Douglas DC-9-31

Service difficulty reports · 7,433

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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 = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR 9513699994Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE FORWARD CARGO DOOR LOWER FITTINGS, FORWARD AND AFT. REPLACED FITTINGS PER SRM 51-30-2.Aug 31, 1995 · N8978E · Doug DC931 · Cargo/Baggage DoorsSDR 9513539963Fuel Heat Valve · malfunctionedNR 2 ENGINE FUEL HEAT SYSTEM CYCLED ON INTERMITTENTLY WHILE SELECTED OFF. OIL TEMPERATURE EXCEEDED NORMAL LIMITS AND A PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED. THE FLIGHT RETURNED TO MEM LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL HEAT VAAug 31, 1995 · N913RW · Doug DC931 · Fuel HeaterSDR 9513399908Door Switch · malfunctionedDURING APPROACH INTO PIT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EMERGENCY GEAR EXTENSION PROCEDURES WERE ACCOMPLISHED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOOR SWITCH AND ADJUSTED LEFT DOOR SWITCH. REPLAAug 30, 1995 · N958N · Doug DC931 · Landing Gear Position and WarningSDR 9513499953Hinge · corrodedDURING H-CHECK, FOUND CORROSION IN THE NR 3 FORWARD FLAP HINGE STUD HOLES. REPLACED HINGE PER CITEXT 09-5740-1-9800.Aug 28, 1995 · N918RW · Doug DC931 · Trailing Edge FlapsSDR 9513489946Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT T-CAP TIE FITTING, FS 604 AT LONGERON 30. REPLACED FITTING PER SRM 51-01.Aug 28, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9513479998Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE LONGERON 29R AND 30 END FITTINGS AT FS 579. REPLACED FITTINGS PER SRM 51-10-3.Aug 28, 1995 · N8934E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9513289953Fittings · corrodedDURING H-CHECK, FOUND CORROSION ON FRAME FITTINGS FORWARD AND AFT OF THE GALLEY SERVICE DOOR FS 168 AND FS 200. REPLACED FITTINGS PER SRM 51-10-04.Aug 26, 1995 · N918RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9513059965Fuel Heat Vlv · malfunctionedNR 1 ENGINE FUEL HEAT INDICATOR ILLUMINATED IN CRUISE. THE ENGINE OIL TEMPERATURE EXCEEDED RECOMMENDED LIMITS, A PRECAUTIONARY SHUTDOWN WAS ACCOMPLISHED AND THE FLIGHT DIVERTED TO TYS LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL HEAT VALVE, INSPECAug 26, 1995 · N911RW · Doug DC931 · Engine Fuel DistributionSDR 9513249968Skin · crackedDURING A-CHECK, FOUND A 7 INCH CRACK IN THE LEFT INBOARD SPOILER LOWER SKIN. REPLACED SPOILER. MFG. P/N 5910055-515.Aug 25, 1995 · N9332 · Doug DC931 · SpoilersSDR 9513089906Dnlock Switch · malfunctionedON APPROACH INTO DTW, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED AND FLAPS AT 25 DEGREES. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND EMERGENCY EQUIPMENT WAS CALLED TO MEET FLIGHT ON LANDING AS A PRECAUTION. AIRCRAFT LANDED Aug 25, 1995 · N956N · Doug DC931 · Landing Gear Position and WarningSDR 95ZZZX5150Engine · failedCLE - FLT 384 - DURING DESCENT, SHUT DOWN NR 2 ENGINE, SN 2161, DUE TO LOW OIL PRESSURE LIGHT ILLUMINATION AND DECREASING OIL QUANTITY. FOUND OIL LEAK AT NR 1 BEARING AND METAL PARTICLES IN OIL SCREEN. CHANGED NR 2 ENGINE. ENGINE OPERATION CHECKED NORMAL. Aug 24, 1995 · N976Z · Doug DC931 · Engine (Turbine/Turboprop)SDR 9513129910Brake · seizedLEFT BRAKE SEIZED ON LANDING INTO EWR. AIRCRAFT CLEARED RUNWAY, BUT WAS UNABLE TO TAXI FORWARD. AIRCRAFT WAS TOWED TO THE GATE. FOUND BINDING IN NR 1 BRAKE ASSEMBLY AND REPLACED BRAKE. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE.Aug 24, 1995 · N960N · Doug DC931 · BrakeSDR 9513019946Skin · crackedDURING ACCEPTANCE CHECK, FOUND SKIN CRACKED BETWEEN FS 148 AND 150, LONGERON 27L. FABRICATED DOUBLER AND INSTALLED PER EA 99-102752 AND SRM 53-04 FIG 8.Aug 22, 1995 · N8926E · Doug DC931 · Fuselage Main, Plate/SkinSDR 9512999991Stringer · crackedDURING ACCEPTANCE CHECK, FOUND LONGERON 15L TO FRAME ATTACHMENT STRAP CRACKED AT FS 207. FABRICATED FILLER AND DOUBLER AND INSTALLED PER EA 99-094137.Aug 21, 1995 · N8957E · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9512989991Press Panel · crackedDURING ACCEPTANCE CHECK, FOUND COCKPIT PRESSURE PANEL CRACKED AT FS 83. FABRICATED DOUBLER AND INSTALLED PER EA 99-102726.Aug 21, 1995 · N8957E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9512979994Skin · damagedDURING ACCEPTANCE CHECK, FOUND RIGHT PYLON TRAILING EDGE SECTION LOWER SKIN TO SECOND RIB WITH ELEVEN LOOSE FASTENERS AT END OF RIB. REPAIRED LOWER SKIN SECTION PER EA 99-094743 AND SRM 51-30-2.Aug 21, 1995 · N8979E · Doug DC931 · Nacelle/Pylon, Plate/SkinSDR CAL950732Receptacle · burnedFLT NR 1579 - FLL - THE CREW REPORTED AN ODOR IN MID CABIN PRIOR TO LANDING AT FLL. MAINTENANCE FOUND PSU RECEPTACLE BETWEEN ROW 12-14 RT BURNED. THE RECEPTACLE AND PSU WERE REMOVED AND REPLACED. THE READING LIGHTS, CALL SWITCH, AND PASSENGER WARNING SIGNS Aug 18, 1995 · N14564 · Doug DC931 · Passenger Compartment EquipmentSDR 9513239998Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 4 BEAM AFT END FITTING. REPLACED FITTING.Aug 18, 1995 · N8934E · Doug DC931 · Cargo/Baggage DoorsSDR 9512769966Anticipator · malfunctionedLEFT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED WHEN POWER WAS APPLIED AT START OF TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED ANTICIPATOR AND THERMOSTAT, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Aug 18, 1995 · N9330 · Doug DC931 · Cabin Temperature Control SystemSDR USAA950900Tire · failedPIT - FLT 1637 - ON TAKEOFF, THE LEFT MAIN OUTBOARD TIRE BLEW. MOST OF THE TIRE WAS INGESTED INTO THE LEFT ENGINE. ON APPROACH BACK TO PIT, THE CREW RECEIVED A GEAR UNSAFE LIGHT. THE CAPTAIN DID A MISSED APPROACH AND CYCLED THE GEAR. WITH THE UNSAFE LIGHT Aug 17, 1995 · N937VJ · Doug DC931 · TireSDR 9513229969Frame · crackedDURING H-CHECK, FOUND A CRACK IN THE LEFT FORWARD OVERWING EMERGENCY EXIT DOOR PAN. REPAIRED PAN (P/N 5913195-1) PER EA 99-97116.Aug 17, 1995 · N9333 · Doug DC931 · Emergency ExitsSDR 9512959969Door Pan · crackedDURING H-CHECK, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT DOOR PAN CRACKED AT TOP EDGE FORWARD SUPPORT AREA. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBLER AND WEB PER EA 99-09711.Aug 17, 1995 · N9333 · Doug DC931 · Emergency ExitsSDR 9512949991Skin · damagedDURING ACCEPTANCE CHECK, FOUND SKIN DAMAGE AT PRESSURE CAP AT UPPER PYLON SPAR CAP FS 965 RIGHT SIDE. REPAIRED PYLON SPAR CAP PER EA 99-1102703.Aug 17, 1995 · N8957E · Doug DC931 · Fuselage Main, Plate/SkinSDR 9512939998Door Pan · crackedDURING H-CHECK, FOUND LEFT AFT FORWARD EMERGENCY EXIT DOOR PAN CRACKED AT LOWER FORWARD STOP. REPLACED DOOR, MFG PART NUMBER 5910159-31.Aug 17, 1995 · N8934E · Doug DC931 · Emergency ExitsSDR 9512929998Door Pan · crackedDURING H-CHECK, FOUND RIGHT FORWARD EMERGENCY EXIT DOOR PAN CRACKED AT UPPER FORWARD STOP. REPLACED DOOR, MFG PART NUMBER 5910159-31.Aug 17, 1995 · N8934E · Doug DC931 · Emergency ExitsSDR 9512919998Door Pan · crackedDURING H-CHECK, FOUND RIGHT AFT EMERGENCY EXIT DOOR PAN CRACKED AT LOWER FORWARD END. REPLACED DOOR, MFG PART NUMBER 5910159-31.Aug 17, 1995 · N8934E · Doug DC931 · Emergency ExitsSDR 9512909998Door Pan · crackedDURING H-CHECK, FOUND LEFT FORWARD EMERGENCY EXIT DOOR PAN CRACKED AT UPPER AFT STOP. REPLACED DOOR, MFG PART NUMBER 5910159-31.Aug 17, 1995 · N8934E · Doug DC931 · Emergency ExitsSDR 9512719955Dir Gyro · malfunctionedFIRST OFFICER'S COMPASS FLAG APPEARED DURING CLIMBOUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NR 2 DIRECTIONAL GYRO AND RMI. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.Aug 17, 1995 · N922RW · Doug DC931 · Directional Gyro and Indicating SystemSDR 9512779989Duct · disconnectedLOSS OF CABIN PRESSURIZATION OCCURRED AT 29,000 FEET, CABIN ALTITUDE CLIMBED TO 11,000 FEET. INITIATED EMERGENCY DESCENT PROCEDURES AND PRESSURE WAS REGAINED AT 17,000 FEET. CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. OXYGEN MASKS DID NOT DEPLOY. Aug 16, 1995 · N8945E · Doug DC931 · Cabin Pressure Control SystemSDR 9513099908Retract Mech · dirtyNOSE LANDING GEAR DOOR DID NOT CLOSE ON GEAR RETRACTION, RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO IND AND LANDED WITHOUT INCIDENT. INSPECTED AND RELATCHED RIGHT NOSE GEAR DOOR, CLEANED DEBRIS FROM BUNGEE CYLINDER. OPERATIONAL CHECK OK, AIRCRAFT RETURNEAug 15, 1995 · N958N · Doug DC931 · Landing Gear Door Retract SectionSDR 9512669903Tq Ind · malfunctionedTHE NR 2 N1 INDICATOR FAILED ON TAKEOFF ROLL, THE TAKEOFF WAS ABORTED. THE N1 INDICATOR WAS PLACED ON MEL AND THE FLIGHT RESUMED ITS SCHEDULED ROUTE. SUBSEQUENT REPLACEMENT OF THE INDICATOR RESTORED NORMAL SYSTEM OPERATION.Aug 15, 1995 · N953N · Doug DC931 · Engine BMEP/Torque IndicatingSDR 9512519978Emergency Exit · wornDURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE RIGHT FORWARD OVERWING EMERGENCY EXIT. REPLACED THE DOOR.Aug 14, 1995 · N9342 · Doug DC931 · Emergency ExitsSDR 9512239912Fuel Heat Valve · malfunctionedNR 1 ENGINE FUEL HEAT VALVE OPENED IN FLIGHT AND COULD NOT BE CLOSED WITH NORMAL PROCEDURES. THE ENGINE OIL TEMPERATURE EXCEEDED RECOMMENDED LIMITS, THE COM PROCEDURES WERE FOLLOWED AND A PRECAUTIONARY SHUTDOWN WAS ACCOMPLISHED. FLIGHT DIVERTED TO DTW AND LAAug 13, 1995 · N961N · Doug DC931 · Engine Fuel DistributionSDR 9512489969Blkhd Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE FS 756 BULKHEAD TO RIGHT KEEL ATTACH FITTING. REPLACED FITTING PER SRM 51-30-5.Aug 11, 1995 · N9333 · Doug DC931 · Fuselage Main, BulkheadSDR 9512259978Release Mech · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS. ALSO, FOUND THAT THE UPPER LATCHES RELEASED PRIOR TO THE LOWER LATCHES AND THAT THE TAILCONE FAILED TO