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 USAA010138Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 328, LBL 54. CORROSION LEVEL 1. INSTALLED UPPER SECTION PER TR 53-10-13 AND SRM 51-10-6. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010137Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .125 INCH, TWO PLACES, BS 1016 AT APPROX STRINGER 3L. INSTALLED DOUBLER PER EA 69021. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010151Skin · crackedCLT - FOUND SKIN CRACKED 1.60 INCH, RIGHT AFT SERVICE DOOR BEAR STRAP. INSTALLED TRIPLER PER SRM 53-30-3. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Service DoorsSDR USAA010150Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 767, STRINGER 13L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 1. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Main, FrameSDR USAA010149Web · crackedCLT - FOUND WEB CRACKED .25 INCH, STATION 767 WEB CRACKED STRINGER 13R. INSTALLED RADIUS BLOCK PER EA 69053. (M)Feb 12, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010148Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 807, STRINGER 11L. REPLACED TIE CLIP PER SRM 51-10-01 AND DWG 69-45156. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010147Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 807, STRINGER 10L. INSTALLED NEW CLIP PER SRM 51-10-1. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010146Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 747, STRINGER 7R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010145Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED, STATION 747, STRINGER 4R. INSTALLED NEW CLIP PER SRM 51-10-1. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010144Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, FUSELAGE SKIN STATION 727A PLUS 8 JUST ABOVE STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-03. (M)Feb 12, 2001 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010201Skin · crackedBOS - FOUND SKIN CRACKED .75 INCH, BETWEEN STATION 787/807 STRINGER 19L. INSTALLED DOUBLER INCORPORATED PREVIOUS PATCH PER SRM 53-30-3 FIG 1. (M)Feb 9, 2001 · N261AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010131Skin · crackedCLT - FOUND OVERNIGHT FUSELAGE SKIN CRACKED 5 INCHES, LOWER FORWARD CORNER OF AFT ENTRY DOOR CUTOUT. INSTALLED REPAIR PLATES PER SRM 53-30-3 FIG 24. (M)Feb 6, 2001 · N247US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010125Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .125 INCH, BS 1016, STRINGER 6L. INSTALLED DOUBLER AND TRIPLER PER SRM 53-10-4 FIG 15. (M)Feb 6, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA01024Angle · crackedCLT - FOUND UPPER CHORD ANGLE CRACKED .5 INCH, STATION 663, RBL 24, WL 201.5. INSTALLED REPAIR ANGLES PER EA 68973. (M)Feb 6, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010123Frame · crackedCLT - FOUND CHORD FRAME CRACKED .75 INCH, STATION 639, WL 210. REMOVED AND REPLACED PER REPAIR DOCUMENT 51-30-2. (M)Feb 6, 2001 · N251AU · Boeing 737201 · Fuselage Main, FrameSDR USAA010112AWeb · crackedCLT - FOUND WEB CRACKED .25 INCH, STATION 334 STRINGER 8R AT FORWARD SERVICE DOOR. REPLACED SHEAR WEB PER DRAWING 65C33288. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010122Shear Tie · crackedCLT - FOUND SHEAR TIE CRACKED .75 INCH, FS 1040 BETWEEN STRINGER 2/3 RT. INSTALLED SHEAR TIE PER DWG 65-46569. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, StructureSDR USAA010121Shear Tie · crackedCLT - FOUND SHEAR TIE CRACKED 1 INCH, STATION 1040 STRINGER 2L AND 3L. INSTALLED REPAIR PER DWG 65 46569. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, StructureSDR USAA010120Skin · crackedCLT - FOUND SKIN CRACKED 2.5 INCH, STATION 727B PLUS 2 AND 727A PLUS 8 STRINGER 18L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010119Floorbeam · crackedCLT - FOUND FLOORBEAM WEB CRACKED 1 INCH, STATION 727, RBL 24.5. FABRICATED REPAIR AND INSTALLED PER EA 68992A. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010118Floorbeam · crackedCLT - FOUND FLOORBEAM WEB CRACKED 1 INCH, STATION 706, LBL 24.5. FABRICATED REPAIR AND INSTALLED PER EA 69008 AND 69031. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010117Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, STATION 695 LBL 45.5. INSTALLED DOUBLER PER SRM 51-40-4. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010116Floor Support · crackedCLT - FOUND FLOOR SUPPORT CRACKED 1 INCH, STATION 540. REPLACED FLOOR SUPPORT PER SRM 51-10-01. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010115Web · crackedCLT - FOUND WEB CRACKED 6 INCHES, STATION 520, RBL 24.5. REPAIRED PER SRM 51-10-10. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010114Doubler · crackedCLT - FOUND PRODUCTION DOUBLER CRACKED 1 INCH, 4 PLACES, BL 0, STATION 370 TO 380. INSTALLED DOUBLER PER EA 69056. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010113Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178 BULKHEAD, WL 224, RBL 2. INSTALLED TRIPLER PER EA 68961 AND EO 5300V153. (M)Feb 5, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010262Bulkhead · crackedCLT - FOUND PRESSURE BULKHEAD CRACKED 6.5 INCHES, BS 1016 PLUS 1 AT STRINGER 6L. INSTALLED FILLER, DOUBLER AND SHIMS. (M)Feb 4, 2001 · N249US · Boeing 737201 · Fuselage Main, BulkheadSDR USAASB01037Apu · malfunctionedBWI- FLT 2993 - EN ROUTE FROM BOS TO FLL, AT FL350, THE APU SHUTDOWN. THE NR 2 CSD/GENERATOR WAS ALREADY ON MEL SO THE CREW DECLARED AN EMERGENCY AND BEGAN TO DIVERT TO BWI. AT FL240, THE APU WAS RESTARTED AND THE EMERGENCY WAS CANCELED. FLIGHT CONTINUED TO Feb 4, 2001 · N259AU · Boeing 737201 · Airborne Auxiliary Power Unit (APU) SystemSDR USAA010248Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 2 SQUARE INCHES, BS 987.9, LBL 20 TO STATION 1016, LBL 6. FABRICATED NEW INTERCOSTAL PER 51-30-0 AND 51-10-1. CORROSION LEVEL1, TASK NR C53-107-02. (M)Feb 3, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB01034Pressure Switch · malfunctionedCLT - FLT 2826 - EN ROUTE FROM MCO TO BOS, THE NR 2 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED ALONG WITH HIGH OIL TEMPERATURE INDICATION ON THE CSD TEMPERATURE GAUGE. CREW DISCONNECTED THE NR 2 ENGINE CSD AND STARTED THE APU. CREW THEN RECEIVED AN APFeb 3, 2001 · N259AU · Boeing 737201 · APU Oil SystemSDR USAASB01032Compressor · stalledCLT - FLT 2676 - EN ROUTE FROM TPA TO LGA, AT FL330, CAPTAIN REPORTED THAT THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. NO ENGINE PARAMETERS WERE EXCEEDED. THROTTLE WAS REDUCED AND THE ENGINE RAN NORMALLY AFTER THE INITIAL STALL. FLIGHT DIVERTED TO CLT AFeb 1, 2001 · N254AU · Boeing 737201 · Engine (Turbine/Turboprop)SDR USAA010099Web · crackedCLT - FOUND WEB CRACKED 3 INCHES, STATION 663.7, BL 0. INSTALLED DOUBLER PER TR 57-10-04. (M)Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010098Floorbeam · crackedCLT - FOUND T-CAP CRACKED 4 INCHES, STATION 663, BL 0. INSTALLED REPAIR ANGLES PER TR 57-10-04 AND EA 69046. (M)Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010097Clip · crackedCLT - FOUND CLIP CRACKED .75 INCH, INTERCOSTAL FUSELAGE FRAME ATTACHED CLIP. INSTALLED DOUBLER PER SRM 51-40-3. (M)Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010096Stiffener · crackedCLT - FOUND STIFFENER CRACKED 2 INCHES, STRINGER 10L 294. INSTALLED STIFFENER PER EA 68991. (M)Jan 30, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010095Skin · crackedCLT - FOUND SKIN CRACKED 14 INCHES BY 8 INCHES, STRINGER 17R TO 19R, STATION 727A. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA010094Skin · crackedCLT - FOUND SKIN CRACKED 2.5 INCHES, LEFT AFT ENTRY DOOR OUTER SKIN STRINGER 17L PLUS 960. INSTALLED DOUBLER PER SRM 53-30-3. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Passenger/Crew DoorsSDR USAA010093Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 747 FRAME PLUS STRINGER 13L. INSTALLED DOUBLER PER SRM 53-10-4. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, FrameSDR USAA010092Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .75 INCH, STATION 663, LBL 23, WL 201.5. INSTALLED DOUBLER PER EA 68798. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010091Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH, STATION 663, LBL 0.0. INSTALLED DOUBLER AND ANGLES PER SRM 53-10-9. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA010090Beam · crackedCLT - FOUND BEAM CRACKED 1.8 INCH, STATION 520, RBL 45.5. REPAIRED DOUBLER PER SB 737-53-1120. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, StructureSDR USAA010089Beam · crackedCLT - FOUND BEAM CRACKED 1.3 INCH, STATION 520-540, LBL 45.5. REPAIRED DOUBLER PER SB 737-53-1120. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, StructureSDR USAA010088Beam · crackedCLT - FOUND BEAM CRACKED 1.5 INCH, STATION 520, LBL 24. REPAIRED DOUBLER PER SB 737-53-1120. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, StructureSDR USAA010087Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED 1 INCH, BS 520, STRINGER 19R. INSTALLED REPAIR PER SRM 51-40-3. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010086Structure · crackedCLT - FOUND INNER CHORD CRACKED 3 INCHES, STATION 294, WL 208. REPLACED CHORD PER SRM 51-10-01. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA010085Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .5 INCH, WL 234, RBL 10. INSTALLED DOUBLER PER SRM 53-10-08. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010084Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD WL 218, RBL 13. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010083Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178, BULKHEAD, WL 218, LBL 12.5. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010082Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250, STATION 178, BULKHEAD WL 218, RBL 10.0. INSTALLED DOUBLER PER EO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA010081Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .250 INCH, STATION 178 BULKHEAD WL 210.5, RBL 6.75. INSTALLED DOUBLER PEREO 5300V153. (M)Jan 29, 2001 · N251AU · Boeing 737201 · Fuselage Main, Bulkhead
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