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 GTIA96NK141Frame · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y446 WITH CORROSION BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW 53-01, FIG 1. (M)Nov 5, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK140Longeron · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y446 AND Y465. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 5, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK138Frame · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y465 WITH CORROSION BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 5, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK137Frame · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y484 WITH CORROSION BETWEEN LONGERON 29 LEFT AND 29 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 5, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR GTIA96NK136Longeron · corrodedDURIGN C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y484 AND Y510. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 5, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK135Longeron · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 25 RIGHT WITH CORROSION BETWEEN Y503 AND Y522. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 5, 1995 · N941ML · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA96NK133Frame · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y503 WITH CORROSION BETWEEN LONGERON 28 RIGHT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M)Nov 5, 1995 · N941ML · Doug DC932 · Fuselage Main, FrameSDR CAL951034Skin · crackedIAH - INSPECTION FOUND A 1.5 INCH CRACK ON FUSELAGE SKIN ADJACENT TO THE LEFT AFT ATTACH ANGLE AT DORSAL FIN AREA. THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-04, FIGURE 27. (X)Nov 5, 1995 · N43537 · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA96NK131Fitting · crackedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT END FITTING, LONGERON 29 RIGHT WITH CRACK AND CORROSION IN Y996. REPLACED END FITTING IN LONGERON 20 RIGHT IAW SRM 51-01 PARA C AND 51-30-2, PART FABRICATED IAW SRM 51-10-2. (M)Nov 4, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL951016Downlock Sensor · inoperativeFLT NR 1100 - LEAVING IAH, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED, AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE RED LIGHT REMAINED ON WITH GEAR RETRACTED. WHEN THE GEAR WAS EXTENDED FOR RETURN TO IAH, INDICATIONS WERE NORMAL. THE NOSE GENov 3, 1995 · N69523 · Doug DC932 · Landing Gear Position and WarningSDR 9517389950Retract Mech · lack of lubeDURING CLIMB, AIRCRAFT EXPERIENCED A SLIGHT ROLL WHEN THE FLAPS WERE RETRACTED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. LUBRICATED FLAP SYSTEM AND OPERATIONAL CHECK GOOD.Nov 3, 1995 · N9346 · Doug DC932 · Trailing Edge Flap Control SystemSDR CA960103501Fuel Shutoff · seized(CAN)ON ENGINE SHUTDOWN, THE RIGHT ENGINE FUEL CONTROL LEVER WOULD NOT MOVE TO THE FUEL OFF POSITION. ENGINE WAS SHUTDOWN USING FIRE SHUT OFF HANDLE. SEVERAL MINUTES LATER THE FUEL SHUT OFF LEVER COULD BE MOVED EASILY. MAINTENANCE ACTION INVOLVED LUBRICATING Nov 2, 1995 · Doug DC932 · Fuel Controlling SystemSDR ABXA9600149Floorbeam · gougedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CABIN FLOORBEAM GOUGED ON THE LOWER FLANGE AT FS 389 BL 2 R. REPAIRED FLOORBEAM IAW ABX REA D953-12915-MR.Nov 2, 1995 · N989AX · Doug DC932 · Fuselage Main, Floor BeamSDR 95ZZZX6374Pressurization · malfunctionedATL/MEM - FLT 512 - CABIN PRESSURE LOST AT FL 240. CABIN ALTITUDE INCREASED TO OVER 15,000 FEET DURING EMERGENCY DESCENT. MASKS DEPLOYED, UNABLE TO CONTROL CABIN WITH MANUAL CONTROLLER. INSPECTED TAIL SECTION FOR BLOWN DUCTS, CHECKED OUTFLOW VALVE, PERFORMENov 2, 1995 · N901VJ · Doug DC932 · Cabin Pressure Control SystemSDR 9522089608Spar Cap · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING REAR SPAR UPPER 'T' CAP XRS 445 TO 454. REPAIRED 'T' CAP (P/N 5911300-1), PER EA 99-102931.Nov 2, 1995 · N608NW · Doug DC932 · Wing SparSDR 9517709610Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL LEFT TIE FITTING FS 37. REPLACED FITTING PER SRM 51-30-2.Nov 2, 1995 · N610NW · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9600173Vane · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FLAP FORWARD MOVEABLE VANE DELAMINATED. REPLACED IAW DC-9 MM 27-51-1.Nov 1, 1995 · N989AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9600172Intercostal · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN INTERCOSTAL BETWEEN LONGERONS 27L AND 28L CORRODED FROM FS 579 TO FS 598. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 1, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9517319604Battery Pack · dischargedDURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS AT ROWS 9 TO 12 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD.Nov 1, 1995 · N604NW · Doug DC932 · Emergency LightingSDR 9517309604Battery Pack · dischargedDURING LINE CHECK, THE TAIL CONE FLOODLIGHTING FAILED TEST. REPLACED THE NACELLE LIGHT BATTERY PACK, OPERATIONAL CHECK GOOD.Nov 1, 1995 · N604NW · Doug DC932 · Emergency LightingSDR 9517139991Relay · malfunctionedDURING CLIMB, THE GREEN NOSE GEAR LIGHT ILLUMINATED. CREW RECYCLED LANDING GEAR AND THE LIGHT REMAINED ILLUMINATED. ALSO, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR SWITCH S1-Nov 1, 1995 · N8957E · Doug DC932 · Landing Gear Position and WarningSDR 9517099604Battery Pack · dischargedDURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 5 TO 9. REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD.Nov 1, 1995 · N604NW · Doug DC932 · Emergency LightingSDR ABXA9600152Panel · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A SPLICED AREA OF THE UPPER WING TRAILING EDGE SKIN ON THE LEFT HAND WING HAD CORROSION ALONG SPLICE AND RIBS. REPAIRED LEFT WING TRAILING EDGE IAW ABX REA D957-12958-MR AND SERVICE REWORK DRAWING 5928669.Oct 31, 1995 · N989AX · Doug DC932 · Wing, Plate/SkinSDR ABXA9600080Doubler · crackedDURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, FOUND CRACKS AROUND FASTENER HOLES ON THE LEFT OVERHEAD EYEBROW WINDOW CORNER, LEFT SIDE DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 31, 1995 · N928AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9600079Doubler · crackedDURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, FOUND CRACKS AROUND FASTENER HOLES ON THE RIGHT OVERHEAD EYEBROW WINDOW CORNER, LEFT SIDE DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-5 AND 51-30-2.Oct 31, 1995 · N928AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9517149924Door · not closedDURING CLIMB, THE AIRCRAFT DID NOT PRESSURIZE. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. FOUND AFT CARGO DOOR OPEN, INSPECTED AND CLOSED DOOR. OPERATIONAL CHECK GOOD.Oct 31, 1995 · N926RC · Doug DC932 · Landing Gear Retraction/Extension SystemSDR ABXA9600181Skin · dentedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD FUSELAGE EXTERIOR SKIN DENTED FORWARD OF FS 427, BELOW LONGERON 28R. REPLACED SKIN SECTION IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5 AND ABX REA D953-13306.Oct 30, 1995 · N989AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9600150Skin · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A REPAIR ON THE RIGHT AFT FUSELAGE SKIN AT FS 935 AND LONGERON 15R HAD CRACKED. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12916-MR.Oct 30, 1995 · N989AX · Doug DC932 · Fuselage Main, Plate/SkinSDR 9517049987Compressor · stalledFLIGHT EXPERIENCED A COMPRESSOR STALL ON TAKEOFF ROLL (ENGINE POSITION UNDETERMINED). THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED BOTH ENGINES AND FOUND NO DISCREPANCIES. SUSPECT THIS EVENT WAS DUE TO SNOW AND SLUSH Oct 30, 1995 · N987US · Doug DC932 · Turbine Engine Compressor SectionSDR GTIA9700174Angle · crackedDTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y816 BETWEEN LONGERON 28 RT AND LONGERON 24 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M)Oct 28, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700173Angle · crackedDTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y 815 BETWEEN LONGERON 27 RT AND LONGERON 24 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M)Oct 28, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9700172Angle · crackedDTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y832 BETWEEN LONGERON 29 RT AND LONGERON 26 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M)Oct 28, 1995 · N941ML · Doug DC932 · Fuselage Miscellaneous StructureSDR CA951129523Duct · disconnected(CAN)PRESSURIZATION UNCONTROLLABLE GOING THROUGH FL200, EMERGENCY DESCENT CARRIED OUT. MAINTENANCE INVESTIGATION REVEALED DUCT CONNECTOR DISCONNECTED AT OUTLET OF LEFT AIR CYCLE MACHINE (ACM). DUCT CONNECT OR REINSTALLED.Oct 28, 1995 · Doug DC932 · Air Distribution SystemSDR 95ZZZX6373Coalescer Bag · dirtyDFW/ATL - FLT 224 - ON DESCENT INTO ATL, LOST PRESSURIZATION. OXYGEN