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 USAA990757Bulkhead Web · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5 WL 200 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990756Bkhd Intercostal · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 25, WL 195 INTERCOSTAL. REPAIRED PER TR 53-10-18. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990755Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 787 BETWEEN STR 8 AND STR 9R. INSTALLED DOUBLER PER EA 65040. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, FrameSDR USAA990754Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5, WL 204 WEB. FABRICATED DOUBLER AND FILLERS PER SRM 53-10-07 AND 08. (M)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990753Bulkhead Angle · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5.5, WL 188 T-ANGLE. FABRICATED 2 ANGLES AND 1 STRAP PER SRM 53-1-08 FIG 205, SHEET 12. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990752Bulkhead Angle · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5.7, WL 181 T-ANGLE. FABRICATED 2 ANGLES AND 1 STRAP PER SRM 53-10-08 FIG 205 SHEET 12. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990751Skin · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .75 INCH CRACK AND 5 INCH CRACK IN SKIN AROUND PANEL 5724L. INSTALLED DOUBLER PER TR 54-40-040. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990711Clip · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT STRINGER TIE CLIP STA 616 STR 2R. INSTALLED DOUBLER PER SRM 53-00-03. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990709Angle · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA VARIOUS SIZES AND PLACES ON Z-ANGLE/GIRT BAR MOUNTS FORWARD ENTRY DOOR AT BS 312 TO BS 344. INSTALLED NEW Z-ANGLE AND GIRT BAR MOUNTS PER SRM 51-40-02 AND SRM 53-10-15. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990708Tie Clip · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 616 STR 1 TIE CLIP. INSTALLED NEW CLIP PER SRM 51-10-02. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990707Skin · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK FORWARD SERVICE DOOR AFT LOWER CUT-OUT BS 324, WL 211 SKIN. INSTALLED DOUBLER AND FILLERS PER SRM 53-10-01. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990706Floorbeam · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK 1.5 INCHES AFT OF STA 663.75 AT BL ZERO BEAM (FRAME). INSTALLED FLOORBEAM REPAIR PER EA 64999 AND BOEING SB 737-57-1210 FIG 4 AND 8. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990679Frame · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 400 BETWEEN STR 8R AND STR 9R. INSTALLED DOUBLER PER SRM 53-00-07. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, FrameSDR USAA990678Web · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT LBL 25 WEB AT HOLES 707, 708, 709, 710, AND 713, WL 203. INSTALLED DOUBLER PER SRM 51-70-13. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990677Skin · crackedDLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK UPPER AFT CORNER OF CUT-OUT FOR ACCESS TO EXTERNAL DOOR HANDLE AFT CARGO DOOR EXTERIOR SKIN. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 52-00-3. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990676Frame · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 480 BETWEEN STR 8 AND STR 9L. CUT-OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, FrameSDR USAA990675Beam · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK LOWER WEB OF RBL 25 AT STA 712 WL 203 BEAM. INSTALLED DOUBLER PER SRM 51-70-13. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990674Web · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK SHEAR WEB LOWER CHORD STA 305.5 STR 4L. INSTALLED DOUBLER PER SRM 51-70-11.Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990661Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STR 8 AND STR 9L IN FUSELAGE FRAME AT FASTENER HOLE. INSTALLED DOUBLER. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, FrameSDR USAA990660Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STR 8 AND STR 9R IN FUSELAGE FRAME AT FASTENER HOLE. FABRICATED REPAIR ANGLE AND FILLER INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, FrameSDR USAA990659Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 807 BETWEEN STR 8 AND STR 9R IN FUSELAGE FRAME AT FASTENER HOLE. INSTALLED DOUBLER PER SRM 53-00-07. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Main, FrameSDR USAA990658Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 616 STR 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990657Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 1006 AT FIRST STRINGER ABOVE FLOOR LEVEL ON RT SIDE TIE CLIP. REPLACED WITH IDENTICAL PART. (X)Aug 3, 1999 · N341US · Boeing 737301 · Fuselage Miscellaneous StructureSDR SWAA991266Light · burnedAIR TURNBACK, 10 MINS AFTER TAKEOFF F/A REPORTED AN ELECTRICAL ODOR AT MID CABIN. FOUND SIDEWALL LIGHT AT ROW 7 ABC AND 8 ABC BURNED INTERNALLY. REMOVED AND REPLACED LIGHT ASSY PER MM.Aug 1, 1999 · N659SW · Boeing 737301 · Passenger Compartment LightingSDR F3LA99107Support · corrodedDEN - DURING C-CHECK, INSPECTION REPORTED LEFT MAIN LANDING GEAR FORWARD UPLOCK SUPPORT SHAFT LUG CORRODED, STA 685. MAINTENANCE REPLACED NR 1 MAIN LANDING GEAR PER MM 32-11-00. TC: 15,691. (X)Jul 31, 1999 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990791Stringer · crackedCLT - DURING Q3 CHECK, FOUND .75 INCH CRACK AT BS 727 STRINGER 18A WEB S18AL. REPAIRED WITH REPLACEMENT REF SB 737-53-1170. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990790Frame · crackedCLT - DURING Q3 CHECK, FOUND VARIOUS 1 INCH AREAS OF CORROSION AT NUTPLATE HOLES IN FRAME/WEB AT BS 605 TO 845 STRINGER 25R TOP FLANGE. REPLACED WITH IDENTICAL PART NUMBER. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990789Intercostal · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT STATION 178, 195 INTERCOSTAL RT SIDE. REPLACED WITH IDENTICAL PART NUMBER. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990788Post · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CAPTAINS UPPER O/B CORNER OF EXTERIOR WINDSHIELD (POST). INSTALLED EXTERNAL DOUBLER PER EA 64979. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990787Skin · crackedCLT - DURING Q3 CHECK, FOUND 3 CRACKS ONE 1.375 INCH, TWO .5 INCH ON SKIN AT NR 1 L/E SLAT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 57-50-01 REV 'H'. (M)Jul 29, 1999 · N338US · Boeing 737301 · Leading Edge DevicesSDR USAA990786Clip · crackedCLT - DURING Q3 CHECK, FOUND .25 INCH CRACK AT TIE CLIP AT STATION 663 S10L. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990785Skin · crackedCLT - DURING Q-3 CHECK, FOUND .5 INCH CRACK E/E COOLING DUCT OUTLET INNER FUSELAGE FUSELAGE SKIN AT BS 380 BL 0. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER 23 INCH BY 40 INCH PER TR 53-30-07 AND BOEING DWG NR 65C33930. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990784Angle · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CREASE BEAM INNER CHORD ANGLE BS 294.5 RBL 45 WL 208. INSTALLED CHORD ANGLE PER SRM 51-10-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990783Splice · crackedCLT - DURING Q3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4LT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990782Splice · crackedCLT - DURING Q-3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4RT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990781Frame · crackedCLT - DURING Q3 CHECK, FOUND .125 INCH CRACK IN FRAME AT STATION 616 RBL 64 WL 201 INBOARD CHORD ANGLE. INSTALLED REPAIR FILLER AND STIFFENING ANGLE PER EA 65007 TR 53-10-23 (737-200). (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990780Frame · crackedCLT - DUIRNG Q-3 CHECK, FOUND .25 INCH CRACK IN FRAME AT BS 480 S9R. INSTALLED DOUBLER PER EA 65009. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990779Tie Clip · crackedCLT - DURING Q3 CHECK, FOUND TIE CLIP CRACKED IN HALF. ALSO, FOUND STRINGER CRACKED BELOW CLIP LOCATION, STATION 616, S-4L. INSTALLED STRINGER DOUBLER PER SRM 53-00-03 FIG 204 AND FABRICATED TIE CLIP AND INSTALLED PER SRM 51-10-1. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990772Stringer · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH AREA OF CORROSION AT STATION 727A PLUS 14 INCHES, STRINGER 26L. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. INSTALLED FABRICATED STRINGER REPAIR CHANNEL ANDRADIUS FILLERS PER SRM 53-00-03 FIG 201. (Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990771Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 6 SQUARE INCH OF CORROSION MED Z-ANGLE UPPER SURFACE. CORROSION LEVEL 2. REPLACED Z-ANGLE PER SRM 51-10-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990770Stabilizer Link · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION RIGHT GEAR STABILIZER LINK ATTACH POINTS. CORROSION LEVEL 2. REMOVED AND REPLACED STABILIZER LINK PER MM 32-32-93 AND 32-13-21. (M)Jul 29, 1999 · N338US · Boeing 737301 · Main Landing GearSDR USAA990769Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 957 AND 987, LBL 45, WL 208 CREASEBEAM INNER CHORD ANGLE. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. INSTALLED NEW CHORD ANGLE PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990768Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 6L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990729Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK FRAME 312 AT STR 5L. CRACK TRIMMED OUT AND DOUBLER INSTALLED PER SRM 53-00-07 FIG 202 AND EA 65075. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990728Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .500 INCH CRACK MAIN ENTRY DOORWAY UPPER HINGE H-STRAP DOORWAY FRAME. FABRICATED AND INSTALLED NEW H-STRAP PER SRM 51-10-02 AND BOEING DWG 90-7822. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990727Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANGLE. REPAIRED PER BOEING DWG NR 69-48985/51-10-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990726Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT ENTRY DOOR CUT-OUT FRAME UPPER FORWARD SECTION AT BOTTOM HOLE FORWARD EDGE FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990725Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STA 639 STR 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990724Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 639 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990723Tie Clip · crackedCLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 616 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous Structure
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