DROP. ADJUSTED TAILCONE PER MM 53-50-3, FUNCTIONAL CHECK OK.Aug 11, 1995 · N9342 · Doug DC931 · Aerodynamic FairingsSDR 9512469946Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 25L END FITTING AT FS 110. REPLACED FITTING PER SRM 51-01.Aug 10, 1995 · N8926E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9512279978Emergency Exit · out of adjustDURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE LEFT AFT OVERWING EMERGENCY EXIT. RERIGGED DOOR PER MM 52-21-0, CHECKED OK.Aug 10, 1995 · N9342 · Doug DC931 · Emergency ExitsSDR 9512459969Fitting · crackedDURING H-CHECK, FOUND CORROSION ON THE FS 160 FITTING FORWARD OF THE GALLEY SERVICE DOOR. REPLACED FITTING PER SRM 51-30-5.Aug 9, 1995 · N9333 · Doug DC931 · Fuselage Miscellaneous StructureSDR 9512429969Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE FORWARD GALLEY SERVICE DOOR LOWER BEAM FORWARD END. REPAIRED BEAM AND REPLACED THE FITTING (P/N 3953686-1) PER SRM 52-05, FIG.25.Aug 8, 1995 · N9333 · Doug DC931 · Galley DoorsSDR 9511839928Uplock Switch · malfunctionedDURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO YYC AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN GEAR UPLOCK SWITCH. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE.Aug 4, 1995 · N8921E · Doug DC931 · Landing Gear Position and WarningSDR 95ZZZX5146Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STA 945 TO STA 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, SRM 51-30-2, AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 67,006 HOURS; 73,957 CYCLES.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM532Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES. TOTAL CYCLES 73,957.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM531Seat Track · corrodedSTL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4. TOTAL CYCLES 73,957.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZM456Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM455Longeron · corrodedSTL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 95ZZZM447Seat Track · corrodedSTL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4.Aug 2, 1995 · N988Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR 9512039969Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR NR 4 AND NR 5 BEAMS FORWARD END FITTINGS. REPLACED FITTINGS PER SRM 51-30-5 PG 1.Aug 2, 1995 · N9333 · Doug DC931 · Cargo/Baggage DoorsSDR ABXA9500646Spar · crackedDURING C - CHECK INSPECTION, FOUND THE RIGHT WING REAR SPAR CAP CRACKED AT THE LOWER FLAP HINGE ATTACH STUDS, STA 164. REPAIRED IAW ABX EA AD-57-03904-MR.Jul 31, 1995 · N906AX · Doug DC931 · Wing SparSDR 95ZZZX4258Fuel Pump · malfunctionedSTL - FLT 340 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 2143, DUE TO ENGINE SURGED AND THROTTLE WOULD NOT CONTROL ENGINE POWER. REPLACED ENGINE FUEL PUMP, MFG PN 378200 AND FUEL CONTROL. MFG PN 743602-4. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME Jul 31, 1995 · N985Z · Doug DC931 · Engine Fuel PumpSDR 9515689994Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 427 BETWEEN LONGERONS 22R TO 23R. REPAIRED PER EA 99-94741.Jul 30, 1995 · N8978E · Doug DC931 · Fuselage Main, Plate/Skin
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