Boeing 737-3B7

Service difficulty reports · 4,722

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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"

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SDR USAA990897Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..5 INCH CRACK STRINGER TIE CLIP STATION 663.75, STRINGER 10R. REMOVED CRACKED TIE CLIP INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990896Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 807 FRAME, STRINGER 9R OVERHEAD BIN ATTACH POINT. INSTALLED REPAIR ANGLE AND FILLER PER EA 65193 AND SRM 53-00-07 FIG 202. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990895Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FUOND .125 INCH CRACK STATION 787 FRAME, STRINGER OVERHEAD BIN ATTACH POINT. INSTALLED REPAIR ANGLE AND FILLER PER EA 65193 AND SRM 53-00-07 FIG 202. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990879Stringer · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION BS 1007, STRINGER 23R, CORROSION LEVEL 1. INSTALLED STRINGER SPLICE PER SRM 53-00-03. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA990878Intercostal · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 178, RBL 22, WL 196 INTERCOSTAL. INSTALLED DOUBLER PER TR 53-10-15 AND SRM 53-10-08. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990871Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 312 TO 344 LBL 45 Z-ANGLE. CORROSION LEVEL 2. REPAIRED PER 53-10-15 AND 51-10-02. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990854Angle · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTINO, FOUND A ..25 INCH CRACK AT DRAG ANGLE VERT FIN ATTACH FITTING. INSTALLED DOUBLER AND FILLERS PER EA 65234 AND 65234A. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Vertical StabilizerSDR USAA990853Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..1 INCH CRACK AT BS 726 STRINGER 18A RIGHT CHORD ANGLE. INSTALLED NEW PART PER EA 65273A. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990852Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES BY 2 INCHES AT STATION 344 FLOORBEAM LBL 45 - RBL 15. CORROSION LEVEL 1. CORROSION TASK NR C 53-107-01. INSTALLED NEW SECTION OF UPPER CHORD WITH REPAIR DOUBLER PER SRM 51-70-12 AND EA 6523Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA990845Intercostal · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A ..75 INCH CRACK BS 278 STRINGER 14R IN RADIUS OF INTERCOSTAL. INSTALLED REPAIR DOUBLER PER SRM 51-70-11 FIG 1. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990844Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A AREA OF CORROSION BS 1016, BBL 0, LBL 12, WL 208 FLOORBEAM. CORROSION LEVEL 1. INSTALLED COMPLETE T-CAP PER SRM 53-10-05 AND EA 65232. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA990836Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 666, LBBL 32.5 PRESSURE DECK. INSTALLED DOUBLER PER EA 65231. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA990835Bracket · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK IN ANGLE RIGHT BS 616 STRINGER 7 AND STRINGER 8 BRACKET. REPLACED BRACKET, FABRICATED NEW PART PER SRM 51-30-01 FIG 2 PG 14. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990834Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK BS 305, STRINGER 4L FRAME. INSTALLED NEW PART PER SRM 51-10-02.. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990833Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION AT STATION 360, RBL 12 FLOORBEAM. CORROSION LEVEL 1. REPAIRED ANGLES PER SRM 53-00-51. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA990832Seat Track · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT SEAT TRACK STATION 887 TO 947, LBL 48. CORROSION LEVEL 1. REPAIRED DOUBLER/SHIMS PER SRM 53-00-52. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA990830Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 24 INCH BY 24 INCH AREA OF CORROSION STATION 312, LBL 12, RBL 12 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA990829Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTINO, FOUND A ..5 INCH BY .5 INCH AREA OF CORROSION STATION 1016, BL 0 TO LBL 12 FLOORBEAM. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER EA 65232. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA990825Stringer · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 908 PLUS 1/2 STRINGER 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-00. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA990820Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 907 STRINGER 9L OVERHEAD BIN ATTACH POINT FRAME. INSTALLED REPAIRED ANGLE PER EA 65193. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990819Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCHCRACK STATION 847 STRINGER 9L OVERHEAD BIN ATTACH POINT FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 65193. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990818Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 887 STRINGER 9L OVERHEAD BIN ATTACH POINT FRAME. REMOVED AND REINSTALLED BRACKET PER SRM 51-40-02. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990817Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK STATION 807 STRINGER 9L OVERHEAD BIN ATTACH POINT FRAME. INSTALLED DOUBLER PER EA 65193. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990816Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 867 STRINGER 9L OVERHEAD BIN ATTACH POINT FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 AND EA 65193. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990815Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 480 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED REPAIR ANGLE PER EA 65193. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990814Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK STATION 480 BETWEEN STRINGER 8R AND 9R FRAME. INSTALLED REPAIR ANGLE PER EA 65193. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990813Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..5 INCH CRACK STATION 663.75 STRINGER 10L TIE CLIP. REPAIRED PER SRM 51-10-02. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990812Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 TO 1.5 INCH CRACK STATION 807 STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990792Frame · corrodedCLT - DURING A Q-2 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION AT FS 500D, LBBL 17 FRAME. CORROSION LEVEL 2. REPAIRED ANGLES FABRICATED PER SRM 53-00-07 FIG 203. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA990767Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK STATION 616 STRINGER 4R TIE CLIP. REPLACED PART PER SRM 51-10-02. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990766Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK STATION 639 STRINGER 4R TIE CLIP. REPLACED PART PER SRM 51-10-02. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990765Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A ..125 INCH CRACK STATION 500A STRINGER 16R TIE CLIP. REPLACED PART PER SRM 51-10-02. (M)Aug 29, 1999 · N397US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR DL733991934Fitting · corrodedTHE LT AND RT NLG DRAG BRACE ATTACH FITTING BORES WERE FOUND WITH CORROSION. THE BORES WERE OVERSIZED TO REMOVE THE CORROSION AND PERMIT INSTALLATION OF .05 THICK WALL REPAIR BUSHINGS. AL-NI-BR REPAIR BUSHINGS WERE INSTALLED IN THE REWORKED BORES PER ER/A 3Aug 28, 1999 · N947WP · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990918Skin · crackedCLT - DURING RON CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK JUST BELOW STR 18R AT STA 727E PLUS 1.5 INCHES TO 727E PLUS 4 INCHES FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (X)Aug 24, 1999 · N384US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR AALA990925Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK IN FUSELAGE FRAME (PARTIALLY SEVERED) AT BS 305 STR 4L. INSTALLED REPLACEMENT WEB PER SRM 51-10-02. (X)Aug 24, 1999 · N397US · Boeing 7373B7 · Fuselage Main, FrameSDR USAASB99205Indication · malfunctionedCLT - FLT 432 - AFTER TAKEOFF AND GEAR RETRACTION FROM CHS, BOTH THE LEFT AND RIGHT MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED WHILE THE NOSE LANDING GEAR INDICATED UP AND DOORS CLOSED. CREW RECYCLED THE GEAR AND RECEIVED NORMAL INDICATION. FLIGHT Aug 19, 1999 · N371US · Boeing 7373B7 · Landing Gear Position and WarningSDR USAASB99201Control Valve · failedCLT - FLT2250 - AIRCRAFT DEPARTED CLT WITH LEFT PACK ON MEL. ON CLIMB-OUT AT APPROXIMATELY 8,000 FEET, CREW LOST THE RIGHT PACK AS THE RIGHT PACK FAIL LIGHT ILLUMINATED. CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT AND DECIDED TO RETURN TO FIELD AT CLT WHERE TAug 13, 1999 · N531AU · Boeing 7373B7 · Pneumatic Distribution SystemSDR USAA990864Stiffener · crackedPIT - DURING CX3 CONV CHECK, FOUND .5 INCH CRACK IN STIFFENER AT STATION 344 INTERCOSTAL. REPLACED ANGLES PER EA 52604. (M)Aug 8, 1999 · N385US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA990863Skin · crackedPIT - DURING CX3 CONV CHECK, FOUND CRACK APPROX .500 INCH IN AFT CARGO DOOR, FLAPPER DOOR CUT OUT (A/C SKIN) UPPER AFT CORNER. REPAIRED PER TYPICAL REPAIR 52-10-01 'A' FIG 1. (M)Aug 8, 1999 · N385US · Boeing 7373B7 · Cargo/Baggage DoorsSDR USAA990862Floorbeam · crackedPIT - DURING CX 3 CONV CHECK, FOUND CRACK APPROX .500 INCH FLOORBEAM AT FS 344 AT LBL 11. REPAIRED PER SRM 53-10-51 AND EA 52604. (M)Aug 8, 1999 · N385US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR DL733991767Light · inopEMERGENCY LIGHTS AT SEATS 1D ABD 14D INOP. RELAMPED TEST GOOD.Aug 8, 1999 · N947WP · Boeing 7373B7 · Emergency LightingSDR USAA990859Skin · crackedPIT - DURING CX3 CHECK, FOUND .3750 INCH CRACK IN SKIN AT AFT ENTRY DOOR UPPER HINGE CUTOUT. DOUBLER INSTALLED PER SRM 53-60-01 FIG 205.Aug 7, 1999 · N384US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA990798Skin · crackedTPA - DURING CX-1 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK BELLY SKIN AFT EQUIPMENT COOLING EXHAUST STA 380 FUSELAGE SKIN. INSTALLED REPAIRED DOUBLER PER TR 53-30-07. (X)Aug 3, 1999 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB99198Charger · failedEWR - PILOT REPORTED THAT THE FORWARD ENTRY DOOR EMERGENCY LIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Jul 28, 1999 · N385US · Boeing 7373B7 · Emergency LightingSDR DL733991661Seal · leakingLEFT WING BODY OVERHEAT ON IN FLIGHT. EXTINGUISHED AFTER 5 MIN. LEFT BLEED CLOSED PER POM. OHMED DETECTORS CHECK GOOD. FOUND PNEU LEAK ON LEFT PACK AT BAND CLAMP ABOVE MOISTURE SEPARATOR. REPLACED SEAL ASSY AT TURBO FAN SUPPLY LINE. LEAK CHECKS GOOD. RAJul 24, 1999 · N952WP · Boeing 7373B7 · Cabin Cooling SystemSDR USAASB99179Chain · out of adjustPIT - FLT 1217 - DURING CLIMB-OUT FROM PIT, CREW NOTICED A VIBRATION THAT CONTINUED AFTER RETRACTING THE GEAR AND THE FLAPS. VIBRATION EVEN REGISTERED ON THE AVM GAUGE FOR THE NR 1 ENIGNE. CREW LEVELED OFF AT FL 230 AND STATED THAT THE VIBRATION WAS MOST NOTJul 20, 1999 · N525AU · Boeing 7373B7 · Stabilizer Control SystemSDR USAASB99177Anti-Ice Valve · failedPIT - FLT 620 - EN ROUTE FROM LAS TO PHL, DURING CRUISE, THE NR 1 ENGINE COWL ANTI-ICE LIGHT ILLUMINATED WHEN SELECTED ON. CREW REDUCED POWER AND LIGHT EXTINGUISHED. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. (M)Jul 19, 1999 · N516AU · Boeing 7373B7 · Air Intake Anti/De-Ice SystemSDR USAA990739Skin · crackedTPA - DURING WALK-AROUND FOUND 1.9 INCH SKIN CRACK AND 1 INCH CRACK IN SKIN AT BS 743 AND S19R AND BS 754.5 AND S19R. INSTALLED DOUBLER MADE OF .090 INCH 2024T3. BOTH CRACKS REPAIRED WITH SAME DOUBLER PER SRM 53-00-01 FIG 202. (X)Jul 19, 1999 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA990738Skin · crackedTPA - DURING WALK-AROUND FOUND 1.9 INCH SKIN CRACK AT BS 727E PLUS 2 INCHES AND S18R. INSTALLED DOUBLER MADE OF .090 INCH 2024T3 PER SRM 53-00-01 FIG 202. (X)Jul 19, 1999 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB99175Uplock Sensor · failedCLT - FLT 249 - DURING CLIMB-OUT FROM CLT, THE RIGHT MLG UNSAFE LIGH TILLUMINATED WITH THE GEAR UP. FLIGHT RETUREND TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK SENSOR.Jul 18, 1999 · N395US · Boeing 7373B7 · Landing Gear Position and Warning
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