Boeing 727-224

Service difficulty reports · 2,252

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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 = '727224'
  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 MZZA98226Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT LBBL 24.75 AT BS 1130. THE CORRODED SEAT TRACK FROM BS 1110 TO BS 1136 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B727 SRM 53-10-5 FIGURESep 28, 1998 · N79743 · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR MZZA98222Doubler · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON RIGHT MAIN WHEEL WELL PRESSURE FLOOR REINFORCEMENT DOUBLER AT BS 901 RBBL 39. THE DAMAGED REINFORCEMENT DOUBLER, P/N 65-18745-421 WAS REMOVED AND REPLACED WITH NEW REINFORCEMENT DSep 28, 1998 · N79743 · Boeing 727224 · Fuselage Miscellaneous StructureSDR 98ZZZX4273Bracket · corrodedDURING C-CHECK, CORROSION WAS NOTED ON 3 EACH BRACKETS, ON ESCAPE SLIDE GIRT BAR FLOOR BRACKETS.Sep 28, 1998 · N69736 · Boeing 727224 · Emergency EquipmentSDR 98ZZZX4272Panel · corrodedDURING C-CHECK, CORROSION WAS NOTED ON EXTERIOR GROUND AIR CONNECTION PANEL.Sep 28, 1998 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR 98ZZZX4169Antenna · corrodedDURING C-CHECK, CORROSION NOTED ON FORWARD ADF LOOP ANTENNA.Sep 28, 1998 · N69736 · Boeing 727224 · Automatic Direction Finder (ADF) SystemSDR 98ZZZX4168Angle · corrodedDURING C-CHECK, CORROSION WAS NOTED ON FRAME STRUCTURE AROUND ADF LOOP ANTENNA BL ZERO - FS 720 APPROXIMATE.Sep 28, 1998 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR 98ZZZX4167Antenna · corrodedDURING C-CHECK, CORROSION WAS NOTED, AFT DME ANTENNA.Sep 28, 1998 · N69736 · Boeing 727224 · DME/TACAN SystemSDR MZZA98259Splice · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP L/E INTERIOR SPLICE PLATE AT WBL 122. THE CORRODED SPLICE PLATE WAS REMOVED AND REPLACED WITH NEW SPLICE PLATE MADE FROM 2024-T3 CLAD SHEET. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98256Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RIGHT WING T/E INBOARD MID FLAP T/E UPPER SKIN AT WBL 80 AND WBL 90. THE DAMAGED SKIN 25.125 INCH BY 2.65 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98255Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT WING T/E INBOARD MID FLAP REAR SPAR LOWER CHORD AFT FLANGE AT WBL 87. THE CORRODED MID FLAP REAR SPAR LOWER CHORD AFT FLANGE 1.375 INCH BY 6.625 INCH WAS TRIMMED OUT Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98247Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASI, CORROSION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP NOSE UPPER SKIN AT WBL 123. THE CORRODED SKIN 1.5 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 57-50-4 FIGURE 2. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98246Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP T/E UPPER SKIN AT WBL 122 AND BETWEEN WBL 129 AND WBL 184. THE DAMAGED SKIN 86.5 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRMSep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98245Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP T/E UPPER SKIN AT WBL 83. THE DAMAGED SKIN 13 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98244Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD AFT FLAP T/E UPPER SKIN AT WBL 105 AND WBL 118. THE DAMAGED SKIN 36 INCH BY 1.8 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98243Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E AFT FLAP LOWER SKIN AT WBL 232. THE DAMAGED SKIN 4 INCH 10.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98242Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E OUTBOARD AFT FLAP T/E UPPER SKIN AT WBL 348. THE DAMAGED SKIN 18 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98241Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E OUTBOARD AFT FLAP UPPER SKIN AT INBOARD AFT CORNER. THE DAMAGED SKIN 3.5 INCH BY 3.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 27, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98225Channel · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON RT AFT LAVATORY INBOARD WALL PARTITION LOWER SUPPORT HAT CHANNEL. THE CORRODED HAT CHANNEL, P/N 65-19606-254 WAS REMOVED AND REPLACED WITH NEW HAT CHANNEL. (M)Sep 26, 1998 · N79743 · Boeing 727224 · Fuselage Miscellaneous StructureSDR MZZA98260Web · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .625 INCH LONG CRACK WAS FOUND ON NR 6 SLAT INTERIOR FORWARD WEB AT SS 156. THE CRACK END WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. (M)Sep 25, 1998 · N79743 · Boeing 727224 · Leading Edge DevicesSDR MZZA98258Stiffener · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT MAIN W/W INBOARD WALL STIFFENER AT BS 933. THE CORRODED STIFFENER WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-4. (M)Sep 25, 1998 · N79743 · Boeing 727224 · Fuselage Miscellaneous StructureSDR MZZA98257Stiffener · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT MAIN W/W INBOARD ALL STIFFENER AT BS 918. THE CORRODED STIFFENER 3 INCH LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-4. (M)Sep 25, 1998 · N79743 · Boeing 727224 · Fuselage Miscellaneous StructureSDR MZZA98254Skin · disbondedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DISBONDED WAS FOUND ON RT WING T/E INBOARD FORE FLAP UPPER SKIN EXISTING FIBERGLASS REPAIR DOUBLER. THE DAMAGED SKIN 13 INCHES BY 1.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 25, 1998 · N79743 · Boeing 727224 · Leading Edge DevicesSDR MZZA98253Beam · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON RT MLG SUPPORT BEAM LOWER SURFACE ATTACH TO INBOARD TRACK AT WBL 127. THE MLG SUPPORT BEAM WAS BLEND OUT REPAIRED PER CMI E/RA NR 5740-01864 DATED OCT 26, 1998. (M)Sep 25, 1998 · N79743 · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR MZZA98239Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP UPPER SKIN AT WBL 72. THE DAMAGED SKIN 7.125 INCH BY 5.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 25, 1998 · N79743 · Boeing 727224 · Leading Edge DevicesSDR MZZA98238Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E OUTBOARD FORE FLAP T/E LOWER SKIN AT WBL 485. THE DAMAGED SKIN 2.5 INCH BY 2.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 25, 1998 · N79743 · Boeing 727224 · Leading Edge DevicesSDR MZZA98252Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 11 SPOILER UPPER SKIN AT WBL 317 AND WBL 327. THE DAMAGED SKIN 18 INCH BY 7 INCH AND 9 INCH DIAMETER WERE TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 24, 1998 · N79743 · Boeing 727224 · SpoilersSDR MZZA9825Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RIGHT WING T/E INBOARD AFT FLAP LOWER SKIN AT WBL 97. THE DAMAGED SKIN 12.5 INCH BY 3.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)Sep 23, 1998 · N79743 · Boeing 727224 · Trailing Edge FlapsSDR MZZA98224Frame · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON R1 SERVICE DOOR LOWER SILL INBOARD CHORD (Z-CHANNEL) UPPER SURFACE BETWEEN BS 300 AND BS 356. THE CORRODED INBOARD CHORD WAS CORROSION CLEANUP AND REPAIRED PER B727 SRM 51-10-06 ASep 23, 1998 · N79743 · Boeing 727224 · Fuselage Main, FrameSDR CALA9801961Battery · dischargedAFT GALLEY OVERHEAD EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY.Sep 19, 1998 · N79750 · Boeing 727224 · Emergency LightingSDR 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 Devices
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