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 CALA9700816Skin · crackedINSPECTION FOUND A 2 INCH CRACK AND TWO .5 INCH CRACKS IN LT FUSELAGE SKIN AT STA 58 TWELVE INCHES BELOW CUSP LINE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4.May 14, 1997 · N33506 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9700814Skin · crackedINSPECTION FOUND A .625 INCH CRACK IN LT FUSELAGE SKIN AT STA 69 TWO FEET BELOW CUSP LINE. REPAIRED IAW SRM 53-01, FIGURE 4.May 14, 1997 · N33506 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9700812Skin · crackedINSPECTION FOUND THREE .25 INCH CRACKS FROM TWO RIVETS IN LT FUSELAGE SKIN AT STA 63 TEN INCHES BELOW CUSP LINE. THE CRACKED AREAS WERE CUT OUT, A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38.May 14, 1997 · N33506 · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9700998Uplatch Mech · lack of lubeAFTER TAKEOFF, RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR, NO CHANGE, FOLLOWED BY THE GEAR DOOR OPEN LIGHT ILLUMINATING. TURNED ON THE RIGHT HYDRAULIC PUMP AND THE GEAR DOOR OPEN LIGHT WENT OUT WITH THE GEAR UNSAFE LIGHMay 14, 1997 · N980AX · Doug DC932 · Landing Gear Retraction/Extension SystemSDR 9711749604Frame · corrodedDURING L-CHECK, FOUND CRACK IN AFT VENTRAL STAIR DOOR JAMB AT UPPER RIGHT DOOR STOP. REPAIRED PER EA 96112919.May 14, 1997 · N604NW · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97377Boost Pump · failedCIRCUIT BREAK POPPED LT FUEL PUMP RT MN TANK DEPLETING LT AND CNT TANKS. DIVERTED TO ALB, COULD NOT RESET LT PUMP. MAINT REMOVED AND REPLACED LT AFT BOOST PUMP, RT GEN VOLT REG.May 13, 1997 · N205ME · Doug DC932 · Fuel Boost PumpSDR GTIA9700305Mic Jack · shortedMYR - FLT 182 - LOSS OF BOTH RADIOS WHILE SITTING ON END OF RUNWAY FOR TAKEOFF. AFTER TAXI BACK TO RAMP AND DURING ENGINE SHUT DOWN, RADIOS STARTED WORKING NORMALLY. INSPECTED COMM SYSTEMS AND FOUND FAULTY MIC JACK (SHORTED INTERNALLY) AT OB'S POSITION. REMMay 13, 1997 · N947ML · Doug DC932 · Audio Integrating SystemSDR CALA9700810Clip · brokenTHE EXTERIOR TAIL CONE RELEASE HANDLE PULLED OUT OF CLIPS AT TEN POUNDS AND 80 POUNDS WAS REQUIRED TO RELEASE TAIL CONE USING EXTERIOR HANDLE. A BROKEN CLIP ON RELEASE HANDLE WAS REPLACED, TIMING BLOCKS WERE ADJUSTED, AND TAIL CONE LATCHES WERE LUBRICATED.May 13, 1997 · N33506 · Doug DC932 · Aerodynamic FairingsSDR 9710149950Battery Pack · dischargedDURING PREFLIGHT CHECK, FLASHLIGHT WAS NOT BLINKING. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.May 13, 1997 · N9346 · Doug DC932 · Emergency LightingSDR 9709649950Battery Pack · dischargedDURING PREFLIGHT CHECK, FLASHLIGHT WAS NOT BLINKING. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.May 13, 1997 · N9346 · Doug DC932 · Emergency LightingSDR 9709459623Casting · corrodedDURING 'M' CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THREE REAR SPAR TO KEEL BEAM CASTINGS FS 699. REPLACED CASTINGS PER SRM 51-30-05.May 11, 1997 · N623NW · Doug DC932 · Fuselage Miscellaneous StructureSDR 9709349922Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.May 11, 1997 · N945N · Doug DC932 · Emergency LightingSDR 9709319621Wire · failedNOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR LOCK/UPLOCK CONDUIT HARNESS ASSEMBLY, OPERATIONAL CHECK NORMAL ON GEAR SWING.May 11, 1997 · N621NW · Doug DC932 · Landing Gear System WiringSDR ABXA9700990Floorbeam · corrodedDURING C-CHECK, FOUND THE FLOORBEAM AFT LOWER FLANGE HEAVILY CORRODED AT F/STA 965 AND LBL 10. REPAIRED IAW ABX REA D953-19401-MR.May 10, 1997 · N986AX · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA97373Window · crackedDURING SERV CHK, FOUND CRACKS IN STEEL DOUB AND RETAIN IN RT AND LT WINDOW. MAINT REPAIRED IAW DAC DRWG 5754688, 5952965 AND ME EO1-56-003.May 9, 1997 · N502ME · Doug DC932 · Flight Compartment WindowsSDR MWEA97372Skin · misrepairedDURING D CHECK, STA 177-187 LONG 23L-25L FUSE SKIN IMPROPER PREVIOUS REPAIR. MAINTENANCE REPAIRED IAW SRM 53-04 FIG 12B