Douglas DC-9-32

Service difficulty reports · 12,755

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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 = 'DC932'
  ORDER BY difficulty_date DESC"

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SDR CALA9801134Web · corrodedINSPECTION FOUND LAV FLOOR WEB CORRODED BETWEEN STA 980 AND 996 AT RBL 59. THE WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Jun 19, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801133Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT RT WING REFUELING STATION. THE CRACK WAS ROUTED OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5730-01564.Jun 19, 1998 · N12538 · Doug DC932 · Wing Miscellaneous StructureSDR TWAA9810806Doubler · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DOUBLER AT RBL 58, FLOOR LINE, CORRODED AT STA 929 TO STA 945. REMOVED CORROSION PER 51-10-03, PARA 30 TO PARA 42. REPAIRED PER SRM 53-01, PG 9. INSTALLED NEW DOUBLER. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. Jun 18, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9810609Skin · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT SEVENTH FASTENER ABOVE LAP SEAM, LONGERON 14, AT FS 1076 ABOVE RT ENGINE PYLON. CRACK IN BEYOND STOP DRILL, UNDER PREVIOUS REPAIR. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 53-04, FIG 18. (M)Jun 18, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9810608Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND SUPPORT ANGLE TO FRONT SPAR CRACKED AT BULKHEAD STATION 604, BETWEEN LONGERON 23R AND 24R. REPLACED CRACKED SUPPORT ANGLE, PER SRM 51-01 PAGE 1, ITEM C, AND INSTALLED FASTENERS PER SRM 51-30-2. (M)Jun 18, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9810607Fasteners · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STATION 700, LEFT SIDE, BOTTOM AND TOP FORWARD FASTENERS ON INNER STRINGER FRAME THAT HOLDS WINDOW INNER SEAL SPACER RUBBER, CRACKED. INNER FRAME REMOVED AND NEW FRAME INSTALLED PER SRM 51-01, PAGE 1 ITEM C. (M)Jun 18, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98753Battery Pack · dischargedBOTH TAIL COMPARTMENT EMERGENCY LIGHTS ARE INOP. MTC REMOVED AND REPLACED BATTERY PACK.Jun 18, 1998 · N215ME · Doug DC932 · Emergency LightingSDR MWEA98748Doublers · mismanufacturedFOUND FWD AND AFT ADF LOOP ANTENNA DOUBLER NOT TO CURRENT SRM STANDARDS. MTC FABRICATED AND INSTALLED NEW DOUBLERS.Jun 18, 1998 · N501ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98747Hinge · wornFOUND CONSIDERABLE FWD AND AFT PLAY ON RIGHT HAND FLYING DOOR. MTC REPLACED WORN HINGE BUSHING ON BOTH HINGE HALVES.Jun 18, 1998 · N501ME · Doug DC932 · Landing Gear DoorsSDR CALA9801125Skin · crackedINSPECTION FOUND A 1/2 CRACK AT FASTENER HOLE OF FUSELAGE SKIN AT AFT CABIN LT SIDE STA 980 ABOVE LONGERON 15L. THE CRACKED AREA OF SKIN WAS CUT OUT. A FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 32 AND 51-10-38.Jun 18, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800195Slide · detachedGALLEY DOOR SLIDE NEEDS REINSTALLING. RESECURED SLIDE IAW MM, PERFORMED REQUIRED INSPECTIONS.Jun 17, 1998 · N916VV · Doug DC932 · Emergency EquipmentSDR TWAA9810605Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION TOP SIDE OF FLOORBEAM, STATION 996 RBL 22 IN TO RBL 50 INCH. REPLACED ANGLE PER SRM 51-01 AND STD PRACTICES. (M)Jun 17, 1998 · N998R · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9810604Bulkhead · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND TIE ANGLE FOR FLOORBEAM, FORMER RING AND PRESSURE BULKHEAD CRACKED AT STATION 996, RBL 58.6 INCHES. VERIFIED BY NDT. REPLACED TIE PALTE PER SRM 51-01 AND STD PRACTICES. (M)Jun 17, 1998 · N998R · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9801606Skin · crackedMCI - DURIN GOP 16 MAINTENANCE CHECK, FOUND LEFT WING TE FIXED UPPER WING PANEL CRACKED AT REAR SPAR, JUST FORWARD AND INBOARD OF INBOARD SPOILER. ACCOMP HFEC CRACK CONTAINMENT PER TWA NDT PART 6 AND 51-00-03. STOP DRILLED END OF CRACK PER SRM 57-01 AND INSTJun 17, 1998 · N995Z · Doug DC932 · Wing, Plate/SkinSDR MWEA98750Cover · detachedTHE GALLEY SLIDE AND COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE AND COVER.Jun 17, 1998 · N209ME · Doug DC932 · Emergency EquipmentSDR MWEA98742Slide · fell offTHE EMERGENCY GALLEY SLIDE FELL OFF. MTC REPAIRED LOOSE RIVET AND REATTACHED GALLEY SLIDE COVER.Jun 17, 1998 · N502ME · Doug DC932 · Emergency EquipmentSDR CALA9801137Panel · corrodedINSPECTION FOUND RT WING NR 3 FLAP LEADING EDGE PANEL CRACKED AND CORRODED AT XFLS 283. THE CORROSION WAS REMOVED AND THE AREA WAS REPAIRED IAW SRM 51-30-2 AND 51-70-2.Jun 17, 1998 · N12538 · Doug DC932 · Leading Edge DevicesSDR CALA9801136Panel · delaminatedINSPECTION FOUND LT FLAP LEADING EDGE PANEL NR 3 DELAMINATED AT XFL 267. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-70-2.Jun 17, 1998 · N12538 · Doug DC932 · Leading Edge DevicesSDR CALA9801135Floor · corrodedINSPECTION FOUND FLOOR PANEL IN FORWARD PIT CORRODED AND DELAMINATED AT STA 378 TO 279. A NEW PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.Jun 17, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801122Skin · corrodedINSPECTION FOUND LT TRAILING EDGE INBOARD FLAP INTERIOR CORRODED AND FINGER DOUBLERS SEPARATED. THE T/E FLAP SKIN WAS REMOVED. NEW SKIN AND BONDED DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-50-9, FIGURE 6, 51-70-2, AND 51-30-2.Jun 17, 1998 · N12538 · Doug DC932 · Trailing Edge FlapsSDR CALA9801121Pan · crackedINSPECTION FOUND A 1/2 CRACK AT AFT END OF BEAM NR 3 FASTENER LOCATION OF AFT CARGO COMPARTMENT DOOR OUTER PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5261C-01000.Jun 17, 1998 · N12538 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9801120Web · corrodedINSPECTION FOUND FORWARD CARGO DOOR INNER WEB CORRODED. THE CORROSION WAS REMOVED AND REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 52-01, 51-10-3, AND 52-30-0.Jun 17, 1998 · N12538 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9801119Pan · crackedINSPECTION FOUND A 0.7 CRACK AT FORWARD END OF BEAM NR 2 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 8.Jun 17, 1998 · N12538 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9801118Floorboard · delaminatedINSPECTION FOUND CABIN FLOORBOARD NR 41 DELAMINATED AT LT SIDE FS 389-465. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-05, 53-21-0, 51-30-2, 51-10-3, 51-70-2, AND 51-20-0.Jun 17, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801117Angle · crackedINSPECTION FOUND THREE CRACKED ANGLES ON RT SIDE OF AFT ENTRY DOOR. THE DOOR SKIN AND ANGLES WERE REMOVED. NEW ANGLES WERE AND DOOR SKIN WERE INSTALLED IAW SRM 51-10-4 AND 51-30-2.Jun 17, 1998 · N12538 · Doug DC932 · Passenger/Crew DoorsSDR VJ9800194Battery Pack · dischargedAFT OVERWING EMERGENCY LIGHTS INOP. REPLACED AFT OVERWING EMERGENCY LIGHT BATTERY PACK IAW MM 33-50.Jun 16, 1998 · N914VV · Doug DC932 · Emergency LightingSDR TWAA9809811Spar · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING INBD TE FLAP HINGE CASTING ATTACH HOLES WITH .75 INCH LONG CRACK INDICATION ON SPAR WEB AT LOWER INBD MOUNT HOLE. INSTALLED REPAIR DOUBLER PER JO 6027 REAR SPAR REPAIR DRAWING. TOTAL TIME: 72,210 HOURS. TJun 16, 1998 · N995Z · Doug DC932 · Trailing Edge FlapsSDR TWAA9809810Frame · bentMCI - DURING OP 16 MAINTENANCE CHECK FOUND STA 544 FORMER RING FOOT BENT BEYOND LIMITS, BETWEEN LONGERONS 28R AND 29R. REPLACED FORMER FOOT PER SRM 53-03, FIG 3 AND SRM 53-04, FIG 38. TOTAL TIME: 72,210 HOURS. TOTAL CYCLES: 84,221. (X)Jun 16, 1998 · N998R · Doug DC932 · Fuselage Main, FrameSDR TWAA9809809Seat Track · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BLENDED BEYOND LIMITS AT STA 200, RBL 22, FLOOR TRACK. REPLACED CORRODED TRACK SECTION PER SRM 51-01, PG 1 ITEM C. STA 200 TO STA 265. TOTAL TIME: 77,783. TOTAL CYCLES: 84,471. (X)Jun 16, 1998 · N998R · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9809807Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 13R CRACKED AT STA 965. CUT AND REMOVED LONGERON FROM JUST AFT OF WINDOW BELT TO STA 972, APPROXIMATELY, TO REMOVE DAMAGED AREA. REPLACED SECTION PER SRM 51-01, PAGE 1 ITEM 6, AND REPAIRED AT SPLICE PER SRJun 16, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98741Slide · detachedTHE GALLEY SERVICE DOOR SLIDE FELL OUT OF DOOR. MTC REINSTALLED SLIDE.Jun 16, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR MWEA98737Skin · damagedLEFT WING LEADING EDGE HAS A PIECE OF SKIN BROKEN OUT BY NUMBER 3 SLAT TRACK CUTOUT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Plate/SkinSDR MWEA98736Skin · damagedDURING MTC HOLES WHERE MISDRILLED ON THE RIGHT HAND WING LOWER SKIN AT STATION XRS 164 BY STRINGER 11R AND 12R. REMOVED DAMAGE AND FABRICATED AND INSTALLED REPAIR BUSHINGS USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Plate/SkinSDR MWEA98735Rib · corrosionCORROSION WAS FOUND ON LT WING INTERNAL RIB AT STATION XRS 164 ON THE LOWER HORIZONTAL FLANGES. REMOVED CORROSION AND INSTALLED REPAIR STRAP USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA98734Stringer · corrosionLEFT WING STRINGER NUMBER 14 HAS BEEN FOUND CORRODED FROM XRS 111 TO XRS 137. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR USING APPROVED USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA98733Stringer · corrosionLEFT WING STRINGER 11 HAS A BLEND OUT AT STATION XRS 79. FABRICATED AND INSTALLED A REPAIR USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA98732Stringer · damagedLEFT WING STRINGER 22 HAS A BLEND OUT AT STATION XRS 73. FABRICATED AND INSTALLED REPAIR STRAP USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA98731Rib · corrosionLEFT WING RIB AT STATION XRS 69 HAS CORROSION ON LOWER RIB CAP. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA98730Stringer · corrodedLEFT WING STRINGER 18 HAS NUMEROUS AREAS CORROSION BETWEEN STA XCW 58.5 TO 69 SOME BLEND OUTS BEYOND LIMITS. INSTALLED ANGLE REPAIR ON LOWER FLANGE OF STRINGER 18 REPAIR IS TEMPORARY FOR 1 GEAR PENDING BOEING DTA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA98729Stringer · damagedLEFT WING STRINGER 22 WAS FOUND CORRODED ON UPPER FORWARD AND AFT LEGS FROM XCW 58 TO XRS 69. REMOVED CORROSION AND FABRICATED AND INSTALLED REPAIR USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA98728Stringer · damagedLEFT WING STRINGER 19 WAS FOUND CORRODED ON UPPER FWD AND AFT LEGS FROM XCW 58 TO XRS 69 0. REMOVED CORROSION AND INSTALLED REPAIRS USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA98727Stringer · corrosionRIGHT WING STRINGER NUMBER 23 HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR STRAPS USING APPROVED DATA FROM XCW 58.5 TO XRS 69.Jun 16, 1998 · N215ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA98726Pan · gougedTHE RIGHT HAND AFT OVERWING EMERGENCY EXIT LOWER PAN WAS FOUND GOUGED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98725Skin · corrodedTHE FUSELAGE SKIN FROM FUSELAGE STATION 588 TO STATION 667 WAS FOUND CORRODED. REMOVED AND REPLACED SKIN USING APPROVED DATA.Jun 16, 1998 · N215ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98724Doubler · corrodedFORWARD CARGO DOOR LOWER CUTOUT DOUBLER AREA HAS CORROSION BLEND OUTS BEYOND LIMITS. INSTALLED INTERIOR TITANIUM DOUBLER REPAIR IAW SRM.Jun 16, 1998 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801124Angle · crackedINSPECTION FOUND A 1.25 CRACK IN L-ANGLE FOR AFT ENTRY DOOR. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REPAIR PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-2A.Jun 16, 1998 · N12538 · Doug DC932 · Passenger/Crew DoorsSDR CALA9801115Pan · crackedINSPECTION FOUND A .25 INCH CRACK AT FORWARD END OF THE BEAM NR 3 DOOR STOP CUTOUT OF AFT CARGO COMPARTMENT DOOR OUTER PAN. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 3.Jun 16, 1998 · N12538 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9801114Fairing · crackedINSPECTION FOUND AFT INBOARD SIDE OF LT WHEEL WELL FORWARD FAIRING CRACKED. THE CRACK WAS STOP DRILLED, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2.Jun 16, 1998 · N12538 · Doug DC932 · Aerodynamic FairingsSDR CALA9801113Floorboard · corrodedINSPECTION FOUND CORROSION AROUND SCREW HOLES OF CABIN FLOORBOARD PANEL NR 44. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-21-0, AND 51-70-2.Jun 16, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801112Skin · corrodedINSPECTION FOUND SKIN CORRODED AT STA 937, LONGERON 20L. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02673.Jun 16, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/Skin
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