N93738, cancelled Apr 12, 2000

Service difficulty reports · 101

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N93738' AND deregistration_id = 'N93738-2000-04-12'
  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 CALA9802082Bearing · wornTHE NOSE GEAR DOORS OPEN LIGHT ON BOTH THE FORWARD AND SECOND OFFICER'S PANELS WERE ILLUMINATED AFTER GEAR RETRACTION DEPARTING BWI. THE WARNING LIGHTS WERE ACCOMPANIED BY RUMBLING AIR NOISE. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT WAS DIVERTED TO Nov 17, 1998 · N93738 · Boeing 727224 · Landing Gear Door Retract SectionSDR CALA9801933Floorbeam · corrodedFLOORBEAM TOP HAS SURFACE CORROSION FS 1130 RBL 12-12. REMOVED FASTENERS. CUT OUT ANGLE DAMAGE. FABRICATED NEW ANGLE, SPLICES. FABRICATED NEW FLOORBEAM TREATED AND INSTALLED PER SRM 51-10-2 AND 51-40-3.Oct 9, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801932Skin · wornRT WING NR 8 SPOILER CENTER CHAFE PAD WORN AND TE WORN/MISSING. DENTS OUT OF LIMITS PER SRM 57-50-1 FIG 5. REMOVED SPOILER PANEL AND SENT OUT FOR REPAIR PER MM 27-62-1.Oct 9, 1998 · N93738 · Boeing 727224 · SpoilersSDR CALA9801931Fitting · corrodedRIGHT WING TO FUSELAGE AT BS 870 FACE AND BORE HAVE CORROSION. ACCOMPLISHED REPAIR BY OVERSIZE HOLE TO REMOVE CORROSION PER ECRA 5310-63775.Oct 9, 1998 · N93738 · Boeing 727224 · Wing, Fuselage Attach FittingsSDR CALA9801929Fitting · corrodedINSPECTION FOUND THE NR 2 AND NR 3 FLAP TRACK FORWARD MOUNT FITTINGS CORRODED. THE FLAP TRACK FITTINGS WERE REPAIRED IAW ECRA 5740-01277.Oct 9, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801928Fitting · corrodedINSPECTION FOUND RT WING NR 6 AND NR 8 FLAP TRACK ATTACH FITTINGS CORRODED. THE CORROSION WAS REMOVED AND THE FITTINGS WERE REPAIRED IAW ECRA 5740-01277.Oct 9, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801912Bottle Pin · corrodedINSPECTION FOUND RT WING TO FUSELAGE BOTTLE PIN, BUSHING, AND RETAINING BOLT CORRODED AT BS 870. THE BOTTLE PIN, BUSHING, AND RETAINING BOLT WERE REMOVED AND REPLACED IAW MM 57-41-1, PAGE 403 AND 57-41-11, PAGE 404.Oct 5, 1998 · N93738 · Boeing 727224 · Wing, Fuselage Attach FittingsSDR CALA9801911Aileron Tab · dentedINSPECTION FOUND LT INBOARD AILERON TAB DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-31.Oct 5, 1998 · N93738 · Boeing 727224 · Aileron TabsSDR CALA9801809Skin · delaminatedINSPECTION FOUND RT INBOARD FOREFLAP SKIN DELAMINATED AT LOWER SURFACE INBOARD MOST END. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.Sep 18, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801795Skin · corrodedINSPECTION FOUND CORROSION IN LT ELEVATOR UPPER TRAILING EDGE SKIN BETWEEN STATIC WICKS. THE CORROSION WAS REMOVED, DOUBLERS WERE INSTALLED IAW SRM 55-20-03.Sep 16, 1998 · N93738 · Boeing 727224 · Elevator, Plate/SkinSDR CALA9801794Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 7 SPOILER. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4, FIGURE 10, 51-10-2 AND 51-30-2.Sep 16, 1998 · N93738 · Boeing 727224 · Wing, Plate/SkinSDR CALA9801793Fitting · corrodedINSPECTION FOUND FITTING CORRODED WHERE RT WING NR 5 FLAP TRACK MOUNTS. THE FITTING AND BUSHING WERE REMOVED AND REPLACED IAW MM 32-11-51, PAGE 401 TO 403 AND MM 20-70-7.Sep 16, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801792Channel · corrodedINSPECTION FOUND RT AFT LAV FLOOR WAS HAT CHANNEL CORRODED AT FS 1140, RBL 24 TO 60. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-2, 51-30-1, AND 51-20-1.Sep 16, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801780Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 348, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-10-5 AND 51-10-2.Sep 16, 1998 · N93738 · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801779Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AROUND MOUNT HOLES AT STA 400, RBL 30. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-8. