Boeing 737-4B7

Service difficulty reports · 5,757

Newest first. General aviation reporting is voluntary.

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 USAA011112Stiffener · crackedCLT - FOUND STIFFENER CRACKED .5 INCH, BS 900 STRINGER 11L. INSTALLED NEW PART PER SRM 51-10-2. (M)Aug 20, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011113Frame · dentedCLT - FOUND FRAME DENTED .5 INCH BY .5 INCH BY .035 INCH, BS 827 STRINGER 24-251. INSTALLED FRAME DOUBLER PER TR 53-60-07. (M)Aug 20, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAASB01238Light · inoperativeTPA - MAINTENANCE FOUND A SEGMENT OF SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY ON SEAT ROW 9ABC. OPS CHECK GOOD. (M)Aug 20, 2001 · N441US · Boeing 7374B7 · Emergency LightingSDR USAASB01239Light · inoperativeTPA - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN SEAT ROWS 6 THROUGH 9 AND 12 THROUGH 19 INOPERATIVE. ALSO, FOUND LEFT EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE FOUND A WIRE SHORTED UNDER SEAT ROW 9, LEFT SIDE. REMOVED AND REPLACED LIGHT ASSEMBLY AT SEAT Aug 20, 2001 · N442US · Boeing 7374B7 · Emergency LightingSDR USAASB01235Charger · inoperativeBDL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 6, 7, 8 AND 9ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK NORMAL. (M)Aug 19, 2001 · N441US · Boeing 7374B7 · Emergency LightingSDR USAASB01236Light · inoperativePIT - PILOT REPORTED THAT THE EMERGENCY LIGHT AT OVERHEAD BIN 25D WAS BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Aug 19, 2001 · N780AU · Boeing 7374B7 · Emergency LightingSDR USAA011062Stringer · dentedCLT - FOUND STRINGER DENTED .5 INCH, STRINGER 16L STATION 400. FABRICATED REPAIR CHANNEL, STRINGER TIE CLIP PER EA 85178. (M)Aug 13, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011063Strap · damagedCLT - FOUND FRAME AND STRAP HAS DRILL DAMAGE .25 INCH, AFT FLANGE OF FRAME AND STRAP, BS 493 ABOVE BS 25R. INSTALLED DOUBLER AT FRAME AND STRAP PER SRM 53-00-07, SRM 51-70-11. (M)Aug 13, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAASB01229Sensor · failedCLT - FLT 1919 - AFTER TAKEOFF FROM CLT, EN ROUTE TO SJU, THE CAPTAIN REPORTED THE AIRCRAFT ACTED AS THOUGH THE FLIGHT/GROUND SWITCH WAS STUCK IN THE GROUND MODE. THE AIRCRAFT WOULD NOT PRESSURIZE AND THE TRANSPONDER AND AUTO THROTTLE WAS INOPERATIVE. NO CIRAug 12, 2001 · N782AU · Boeing 7374B7 · Landing Gear SystemSDR USAA011039Web · crackedCLT - FOUND WEB WITH SEVERAL CRACKED .75 TO .5 INCH, BS 178 WL 201 TO WL 213, LBL 5 TO LBL 6. INSTALLED DOUBLER PER EO 5300V153. (M)Aug 8, 2001 · N444US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011045Frame · crackedCLT - FOUND LEFT/RIGHT SIDE CHORD WITH APPROXIMATELY 1 INCH CRACK, BS 178, WL 207, RBL 27 AND LBL 27. SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)Aug 8, 2001 · N444US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010996Frame · dentedCLT - FOUND FRAME DENTED .5 INCH BY 1 INCH, BS 867 S24L. REPAIR DOUBLER INSTALLED PER TR 53-60-07. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010997Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 727D BETWEEN STRINGER 8/9L. REPAIR DOUBLER INSTALLED PER TR 53-10-14. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010998Floorbeam · corrodedCLT - FOUND T-CAP CORRODED .5 INCH BY .5 INCH, BS 986 RBL 16 RBL 40. T-CAP REPLACED PER TR 53-60-01. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010999Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH BY 30 INCHES, BS 312 AND BS 344. INSTALLED Z-ANGLE PER SRM 51-10-02. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA011000Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9 AT BS 867R. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011001Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 2 INCHES, BS 344 LBL 6 TO RBL 6. INSTALLED T-CAP PER SRM 53-10-51 SRM 51-40-02 SRM 51-40-00. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA011002SkinCLT - FOUND SKIN WITH BLENDED AREA 1.5 INCH BY .200 INCH BY .180 INCH, BS 440 FORWARD CARGO DOOR CUTOUT STRUCTURE. REWORK BLENDED AREA PER SRM 53-30-15. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011003Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 40 INCH, BS 312 LBL 28 TO RBL 22. REMOVED DAMAGED T-CAP AND INSTALLED A NEW SECTION PER BOEING 737-400 SRM 53-10-51. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA011005Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9 AT BS 907R. FRAME DOUBLER INSTALLED PER TR 53-10-14. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011006Skin · dentedCLT - FUOND SKIN DENTED 1 INCH BY 1.25 INCH BY .030 INCH, BS 927 STRINGER 21L. FILLERS AND DOUBLER INSTALLED PER SRM 51-20-01 SRM 53-00-01. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011007Angle · corrodedCLT - FOUND Z-ANGLE CORRODED .5 INCH BY .5 INCH, BS 960 BS 993 LBL 65. REPAIR AND REPLACE Z-ANGLE PER SRM 51-10-02. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA011010Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, BS 291 AND S12R. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-05. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA011011Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, BS 291 AND S12R. REMOVED AND REPLACED SUPPORT ANGLE PER 51-40-05. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA011012Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9R AT BS 727D. REPAIR DOUBLER INSTALLED PER TR 53-10-14. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011013Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGERS 8-9 AT BS 867L. REPAIR DOUBLER INSTALLED PER TR 53-10-14. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011014Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 616, RBL 64 INCHES, 8 INCHES BELOW FLOOR. INSTALLED FILLER AND STIFFENER ANGLE PER TR 53-62-01, HT J020-37-22. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011015Skin · dentedCLT - FOUND SKIN DENTED 2.5 INCH BY 1.5 INCH BY .080 INCH, BS 927 STRINGER 18L. INSTALLED DOUBLER PER SRM 53-00-01 SRM 53-60-01 EA NR 69903. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011016Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .35 INCH, BS 178, LBL 6.5, WL 212. DOUBLER INSTALLED PER EO 5300V153. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA011017Bulkhead · crackedCLT - FOUND PRESSURE WEB WITH NUMEROUS CRACKS RANGING FROM .250 INCH TO .600 INCH, BS 178 WL 188 TO 206, RBL 6.5 TO LBL 5. DAMAGED REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA011018Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGER 8-9R AT BS 947.5. INTALLED DOUBLER PER TR 53-10-14. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011019Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, INBOARD RIVET BETWEEN STRINGER 8-9L AT BS 827. REPAIR DOUBLER INSTALLED PER TR 53-10-14. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011020Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED APPROX 10 SQUARE INCHES, BS 947 RBL 5 TO LBL 14. DAMAGE REMOVED AND T-CAP REPLACED PER TR 53-60-02. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA011022SkinCLT - FOUND SKIN WITH 1 INCH CUTOUT, PREVIOUSLY INSTALLED DOUBLER, 7 INCHES BY 10 INCHES, BS 500B-500C, AT S22L 23L. PREVIOUSLY INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011004Skin · dentedCLT - FOUND SKIN DENTED 12.5 INCH BY 5 INCH, LEFT SIDE AT STATION 420 STRINGERS 15 THROUGH 17. INSTALLED DOUBLER PER SRM 53-00-01. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA011008Angle · crackedCLT - FOUND WEB ANGLE CRACKED 2 INCHES, BS 291.5 AND 9R. WEB ANGLE PART NR 65-45807-31 INSTALLED PER SRM 51-40-05. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA011009Angle · crackedCLT - FOUND WEB ANGLE CRACKED 2 INCHES, BS 291.5 AND 10R. REPLACED WITH ANGLE PART NR 65-45807-33 PER SRM 51-40-05. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA011021SkinCLT - FOUND SKIN WITH PREVIOUSLY INSTALLED REPAIR 1 INCH BY 4 INCH, STATION 1074 BETWEEN S17R AND S14R. PREVIOUSLY INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 210 SHEET 3. (M)Aug 7, 2001 · N449US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAASB01219Outflow Valve · stuckBWI - FLT 282 - ON CLIMB-OUT, THROUGH FL230, THE AIRCRAFT EXPERIENCED A RISE IN CABIN PRESSURE FOLLOWED BY THE ALTITUDE WARNING HORN. CREW WAS UNABLE TO CONTROL CABIN PRESSURE IN AUTO OR STANDBY MODE. CREW DESCENDED FLIGHT TO FL120 AND WAS ABLE TO CONTROL ALTIAug 2, 2001 · N780AU · Boeing 7374B7 · Pressure Regulator/Outflow ValveSDR USAA011069Frame · corrodedPIT - FOUND FRAME CORRODED 4 INCHES BY .500 INCHES CORRODED, FORWARD FUSELAGE DOOR FRAME BS 794 ABOVE S25R. CORROSION LEVEL 1, TASK NR C53-100-01. INSTALLED DOUBLER PER SRM 53-60-15 AND EA 71737. (M)Aug 1, 2001 · N441US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010953Bulkhead · crackedPIT - FOUND BULKHEAD WITH THREE CRACKS 1 INCH EACH, BS 178 LBL/RBL 6 INCHES BELOW WL 207 AND BL0 WL 184. CUT OUT DAMAGED AREAS, INSTALLED DOUBLER AND FILLERS PER EO 5300V153. (M)Jul 30, 2001 · N430US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010952Frame · crackedPIT - FOUND SIDE CHORD CRACKED 1.5 INCH, BS 178 LBL 24 WL 207. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER EO 5300V157. (M)Jul 30, 2001 · N430US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010954Frame · crackedPIT - FOUND SIDE CHORD CRACKED 2 INCHES, BS 178 RBL 24 WL 207. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER EO 5300V157. (M)Jul 30, 2001 · N430US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010950SkinPIT - FOUND SKIN WITH OVAL WEAR MARK, .071 INCH .375 INCH DIAMETER, RIGHT A/C BAY ABOVE ACM VALVE CENTER TANK LOWER SKIN. REAMED DAMAGE TO .25 INCH DIAMETER, INSTALLED FASTENER SAME SIZE AS HOLE PER EA 71719. (M)Jul 28, 2001 · N441US · Boeing 7374B7 · Fuselage Structure (General)SDR USAA010949ElevatorPIT - FOUND ELEVATOR HAS CARBON DELAMINATION, .040 INCH DEEP BY .25 INCH DIAMETER, BOTTOM SIDE OF ELEVATOR 52 INCHES FROM BOTTOM END. REPAIR PER SRM 55-20-1 AND 51-70-17 PER EA 71791. (M)Jul 25, 2001 · N441US · Boeing 7374B7 · Empennage StructureSDR USAASB01209Indicator · failedCLT - FLT 1528 - IN PREPARATION FOR LANDING AT CLT, FROM MIA, THE TRAILING EDGE FLAPS FAILED TO EXTEND WHEN SELECTED. THE LEADING EDGE DEVICES DID DEPLOY TO FULL EXTEND. THE FLAP POSITION INDICATOR SHOWED A SMALL SPLIT AT ONE UNIT AND THE TRAILING EDGE CIRCUJul 19, 2001 · N439US · Boeing 7374B7 · Flight Control SystemSDR USAASB01208Light · unsecureBWI - MAINTENANCE FOUND THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESECURED THE RIGHT FORWARD EXTERIOR EMERGENCY EXIT BULB INTO ASSEMBLY. OPS CHECK GOOD. (M)Jul 18, 2001 · N439US · Boeing 7374B7 · Emergency LightingSDR USAASB01201Seal · failedCLT - FLT 1157 - SHORTLY AFTER TAKEOFF FROM CLT, EN ROUTE TO PBI, THE CABIN DEPRESSURIZED AT ABOUT 4,500 FEET. AIR WAS REPORTEDLY LEAKING FROM THE FORWARD MAIN ENTRY DOOR. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO OXYGEN MASKS Jul 15, 2001 · N445US · Boeing 7374B7 · DoorsSDR USAA010796Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 24 INCH AREA, BS 344, LBL 12 TO RBL 12. DAMAGE REMOVED, REPLACED T-CAP SECTION PER SRM 53-10-51. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010795Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCH BY 90 INCH AREA, BS 987, DOOR TO DOOR. REMOVED AND REPLACED FLOORBEAM T-CAP PER TYPICAL REPAIR 53-60-01. (M)Jul 10, 2001 · N440US · Boeing 7374B7 · Fuselage Main, Floor Beam
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