Boeing 737-301

Service difficulty reports · 4,797

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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 aircraft_model_key = '737301'
  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 USAA001219Beam · crackedCLT - FOUND SHEAR BEAM SHELF CRACKED .75 INCH, STRINGER 18A SHEAR BEAM WEB STATION 726, LBL 60.5, WL 188. INSTALLED NEW SHELF PER EA 67690 DWG 65 46877. (M)Aug 8, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001218Track · corrodedCLT - FOUND TIE DOWN TRACK CORRODED 6 INCHES BY 2 INCHES, FS 787 TO 947 TRACK TIE DOWN, RBL 13. REMOVED AND REPLACED PER SRM 53-00-53. (M)Aug 8, 2000 · N353US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAASB00209Engine · stalledORD - FLT 1142 - DURING CLIMB-OUT AT FL080, THE NR 1 ENGINE THROTTLE ADVANCED RAPIDLY AND EGT WENT TO THE LIMIT. AUTOTHROTTLES WERE DISCONNECTED. ABOUT ONE MINUTE LATER, THE NR 1 ENGINE COMPRESSOR STALLED AND EGT RAPIDLY CLIMBED. THROTTLES WERE BROUGHT BACKAug 6, 2000 · N356US · Boeing 737301 · Engine (Turbine/Turboprop)SDR USAA001152Skin · corrodedCLT - FOUND INNER DOOR SKIN CORRODED 1 INCH BY 4 INCH AREA, FS 847 STRINGER 25R. CORROSION LEVEL 1. REMOVED AND REPLACED PER SRM 53-00-07 AND SRM 51-40-02. (M)Aug 4, 2000 · N353US · Boeing 737301 · Passenger/Crew DoorsSDR USAA001151Door Frame · corrodedCLT - FOUND FRAME CORRODED 2 INCHES BY 6 INCHES, STATION 787 PLUS 6 AFT CARGO DOOR FRAME. CORROSION LEVEL 1, C53-208-01. INSTALLED DOUBLER PER SRM 51-70-11 AND 53-00-07 FIG 201. (M)Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, StructureSDR USAA001150Door Frame · corrodedCLT - FOUND FRAME CORRODED 2 INCHES BY 5 INCHES, FORWARD SERVICE DOOR AFT FRAME BELOW FLOOR LEVEL. CORROSION LEVEL 1, C53-107-02. REMOVED AND REPLACED Z-ANGLE PER DWG 65 45875. (M)Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, StructureSDR USAA001156Frame · crackedCLT - FOUND FRAME WEB CRACKED .25 INCH, STATION 807 STRINGER 9RT. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001155Frame · crackedCLT - FOUND FRAME WEB CRACKED .25 INCH, STATION 887 FRAME WEB STRINGER 9 RT. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001154Frame · crackedCLT - FOUND FRAME WEB CRACKED .25 INCH, STATION 847 FRAME WEB STRINGER 9 LT. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001153Frame · crackedCLT - FOUND FRAME WEB CRACKED .25 INCH, STATION 827 FRAME WEB STRINGER 9 LT. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001142Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, UPPER FORWARD CORNER FORWARD SERVICE DOOR CUTOUT. REMOVED AND REPLACED DAMAGE PART PER SRM 51-10-02. (M)Aug 2, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001122Bushing · corrodedCLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZONTAL STAB LOWER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1 C-53-701-02. REMOVED CORROSION PER SRM 55-10-10. (M)Aug 1, 2000 · N354US · Boeing 737301 · Horizontal Stabilizer StructureSDR USAA001121Bushing · corrodedCLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZ STAB UPPER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1. REMOVED CORROSION PER SRM 55-10-10. (M)Aug 1, 2000 · N354US · Boeing 737301 · Horizontal Stabilizer StructureSDR USAA001120Stringer · corrodedCLT - FOUND STRINGER CORRODED 2 INCHES, STATION 969, STRINGER 29L. CORROSION LEVEL 1. