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 USAA010242Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 827 FRAME RT SIDE BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TYP REP 53-10-14. (M)Feb 18, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010240Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 867 RIGHT SIDE BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TYP REP 53-10-14. (M)Feb 18, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAASB01050Arm · out of rigPHL - FLT 1484 - ON CLIMB-OUT FROM PHL, EN ROUTE TO BTV, THE AIRCRAFT WOULD NOT PRESSURIZE. THE FORWARD MAIN ENTRY DOOR DID NOT SEAL PROPERLY. CREW NOTED THAT NO DOOR INDICATION WAS GIVEN BEFORE TAKEOFF. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FUFeb 18, 2001 · N436US · Boeing 7374B7 · DoorsSDR USAA010279Frame · crackedCLT - FOUND SIDE CHORD .5 INCH, BS 178 LEFT SIDE CHORD WL 207. REMOVED DAMAGE AND SPLICED IN NEW CHORD PER EO 5300V157 PLUS EO 69141. (M)Feb 15, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010276Skin · crackedCLT - FOUND SKIN CRACKED .750 AND .250 INCH, STATION 10 RBL OF 0. INSTALLED REPAIR DOUBLER. (M)Feb 15, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA010273Angle · crackedCLT - FOUND ANGLE CRACKED 2 INCHES, STATION 298 LOWER FRAME DOOR INBOARD CORNER. INSTALLED DOUBLER. (M)Feb 15, 2001 · N435US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010272Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 400 BETWEEN STRINGER 8 AND 9 LEFT. FRAME REPAIR SRM 53-00-07. (M)Feb 15, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010251Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 36 INCHES, STATION 950-986 RBL 4, RT Z-ANGLE. BURNISH OUT CORROSION PRIME AND ALODINE PER SRM 51-10-02. (M)Feb 15, 2001 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010278Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 480 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. INSTALLED FRAME DOUBLER. (M)Feb 14, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010275Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 380 FRAME RIGHT SIDE STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Feb 14, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010274Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 440 RIGHT SIDE STRINGER 8R AND 9R. INSTALLED DOUBLER. (M)Feb 14, 2001 · N435US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010271Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH IN SEVERAL AREAS, STATINO 312, BL 0 RBL 12, LBL 7, 32, 39. REPLACED T-CAP. (M)Feb 13, 2001 · N435US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAASB01042Smoke Detector · malfunctionedTPA - FLT 589 - EN ROUTE FROM PHL-TPA, THE FORWARD CARGO COMPARTMENT FIRE LIGHT AND CAUTION ILGHTS ILLUMINATED FOR 60 SECONDS, THEN EXTINGUISHED. CREW DID NOT FIRE THE BOTTLES AS THE LIGHTS REMAINED EXTINGUISH. SYSTEM WAS ALREADY ON MEL FOR A CARGO FIRE PROTFeb 8, 2001 · N448US · Boeing 7374B7 · Smoke DetectionSDR USAA010128Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 20 INCHES, FLOORBEAM 986.5 UPPER CHORD FROM LBL 51 TO RBL 51. REMOVED AND REPLACED UPPER CHORD PER TR 53-60-01 A. (M)Feb 6, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010129Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 1 INCH, STATION 312, 15 INCHES LEFT OF CENTER. CORROSION LEVEL 2 C53-107-02. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)Feb 6, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010130Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 1 INCH, STATION 312, 7 INCHES LEFT CENTER. CORROSION LEVEL 2 C53-107-02. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)Feb 6, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010127Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 727F BETWEEN STRINGER 9L AND 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)Feb 6, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010126Frame · crackedCLT - FOUND FRAME .5 INCH, STATION 867 BETWEEN STRINGER 9L AND 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)Feb 6, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010110Stringer · corrodedCLT - FOUND STRINGER CORRODED .5 INCH BY 4 INCHES, BS 500F PLUS 13 INCHES TO 17 INCHES, STRINGER 26L OUTBOARD UPPER FLANGE. REPAIRED PER SRM 53-00-03. CORROSION LEVEL 1 C53-208-01. (M)Feb 5, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA010109Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 6 INCHES, STATION 344, BL 0 TO RBL 6. INSTALLED T-CAP PER 53-10-51 FIG 205. CORROSION LEVEL 1. (M)Feb 5, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010103Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, STATION 328, RBL 24-60. CORROSION LEVEL 1. REMOVED T-CAP AND INSTALLED NEW ONE PER SRM 53-10-51. (M)Jan 30, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010101Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 747 BETWEEN STRINGER 9L AND 8L. INSTALLED DOUBLER PER TR 53-10-14. (M)Jan 30, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010102Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 727D BETWEEN STRINGER 9R AND 8R. INSTALLED DOUBLER PER TR 53-10-14. (M)Jan 30, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010104Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 727B BETWEEN STRINGER 9R AND 8R. FABRICATED DOUBLER AND INSTALLED PER TR 53-10-14. (M)Jan 30, 2001 · N432US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010070Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED .5 INCH, STATION 947, LBL 4 TOP OF FLOORBEAM. INSTALLED NEW T-CAP SECTION PER SRM 53-00-51. (M)Jan 29, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010074Floorbeam · corrodedCLT - FOUND FLOORBEAM TOP CAP CORRODED .75 INCH BY .75 INCH, BS 967, RBL 29.5 AND RBL 30. INSTALLED REPAIR PARTS PER SRM 53-00-51 FIG 201 AND 202. (M)Jan 29, 2001 · N432US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010071Skin · crackedCLT - FOUND SKIN CRACKED .875 INCH, FS 215, 2 INCHES FORWARD FRONT SPAR OUTBOARD MID SPAR ATTACH FITTING. REPAIRED PER EA 69037. (M)Jan 29, 2001 · N432US · Boeing 7374B7 · Wing, Plate/SkinSDR USAA010072Skin · crackedCLT - FOUND SKIN CRACKED .75 INCH, LOWER LEFT WING SURFACE PYLON AFT ENGINE MOUNT OUTBOARD WBL 198. REPAIRED PER EA 69037. (M)Jan 29, 2001 · N432US · Boeing 7374B7 · Wing, Plate/SkinSDR USAA010073Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STRINGER 10R, STATION 663. REPLACED WITH NEW TIE CLIP PER SRM 51-10-02. (M)Jan 29, 2001 · N432US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAASB01023Iru · failedPHL - FLT 99 - EN ROUTE FROM PHL-SJU, THE NR 1 INERTIAL REFERENCE SYSTEM FAULT LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 INERTIAL REF UNIT. BJan 26, 2001 · N785AU · Boeing 7374B7 · Inertial Guidance SystemSDR USAA010065Angle · corrodedCLT - FOUND CHORD Z-ANGLE CORRODED 52 INCHES, RIGHT CREASE BEAM STATION 294.5 AFT OF 344 INNER CHORD. INSTALLED NEW SECTION PER SRM 51-10-02. (M)Jan 23, 2001 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010066Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 48 INCHES, CREASEBEAM STATION 312 TO 360 INNER CHORD. CORROSION LEVEL 1. INSTALLED NEW Z-ANGLE PER SRM 51-10-2. (M)Jan 23, 2001 · N434US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA010067Floorbeam · corrodedCLT - FOUND BEAM CHORD CORRODED 3 INCHES, FLOORBEAM 328 UPPER CHORD LBL 33 - RBL 65. INSTALLED REPAIR DOUBLER AND T-CAP PER SRM 53-10-54 FIG 205. (M)Jan 23, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010057Floorbeam · corrodedCLT - FOUND BEAM CHORD CORRODED 56 INCHES, FLOORBEAM 312, LBL 17.5 INCH TO RBL 11 INCH. NEW T-CAP SECTION INSTALLED PER SRM 53-10-51 AND 51-20-01. (M)Jan 22, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010058Floorbeam · corrodedCLT - FOUND CORROSION ON FLOORBEAM 1 INCH BY 1 INCH, STATION 344, LBL 12 - RBL 12 UPPER CHORD SURFACE. INSTALLED REPAIR PART AND ANGLES PER SRM 53-10-51 FIG 205. (M)Jan 22, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010055Bulkhead · crackedCLT - FOUND CRACKS IN WEB, .5 INCH, .25 INCH AND 1 INCH, STATION 178 BETWEEN LBL 7 AND RBL 7, WL 188 AND WL 201. INSTALLED DOUBLER PER SRM 53-10-08 FIG 211. (M)Jan 22, 2001 · N434US · Boeing 7374B7 · Fuselage Main, BulkheadSDR USAA010056Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED .5 INCH, STATIN 520, RBL 45 IN RADIUS UPPER CHORD/WEB. INSTALLED REPAIR PER SRM 53-00-51 FIG 201. (M)Jan 22, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010060Skin · crackedCLT - FOUND PYLON SKIN CRACKED .5 INCH, TOP OF NR 1 PYLON LOWER AFT CORNER PYLON PANEL 5727L. INSTALLED DOUBLER PER TR 54-30-07. (M)Jan 22, 2001 · N448US · Boeing 7374B7 · Nacelle/Pylon, Plate/SkinSDR USAA010050Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCH BY 4 INCH, TOP OF FLOORBEAM STATION 986.5, LBL 6-43. REPLACED FLOORBEAM PER TR 53-60-01. (M)Jan 16, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010049Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 2.25 INCH BY 27 INCHES, RT AFT SERVICE DOOR Z-ANGLE STATION 956-996, RBL 53. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. (M)Jan 16, 2001 · N434US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010033Pressure Panel · crackedCLT - FOUND SKIN CRACKED, LEFT MLG UPPER PRESS DECK BS 664, LBL 32, WL 203. INSTALLED DOUBLER PER TR 53-60-04. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, StructureSDR USAA010023Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 3 INCHES, AT 967, RBL 17 AND 31. CORROSION LEVEL 1. REPAIRED DOUBLER, TRIPLER AND FILLER PER SRM 53-30-51. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA010026Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 867 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010027Frame · crackedCLT - FOUND FRAME CRACKED .500 INCH, BS 867 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010028Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 827 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010029Frame · crackedCLT - FOUND FRAME CRACKED .50 INCH, BS 827 BETWEEN STRINGER 8 AND 9L. INSTALLED DOUBLER PER PER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010030Frame · crackedCLT - FOUND FRAME CRACKED, BS 727D BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010031Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 727D BETWEEN STRINGER 8R AND 9R. REINSTALLED OVERSIZED FASTENER PER SRM 51-40-03. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010032Frame · crackedCLT - FOUND FRAME CRACKED .500 INCH, BS 907 BETWEEN STRINGER 8R AND 9R AND 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14 AND SRM 53-00-07 FIG 202. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, FrameSDR USAA010034Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 380, BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Jan 15, 2001 · N434US · Boeing 7374B7 · Fuselage Main, Frame
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