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 USAA010737Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 747 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010738Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 440 AT S8L. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010739Clip · crackedPIT - FOUND CLIP CRACKED .25 INCH, BS 360 AT S13L. FABRICATED, HEAT TREATED AND INSTALLED PER SRM 53-00-07 FIG 205. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010740Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 440 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010710Bulkhead · crackedPIT - FOUND BULKHEAD CRACKED .125 INCH, STATION 178 BETWEEN LBL 5.7 AND 17. REPAIRED DOUBLER, FILLER PER SRM 53-10-08 PAGES 265-269. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, StructureSDR USAA010728Skin · crackedPIT - FOUND SKIN CRACKED .095 INCH, LOWER HINGE CUTOUT. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 52-10-01 S/B 737-52-1096. (M)May 17, 2001 · N586US · Boeing 737301 · DoorsSDR USAA010708Web · crackedPIT - FOUND WEB CRACKED .75 INCH, STATION 178 BULKHEAD WL 184. REPAIRED FILLERS, DOUBLERS AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010711Web · crackedPIT - FOUND WEB CRACKED 5 INCHES, STATION 178 BULKHEAD RIGHT FLOOR WEB AT WL 207. REMOVED AND REPLACED FLOORWEB. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010712Angle · crackedPIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD RIGHT CHORD ANGLE AT WL 207. REPAIRED DOUBLER, CHORD, CLIPS, SPLICE ANGLE PER SRM 53-10-08. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010713Angle · crackedPIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD LEFT CHORD ANGLE AT WL 207. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010714Web · crackedPIT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD LBL 5.7 WL 200, LOWER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, StructureSDR USAA010715Web · crackedPIT - FOUND WEB CRACKED .25 INCHES IN LENGTH, STATION 178 BULKHEAD LBL 5.7 WL 210 UPPER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010716Clip · crackedPIT - FOUND CLIP CRACKED .25 INCH, BS 639 AT S11L. MANUFACTURED, HEAT TREATED, INSTALLED CLIP PER BOEING PRINT 66-2411241-1. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010718Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, BS 787 BETWEEN 58L AND 59L. INSTALLED DOUBLER PER T/R 53-10-14. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, StructureSDR USAA010723Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BS 480 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70650. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010724Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 500C AT STRINGER 8R. ROUTED OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70647. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010725Angle · crackedPIT - FOUND ANGLE CRACKED 1.5 INCH, BS 616 BELOW S17L. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-62-01. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010727Angle · crackedPIT - FOUND ANGLE CRACKED .5 INCH, BS 454 AT OUTBOARD FLOOR PANEL SUPPORT ANGLE. MANUFACTURED NEW CLIP AND INSTALLED, HEAT TREAT. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010726Angle · crackedPIT - FOUND ANGLE CRACKED 1.5 INCHES, BS 616 BELOW STRINGER S17R. REMOVED DAMAGED, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-62-01. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010707Web · crackedPIT - FOUND WEB CRACKED .5 INCH, FORWARD PRESSURE BULKHEAD STATION 178. REPLACED WEB. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010701Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 380 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 201. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010702FramePIT - FOUND INDICATION BY HFEC IS DOUBLE FLUSH RIVET, BS 380 AT S8L. CUT OUT DAMAGE, INSTALLED FILLERS AND DOUBLER PER SRM 53-00-07 PAGE 203-206. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010705Web · crackedPIT - FOUND WEB CRACKED .5 INCHES LONG, STATION 178 BULKHEAD ANTENNA MOUNT RIGHT. FILLER, DOUBLER, SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010706Web · crackedPIT - FOUND WEB CRACKED .25 INCH, BS 178 BULKHEAD LOWER LT ANTENNA MOUNT. FILLER, DOUBLERS, SHIMS PER SRM 53-10-08 FIG 211. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010703StringerPIT - FOUND STRINGER CUT TO FASCILITATE CLIP REMOVAL, BS 967 AT S25L. SPLICED STRINGER PER SRM 53-00-3. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010697Structure · corrodedPIT - FOUND CORROSION 1 INCH BY 6 INCH, LT WING 7211 OPENING. CORROSION LEVEL 1, TASK NR C53-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGE 213-216. (M)May 17, 2001 · N586US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010696Structure · corrodedPIT - FOUND CORROSION 1 INCH BY 4 INCH AREA, LT WING 7204L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M)May 17, 2001 · N586US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010695Structure · corrodedPIT - FOUND MATING SURFACE 1 INCH BY 3 INCH, LT WING 7213L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216.May 17, 2001 · N586US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010693Structure · corrodedPIT - FOUND MATING SURFACE 1 INCH BY 4 INCH AREA OF CORROSION, LT WING 7202L OPENING. CORROSION LEVEL 1 TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M)May 17, 2001 · N586US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010692Structure · corrodedPIT - FOUND MATING SURFACE CORRODED 1 INCH BY 5 INCH AREA, LT WING 7210L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION ROT PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M)May 17, 2001 · N586US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010689Web · corrodedPIT - FOUND WEB CORRODED 2 INCHES BY 3 INCHES, BS 947.5 TO 986.5, CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED CORROSION, TREAT, PRIME, FABRICATE NEW SECTIONS AND INSTALLED. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA0100690Structure · corrodedPIT - FOUND MATING SURFACE CORRODED, 1 INCH BY 6 INCH AREA, LEFT WING 7217L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01, PAGES 213-216. (M)May 17, 2001 · N586US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010691Structure · corrodedPIT - FOUND MATING SURFACE CORRODED 1 INCH BY 3 INCHES, LT WING 7214L. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PGS 213-216. (M)May 17, 2001 · N586US · Boeing 737301 · Wing Main, Frame StructureSDR USAA010687Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED 1 INCH BY 4 INCHES, LT INBOARD AFT OF BS 344. CORROSION LEVEL 1, TASK NR C53-107-01. CUT OUT DAMAGE, INSTALLED NEW AND SPLICE PER SRM 53-00-52, FIG 203. (M)May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010717Web · crackedPIT - FOUND WEB CRACKED .5 INCH, AT BL0 B5712 BELOW FLOORBEAM CAP, LEFT SIDE. INSTALLED REPAIR DOUBLERS PER EA 71067. (M)May 16, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010719Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, BS 867 BETWEEN 58L-59L. INSTALLED DOUBLER PER T/R 53-10-14. (M)May 16, 2001 · N586US · Boeing 737301 · Fuselage Structure (General)SDR USAA010720Angle · crackedPIT - FOUND ANGLE CRACKED 1 INCH, STATION 540 LEFT WING ROOT 2 INCHES ABOVE STRINGER. REMOVED DAMAGED AREA, INSTALLED FILLER, REPAIR ANGLE PER TR 53-50-03. (M)May 16, 2001 · N586US · Boeing 737301 · Wing StructureSDR USAA010721Angle · crackedPIT - FOUND ANGLE CRACKED 1 INCH, STATION 540 RIGHT WING ROOT 2 INCHES ABOVE STRINGER 22R. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR ANGLE PER TR 53-50-03. (M)May 16, 2001 · N586US · Boeing 737301 · Wing StructureSDR USAA010722Skin · delaminatedPIT - FOUND WING LEADING EDGE DELAMINATED 6 INCHES BY 8 INCH AREA, LEFT WING LEADING EDGE AT STATION 559. REMOVED DAMAGED LAYERS, DRILLED OUT BRACKET FOR MOUSE TRAP PER SRM 51-70-17. (M)May 16, 2001 · N586US · Boeing 737301 · Wing, Plate/SkinSDR USAA010698Angle · corrodedPIT - FOUND ANGLE PLATE ATTACH 2 INCHES BY 6 INCH, BETWEEN 767 AND 793 FORWARD SIDE OF AFT CARGO DOOR OPEN. CORROSION LEVEL 1, TASK C53-208-01. CLEANED CORROSION FROM ANGLE AND REPAIRED ANGLE PLATE PER SRM 51-21-21. (M)May 16, 2001 · N586US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA010593Frame · corrodedPIT - FOUND UPPER CHORD CORRODED 1 INCH BY 3 INCHES CORROSION, BS 967. CORROSION LEVEL 1, TASK NR C53-107-02. CLEAN/TREAT/PRIME AND INSTALL STRAP PER EA 70646 IAW SRM 53-00-51. (M)May 16, 2001 · N586US · Boeing 737301 · Fuselage Main, FrameSDR USAA010592Frame · corrodedPIT - FOUND UPPER CHORD CORRODED 1 INCH BY 4 INCHES, BS 986.5. CORROSION LEVEL NR 1, TASK NR C53-107-02. CLEAN/TREAT/PRIME, ALSO CUT OUT DAMAGE SPLICE IN NEW STRUCTURE PER TYP REPAIR 53-60-01. (M)May 16, 2001 · N586US · Boeing 737301 · Fuselage Main, FrameSDR USAA010591Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED .5 INCH BY 1 FOOT, STATION 344 UNDER FLOORBOARD NR 8. SPLICED IN BEAM REPAIR. (M)May 16, 2001 · N586US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA010590Beam · corrodedPIT - FOUND BEAM CORRODED 4 AREAS 2 INCHES, SUPPORT FOR FLOORBOARD NR 6. CORROSION LEVEL 1, TASK NR 53-107-02. SPLICED IN BEAM SECTION THAT WAS BLENDED BEYOND LIMITS PER SRM 53-10-51. (M)May 16, 2001 · N586US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB01136Uplock Sensor · faultyPHL - FLT 1922 - AFTER GEAR RETRACTION, WITH GEAR HANDLE IN 'UP' POSITION, THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. CREW EXTENDED THE GEAR AND RECEIVED THREE GREEN LIGHTS. CREW RETRACTED GEAR AND AGAIN RECEIVED THE NOSE GEAR RED LIGHT. CREW DECIDED TO May 13, 2001 · N577US · Boeing 737301 · Landing Gear Position and WarningSDR USAASB01133Controller · failedBOS - FLT 1116 - ON CLIMB-OUT FROM BOS, EN ROUTE PHL AT 6,000 FEET, THE CABIN RATE OF CLIMB WAS FLUCTUATING FROM 3,000 FEET PER MINUTE TO 2,000 FEET PER MINUTE IN AUTO MODE. MANUAL MODE WAS INOPERATIVE. AIRCRAFT FAILED TO PRESSURIZE, SO THE FLIGHT RETURNED TMay 11, 2001 · N591US · Boeing 737301 · Cabin Pressure ControllerSDR SWAA011413Slide · unserviceableDURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.May 11, 2001 · N660SW · Boeing 737301 · Escape SlideSDR USAA010531Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 827 AT STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 10, 2001 · N584US · Boeing 737301 · Fuselage Main, FrameSDR USAA010530Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 727B, STRINGER 9R. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-10-14. (M)May 10, 2001 · N584US · Boeing 737301 · Fuselage Main, FrameSDR USAA010529Tie Clip · crackedCLT - FOUND TIE CLIPS CRACKED .25 INCH, BS 908, STRINGER 4L AND 5L. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10-2. (M)May 10, 2001 · N584US · Boeing 737301 · Fuselage Miscellaneous Structure
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