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-03. (M)Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001119Shear Tie · corrodedCLT - FOUND FRAME SHEAR TIE CORRODED 1 INCH BY 2 INCHES, FRAME 947 OUTBOARD OF STRINGER 27L. REPLACED SHEAR TIE PER 51-10-02. CORROSION LEVEL 1. (M)Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, StructureSDR USAA001118Frame · corrodedCLT - FOUND CORROSION 5 INCHES BY 8 INCHES, STATION 727 BETWEEN STRINGER 27R AND 27L. CORROSION LEVEL 1 C53-208-01. REPLACED CHORD ANGLE PER SRM 53-00-01. (M)Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001117Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 15 INCHES, STATION 344 FROM RBL 2 TO LBL 13 FLOOR LEVEL. REPLACED T-CAP PER SRM 53-10-51. CORROSION LEVEL 1. (M)Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001125Pressure Panel · crackedCLT - FOUND PRESSURE DECK WITH TWO CRACKS .5 INCH AND 1 INCH, PRESS DECK MLG WHEEL WELL STRINGER 663, LBL 30. REMOVED DAMAGE INSTALLED REPAIR DOUBLER AND FILLER PER TR 53-60-04. (M)Aug 1, 2000 · N354US · Boeing 737301 · Fuselage Floor PanelSDR USAA001124Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 2 INCHES, STATION 328, LBL 49. CORROSION LEVEL 1, C53-107-01. REMOVED CORROSION AND INSTALLED NEW T-CAP PER SRM 51-70-12 FIG 1. (M)Aug 1, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001123Beam · crackedCLT - FOUND SUPPORT BEAM CRACKED .375 INCH, LEFT MLG SUPPORT BEAM. ACCOMPLISHED INTERMIN REPAIR PER EA 67644 AND TR 57-40-13. (M)Aug 1, 2000 · N354US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USDAA001116Floor Support · crackedCLT - FOUND FLOOR SUPPORT WITH 3 INCH CRACKS, STATION 380-400, 0 BBL. REPLACED FLOOR SUPPORT PER REPAIR 51-10-02. (M)Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001115Stringer · crackedCLT - FOUND STRINGER FLANGE .375, STATION 360, STRINGER 14L. REPLACED STRINGER SPLICE PER DWG 65-61777-503. (M)Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001114Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, AFT UPPER CORNER WINDOW CUTOUT. INSTALLED DOBLER PER EA 67657. (M)Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001113Skin · crackedCLT - FOUND SLAT SKIN WITH 7 CRACKS, .5 INCH EACH, NR 5 SLAT LOWER SKIN SURFACE INBOARD OF HEAT TUBE. INSTALLED DOUBLER PER DWG 65C30133. (M)Aug 1, 2000 · N353US · Boeing 737301 · Leading Edge DevicesSDR USAASB00204Duct · severedBOS - FLT 6507 - FLIGHT RETURNED TO FIELD AT BOS DUE TO AN ELECTRICAL SMELL THROUGHOUT THE CABIN. CAPTAIN ELECTED TO RETURN TO BOS AFTER NUMEROUS COMPLAINTS FROM THE FLIGHT ATTENDANTS AND PASSENGERS. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOUAug 1, 2000 · N349US · Boeing 737301 · Air Distribution SystemSDR USAA001534Skin · corrodedPIT - FOUND CORROSION ON HORIZ STAB LE, NR 5 RIB PANEL 9450. CORROSION LEVEL 1. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-20-02. (M)Jul 31, 2000 · N577US · Boeing 737301 · Horizontal Stabilizer, Plate/SkinSDR USAA001085Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCH AREA, STATION 294.5, RBL 45. REMOVED AND INSTALLED FABRICATED ANGLE PER SRM 53-10-08 AND 51-40-02. (M)Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001076Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH IN 15 AREAS, BS 312 UPPER CHORD FRAME RBL 36, LBL 15. CORROSION LEVEL 1. FABRICATED NEW FLOORBEAM T-CAP PER SRM 53-10-08, 53-10-51. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001075Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 5 INCHES, STATION 360, BBL 0. CORROSION LEVEL 1, C53-107-01. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-51. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001079Frame · crackedCLT - FOUND FRAME WEB CRACKED .025 INCH, STATION 847 AT BIN SUPPORT ANGLE INBOARD STRINGER 9RT. INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001078Frame · crackedCLT - FOUND FRAME WEB CRACKED .250 INCH, STATION 727E, STRINGER 9RT, FASTENER HOLE. REMOVED DAMAGE AND INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001077Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 480, BETWEEN STRINGER 8/9L. REMOVED DAMAGE AND INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001074Frame · crackedCLT - FOUND FRAME CHORD CRACKED 2 INCHES, FORWARD SIDE OF FUSELAGE FRAME 616, 60.5 INCH RBL 6 INCHES. INSTALLED FILLER AND STIFFENER PER TR 53-62-01. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, FrameSDR USAA001073Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT. INSTALLED REPAIR KIT PER BOEING DRAWING 65C2787. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001072Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, RIGHT ACCESS CUTOUT OUTBOARD EDGE PANEL 5828R. INSTALLED EXTERNAL DOUBLER PER TR 54-30-07. (M)Jul 31, 2000 · N353US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA001071Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, RIGHT PYLON ACCESS HOLE CUTOUT AT OUTBOARD EDGE. INSTALLED EXTERNAL DOUBLER PER TR 54-30-07. (M)Jul 31, 2000 · N353US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA001070Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .25 INCH, STATION 178 RBL .5 TO LBL .5, WL 188. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001069Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .75 INCH, BS 290, STRINGER 11 AND 12R. REPLACED INTERCOSTAL SRM 51-10-02. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001068Support Bracket · crackedCLT - FOUND SUPPORT ANGLE CRACKED 4 INCHES, STATION 294-298, RBL 54. INSTALLED NEW ANGLE PER SRM 51-10-02. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001067Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 294.5, STRINGER 7L. FABRICATED AND INSTALLED PART PER SRM 51-10-02. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Structure (General)SDR USAA001090Splice · crackedCLT - FOUND STRINGER SPLICE CRACKED .25 INCH, STRINGER 4R SPLICE STATION 907. REMOVED DAMAGE AND INSTALLED PER SRM 51-10-02. (M)Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001089Frame · crackedCLT - FOUND FRAME CRACKED .025 INCH, AFT SIDE FRAME 847 AT TWO RIVETS JUST ABOVE STRINGER 9L. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-00-07 FIG 201 AND TR 53-10-14A. (M)Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, FrameSDR USAA001088Skin · crackedCLT - FOUND SKIN CRACKED .375 INCH, FUSE SKIN AT LOWER AFT CORNER OF DOOR CUTOUT. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-10-01 FIG 202. (M)Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001087Door Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR JAMB FORWARD FRAME AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED PER SRM 51-40-02 AND BOEING DWG 65 45807. (M)Jul 31, 2000 · N354US · Boeing 737301 · Fuselage Main, StructureSDR USAA001086Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, HORIZ STAB CENTER BOX LOWER CHORD TO WEB. INSTALLED NEW ANGE PER TR 51-10-02. (M)Jul 31, 2000 · N354US · Boeing 737301 · Horizontal Stabilizer StructureSDR USAA001084Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 908, STRINGER 7L. REMOVED AND INSTALLED NEW CLIP PER SRM 51-10-02. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001083Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 908, STRINGER 6L. REMOVED AND INSTALLED NEW CLIP PER SRM 51-10-02. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001082Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, STATION 908, STRINGER 6RT. DRILLED NEW TIE CLIP AND INSTALLED PER SRM 51-10-02. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001081Stringer · crackedCLT - FOUND STRINGER CRACKED .250 INCH, STATION 908, STRINGER 4R. REPLACED STRINGER SPLICE PER SRM 51-10-2. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001080Frame · crackedCLT - FOUND FRAME WEB CRACKED .25 INCH, STATION 887 FRAME WEB AT STRINGER 9LT. REMOVED DAMAGE AND INSTALLED DOUBLER PER TR 53-10-14. (M)Jul 31, 2000 · N353US · Boeing 737301 · Fuselage Main, Frame
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