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8.Sep 16, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801769Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER FORWARD RT DORSAL FIN ATTACH ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW EA 5340-01012.Sep 15, 1998 · N93738 · Boeing 727224 · Vertical StabilizerSDR CALA9801768Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK AT TOP FLANGE OF INTERCOSTAL THREE INCHES AFT OF FLOOR FRAME FS 970, BL 0. THE TOP FLANGE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2 AND 51-20-1.Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801767Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL AT FS 1120, BL 0. THE TOP FLANGE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-20-1 FIGURE 7.Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801766Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 683 TO 688. THE CORROSION WAS REMOVED IAW SRM 51-10-6. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3, FIGURE 6. A REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 6 AND 51-10-2.Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CALA9801765Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1034, RBL 12-24. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-00 AND 51-10-2.Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801745Panel · crackedINSPECTION FOUND A .375 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 12 SPOILER INBOARD HINGE AREA. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4 AND 51-30-2.Sep 14, 1998 · N93738 · Boeing 727224 · Wing, Plate/SkinSDR CALA9801744Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ANGLE AT RT INBOARD MIDFLAP JUST OUTBOARD OF NR 5 FLAP CARRIAGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801743Pad · corrodedINSPECTION FOUND CORROSION AT RT WING AFT FALSE SPAR PAD WHERE NR 5 AND NR 6 FLAP TRACKS MOUNT. THE FLAP TRACK MOUNT PADS WERE REMOVED IAW SRM 51-30-2. NEW MOUNT PADS WERE INSTALLED IAW SRM 51-10-6, 51-10-1, AND 51-30-2.Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801742Skin · corrodedINSPECTION FOUND LT ELEVATOR SKIN UPPER SURFACE CORRODED AROUND STATIC WICK BASE. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-20-03.Sep 14, 1998 · N93738 · Boeing 727224 · Elevator, Plate/SkinSDR CALA9801741Skin · crackedINSPECTION FOUND A .75 INCH AND .1093 INCH CRACK IN RT WING LOWER TRAILING EDGE OF INBOARD MIDFLAP, 34 INCHES FROM INBOARD END. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 57-50-4, FIGURE 1.Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801740Skin · crackedINSPECTION FOUND A .3125 INCH CRACK AT RT OUTBOARD FOREFLAP LOWER LEADING EDGE SKIN ABOVE NR 7 FLAP TRACK AREA, 54 INCHES FROM INBOARD END. A DOUBLER WAS INSTALLED IAW SRM 57-50-4, FIGURE 1, 51-10-6, AND 51-10-2.Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801739Channel · corrodedINSPECTION FOUND AFT LAV FLOOR HAT CHANNEL CORRODED AT FS 1140-1170, RBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2, PAGE 2, 51-10-2, AND 51-40-5.Sep 14, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801738Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN NR 2 SLAT PANEL ATTACH ANGLE BY ANTI-ICE DUCT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, FIGURE 4.Sep 14, 1998 · N93738 · Boeing 727224 · Leading Edge DevicesSDR CALA9801737Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN NR 3 SLAT LOWER ATTACH ANGLE FOR PANELS AT ACTUATOR ATTACH AREA. THE CRACK WAS ROUTED OUT. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-4, FIGURE 3.Sep 14, 1998 · N93738 · Boeing 727224 · Leading Edge DevicesSDR CALA9801736Track · corrodedINSPECTION FOUND NR 4 FLAP TRACK FORWARD CLEVIS CORRODED ON BOTH SIDES. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.Sep 14, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801705Angle · crackedINSPECTION FOUND A 4 INCH CRACK IN ANGLE AND DOUBLER AT RT WING FIXED LEADING EDGE RIB AT SLAT STA 0. