Boeing 737-4B7

Service difficulty reports · 5,757

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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 = '7374B7'
  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 USAASB00248Regulator · failedDCA - FLT 1893 - EN ROUTE FROM CLT-DCA, AT FL270, THE RIGHT ENGINE BLEED TRIPPED OFF FOLLOWED BY THE LEFT ENGINE BLEED TRIPPING OFF. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DESCENDED TO FL100. PERFORMED AUTO FAIL AND UNSCHEDULED PRESSURE CHANGE CSep 6, 2000 · N441US · Boeing 7374B7 · Pneumatic Distribution SystemSDR USAASB00247Module · faultyPHL - FLT 1541 - EN ROUTE FROM ROC TO PHL, DURING FLIGHT, THE FIRE WARNING LIGHTS ILLUMINATE INTERMITTENTLY FOR NO APARENT REASON, ESPECIALLY DURING TAXI, TAKEOFF AND LANDING ROLL OUT. MAINTENANCE CHECKED FIRE WARNING LIGHTS CIRCUIT FOR SHORTS TO GROUND. NONSep 6, 2000 · N435US · Boeing 7374B7 · Fire DetectionSDR USAA001413Plate · corrodedCLT - FOUND CORROSION ON CAM PLATE .5 INCH BY .5 INCH TWO PLACES, FORWARD ENTRY DOOR UPPER CAM PLATE MOUNT. REPLACED CAM PLATE PER SRM 51-10-02. (M)Sep 1, 2000 · N427US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAASB00235Battery Pack · dischargedCLT - DURING WEEKLY CHECK, MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Aug 30, 2000 · N781AU · Boeing 7374B7 · Emergency LightingSDR USAA001394Skin · damagedTPA - FOUND DOOR SKIN DAMAGED 3 INCHES BY 6 INCHES, FORWARD CARGO DOOR TOP CENTER OF DOOR. INSTALLED DOUBLER PER SRM 52-00-01 FIG 202. (M)Aug 30, 2000 · N434US · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAA001386Frame · crackedCLT - FOUND FRAMED CRACKED .25 INCH, STATION 747 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 29, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001385Frame · crackedCLT - FOUND FRAME CRACKED 2 INCHES, BS 480, STRINGER 22L TO 23L. INSTALLED DOUBLER PER EA 67893. (M)Aug 29, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001384Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 400 BETWEEN STRINGER 8 AND STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 29, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001383Skin · crackedCLT - FOUND SKIN PYLON CRACKED 1.5 INCHES, NAC STATION 212 PANEL ACCESS 5727L. INSTALLED DOUBLER PER TR 54-30-07. (M)Aug 29, 2000 · N427US · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA001373Skin · crackedCLT - FOUND SKIN CRACKED .125 INCH, OUTBOARD END LOWER SKIN. INSTALLED DOUBLER PER TR 57-50-01 REV H. (M)Aug 29, 2000 · N427US · Boeing 7374B7 · Wing, Plate/SkinSDR USAA001372Flange · crackedCLT - FOUND FLANGE WITH THREE 1 INCH CRACKS, BL 0, BS 927 TO 947. FABRICATED REPLACEMENT FLANGE PER SRM 53-60-51. (M)Aug 29, 2000 · N427US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001371Frame · crackedCLT - FOUND CHORD CRACKED .25 INCH, STATION 178 BULKHEAD SIDE CHORD RBL 27, WL 207.5. TEMP REPAIR STOP DRILLED CRACK AND INSTALLED ANGLE PER EA 67901. (M)Aug 29, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAASB00230Bolt · wornCLT - FLT 309 - ON CLIMB-OUT FROM CLT, ACCELERATING ABOVE 280 KNOTS, CREW NOTED A FLUTTER IN FLIGHT CONTROLS. FLIGHT ATTENDANT REPORTED A STRONGER VIBRATION IN TAIL AREA. AS AIRSPEED INCREASED, FREQUENCY AND INTENSITY OF VIBRATION INCREASED. CREW SLOWED AIRAug 26, 2000 · N434US · Boeing 7374B7 · Elevator, Tab StructureSDR USAA001354Clevis · corrodedCLT - FOUND FORWARD UPPER LUG CLEVIS CORRODED .5 INCH BY .75 INCH, RIGHT HORIZ STAB. INSTALLED NEW BUSHING PER SRM 55-10-10 AND SRM 20-10-03. (M)Aug 25, 2000 · N427US · Boeing 7374B7 · Empennage Flight Control Surfaces, Attach FittingsSDR USAA001353Frame · corrodedCLT - FOUND FRAME CORRODED 3 INCHES BY 3 INCHES, FORWARD DOOR FRAME STATIN 794, STRINGER 25R. CORRODED LEVEL 1 C 53-202-01. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 53-60-53 PAGE 112. (M)Aug 25, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001352Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 7 INCHES, BS 947, LBL 11, LBL 4, RBL 4, RBL 12. INSTALLED DOUBLER PER TR 53-60-02A. (M)Aug 25, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001323Frame · corrodedCLT - FOUND FRAME CORRODED 1 INCH BY 3 INCH AREA, STATION 867, BL 0. REPAIRED PER SRM 53-60-53 PAGE 112 FIG 101 DETAIL XIV. CORROSION LEVEL 1. (M)Aug 24, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001322Splice · crackedCLT - FOUND SPLICE WITH TWO CRACKS .25 INCH, BS 908 AT STRINGER 4L. INSTALLED NEW SPLICE PER SRM 51-10-02. (M)Aug 24, 2000 · N427US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001321Bulkhead · crackedCLT - FOUND BULKHEAD LEFT SIDE CRACKED .375 INCH, STATION 178 CHORD LBL 27, WL 207.5. INSTALLED REPAIR ANGLE PER SRM 53-10-08. (M)Aug 24, 2000 · N427US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA001324Angle · corrodedCLT -FOUND Z-ANGLE CORRODED 1.5 INCH BY 1.5 INCH, FROM BS 947 TO BS 986, AFT ENTRY DOOR. REPLACED Z-ANGLE PER SRM 51-10-2. (M)Aug 24, 2000 · N427US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001306Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 727B BETWEEN STRINGER 8L AND STRINGER 9L. FABRICATED FRAME DOUBLER AND INSTALLED PER TR 53-10-14. (M)Aug 22, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001308Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 927, BL 0. REMOVED CORROSION FABRICATED REPAIR AND INSTALLED PER SRM 53-00-51 FIG 202. (M)Aug 22, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001307Frame · crackedCLT - FOUND CHORD CRACKED .5 INCH, BS 601, WL 201, LEFT OVERWING EXIT. INSTALLED REPAIR ANGLE PER EA 67868 AND TR 53-62-01. (M)Aug 22, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001293Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 663, STRINGER 10R. INSTALLED NEW CLIP PER SRM 51-10-02. (M)Aug 18, 2000 · N427US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001292Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 663, S10L. INSTALLED NEW CLIP PER SRM 51-10-02.Aug 18, 2000 · N427US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001291Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, RBL 6, WL 201, STATION 178 BULKHEAD. REMOVED DAMAGE AND INSALLED DOUBLER PER EA 67855 AND SRM 53-10-08. (M)Aug 18, 2000 · N427US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA001290Fitting · corrodedCLT - FOUND CORROSION LEFT STAB FORWARD UPPER LUG. INSTALLED NEW BUSHING PER SRM 55-10-10. CORROSION LEVEL 1. (M)Aug 18, 2000 · N427US · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA001289Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .250 INCH, BS 986, LBL 4 TO RBL 38 NUTPLATE HOLES. CORROSION LEVEL 1, C53-107-02. SPLICED T-CAP PER TR 53-60-01. (M)Aug 18, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001295Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 867 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 18, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001294Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 727F BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 18, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001278Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 500C BETWEEN STRINGER 8L AND 9L. REPAIRED PER TR 53-10-14. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001277Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 440 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 55-10-14 AND 53-00-07. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001276Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 380 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001275Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 827 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 55-10-14 AND SRM 53-00-07. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001274Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 827 BETWEEN STRINGER 8L AND 9L. FABRICATED DOUBLER PER TR 53-10-14. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001273Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 344. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND DOUBLER PER SRM 53-10-51. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001272Floorbeam · corrodedFOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH, STATION 328, LBL 30 T-CAP OF FLOORBEAM. CORROSION LEVEL 1. FABRICATED NEW SPLICE ANGLE AND FILLER PER SRM 51-70-12 FIG 1. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001279Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 747 BETWEEN STRINGER 8R AND 9R. FABRICATED DOUBLER PER TR 53-10-14. (M)Aug 17, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001271Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .0500 INCH, BS 967, LBL 18.5. INSTALLED REPAIR ANGLES PER SRM 53-10-51. (M)Aug 16, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001270Frame · crackedCLT - FOUND FRAME CRACKED, STATION 787 BETWEEN STRINGER 8L AND 9L. INSTALLED PER SRM 51-40-03. (M)Aug 16, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001269Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 440 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 16, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001268Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 480 BETWEEN STRINGER 8L AND 9L. DRILLED OUT CRACK, INSTALLED FASTENER PER SRM 51-10-02. (M)Aug 16, 2000 · N427US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA001255Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .25 INCH, STATION 312, LBL 20 - RBL 20 UPPER CHORD T-CAP SCREW HOLES. REPAIRED DOUBLER/SPLICE OF NEW T-CAP PER SRM 53-00-51 FIG 201. (M)Aug 15, 2000 · N427US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAASB00216Battery Pack · dischargedATL - DURING OVERNIGHT CHECK, MAINTENANCE FOUND A SECTION OF FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1136 BATTERY PACK. OPS CHECK GOOD. (M)Aug 12, 2000 · N447US · Boeing 7374B7 · Emergency LightingSDR USAASB00215Charger · failedPHL - MAINTENANCE FOUND THE MID-CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMVOED AND REPLACED THE BATTERY PACK (P/N AD2013-1A) AND CHARGER ASSY. OPS CHECK GOOD. (M)Aug 11, 2000 · N447US · Boeing 7374B7 · Emergency LightingSDR USAASB00213Panel · failedFLL - FLT 1167 - EN ROUTE FROM PHL-FLL, AT FL 350, THE LEADING EDGE FLAPS TRNSIT LIGHT ILLUMINATED ALONG WITH THE NR 4 FLAP TRANSIT LIGHT ON OVERHEAD PANEL. LIGHTS REMAINED ON FOR APPROX 5-8 MINUTES, THEN EXTINGUISHED. NO ROLL OR ABNORMAL CONTROL RESPONSE WAAug 8, 2000 · N438US · Boeing 7374B7 · Trailing Edge Flap Control SystemSDR USAA001144Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 3 INCHES BY 6 INCHES, STATION 986.5 FULL LENGTH OF BEAM. INSTALLED NEW T-CAP, SPLICE ANGLE AND STRAP PER SRM 53-00-51. CORROSION LEVEL 2, C53-107-02. (M)Aug 2, 2000 · N433US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001143Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH BY 1 INCH AREA, STATION 947. CORROSION LEVEL 2, C53-107-02. REMOVED DAMAGE SPLICED IN T-CAP PER TR 53-60-02A. (M)Aug 2, 2000 · N433US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA001132Floor Support · corrodedCLT - FOUND FLOOR SUPPORTS CORRODED 2 INCHES BY 16 INCHES, STATION 967 FLOOR SUPPORTS. INSTALLED REPAIR ANGLES PER 53-00-51. (M)Aug 1, 2000 · N433US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA001131Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 727F LT SIDE FUSELAGE BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 1, 2000 · N433US · Boeing 7374B7 · Fuselage Main, Frame
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