED STRAP 65-47957-11 SRM 51-10-01. (M)Sep 13, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA011306Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 847 JUST ABOVE STRINGER 26R. INSTALLED DOUBLER. (M)Sep 12, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011302Shear Tie · crackedCLT - FOUND SHEAR TIE CRACKED .5 INCH, AT STRINGER 25R TO FRAME AT STATION 947.5. REPLACE TIE CLIP. (M)Sep 12, 2001 · N265AU · Boeing 737201 · Fuselage Main, StructureSDR USAA011279Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 4 INCHES, STATION 663 BL 0. INSTALLED WEB, SPLICE ANGLE REPAIR. (M)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR 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)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR 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)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR 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)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011290Floorbeam · corrodedCLT - FOUND BEAM/CHANNEL/WEB CORRODED 5 INCHES, BS 1014-1019 BBL 0 LBL 6. INSTALLED T-CAP. (M)Sep 11, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011261Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 4 FEET BY 2 INCHES, STATION 328, BL 0 RIGHT TO SERVICE DOOR. FABRICATED AND INSTALLED T-CAP. (M)Sep 8, 2001 · N265AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA011291Skin · dentedCLT - FOUND SKIN DENTED 1 INCH, BS 280 STRINGER 24R. REMOVED DAMAGE, INSTALLED REPAIR PER SRM 53-30-3. (M)Sep 6, 2001 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB01109Power Supply · inoperativeBWI - THE OUTSIDE AND AFT EXIT IDENTIFIER LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)Apr 3, 2001 · N265AU · Boeing 737201 · Emergency LightingSDR 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)Mar 29, 2001 · N265AU · Boeing 737201 · Emergency LightingSDR USAA010295Stringer · crackedTPA - FOUND STRINGER CRACKED 1.25 INCH, STRINGER 27, STATION BS 947. INSTALLED PART PER SRM 53-10-3 FIG 1. (M)Mar 20, 2001 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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 FURTHDec 26, 2000 · N265AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR 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 RJul 26, 2000 · N265AU · Boeing 737201 · Air Data ComputerSDR 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)Nov 29, 1999 · N265AU · Boeing 737201 · Emergency LightingSDR USAASB99280Battery · dischargedALB - MAINTENANCE FOUND THE COCKPIT EMERGENCY EXIT SIGN INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPERATIONAL CHECK GOOD. (X)Nov 19, 1999 · N265AU · Boeing 737201 · Emergency LightingSDR 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 OJun 25, 1999 · N265AU · Boeing 737201 · Engine Anti-Icing SystemSDR 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)May 30, 1999 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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 NOTEDDec 12, 1998 · N265AU · Boeing 737201 · Cabin Cooling SystemSDR 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)Sep 9, 1997 · N265AU · Boeing 737201 · Emergency LightingSDR 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.Sep 9, 1997 · N265AU · Boeing 737201 · Emergency LightingSDR 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)Aug 22, 1997 · N265AU · Boeing 737201 · Fuselage Main, FrameSDR 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)Aug 22, 1997 · N265AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR 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)Aug 22, 1997 · N265AU · Boeing 737201 · Fuselage Main, BulkheadSDR 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)Dec 30, 1996 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 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 WARNJun 23, 1996 · N265AU · Boeing 737201 · Passenger Compartment EquipmentSDR 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)Mar 28, 1996 · N265AU · Boeing 737201 · Trailing Flap Position Indicating SystemSDR 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 PRESSURESep 23, 1995 · N265AU · Boeing 737201 · Engine Oil Pressure
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