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-40-3, FSep 10, 1998 · N93738 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9801704Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN BRACKET WHERE RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2.Sep 10, 1998 · N93738 · Boeing 727224 · Leading Edge Slat ActuatorSDR CALA9801703Doubler · crackedINSPECTION FOUND A .5 INCH CRACK IN DOUBLER INSIDE LT INBOARD FLAP AT AFT END OF INBOARD FLAP TRACK CARRIAGE SPINDLE CUTOUT. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-1 AND 51-30-2.Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801702Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT O/B MIDFLAP O/B END RIB FORWARD OF MID SPAR. THE CRACK WAS STOP DRILLED. A DOUBLER ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 4.Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801701Skin · dentedINSPECTION FOUND FUSELAGE SKIN AND RIB DENTED JUST AFT OF NLG AFT DOOR. THE RIB AND SKIN WERE REMOVED AND REPLACED IAW SRM 51-10-1.Sep 10, 1998 · N93738 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9801700Pad · corrodedINSPECTION FOUND BOTTOM SURFACE OF SPOILER BEAM PAD CORRODED WHERE NR 3 FLAP TRACK MOUNTS. THE FLAP TRACK MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-2, PAGE 1 AND 51-30-2, PAGE 14.Sep 10, 1998 · N93738 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9801699Track · corrodedINSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801695Track · corrodedINSPECTION FOUND RT WING NR 8 FLAP TRACK FORWARD ATTACH LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00.Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801694Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN OUTBOARD BRACKET WHERE RT WING NR 5 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge Flap ActuatorSDR CALA9801693Hat Channel · corrodedINSPECTION FOUND HAT CHANNEL CORRODED AT FS 1150, LBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.Sep 10, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801692Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 45-65. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2.Sep 10, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801691Skin · corrodedINSPECTION FOUND RT ELEVATOR SKIN LOWER SURFACE CORRODED. THE CORRODED AREA WAS CUT OUT AND A NEW FITTING AND DOUBLER WERE INSTALLED IAW SRM 55-20-3, FIGURE 2, PAGE 2, 51-10-2, AND 51-40-5.Sep 10, 1998 · N93738 · Boeing 727224 · Elevator, Plate/SkinSDR CALA9801690Carriage · corrodedINSPECTION FOUND NR 7 FLAP OUTBOARD FLAP INBOARD CARRIAGE CORRODED. THE FLAP CARRIAGE WAS REMOVED AND REPLACED IAW MM 57-53-2.Sep 10, 1998 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801679Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 22.5 TO 24.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-8 AND 51-30-2.Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801678Angle · crackedINSPECTION FOUND A .375 CRACK IN ANGLE AT INTERCOSTAL AT BS 950A-950B, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2.Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801677Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 1067, RBL 12-24 AND RBL 45-65. THE FLOOR SUPPORTS WERE REMOVED AND A NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-1AND 51-10-2.Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801676Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 24-45. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801675Web · corrodedINSPECTION FOUND RT WEB CORRODED AT FS 1122, RBL 65. THE CORRODED AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-2, 51-10-1, PAGE 4, AND 51-30-2.Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801674Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT TOP FLANGE SCREW HOLE FS 1050, RBL 35. THE CORRODED AREA WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 53-10-5, FIGURE 7.Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801673Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1140, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-10-1, AND 51-30-2.Sep 9, 1998 · N93738 · Boeing 727224 · Fuselage Miscellaneous Structure
Back to N93738, cancelled Apr 12, 2000