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 USAA001810Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 706, STRINGER 11L. REMOVED AND REPLCED TIE CLIP PER SRM 51-10-02. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001809Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, LOWER INBOARD CORNER STATION 294 AT STRINGER 11R. INSTALLED REPAIR DOUBLER PER SRM 51-70-11 FIG 1. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001808Angle · crackedCLT - FOUND SHELF ANGLE CRACKED .5 INCH, AT STATION 291 BELOW STRINGER 11R. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-10-02. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001807Angle · crackedCLT - FOUND .5 INCH CRACK ON SHELF ANGLE AT STATION 272, STRINGER 14R L/B CORNER. REPLACED WITH NEW SHELF PER SRM 51-40-00. (M)Oct 25, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001799Shear Tie · corrodedCLT - FOUND SHEAR TIE CORRODED 6 INCHES, STATION 727E BETWEEN RBBL 8.10 TO RBBL 3.0. REPAIRED DOUBLER PER SRM 53-00-07. (M)Oct 23, 2000 · N356US · Boeing 737301 · Fuselage Main, StructureSDR USAA001800Stringer · corrodedCLT - FOUND STRINGER CORRODED .375 INCH BY .375 INCH, STATION 837 STRINGER 21. CORROSION LEVEL 1. INSTALLED REPAIR ANGLE PER SRM 53-00-03 FIG 201. (M)Oct 23, 2000 · N356US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001801Stringer · corrodedCLT - FOUND STRINGER CORRODED .125 INCH BY .125 INCH, STATION 757, STRINGER 21. CORROSION LEVEL 1. INSTALLED REPAIR ANGLE PER SRM 53-00-03 FIG 201. (M)Oct 23, 2000 · N356US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001802Web · crackedCLT - FOUND WEB CRACKED .500 INCH, LOWER CHORD WEB LOWER AFT DOOR STOP FITTING. INSTALLED REPAIR ANGLE AND FILLER PER EA 68206. (M)Oct 23, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR SWAA002120Skin · crackedDURING SCHEDULED A1 CHECK, FOUND 3.5 FUSELAGE SKIN CRACK AT BS 750, STR 23R. REPAIRED SKIN PER SRM.Oct 23, 2000 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001780Channel · crackedCLT - FOUND VERTICAL CHANNEL CRACKED .5 INCH, 178 BULKHEAD, WL 190, LBL 5.5. INSTALLED REPAIR ANGLES AND STRAPS PER SRM 53-10-08. (M)Oct 19, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001781Bulkhead · crackedCLT - FOUND BULKHEAD WITH CRACKS 3.5 INCHES, STATION 178 BETWEEN WL 201 AND 213, RBL 7 TO LBL 5.7. INSTALLED REPAIR DOUBLER PER SRM 53-10-08, EA 68284 EO 5300V153. (M)Oct 19, 2000 · N356US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001782Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, WL 207, LBL 27 STATION 178. FABRICATED NEW WEB AND INSTALLED PER SRM 51-10-2. (M)Oct 19, 2000 · N356US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001783Floor Support · crackedCLT - FOUND FLOOR STRUCTURE 1 INCH, WL 207, RBL 27, STATION 178 BULKHEAD. FABRICATED NEW WEB INSTALLED PER SRM 51-10-02. (M)Oct 19, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001784Frame · crackedCLT - FOUND CHORD ANGLE CRACKED 1 INCH, RIGHT SIDE WL 207, RBL 29. INSTALLED REPAIR ANGLE PER SRM 51-40-00 AND 53-10-08 AND EA 68225. (M)Oct 19, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001773Floorbeam · corrodedCLT - FOUND FLOORBEAM CRACKED 1 INCH BY 10 INCHES, STATION 312 BETWEEN LBL 30 AND RBL 12. CORROSION LEVEL 1. INSTALLED UPPER CHORD REPAIRED T-CAP PER SRM 53-10-51. (M)Oct 18, 2000 · N356US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001763Fitting · crackedCLT - Q-4, FITTING CRACKED .75 INCH AT RIGHT MLG SUPPORT BEAM OUTBOARD FITTING UPPER INBOARD BOLT HOLE. REPAIRED PER TR 57-40-13. (X)Oct 16, 2000 · N356US · Boeing 737301 · Fuselage, Landing Gear Attach FittingsSDR USAA001762Gusset · crackedCLT - GUSSET CRACKED 1 INCH AT BS 259, BBL ZERO TOP OF N/G WELL. INSTALLED NEW GUSSET PER DWG 65 45819. (X)Oct 16, 2000 · N338US · Boeing 737301 · Fuselage Main, StructureSDR USAA001761Frame · crackedCLT - CHORD CRACKED 1.5 INCHES AT BS 178, WL 207, LBL 26. FABRICATED NEW WEB PER SRM 51-10-02. (X)Oct 16, 2000 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA001760Skin · crackedCLT - FUSELAGE SKIN CRACKED 1.5 INCHES AT AFT END EQUIPMENT COOLING VENT HOLE STA 380, STR 28L. INSTALLED DOUBLER PER EA 68269A. (X)Oct 16, 2000 · N335US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001730Floorbeam · corrodedCLT - Q-4, FLOORBEAM CORRODED, .25 INCH, CORROSION LEVEL 1, STA 328, BL ZERO. INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-10-51 FIG 206. (X)Oct 12, 2000 · N356US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001712Intercostal · crackedCLT - Q-4, INTERCOSTAL CRACKED, 2 INCHES, BS 179, WL 195, RBL 24. REPLACED INTERCOSTAL PER SRM 51-10-02. (X)Oct 10, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001711Intercostal · crackedCLT - Q-4, INTERCOSTAL CRACKED, 2 INCHES, BS 179, WL 195, LBL 24. REPLACED INTERCOSTAL PER 51-10-02. (X)Oct 10, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR UAAA001709Bulkhead · crackedCLT - WEB CRACKED, .50 INCH, BS 178, WL 207, LBL 26. FABRICATED AND INSTALLED NEW WEB PER SRM 51-10-02. (X)Oct 10, 2000 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001708Intercostal · crackedCLT - DROP IN INTERCOSTAL CRACKED, 2 INCHES, BS 178, WL 195, LBL 24. REPAIRED PER SRM 53-10-08 FIG 207. (X)Oct 10, 2000 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00291Battery · faultyPIT - FLT 2149 - EN ROUTE FROM PHL/STL, AN UNIDENTIFIED ELECTRICAL ODOR WAS NOTED IN THE CABIN. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE BATTERY CHARGER CIRCUIT BREAKER TRIPPED. REMOVED ANOct 10, 2000 · N588US · Boeing 737301 · Battery/Charger SystemSDR USAA001701Crease Beam · crackedCLT - Q-4, BEAM WEB CRACKED 1.5 INCHES AT LEFT CREASE BEAM STA 616. REPLACED WEB PER SRM 51-10-02. (X)Oct 9, 2000 · N356US · Boeing 737301 · Fuselage Main, StructureSDR USAA001700Stringer · crackedCLT - Q-4, STR 18A SHELF CRACKED .25 INCH. INSTALLED NEW 18A SHELF AND SHIMS PER SRM 51-10-02. (X)Oct 9, 2000 · N356US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001699Frame · crackedCLT - Q-4, INNER CHORD ANGLE CRACKED .50 INCH AT STA 616 LT BELOW FLOOR LEVEL STR 17. INSTALLED FABRICATED DOUBLER AND FILLER PER TR 53-62-01. (X)Oct 9, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001702Crease Beam · corrodedCLT - Q-4, CREASE BEAM WEB CORRODED, 50 INCH, CORROSION LEVEL 1, LEFT CREASE BEAM STA 621. REPLACED WEB PER SRM 51-10-02. (X)Oct 9, 2000 · N356US · Boeing 737301 · Fuselage Main, StructureSDR USAASB00289Duct · leakingTPA - FLT 1515 - EN ROUTE FROM CLT TO CUN, THE LT WING-TO-BODY OVERHEAT LIGHT ILLUMINATED AND REMAINED ON FOR TWENTY MINUTES AFTER QUICK REFERENCE HANDBOOK PROCEDURES ACCOMPLISHED. FLIGHT DIVERTED TO TPA, LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLAREOct 6, 2000 · N342US · Boeing 737301 · Pneumatic Distribution SystemSDR AWXA0000721O-Ring · leakingSYSTEM A HYD LEAK, DIVERTED TO ICT. REPLACED O RING IN THRUST REVERSER SHUTTLE VALVE, SERVICED HYD SYSTEM, AND RAN A SYSTEM HYDRAULICS, NO LEAKS.Oct 6, 2000 · N326AW · Boeing 737301 · Engine Thrust ReverserSDR USAA001688Frame · crackedCLT - Q-4, BELT FRAME CRACKED .125 INCH AT BS 887, STR 9R. INSTALLED REPAIR CHANNEL PER EA 68156 AND TR 53-10-14. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001687Frame · crackedCLT - Q-4, BELT FRAME CRACKED .125 INCH AT BS 867, STR 9R. INSTALLED REPAIR CHANNEL PER EA 68156 AND TR 53-10-14. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001686Frame · crackedCLT - Q-4, BELT FRAME CRACKED .125 INCH, BS 867, STR 9L. INSTALLED REPAIR CHANNEL PER EA 68156 AND TR 53-10-14. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001685Frame · crackedCLT - Q-4, BELT FRAME CRACKED .125 INCH AT BS 847, STR 9R. INSTALLED REPAIR CHANNEL PER EA 68156 AND TR 53-10-14. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001684Frame · crackedCLT - Q-4, BELT FRAME CRACKED .5 INCH AT BS 827, STR 9R. INSTALLED REPAIR CHANNEL PER EA 68156 AND TR 53-10-14. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001683Frame · crackedCLT - Q-4, BELT FRAME CRACKED .125 INCH AT BS 767, STR 9R. INSTALLED REPAIR CHANNEL PER EA 68156 AND TR 53-10-14. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Main, FrameSDR USAA001682Tie Clip · crackedCLT - Q-4, TIE CLIP CRACKED .250 INCH AT STA 616, STR 3R. REPLACED TIE CLIP PER SRM 51-40-00. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001681Tie Clip · crackedCLT - Q-4, TIE CLIP CRACKED .180 INCH AT STA 616, STR 1. REPLACED TIE CLIP PER SRM 51-40-00. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001680Crease Beam · crackedCLT - Q-4, CREASE BEAM WEB CRACKED 1 INCH AT STA 578 RT FLOOR LEVEL STR 17. REPLACED WITH WEB PER SRM 51-10-2. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Main, StructureSDR USAA001679Tie Clip · crackedCLT - Q-4, TIE CLIP CRACKED .250 INCH STA 578, STR 8L. REPLACED TIE CLIP PER SRM 51-10-02. (X)Oct 4, 2000 · N356US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001675Floorbeam · corrodedCLT - C-6, FLOORBEAM CORRODED, 34 INCHES, CORROSION LEVEL 1 C53-107-02, STA 344 BETWEEN STR 17L AND STR 17R. INSTALLED T-CAP AND SPLICE ANGLE PER SRM 53-10-51. (X)Oct 3, 2000 · N573US · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA0000710Intercostal · crackedC-CHECK, FWD CARGO PIT FS 440 - 460, RBL 18, CARGO DOOR HOLD OPEN LATCH INTERCOSTAL CRACKED AT FLOORBEAM ATTACH. REMOVED AND REPLACED NEW INTERCOSTAL IAW 737 SRM 51-40-02.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage, Door HingeSDR AWXA0000709Floorbeam · corrodedC-CHECK CORROSION, T CAP CORRODED OUT OF LIMITS AFTER REWORK AT FS 967, RBL 20-50. REPAIRED T-CAP IAW 737 SRM 53-00-51, FABBED AND INSTALLED REPAIR STRAPS IAW 737 SRM 53-00-51.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA0000708Structure · corrodedC-CHECK CORROSION LEVEL 1. BILGE SUB-FLOOR AT FS 727D, LBL 17-20, CORRODED. CUT-OUT DAMAGED SUB FLOOR, FAB''D REPAIR ANGLES, INSTALLED REPAIR PARTS AND NEW SECTION OF FLOOR IAW 737 SRM 53-00-53 FIG 202, TREATED AND TOP COATED IAW 737 SRM 51-20-01.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA0000707Frame · crackedC-CHECK, SIDE CHORD CRACKED AT FS 178, LBL 36, WL 195 AND WL 207. CUT OUT DAMAGED AREA IAW SIA 53-003-00, FABBED AND INSTALLED SPLICE PLATE IAW 737 SIA 53-003-00 AND SRM 51-40-02.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000706Floorbeam · corrodedC-CHECK CORROSION LEVEL 1. UPPER T CAP AT FS 1016, LBL 4, CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA IAW 737 SRM 53-01-51 FIG 202, FABBED REPAIR PARTS IAW 737 SRM 53-10-51 FIG 202, AND INSTALLED REPAIR IAW 737 SRM 51-40-02.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA0000705Pressure Panel · crackedC-CHECK, CABIN SUB-FLOOR AT FS 664, RBL 50, PRESSURE WEB CRACKED, O/B OF WIRE FEED THROUGH. CUT OUT DAMAGED WEB, FABRICATED AND INSTALLED REPAIR PARTS IAW ER 03-5310-00243DL1.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage Main, BulkheadSDR AWXA0000704Support Bracket · corrodedC-CHECK CORROSION LEVEL 1. DIAGONAL FLOOR BEAM SUPPORT AT FS 1016, LBL 12, CORRODED, AFT LAV AREA GUSSET. REMOVED DAMAGED PART IAW 737 SRM 51-40-02, FABRICATED REPLACEMENT PART IAW DWG 65-46812, AND INSTALLED REPAIR IAW 737 SRM 51-40-03.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA0000703Skin · dentedC-CHECK, FUSLAGE SKIN AND INNER T CHORD BETWEEN FS 360 TO 380, STR 17L TO 18L, DENTED. REMOVED DAMAGED AREA AND REPAIRED SKIN IAW 737 SRM 53-00-01 FIG 201. REPAIRED T CHORD IAW 737 SRM 51-70-12 FIG 1.Oct 3, 2000 · N324AW · Boeing 737301 · Fuselage Main, Plate/Skin
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