SHT 4.May 9, 1997 · N216ME · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9700995Power Supply · defectiveDURING SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 MM.May 9, 1997 · N904AX · Doug DC932 · Emergency LightingSDR ABXA9700989Floorbeam · corrodedDURING C-CHECK, FOUND THE FLOORBEAM AT F/STA 965, LBL 47 LOWER FLANGE HEAVILY CORRODED. REPAIRED IAW ABX REA D953-19407-MR.May 9, 1997 · N986AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9700988Frame · crackedDURING C-CHECK, FOUND LT FUSELAGE FRAME AT F/STA 617, LONGERON 14L CRACKED. REPAIRED FRAME IAW ABX REA D53-19396-MR.May 9, 1997 · N986AX · Doug DC932 · Fuselage Main, FrameSDR ABXA9700981Control Cable · corrodedDURING C-CHECK, FOUND THE LANDING GEAR CONTROL CABLES HEAVY RUSTED INSIDE THE PULLEY JUST ABOVE THE LANDING CONTROL VALVE. REPLACED CABLE RUN 102A IAW DC9 MM 32-31-0.May 7, 1997 · N986AX · Doug DC932 · Landing Gear Retraction/Extension SystemSDR ABXA9700980Control Cable · corrodedDURING C-CHECK, FOUND THE EMERGENCY FUEL SHUTOFF CABLE INSIDE THE PULLEY JUST BELOW THE PRESSURE FAIRLEAD IN TOP OF LT WHEEL WELL HEAVILY RUSTED. REPLACED CABLE RUN 140C IAW DC9 MM 76-20-0.May 7, 1997 · N986AX · Doug DC932 · Engine Emergency Shutdown SystemSDR ABXA9700979Control Cable · corrodedDURING C-CHECK, FOUND THE EMERGENCY FUEL SHUTOFF CABLE INSIDE THE FORWARD PULLEY JUST BELOW THE PRESSURE FAIRLEAD IN TOP OF RT WHEEL WELL HEAVILY RUSTED. REPLACED CABLE RUN 149C IAW DC9 MM 75-20.May 7, 1997 · N986AX · Doug DC932 · Engine Emergency Shutdown SystemSDR ABXA9700978Hinge Fitting · crackedDURING C-CHECK, FOUND THE LT HINGE FITTING F/STA 1059 FOR AFT VENTRAL DOOR CRACKED. REMOVED AND REPLACED HINGE FITTING IAW DC9 SRM 51-30-1 AND 52-63-00.May 7, 1997 · N986AX · Doug DC932 · Entrance StairsSDR ABXA9700977Skin · corrodedDURING C-CHECK, FOUND THE FUSELAGE SKIN UNDER THE RT STATIC PORT PLATE CORRODED. REMOVED CORROSION AND REPAIRED SKIN IAW DC9 SRM 51-30-2 AND 51-30-5.May 7, 1997 · N986AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9700976Seat Track · corrodedDURING C-CHECK, FOUND SEAT TRACK CORRODED AT F/STA 200 RBL 44. REPLACED SEAT TRACK IAW DC9 SRM 51-30-1, 51-30-5, AND 51-30-4.May 7, 1997 · N986AX · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9700975Skin · corrodedDURING C-CHECK, FOUND THE FUSELAGE SKIN UNDER THE LT STATIC PORTED PLATE CORRODED. FABRICATED INTERNAL DOUBLER (P/N 5920419-3) AND REPAIRED IAW ABX REA D953-19365.May 7, 1997 · N986AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9700974Angle · crackedDURING C-CHECK, FOUND A CRACKED INTERCOSTAL ATTACH ANGLE CRACKED AT F/STA 237 BETWEEN LONGERONS 27R AND 28R. REPLACED CRACKED INTERCOSTAL ATTACH ANGLE IAW DC9 SRM 51-30-5.May 7, 1997 · N986AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9700971Angle · crackedDURING C-CHECK, FOUND NR 1 PYLON LOWER OUTBOARD ANGLE CRACKED FORWARD OF AFT ENGINE MOUNT. REPAIRED IAW ABX REA D954-19336.May 7, 1997 · N986AX · Doug DC932 · Nacelle/Pylon StructureSDR 9709189940Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK NORMAL.May 7, 1997 · N3322L · Doug DC932 · Emergency LightingSDR CA970603014Controller · inoperative(CAN) AT FLIGHT LEVEL 350 EXPERIENCED RAPID DECOMPRESSION, FLIGHT DESCENDED UNDER MANUAL AND REGAINED CONTROL AT FL260. MANUALLY DEPLOYED OXYGEN MASKS. TRIED AUTO PRESSURIZATION AGAIN, NO LUCK. MAINTENANCE CHANGED #2 PRESSURIZATION CONTROLLER AND SYSTEM CHECKEMay 6, 1997 · Doug DC932 · Cabin Pressure ControllerSDR VJ970235Anti-Skid Contl · malfunctionedLT ANTI-SKID LIGHT CAME ON AS TAKEOFF ROLL COMMENCED. ABORTED TAKEOFF PRIOR TO 60 KNOTS, RETURNED TO GATE. REPLACED ANTI-SKID CONTROL BOX PER MM 32-00, CHECKED GOOD WITH SELF TEST.May 5, 1997 · N932VV · Doug DC932 · Brake Anti-Skid SectionSDR MWEA97364Skin · puncturePILOT REPORTS, ON WALKAROUND IN MKE FOUND SMALL PUNCTURE IN SKIN LEFT SIDE JUST FWD OF GROUND FLOOD LIGHT. CAUSE IS UNKNOWN. MTC INSTALLED INTERNAL DOUBLER REPAIR IAW SRM 53-04 FIG 