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 USAA000468Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, STATION 380, LBL 3, FUSELAGE SKIN. INSTALLED DOUBLER PER TR 53-30-07. (M)Mar 27, 2000 · N350US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000469Frame · crackedCLT - FOUND CHORD CRACKED .5 INCH, BS 616, WL 202 RIGHT SIDE INNER FRAME CHORD AT LOWER FAST. REPAIRED DOUBLER PER TR 53-62-01. (M)Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR SWAA000576Bracket · looseDURING SCHEDULED BC2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR STOW BRACKETS LOOSE. SECURED BRACKETS PER MM.Mar 25, 2000 · N659SW · Boeing 737301 · Escape SlideSDR USAA000453Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .350 INCH, BS 291.5 BETWEEN STRINGER 10R AND 11R. REPAIRED PER SRM 51-40-02. (M)Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000454Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, BS 663 STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000455Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .500 INCH, BS 887, STRINGER 1. REPAIRED PER SRM 51-40-02 AND 51-10-00. (M)Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000456Floorbeam · corrodedFOUND FLOORBEAM CORRODED 1.5 INCH BY 2 INCHES, BS 312, LBL 20, RBL 20. INSTALLED UPPER T-CAP PER SRM 53-10-51 FIG 205. (M)Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAASB00084Valve · failedCLT - FLT 1403 - EN ROUTE FROM TPA-LGA, THE ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT OUTBOARD MAIN LANDING GEAR ANTI-SKID VALVE HAD FAULTED. REMOVED AND REPLACED THE LEFTMar 24, 2000 · N338US · Boeing 737301 · Brake Anti-Skid SectionSDR USAA000444Frame · corrodedCLT - FOUND FRAME CORRODED 2 INCHES BY 4 INCHES, STATION 947, WL 208, RBL 53. CORROSION LEVEL 1. REPAIRED PER SRM 51-10-2. (M)Mar 23, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000445Keelbeam · corrodedCLT - FOUND KEEL BEAM CHORD CORRODED 18 INCHES, STATION 709-727. CORROSION LEVEL 1. REMOVED CORROSION AND REPAIRED PER SRM 53-60-12. (M)Mar 23, 2000 · N562AU · Boeing 737301 · Fuselage Main, KeelSDR USAA000446Skin · crackedCLT - FOUND SLAT EXTERNAL SKIN CRACKED 1 INCH, NR 3 SLAT LOWER SKIN TRAILING EDGE AT ACTUATOR ATTACH LOCATION. REPAIRED PER BOEING DWG 65C30133. (M)Mar 23, 2000 · N562AU · Boeing 737301 · Leading Edge DevicesSDR USAA000447Splice · crackedCLT - FOUND STRINGER SPLICE CRACKED .25 INCH, IN STRINGER SPLICE AT STRINGER 4L, JUST AFT OF FS 907. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-10-02. (M)Mar 23, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000448Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, TIE CLIP AFT SIDE STATION 663.75 STRINGER 10R. REPAIRED PER SRM 51-10-02 AND 51-40-02. (M)Mar 23, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000449Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727A, STRINGER 4L. REPAIRED PER SRM 51-10-02 AND 51-40-02. (M)Mar 23, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000450Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727A, STRINGER 5L. REPAIRED PER SRM 51-10-02 AND 51-40-02. (M)Mar 23, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00081Fire Loop · failedBOS - FLT 6509 - ON CLIMB-OUT FROM BOS, AT 5,000 FEET, CREW RECEIVED A FLASHING FAULT LIGHT AND A NR 2 ENGINE OVERHEAT LIGHT. CLIMBING THROUGH 8,000 FEET, LIGHT REMAINED ON STEADY. APPROXIMATELY TWO MINUTES AFTER CAPTAIN PLACED THE NR 2 ENGINE AT IDLE THRUSTMar 23, 2000 · N340US · Boeing 737301 · Fire DetectionSDR USAASB00080Shaft · failedPHL - FLT993 - UPON PREPARATION FOR LANDING FINAL AT PHL, THE FLAPS WOULD NOT EXTEND OR RETRACT PAST 10 DEGREES. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE MIDFLAP TORQUE SHAFT CLEARANCE DOOR FOR Mar 23, 2000 · N584US · Boeing 737301 · Trailing Edge Flap Control SystemSDR USAA000433Channel · corrodedCLT - FOUND CHANNEL 1 INCH BY 3 INCHES CORRODED, BETWEEN BS 727D AND 727E BL 0. INSTALLED DOUBLER PER EA 66802. (M)Mar 22, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000434Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2 INCHES BY 50 INCHES, RT SERVICE DOOR RBL 52, STATION 947-1006, WL 208. REPLACED Z-ANGLE PER SRM 51-10-02. (M)Mar 22, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000435Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STATION 663, STRINGER 10R CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)Mar 22, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000436Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, FS 616 STRINGER 4L. REPLACED CLIP PER SRM 51-10-02. (M)Mar 22, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000437Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 663, STRINGER 9L. REPLACED TIE CLIP PER SRM 51-10-02. (M)Mar 22, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000438Floorbeam · corrodedCLT - FOUND T-CAP BEAM CORRODED 2.25 INCH, STATION 986.5 TOP OF FLOORBEAM. REPLACED T-CAP AND INSTALLED DOUBLER PER TR 53-10-05 AND SRM 53-10-02. (M)Mar 22, 2000 · N350US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000396Web · crackedCLT - FOUND VERTICAL WEB CRACKED .25 INCH, STATION 312, RBL 14 FASTENER HOLE. INSTALLED DOUBLER PER SRM 53-10-51. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000389Fitting · crackedCLT - FOUND FITTING CRACKED .25 INCH, MLG BEAM OUTBOARD SUPPORT FITTING RIGHT SIDE. REPAIRED PER TR 57-40-13. (M)Mar 21, 2000 · N350US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAA00390Fitting · crackedCLT - FOUND FITTING CRACKED .25 INCH, MLG BEAM OUTBOARD SUPPORT FITTING LEFT WING. REPAIRED PER TR 57-40-13. (M)Mar 21, 2000 · N350US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAA000391Stringer · crackedCLT - FOUND SHELF CRACKED .50 INCH, S18A SHELF LT SIDE. INSTALLED NEW SHELF PER EA 66814. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA000392Stringer · crackedCLT - FOUND SHELF CRACKED .50 INCH, S18A SHELF RT SIDE. INSTALLED NEW SHELF PER EA 66814. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA000393Stiffener · crackedCLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, BS 178, LBL 7, WL 183. INSTALLED REPAIR ANGLES AND STRAPS PER SRM 53-10-08 FIG 205. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000394Intercostal · crackedCLT - FOUND INTERCOSTAL WEB .5 INCH CRACKED, STATION 294, BETWEEN STRINGER 11R AND 12R. REPAIRED PER SRM 51-10-2. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000395Intercostal · crackedCLT - FOUND INTERCOSTAL WEB CRACKED .5 INCH, STATION 294, BETWEEN STRINGER 12R AND 13R. REPLACED WEB PER SRM 51-10-02. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000397Web · crackedCLT - FOUND WEB CRACKED .5 INCH, FRT OF FLOORBEAM STATION 328, LBL 28, WL 208. REPAIRED PER SRM 51-10-2.(M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000398Web · crackedCLT - FOUND WEB CRACKED 1 INCH, BL 0 FROM BS 344 TO 360. INSTALLED NEW WEB. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000399Angle · crackedCLT - FOUND TOP WEB ANGLE CRACKED IN TWO PLACES .5 INCH AND .250 INCH, BETWEEN BS 380 AND 400 BL 0. INSTALLED NEW ANGLE PER SRM 51-70-3 AND 51-10-2. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000400Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 480, STRINGER 9R. INSTALLED FRAME REPAIR PER TR 53-10-14. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, FrameSDR USAA000401Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 480, STRINGER 9L. INSTALLED DOUBLER PER EA 66866. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, FrameSDR USAA000402Frame · crackedCLT - FOUND FRAMED CRACKED, BS 500L STRINGER 9R. INSTALLED DOUBLER PER EA 66866. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, FrameSDR USAA000403Angle · crackedCLT - FOUND ANGLE CRACKED 1.5 INCH, STATION 540 STRINGER 22R RAM AIR SUPPORT ANGLE. INSTALLED REPAIR ANGLE PER TR 53-50-03. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000404Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .5 INCH, STATION 685, LBL 48 FLOORBEAM. FABRICATED 2 REPAIR ANGLES AND INSTALLED PER EA 66828. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000415Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 1016, LBL 6. INSTALLED DOUBLER PER SRM 53-00-51 FIG 203. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000416Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2 INCHES BY 20 INCHES, SERVICE ENTRY DOOR Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)Mar 21, 2000 · N350US · Boeing 737301 · Service DoorsSDR USAA000417Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 24 INCHES, STATION 344, LBL 0 TO LBL 48. REMOVED AND REPLACED DOUBLER PER SRM 53-10-51. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000418Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY .25 INCH, STATION 328. SPLICED IN NEW T-CAP PER SRM 51-70-12 FIG 1. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000419Stiffener · corrodedCLT - FOUND STIFFENER CORRODED, STATION 1016 BULKHEAD STIFFENING ANGLE BL 0. CORROSION LEVEL 1. SPLICED IN NEW SECTION PER DRAWING 65C28106. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000420Pressure Panel · corrodedCLT - FOUND PRESSURE WEB SKIN CORRODED, BS 1016 BULKHEAD AND PRESSURE WEB BL 0. REMOVED AND DOUBLER INSTALLED PER EA 66860. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000421Keelbeam · corrodedCLT - FOUND KEELBEAM CORRODED 1 INCH BY 3 INCHES, LBL 6.5 KEELBEAM VERTICAL FLANGE INBOARD STATION 540. REPAIRED PER SRM 53-60-12 AND BOEING DRAWING 6562125. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, KeelSDR USAA000422Stringer Clip · crackedCLT - FOUND CLIP CRACKED .625 INCH, STRINGER CLIP AT STRINGER 3R AND FS 1006. REPAIRED PER SRM 51-10-2. (M)Mar 21, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000427Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 42 INCHES, STATION 947 TO 1006, LBL 52 LT AFT ENTRY DOOR SILL. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)Mar 21, 2000 · N250US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000428Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 20 INCHES, STATION 947 TO 1006, LBL 52. REMOVED AND REPLACED Z-ANGLE PER SRM 51-10-02. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000429Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY .5 INCH, FLOORBEAM 270 JUST AFT OF GEAR VIEW FINDER. INSTALLED NEW Z-ANGLE PER TR 53-20-08. (M)Mar 21, 2000 · N350US · Boeing 737301 · Fuselage Main, Floor Beam
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