Boeing 737-2X6C

Service difficulty reports · 1,351

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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 = '7372X6C'
  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 ASAA0210134Floorbeam · corrodedPAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 294, LEFT BUTTOCK LINE 20, RIGHT BUTTOCK LINE 60 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)May 28, 2002 · N746AS · Boeing 7372X6C · Fuselage Main, Floor BeamSDR ASAA0210133Beam · corrodedPAE - DURING SCHEDULED C-CHECK, FOUND CREASE BEAM WEB AT BS 332-344, RIGHT BUTTOCK LINE 61-64 CORRODED. REPAIRED CREASE BEAM WEB PER SRM. (M)May 27, 2002 · N746AS · Boeing 7372X6C · Fuselage Main, StructureSDR ASAA0210132Floorbeam · corrodedPAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 312, WATERLINE 208 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)May 26, 2002 · N746AS · Boeing 7372X6C · Fuselage Main, Floor BeamSDR ASAA0210131Stringer · corrodedPAE - DURING SCHEDULED C-CHECK, FOUND STRINGER 26R AT BS 536 CORRODED. REPAIRED STRINGER PER SRM. (M)May 20, 2002 · N746AS · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR ASAA0210130Floorbeam · corrodedPAE - DURING SCHEDULED C-CHECK, FOUND FLOORBEAM AT BS 1006, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M)May 18, 2002 · N746AS · Boeing 7372X6C · Fuselage Main, Floor BeamSDR TSAA0233135Battery Pack · dischargedREPLACED LEFT OVERWING IDENT EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.May 13, 2002 · N816AL · Boeing 7372X6C · Emergency LightingSDR TSAA0233118Battery Pack · dischargedREPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Apr 18, 2002 · N816AL · Boeing 7372X6C · Emergency LightingSDR ASAA0210077Receiver · inoperativeANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT SEAT PALLET 3-3 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT SEAT PALLET 3-3, THEN LIGHTS OPERATED NORMAL. (M)Apr 3, 2002 · N746AS · Boeing 7372X6C · Emergency LightingSDR TSAA0252092Guide · out of adjustFLT 46 - HNL-ITO - FORWARD ENTRY DOOR LIGHT CAME ON DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUSTED THE ROLLER GUIDE SERRATED PLATES AND GUIDE ARM. OPERATIONAL CHECKS WEREMar 27, 2002 · N816AL · Boeing 7372X6C · Passenger/Crew DoorsSDR TSAA0251083Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 26 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTEFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251066Bulkhead · corrodedREMOVED CORROSION AT 1016 SKIN BULKHEAD AND ATTACHING FRAME AFT SIDE OF BULKHEAD BETWEEN LBL 5 TO RBL 5 IAW SRM 53-10-1 FIGURE 1 DETAIL 16. CUT OUT ACCESS HOLE AFT OF BULKHEAD PER DRAWING 65C28106. DOUBLER AND FILLER COMPLETED IAW DRAWING 65C28106. CUT OUT Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, BulkheadSDR TSAA0251075Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 10 RT AT BS 500B PLUS 10 UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS AFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251076Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10, BS 4200 PLUS 10 AND BS 500 PLUS 10 ON WINDOW NR 1 RIGHT LOWER AFT CORNER. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251077Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 1 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRIFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251078Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S14R BS 360 PLUS 10 ON WINDOW NR 2 RIGHT UPPER FORWARD CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251079Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S14L BS 727 PLUS 10 ON WINDOW NR 20 LEFT LOWER FORWARD HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, QFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251080Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10L BS 827 PLUS 10 ON WINDOW NR 24 LEFT UPPER AFT HOLES NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251081Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS BETWEEN S10L BS 767 PLUS 10 AND BS 827 PLUS 10 ON WINDOW NR 25 LEFT UPPER AFT HOLES NR 10. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251082Skin · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R AND S14R ON WINDOW NR 24 RT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATED FILLERS, DOUBLER AND TFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0251067Floorbeam · corrodedFOUND CORROSION ON THE EXISTING UPPER FLANGE FLOORBEAM REPAIR AT STATION 1016, WL 208 BBI 0 TO LBL 15. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR TSAA0251069Keelbeam · corrodedFOUND CORROSION ON THE KEEL BEAM ON RIGHT LOWER FLANGE IN RIGHT AC BAY AT STATION 557 TO STATION 567, STATION 584 AND STATION 608. BLENDOUT THE CORROSION THEN FLAT PEENED IAW SOPM CHAPTER 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, KeelSDR TSAA0255063Spar · corrodedFOUND CORROSION ON LEFT REAR SPAR CHORD 6 INCHES UP FROM VERTICAL STABILIZER ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Vertical Stabilizer, Spar/RibSDR TSAA0255064Spar · corrodedFOUND CORROSION ON LEFT REAR SPAR CHORD 46 INCHES UP FROM VERTICAL STABILIZER FIN BETWEEN STATION 99.5 AND 108.7 ATTACH LUG. BLENDED OUT THE CORROSION AND INSTALLED TAPERED FILLERS. REPAIR ACCOMPLISHED IAW ECO 2509. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Vertical Stabilizer, Spar/RibSDR TSAA0251074Floor Support · corrodedIDENTIFIED CORROSION ON FLOOR SUPPORT DIAGONAL LEFT BETWEEN STATION 1006 AND STATION 1016 LBL 5. REMOVED CORROSION IAW SRM 53-10-1 DETAIL I, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR TSAA0251068Keelbeam · corrodedFOUND CORROSION ON THE KEEL BEAM LOWER CHORD. CONFIRMED CORROSION REMOVED AND NO EVIDENCE OF CRACKS USING HFEC METHOD. REPAIR COMPLETED IAW ECO 3269. AIRCRAFT RETURNED TO SERVICE. (M)Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, KeelSDR TSAA0251084Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S10R ON WINDOW NR 26 RIGHT LOWER FORWARD HOLE NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREA. FABRICFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251085Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R AND S14R ON WINDOW NR 26 RIGHT UPPER AFT HOLES NR 9 AND NR 10. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251086Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON S-10R BS 867 PLUS 10 ON WINDOW NR 29 RIGHT UPPER AFT HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED ARFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251087Window Frame · crackedPEFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS AT S-14R BS 420 ONWINDOW NR 4 RIGHT LOWER AFT CORNER HOLE NR 8. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS.Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251088Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 5 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251089Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATIONS ON WINDOW NR 6 RIGHT UPPER FORWARD CORNER HOLE NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. FABRICATFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251090Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION IAW ECO 3250R1. FOUND CRACK INDICATION ON WINDOW NR 8 RIGHT UPPER FORWARD CORNER HOLE NR 8 AND NR 9. TRIMMED OUT HOLES IN DAMAGED AREA TO .40 INCH AS INSURANCE CUT. HFEC INSPECTED EDGE OF THE TRIMMED AREAS. Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0251091Stringer · crackedFOUND CRACKES ON STRINGER 6L AND 7L FORWARD LAV SIDEWALL AREA. TRIMMED OUT DAMAGED PORTIONS OF INTERCOSTAL IAW SRM 51-40-3 FIGURE 1. VERIFIED NO FURTHER CRACKS USING HFEC METHODS AROUND THE TRIMMED OUT AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-Feb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR TSAA0251094Rib · crackedFOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CRACKS ON VARIOUS SUPPORT RIBS LISTED FROM INBOARD TO OUTBOARD NR 2, 3, 4, 5, 6, 7, AND 8. CUT AND REMOVED PORTIONS OF FORMED SECTIONS. FABRICATED REPAIR PARTS FROM .040 AND .050 INCH THICK 2024 T3. ASSEMBLFeb 26, 2002 · N816AL · Boeing 7372X6C · Horizontal Stabilizer, Spar/RibSDR TSAA0251095Stringer · damagedDAMAGED STRINGER BETWEEN FS 1040 AND FS 1064 STRINGER 27L. REMOVED DAMAGED SECTION IAW SRM 51-40-3 FIGURE 1. FABRICATED REPAIR DOUBLER USING .040 INCH THICK 2024 T3 IAW SRM 51-20-1 PAGES 10A TO 22. PROTECTED MATERIAL USING AN IRIDITE SOLUTION APPLICATION IAFeb 26, 2002 · N816AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR 2002F00409Battery · dischargedSEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT ROW 20, THEN LIGHTS OPERATED NORMAL. REF ASAA0210054. (M)Feb 21, 2002 · N746AS · Boeing 7372X6C · Emergency LightingSDR ASAA0210054Battery · dischargedSEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 20 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER AT ROW 20, THEN LIGHTS OPERATED NORMAL. (M)Feb 21, 2002 · N746AS · Boeing 7372X6C · Emergency LightingSDR ASAA0210053Battery · dischargedANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROWS 7 AND 8 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AT ROWS7 AND 8, THEN LIGHTS OPERATED NORMAL. (M)Feb 14, 2002 · N747AS · Boeing 7372X6C · Emergency LightingSDR TSAA0233044Battery Pack · inoperativeREPLACED NR 2 FLOOR PATH EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Feb 14, 2002 · N817AL · Boeing 7372X6C · Emergency LightingSDR ASAA0210049Light · inoperativeANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLET 7-4 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER, THEN LIGHTS TESTED NORMAL. (M)Feb 5, 2002 · N747AS · Boeing 7372X6C · Emergency LightingSDR ASAA0210008Bulkhead · crackedANC - DURING SCHEDULED MAINTENANCE, FOUND AFT PRESSURE BULKHEAD AT BS 1016, RBL 1 CRACKED. REPAIRED PER EA. (M)Jan 8, 2002 · N746AS · Boeing 7372X6C · Fuselage Main, BulkheadSDR TSAA0133171Battery Pack · dischargedREPLACED NR 2 FLOOR PROXIMATELY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 2, 2001 · N817AL · Boeing 7372X6C · Emergency LightingSDR TSAA0133170Battery Pack · dischargedREPLACED AFT ENTRY EMERGENCY IDENT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 1, 2001 · N816AL · Boeing 7372X6C · Emergency LightingSDR TSAA0153154Skin · corrodedDISCOVERED BULGING AT BS 1088, S-20R FUSELAGE SKIN. REMOVED THE CORRODED PORTION OF THE STRAP, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. RECEIVED 8110-3 APPROVAL. AIRCRAFT RETURNED TO SERVICE. (M)Nov 15, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA0153157Window Frame · crackedPERFORMED WINDOW CORNER FASTENER HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN NUMEROUS AREAS AT LT FUSELAGE WINDOW CORNERS; 2 BETWEEN BS 500-520 AND 33 BETWEEN BS 727-907, RT FUSELAGE WINDOW CORNERS; 8 BETWEEN BS 360-540 AND 1 AT BS 727A-727Nov 14, 2001 · N817AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA0157155Skin · corrodedDISCOVERED CORROSION ON LEFT LOWER WING SURFACE, WS 500. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)Nov 9, 2001 · N817AL · Boeing 7372X6C · Wing, Plate/SkinSDR TSAA0157156Skin · corrodedDISCOVERED CORROSION AT LEFT LOWER WING SURFACE, WS 515.5. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)Nov 7, 2001 · N817AL · Boeing 7372X6C · Wing, Plate/SkinSDR ASAA0110638Guide · out of adjANC - L1 DOOR DIFFICULT TO CLOSE. ADJUSTED GUIDE ARM, THEN OPS CHECKED GOOD. (M)Nov 6, 2001 · N746AS · Boeing 7372X6C · Passenger/Crew DoorsSDR ASAA0110636Connector · disconnectedSEA - OVERHEAD EMERGENCY EXIT SIGN AT ROW 20 DOES NOT ILLUMINATE. RECONNECTED CANNON PLUG, THEN OPS CHECKED GOOD. (M)Nov 5, 2001 · N746AS · Boeing 7372X6C · Light System WiringSDR ASAA0110637Hinge · lack of lubeANC - L1 DOOR DIFFICULT TO CLOSE. LUBED DOOR HINGE ATTACH POINTS, THEN OPS CHECKED GOOD. (M)Nov 5, 2001 · N746AS · Boeing 7372X6C · Passenger/Crew Doors
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