Boeing 737-201

Service difficulty reports · 2,471

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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 = '737201'
  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 USAA000012Tie Clip · crackedFOUND TIE CLIP CRACKED AT BS 559, STRINGER 8R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000011Tie Clip · crackedFOUND TIE CLIP CRACKED AT BS 847 STRINGER 10R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000010Tie Clip · crackedFOUND TIE CLIP CRACKED AT BS 663 STRINGER 10R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000009Tie Clip · crackedTIE CLIP HAS 2 CRACKS AT BS 663 STRINGER 10L.. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000008Tie Clip · crackedTIE CLIP CRACKED AT BS 827 STRINGER 4R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000007Tie Clip · crackedTIE CLIP CRACK AT BS 767 STRINGER 10R. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000006Tie Clip · crackedFOUND TIE CLIP CRACKED AT BS 639. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Main, StructureSDR USAA000005Tie Clip · crackedTIE CLIP CRACKED AT BS 907, STRINGER 2L. INSTALLED NEW TIE CLIP PER EO 5393G227. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000004Web · crackedWEB CRACKED AT BS 616 STRINGER 17L. INSTALLED NEW CREASE BEAM WEB PER SRM 51-10-1. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA000003Frame · crackedFRAME CRACKED AT BS 290 STRINGER 12R AND 13R.. INSTALLED NEW CHORD ANGLE PER SRM 51-10-1. (M)Jan 11, 2000 · N243US · Boeing 737201 · Fuselage Main, FrameSDR USAASB00009Engine · failedTPA - FLT 2746 - ON CLIMB-OUT FROM TPA, AT FL150, CREW REPORTED THE NR 1 ENGINE OIL PRESSURE WENT TO RED LINE WITH ENGINE TEMPERATURE FOLLOWING SHORTLY THEREAFTER. CREW SHUTDOWN THE NR 1 ENGINE, ADVISED AIR TRAFFIC CONTROL OF THE PROBLEM AND DECLARED AND EMERJan 10, 2000 · N249US · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA991500Skin · crackedCLT - DURING Q-1 CHECK EDDY CURRENT AND VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 330, STRINGER 17R LOWER FORWARD CORNER OF FORWARD SERVICE DOOR. INSTALLED DOUBLER, TRIPLER AND QUADRUPLER PER SRM 53-30-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA991493Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH AREA OF CORROSION AT BS 328, RBL 19 FLOORBEAM. CORROSION LEVEL 1. INSTALLED T-CAP PER SRM 53-10-9. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991492Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 178 BULKHEAD AFT SIDE LBL 5 VERTICAL ANGLE. INSTALLED REPAIR ANGLE PER SRM 53-10-11. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991491Web · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK BS 360, STRINGER 16L WEB. INSTALLED DOUBLER PER EA 66284. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991490Doubler · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 1138, STRINGER 5R HORIZONTAL STAB CUTOUT DOUBLER.. INSTALLED FILLER AND DOUBLER PER EA 66420 AND SRM 53-00-01 FIG 201. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA991489Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 597 JUST BELOW STRINGER 17R FRAME. INSTALLED DOUBLER PER SRM 53-10-2 FIG 5 AND EA 66417. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, FrameSDR USAA991488Web · crackedCLT - DURNG Q-1 CHECK VISUAL INSPECTION, FOUND 5 CRACKS .25 INCH STATION 706-717, RBL 24, WL 202 WEB. INSTALLED FILLER AND DOUBLER PER SRM 51-40-2 FIG 1. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991487Floorbeam · crackedCLT - DURNG Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 663, BL 0 FLOORBEAM. INSTALLED DOUBLER PER TR 57-10-04. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991486Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .625 INCH CRACK UPPER CHORD BULKHEAD STATION 663, RBL 24, WL 202 ANGLE. INSTALLED REPAIR ANGLE PER TR 57-10-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991485Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 17 INCHES TOP OF FLOORBEAM STATION 986, RBL 7-11, CORROSION LEVEL 1. REPLACED T-CAP PER SRM 5. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991484Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION STATION 1006, LBL 29 FLOORBEAM, CORROSION LEVEL 1. REPLACED T-CAP PER SRM 53-10-09 FIG 7. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991483Mount · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION STATION 777, BL 0 VHF ANTENNA MOUNT. CORRSION LEVEL 1. REPLACED PART PER 51-10-01 AND 51-30-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · VHF Communications SystemSDR USAA991482Stringer · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION BS 993, STRINGER 20R, CORROSION LEVEL 1. SPLICED IN NEW SECTION PER SRM 53-10-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA991481Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION STATION 344, LBL 65 FORWARD ENTRY DOOR Z-ANGLE. CORROSON LEVEL 2. REPLACED Z-ANGLE PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991474Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 34 INCH AREA OF CORROSION STATION 294.5, LBL 13 TO RBL 21 FLOORBEAM, CORROSION LEVEL 2. REPAIRED PER TR 53-10-04B. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991473Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 16 INCH AREA OF CORROSION STATION 259, RBL 9 - LBL 8 SUPPORT ANGLE/FLOOR. CORROSION LEVEL 1. REPLACED CHORD ANGLES, FLOOR PANEL, FILLERS, SPLICE AND VERTICAL ANGLES PER TR 53-10-16. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991472Fitting · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 727, BL 0, WL 206 FITTING. INSTALLED REPLACEMENT FITTING AND MOD PER EO 5394G176. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991471Bracket · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 322.5, LBL 65 BRACKET. FABRICATED BRACKET PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991470Bracket · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK UNDER FORWARD ENTRY DOOR STATION 322 BRACKET. FABRICATED BRACKET PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991469Frame · crackedCLT - DURNG Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 663, WL 202, LBL 24 UPPER CHORD. INSTALLED DOUBLER PER TR 57-10-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, FrameSDR USAA991464Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 794.3, STRINGER 26R FLOOR SUPPORT BEAM, CORROSION LEVEL 2. INSTALLED NEW FLOOR SUPPORT SECTION PER SRM 53-10-05. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA991463Shear Beam · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK INBOARD AFT EDGE 18A SHEAR BEAM LEFT SIDE. INSTALLED NEW PARTS PE REPAIR DOCUMENT 51-10-1. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991455Shear Tie · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 616 STRINGER 4R SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991454Bracket · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK STATION 360 LEFT BRACKET. REMOVED AND REPLACED PER SRM 51-10-1. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991453Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 CRACKS APPROX 1.5 INCH LONG AT BS 960 AFT SERVICE DOOR CUTOUT LOWER FORWARD CORNER SKIN. INSTALLED FILLER, DOUBLER AND TRIPLER PER SRM 53-30-03. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA991407Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 887, STRINGER 6L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991406Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 344, STRINGER 11R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991405Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B, STRINGER 6 TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991404Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 787, STRINGER 7R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991403Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 847, STRINGER 10L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991402Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867, STRINGER 4L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991401Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 400, STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991400Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 907, STRINGER 16R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991399Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 907, STRINGER 16L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991398Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 767, STRINGER 4R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991397Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 767, STRINGER 9L TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991396Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 767, STRINGER 47R, TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-01. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991395Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A . 5 INCH CRACK STATION 500B, STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA991394Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500A, STRINGER 10 TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Jan 10, 2000 · N263AU · Boeing 737201 · Fuselage Miscellaneous Structure
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