MASKS DID NOT DROP DUE TO FLIGHT LEVEL. INSTALLED BOTH RIGHT AND LEFT AIR CYCLE MACHINE SUPPLY DUCTS, AND RIGHT AND LEFT COALESCER BAGS.Oct 28, 1995 · N918VV · Doug DC932 · Humidity Control SystemSDR 9522249610Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING TRAILING EDGE FLAP OUTBOARD AFT LOWER SPAR CAP STA 335. REPAIRED CAP (P/N 5912125-1) PER EA 12-5750-9-C0618.Oct 27, 1995 · N610NW · Doug DC932 · Trailing Edge FlapsSDR 9522079601Longeron · corrosionDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 30 AT FS 690. REPAIRED LONGERON (P/N 9915525-1), PER EA 12-5315-9-C0609.Oct 27, 1995 · N601NW · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9517249603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 12L END FITTING AT FS 1104 TO 1121. REPLACED THE END FITTING PER SRM 53-02 AND 51-30.Oct 27, 1995 · N603NW · Doug DC932 · Fuselage Miscellaneous StructureSDR 9517009918Retract Mech · lack of lubeON APPROACH DURING SLAT EXTENSION, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND A SLIGHT ROLL WAS EXPERIENCED BEFORE BOTH SLATS WERE FULLY EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED SLATS AND LUBRICATED SLAT ROLLERS. OPERATIONAL CHECK GOOD.Oct 27, 1995 · N940N · Doug DC932 · Leading Edge Slat Control SystemSDR 9516959920Door Warning · activatedDURING TAKEOFF ROLL IND-MEM AT APPROXIMATELY 20 KNOTS, THE AFT CABIN DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF WITHOUT FURTHER INCIDENT AND RETURNED TO THE GATE. DEFERRED REPAIR PER MEL 33-17A.Oct 27, 1995 · N942N · Doug DC932 · Door Warning SystemSDR 96ZZZX14Throttle · misriggedMAINTENANCE INSPECTION FOUND FUEL SHUT-OFF AND THROTTLE CONTROLS MISRIGGED.Oct 26, 1995 · N8270A · Doug DC932 · Power LeverSDR ABXA9600155Longeron · splicedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND WHILE REPLACING THE AFT PRESSURE BULKHEAD LOWER TEE SECTION AT FS 996, LONGERON 25L, HAD TO BE CUT AND REPAIRED. REPAIRED LONGERON IAW ABX REA D953-13040-MR.Oct 25, 1995 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9600132Blkhd Tee Cap · defectiveDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LOWER TEE CAP SECTION HAD TWO DRILL STARTS. REPLACED LOWER TEE CAP IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 25, 1995 · N989AX · Doug DC932 · Fuselage Main, BulkheadSDR 95ZZZX6372Window Heat Cntl · malfunctionedATL - FLT 919 - AIRCRAFT RETURN, ON THE CLIMB, OUT OF ATL AT 17,000 FEET, 300 KNOTS, THE FIRST OFFICER DISCOVERED FORWARD OUTER PANE WINDOW SPIDER-WEBBED. REFERENCE, OPERATOR CONTROL NR 95ZZZX6371.Oct 25, 1995 · N919VV · Doug DC932 · Windshield/Door Rain/Ice RemovalSDR 95ZZZX6371Windshield · failedATL - FLT 919 - AIRCRAFT RETURN, ON THE CLIMB-OUT OF ATL AT 17,000 FEET, 300 KNOTS, THE FIRST OFFICER DISCOVERED FORWARD OUTER PANE WINDOW SPIDER-WEBBED. REFERENCE, OPERATOR CONTROL NR 95ZZZX6372.Oct 25, 1995 · N919VV · Doug DC932 · Flight Compartment WindowsSDR CAL951020Skin · corrodedHOU - INSPECTION FOUND CORROSION ON SKIN AT STA 250 BELT FRAME, LONGERON 25L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. (X)Oct 24, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/SkinSDR CAL950991Fitting · corrodedHOU - INSPECTION FOUND INTERGRANULAR CORROSION AT BELTFRAME STATION 832, FITTING TO RIGHT CUSP. THE FITTING WAS REPLACED IAW SRM 51-30-0. (M)Oct 24, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9600138Jamb · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE APU CUTOUT FORWARD JAMB CRACKED IN THREE PLACES BETWEEN LONGERON 24L TO 24R. REPAIRED IAW ABX REA D953-13027. REINSTALLED JAMB IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 24, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 9522069608Frame · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 598 FRAME BETWEEN LONGERONS 19R TO 23R INBOARD FLANGE. REPAIRED FRAME (P/N 9919621-2), PER EA 99-102766.Oct 24, 1995 · N608NW · Doug DC932 · Fuselage Main, FrameSDR ABXA9600162Skin · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN EXISTING REPAIR ON THE FUSELAGE EXTERIOR SKIN AT FS 965 AND LONGERON 14L CRACKED. REPAIRED SKIN IAW ABX REA D953-13181-MR.Oct 23, 1995 · N989AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9600161Frame · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE CORROSION BLEND OUT AT LONGERON 29R AT FS 897 BEYOND LIMITS. REPAIRED FRAME IAW ABX REA D953-13169-MR.Oct 23, 1995 · N989AX · Doug DC932 · Fuselage Main, Frame
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