38.May 5, 1997 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA97363Rib · corrodedDURING D-CHECK, RT WING LEAD EDGE RIB VERT WEB STA XIS335 CORRODED. MAINT REMOVED AND REPLACED IAW SRM 51-30.May 5, 1997 · N216ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA97362Spar · corrodedDURING D-CHECK, STA XHR 205 TO 198 FWD RT HORIZ STAB AFT SPAR UP CAP CORRODED. MAINT REPAIRED IAW DAC TELEX SVC-MSP-0293/CB, SRM 55-02.May 5, 1997 · N216ME · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR MWEA97361Longeron · damagedDURING D-CHECK, IMPROP PREVIOUS REPAIR LONG L17L STA 965. MAINT REMOVED AND REPLACED IAW SRM 53-02.May 5, 1997 · N216ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA97360Rib · damagedDURING D-CHECK, TEMP REPAIRS LT WING NOSE RIB STA XIS83. MAINT REMOVED AND REPLACED IAW SRM 57-01 PAGE 1.May 5, 1997 · N216ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA97359Seat Track · corrosionDURING D-CHECK, STA 200 TO 237 NR 2 SEAT TRACK LWR SURF UP FLANG CORRODED. MAINT REPAIRED IAW SRM 53-05 FIG 4D AND INSTALLED IAW SRM 51-30.May 5, 1997 · N216ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA97358Door Jamb · damagedDURING D-CHECK, HEAVY CHAFE MARK ON AFT VENT DOOR JAMB LT LWR LOCK PIN. MAINT REPAIRED IAW SRM 53-05 FIG 69 SHTS 1 AND 2.May 5, 1997 · N216ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA97357Frame · damagedDURING D-CHECK, IMPROP PREVIOUS REPAIR RT FRAME STA 980 L17R. MAINT REPAIRED IAW SRM 53-03 FIG 32.May 5, 1997 · N216ME · Doug DC932 · Fuselage Main, FrameSDR MWEA97356Frame · damagedDURING D-CHECK, IMPROPER PREVIOUS REPAIR ON LT FRAME STA 980 L17L. MAINT REPAIRED IAW SRM 53-03 FIG 32.May 5, 1997 · N216ME · Doug DC932 · Fuselage Main, FrameSDR MWEA97355Longeron · damagedDURING D-CHECK, FOUND PREVIOUS REPAIR ON LONG STA 965 L17R. MAINT REPAIRED IAW SRM 53-02 FIG 2.May 5, 1997 · N216ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700713Longeron · crackedINSPECTION FOUND FOUR .25 INCH CRACKS IN LONGERON 17L BETWEEN STA 965 AND 980. A NEW LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 2.May 5, 1997 · N12507 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700712Shear Clip · crackedINSPECTION FOUND A .25 INCH CRACK IN SHEAR CLIP AT STA 980, LONGERON 14L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-03.May 5, 1997 · N12507 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700711Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN ANGLE AT STA 964, LONGERON 16L. THE ANGLE WAS REPLACED IAW SRM 51-10-4.May 5, 1997 · N12507 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700710Longeron · crackedINSPECTION FOUND A .25 INCH CRACK IN LONGERON 16R AT STA 965. A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.May 5, 1997 · N12507 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700709Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN ANGLE AT STA 945, LONGERON 15R. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.May 5, 1997 · N12507 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9700708Longeron · crackedINSPECTION FOUND A .25 INCH CRACK IN LONGERON 17R AT STA 965. A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.May 5, 1997 · N12507 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9700707Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN ANGLE AT STA 964, LONGERON 17R. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-0.May 5, 1997 · N12507 · Doug DC932 · Fuselage Miscellaneous StructureSDR 9709159941Rmi · malfunctionedLOSS OF NR 1 RMI AND FIRST OFFICER'S COMPASS OCCURRED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. REPLACED NR 1 DIRECTIONAL GYRO AND NR 1 RMI AS A PRECAUTION.May 5, 1997 · N3324L · Doug DC932 · Visual Omnirange (VOR) SystemSDR VJ970234Slide Cover · not securedEMERGENCY SLIDE PACK ON GALLEY DOOR NOT SECURE. RESECURED R1 DOOR SLIDE COVER PER MM 25-60.May 4, 1997 · N935VV · Doug DC932 · Emergency Equipment
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