Boeing 737-3B7

Service difficulty reports · 4,722

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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 = '7373B7'
  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 USAA980443Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH CORRODED AREA BS 967 RBL 49 BEAM INST PAX FLOOR. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-10-05. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980442Web · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK SHEAR BEAM WEB 518A RIGHT BS 721. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980441Frame · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2 INCH CORRODED AREA BS 827 BETWEEN STRINGER 28L AND STRINGER 28R RBL 2 BOTTOM FRAME. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-00-07. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980440Web · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CRACKED AREA .25 INCH FORWARD SERVICE DOOR OPENING LWR FWD CORNER BS 294 STRINGER 17R FLOOR LEVEL. INSTALLED DOUBLER PER SRM 51-70-11. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980425Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS .5 INCH BY .5 INCH BY 26 INCH BS 328 LB 12 TQ RBL 14, WL 208.1 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER SRM 51-70-12. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980424Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 2 INCH CORRODED AREA STATION 1006 BEAM T-CAP RBL 10. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-58-53500-012. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980423Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION BS 986.5 LBL 4, 11, 21 AND LOWER SURFACE LBL 36 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP UPPER CHORD PER SRM 53-00-51 AND EA 62431. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980422Splice · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND STRINGER SPLICE CRACKED AROUND 4 RIVET HOLES .125 INCH EACH STRINGER AT STATION 907 STRINGER 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-40-02. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980421Channel · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 360 STRINGER 4L V-CHANNEL. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980420Stringer · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500D AND STRINGER 28L. INSTALLED DOUBLERS PER SRM 53-30-12. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA980419Stringer · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND THREE .5 INCH CRACKS FROM RIVET TO RIVET STRINGER 4L STATION 907. NEW STRINGER SPLICE INSTALLED PER SRM 51-10-02. (M)Sep 30, 1998 · N393US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA980418Frame · dentedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH DENT STATION 747 AND STRINGER 24L, 727E AND STRINGER 25L AND 767 AND STRINGER 21L FRAME. INSTALLED REPAIR ANGLES STATION 727E, STATION 747 STRINGER 24L AND STATION 767 STRINGER 21L PER EA 6239Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980417Skin · damagedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH HOLE IN FORWARD FUSELAGE STATION 189, 2 FT FORWARD AND 1 FT DOWN FROM 1ST OFFICERS WINDOW ON SKIN. REPAIRED EXISTING INTERMI REPAIR TO PERMANENT REV A PER EA 58180A. (M)Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA980416Housing · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT INBOARD FLANGE OF UPPER HINGE HOUSING FOR FORWARD SERVICE DOOR FRAME 294.5. INSTALLED DOUBLER PER TR 53-10-11. (M)Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980391Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION STATION 1006 LBL 2 BEAM INST PASS FLOOR. CORROSION TASK NR C53-107-02. INSTALLED REPAIR ANGLES PER SRM 53-30-51. (M)Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980388Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 14 INCH AREA OF CORROSION STATION 328 LBL 51 TO RBL 65 FLOORBEAM UPPER CHORD. CORROSION TASK NR C63-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M)Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980387Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH BY 50 INCH AREA OF CORROSION STATION 344 BLO TO LBL 50 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M)Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980386Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 72 INCH AREA OF CORROSION CLIPNUT HOLES STATION 312 LBL 36 TO RBL 36 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M)Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980385Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 10 INCH AREA OF CORROSION STATION 967 LBL 5 TO RBL 5 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED REPAIR ANGLES PER SRM 53-30-51. (M)Sep 17, 1998 · N534AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAASB98239Unknown · odorLGA - FLT 1157 - EN ROUTE FROM BUF TO LGA, THE FLIGHT ATTENDANT IN THE AFT GALLEY REPORTED A BURNING ODOR, BUT COULD NOT IDENTIFY ORIGIN. ODOR DISSIPATED WHEN LIGHTS TURNED OFF AND CIRCUIT BREAKERS WERE PULLED. FLIGHT CONTINUED AND LANDED AT LGA WITHOUT FURTSep 13, 1998 · N389US · Boeing 7373B7 · Passenger Compartment LightingSDR USAASB98238Valve · cloggedCLT - FLT 61 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT UPON CLIMB-OUT FROM CLT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND AN INSULATION BLANKET STUCK IN THE UPPER PRESSURIZATION SAFETY RSep 11, 1998 · N531AU · Boeing 7373B7 · Pressure Regulator/Outflow ValveSDR USAASB98237Bearing · failedCLT - FLT 1782 - CAPTAIN REPORTED THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS AT FL 370, REPEATED AT FL 350, THEN A SUSTAINED SURGING AT FL 310. CREW ELECTED TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. DURING TAXISep 11, 1998 · N514AU · Boeing 7373B7 · Turbine SectionSDR USAA980392Skin · crackedCLT - DURING RON VISUAL INSPECTION, FOUND A 2 INCH CRACK ON STRINGER 24L FROM 2-5 INCH FORWARD OF STATION 727E ON SKIN. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M)Sep 9, 1998 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB98229Light · inoperativeROC - MAINTENANCE FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT ON SEAT 22 END BAY INOP. MAINTENANCE FOUND THE WIRES PULLED OUT OF LAMPHOLDER. REMOVED AND REPLACED THE LAMPHOLDER. OPERATIONAL CHECK GOOD. (M)Sep 3, 1998 · N387US · Boeing 7373B7 · Emergency LightingSDR USAA980379Skin · crackedTPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK ON DOOR OUTER SKIN FORWARD SERVICE DOOR LOWER HINGE CUTOUT AFT UPPER CORNER. INSTALLED DOUBLER MADE FROM .063 2024 T-3 PER EA 62369 AND SB 737-52-1096. (M)Aug 30, 1998 · N396US · Boeing 7373B7 · Landing Gear DoorsSDR USAA980378Skin · crackedTPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND AN .25 INCH CRACK IN EXTERNAL SKIN AFT OF EQUIPMENT COOLING DUCT OUTLET STATION 380 LBL 30. INSTALLED DOUBLER OF .100 2024 T-3 PER EA 62368 SB 737-53-1117 REV 1. (M)Aug 30, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA980377Skin · crackedTPA - DURING A CX-1 CHECK EDDY CURRENT INSPECTION, FOUND A .625 INCH CRACK BELLY SKIN .063 STA 380. INSTALLED DOUBLER PER EA 62363 2024 T-3, SB 737-53-1117. (M)Aug 28, 1998 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA980371Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF CREASEBEAM INNER CHORD RBBL BETWEEN STATION 294.5 TO STATION 331. CORROSION TASK NR C53-107-02. INSTALLED SPLICE PER DRAWING 6545875 AND SRM 51-10-02. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA980370Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 11 INCH AREA OF CORROSION ON UPPER FLOORBEAM CHORD STATION 1016 LBL 15, CORROSION TASK NR C53-107-02. INSTALLED 11.5 INCH DOUBLER PER SRM 53-00-51 FIG 203. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980369Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON 'T' CAP OF FLOORBEAM 65 INCH BY 3.5 INCH STATION 312 LBL 8 RBL 56 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. FABRICATED 'T' CAP ANGLES PER TR 53-10-03. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980368Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBEAM BOARD SCREW HOLES .5 INBY .5 BY 70 INCH STATION 328 BETWEEN RBL 14 TO RBL 56 UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP SECTION PER SRM 53-10-51. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980367Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBOARD SCREW HOLES .5 INCH BY .5 INCH BY 25 INCH STATION 344 BETWEEN LBL 14 TO RBL 11 UPPER CHORD FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW 'T' CAP AND SPLICED ANGLES PER TR 53Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980366Skin · crackedCLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT SERVICE DOOR INSIDE UPPER FRAME SKIN, UPPER HINGE ARM CLOSEOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07 AND EA 62249. (M)Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA980376Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION STATION 1006 LBL 12 FLOORBEAM. CORROSION TASK NR C53-107-20. SPLICED FLOORBEAM SECTION PER SRM 53-00-51 FIG 202. (M)Aug 26, 1998 · N384US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980375Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 14 INCH AREA OF CORROSION STATION 967 LBL 30 FLOORBEAM. CORROSION TASK NR C53-107-20. REPLACED UPPER FLOORBEAM T-CAP PER TR 53-10-05. (M)Aug 26, 1998 · N384US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980374Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 BY .5 BY .92 INCH AREA OF CORROSION AROUND SCREW HOLES BS 947 LBL 36 TO RBL 56 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED UPPER T-CAP REPAIR PER TR 53-10-05. (M)Aug 26, 1998 · N384US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980346Floorbeam · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION ON FLOORBEAM AT BS 344 LBL 09 UPPER CHORD. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS AND ANGLES PER REPAIR DOCUMENT 53-10-51. (M)Aug 26, 1998 · N384US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAASB98219Battery Pack · dischargedROC - MAINTENANCE FOUND SEVERAL FORWARD EMERGENCY LIGHTS FAIL AFTER APPROXIMATELY TWENTY SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE M1132 POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)Aug 23, 1998 · N530AU · Boeing 7373B7 · Emergency LightingSDR USAASB98210Light · inoperativeCLT - PILOT REPORTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 12 IS INOP. MAINTENANCE REMOVED AND REPLACED TWO LAMPHOLDER ASSEMBLIES AT SEAT ROW 12. OPERATIONAL CHECK GOOD. (M)Aug 13, 1998 · N510AU · Boeing 7373B7 · Emergency LightingSDR DL733981597Skin · crackedR1 DOOR CUTOUT SKIN CRACKED AT AFT LWR CORNER. INSTALLED REPAIR PER SRM 53-10-01 FIG 202.Aug 3, 1998 · N951WP · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR DL733981588Skin · gougedREPAIRED GOUGE ON FUSELAGE SKIN AT STA 400 BELOW STRINGER 19 LEFT PER SRM 53-00-01 FIG 210.Aug 1, 1998 · N951WP · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA980349Frame · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 41 INCH CORRODED AREA RIGHT CREASE BEAM INNER CHORD BS 295 AND BS 336. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980333Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 32 INCH CORRODED AREA AROUND FLOORBOARD SCREW HOLES IN 'T' CAP FLOORBEAM STATION 344 RBL 10 TO LBL 22. CORROSION TASK NR C53-107-02. INSTALLED NEW 'T'CAP PER T/R 53-10-03. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA980332Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN STRINGER 8 LT AND STRINGER 9 LEFT ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 BAC ADVISORY 737258. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980331Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 400 BETWEEN STRINGER 8 LT AND STRINGER LT ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980330Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 440 BETWEEN STRINGER 8 LT AND STRINGER 9 LT ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980329Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STATION 827, STRINGER 8 RIGHT, STRINGER 9 RIGHT ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980328Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867 BETWEEN STRINGER 8 RT AND STRINGER 9 RT FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980327Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867 BETWEEN STRINGER 8 LEFT AND STRINGER 9 LEFT FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA980326Frame · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .12 5INCH CRACK STATION 480 BETWEEN 5-8 RIGHT AND 5-9 RIGHT BODY FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND BAC ADVISORY 737258. (M)Jul 31, 1998 · N533AU · Boeing 7373B7 · Fuselage Main, Frame
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