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 9505509995Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FLOORBEAM TO KEEL ATTACH FITTING FS 718. REPLACED FITTING PER SRM 51-01.Apr 5, 1995 · N8979E · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950420Finger Doubler · corrosionPIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED FINGER DOUBLER FROM STATION 965 TO 996 LONG 26R. REMOVED AND REPLACED FINGER DOUBLER PER DACO DWG. (M)Apr 4, 1995 · N938VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950419Skin · dentPIT - DURING Q-1 CHECK INSPECTION, FOUND A DENT .075 INCH DEEP .75 INCH LONG AT STATION 983 LONGERON 25L AND 24L. INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-04 FIG 38. (M)Apr 4, 1995 · N938VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR 9505399963Sub Floor · oil cannedDURING PERIODIC CHECK, FOUND OIL CANNING IN THE GALLEY SUB FLOOR FS 75 TO 229, RIGHT SIDE. REPAIRED PER EA 99-097069.Apr 4, 1995 · N913RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9505379958Fitting · crackedDURING PERIODIC CHECK, FOUND 4 TO 6 INCH CRACK IN LONGERON 26L END FITTING AT FS 590. REPLACED FITTING PER SRM 51-30-0.Apr 4, 1995 · N917RW · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9500318Door · delaminatedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ARTICULATING DOOR DELAMINATED, APPROXIMATELY 30 SQUARE INCHES. REPLACED LEFT OUTBOARD FLYING DOOR IAW DC-9 M.M. 32-12-1.Apr 3, 1995 · N929AX · Doug DC931 · Landing Gear DoorsSDR USAA950303Cylinder · leakingCLT - FLT 0741 - ON CLIMB-OUT, THE RED GEAR UNSAFE LIGHT AND YELLOW GEAR DOOR OPEN LIGHT ILLUMINATED. CAPTAIN DECLARED AND EMERGENCY AND FLIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE LEFT MAIN GEAR ACTUATING CYCLINDER. OPERATIONS CHECKED GOOD. (W)Apr 1, 1995 · N977VJ · Doug DC931 · Landing Gear ActuatorSDR USAA950302Line · dirtyCLT - FLT NR 0275 - CREW REPORTED FUMES IN COCKPIT. OXYGEN MASKS WERE USED AND AN EMERGENCY WAS DECLARED. MAINTENANCE CLEANED THE ANTI-ICE FLUID LINE AND ELBOW AT SOLENOID, FIRST OFFICERS SIDES. OPERATIONS CHECKED GOOD. (W)Apr 1, 1995 · N972VJ · Doug DC931 · Water Line Anti-Ice SystemSDR ABXA9500319Intercostal · crackedDURING C-CHECK INSPECTION FOUND THE UPPER FLANGE OF AN INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL IAW ABX REA D953-11304-MR.Apr 1, 1995 · N929AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 9505349948Spar Cap · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 1.25 INCH CRACK IN THE LEFT ELEVATOR SPAR CAP STA 156 AND A .75 INCH CRACK IN THE RIGHT ELEVATOR SPAR CAP STA 74. OVERHAULED BOTH PER CMM 27-27-30.Apr 1, 1995 · N8929E · Doug DC931 · Elevator, Spar/RibSDR USAA950418Longeron · crackedPIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 16R AT STATION 965 RT LAV. ACCOMPLISHED LONGERON SPLICE REPAIR PER SRM 53-02 FIG 4. (M)Mar 31, 1995 · N938VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA950417Skin · damagedPIT - DURING Q-1 CHECK INSPECTION, FOUND TEMP REPAIR STATION 1096 LONGERON 42. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-01 FIG 2. (M)Mar 31, 1995 · N938VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500317Frame · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05; S.B. 53-131, FOUND RIGHT MAIN FRAME AT STA 737 CRACKED IN FORWARD INBOARD WEB. REPLACED MAIN FRAME AT STA 737R IAW DC-9 SRM 51-30-5 AND 51-30-2.Mar 31, 1995 · N929AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9500316Skin · oil canningDURING C-CHECK INSPECTION FOUND FUSELAGE SKIN TO BE OIL CANNING, 1 INCH DIAMETER AT FUSELAGE STATION 362, LONGERONS 21 AND 22R. REPAIRED SKIN IAW ABX REA D953-11287-MR.Mar 31, 1995 · N929AX · Doug DC931 · Fuselage Main, Plate/SkinSDR 9505319963Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE LONGERON 29L END FITTING AT FS 583. REPLACED FITTING PER SRM 53-03 FIG 3.Mar 31, 1995 · N913RW · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950416Beltframe · gougedPIT - DURING Q-1 CHECK INSPECTION, FOUND GOUGE IN STATION 1076 BELTFRAME LONGERON 20R. SPLICED IN SECTION OF BELTFRAME PER SRM 53-03 FIG 32. (M)Mar 30, 1995 · N938VJ · Doug DC931 · Fuselage Main, FrameSDR USAA950304Fuel Pump · failedPIT - FLT 0233 - LOW POWER ON THE RIGHT ENGINE ON CLIMB-OUT. FLIGHT RETURNED TO PIT. SINGLE ENGINE TIME WAS TWELVE MINUTES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP. THE RIGHT ENGINE FUEL CONTROL UNIT WAS ALSMar 30, 1995 · N979VJ · Doug DC931 · Engine Fuel PumpSDR ABXA9500321Frame · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FUSELAGE FRAME AT STA 658 CRACKED AT LONGERON 19R. REPAIRED IAW DC-9 SRM 53-03, FIGURE 16.Mar 30, 1995 · N929AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9500320Frame · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FUSELAGE FRAME AT STA 639 CRACKED AT LONGERON 19R. REPAIRED IAW DC-9 SRM 53-03, FIGURE 16.Mar 30, 1995 · N929AX · Doug DC931 · Fuselage Main, FrameSDR 95ZZZX1856Control Unit · malfunctionedPIT - FLT 0233 - LOW POWER ON THE RIGHT ENGINE ON CLIMB-OUT. FLIGHT RETURNED TO PIT. SINGLE ENGINE TIME WAS TWELVE MINUTES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP. THE RIGHT ENGINE FUEL CONTROL UNIT WAS ALSMar 30, 1995 · N979VJ · Doug DC931 · Fuel Control/Turbine EnginesSDR 9505309980Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE FORWARD CARGO DOOR BEAM END FITTING FORWARD END. REPLACED FITTING.Mar 30, 1995 · N9344 · Doug DC931 · Cargo/Baggage DoorsSDR 9505299914Shroud · crackedDURING PERIODIC CHECK, FOUND ONE INCH CRACK IN THE APU HOUSING SHROUD LEFT SIDE RADIUS. REPAIRED PER EA 99-097422.Mar 30, 1995 · N964N · Doug DC931 · Fuselage Miscellaneous StructureSDR 9505289990Bracket · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO INCH CRACK IN A PANEL ATTACH ANGLE RIGHT WING LEADING EDGE LOWER SURFACE WS 118. REPAIRED PER XEA X9-57-18.Mar 30, 1995 · N8950E · Doug DC931 · Wing Miscellaneous StructureSDR 9505279988Frame · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN MAIN FRAME FS 658 ABOVE LONGERON 19L. REPAIRED PER EA X9-53-75.Mar 30, 1995 · N8944E · Doug DC931 · Fuselage Main, FrameSDR 9505269980Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT WING NR 2 FLAP HINGE FITTING WS 154. REPLACED FITTING PER CITEXT 09-5740-1-9800.Mar 29, 1995 · N9344 · Doug DC931 · Wing, Control Surface Attach FittingsSDR USAA950415Pan · crackedPIT - DURING Q-1 CHECK INSPECTION, FOUND .125 INCH CRACK FWD STOP AND .25 INCH CRACK AFT STOP LEFT AFT EMERGENCY EXIT WINDOW. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-20-03. (M)Mar 28, 1995 · N938VJ · Doug DC931 · Emergency ExitsSDR ABXA9500328Cap · corrodedDURING DC-9 ELEVATOR OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE INBOARD LEADING EDGE CAP OF THE RIGHT ELEVATOR. REPLACED WITH SERVICEABLE CAP IAW DC-9 SRM 27-30.Mar 28, 1995 · N942AX · Doug DC931 · Trailing Edge FlapsSDR 9504999914Release Mech · defectiveDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. REPLACED TAILCONE. CHECKED OK.Mar 28, 1995 · N964N · Doug DC931 · Aerodynamic FairingsSDR 9504989914Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE NR 3 RIGHT FORWARD FLAP HINGE FITTING. REPLACED FITTING PER CITEXT 09-5740-1-9800.Mar 28, 1995 · N964N · Doug DC931 · Wing, Control Surface Attach FittingsSDR 9505159992Retract Mech · lack of lubeLANDING GEAR WAS SLOW TO RETRACT DURING CLIMBOUT FROM MEM VIBRATION WAS ALSO EXPERIENCED. RECYCLED GEAR AND ALL ACTIONS WERE EXTREMELY SLOW. FLIGHT CONTINUED TO DESTINATION DCA AND LANDED WITHOUT INCIDENT. CHECKED RIGGING AT LANDING GEAR CONTROL VALVE. FREMar 27, 1995 · N8960E · Doug DC931 · Landing Gear Retraction/Extension SystemSDR USAA950414Skin · damagedPIT - DURING Q-1 CHECK INSPECTION, FOUND TEMP REPAIR STATION 110 JUST ABOVE AFT RT MLG DOOR. INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-04 FIG 38. (M)Mar 24, 1995 · N938VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR 95ZZZX1756Skin · delaminationRIGHT WING OUTBOARD SPOILER DELAMINATED ON UPPER SURFACE. REPAIRED SPOILER PER SRM 51-70-2. AIRCRAFT TT, 54,495 HRS.Mar 24, 1995 · N650UG · Doug DC931 · SpoilersSDR 95ZZZX1755Spar Cap · corrosionLEFT WING FLAP, STA XFLS 168.5, AFT LOWER SPAR CAP HAS CORROSION BULGE. REPAIRED CAP PER DALFORD AVIATION XEA NR X9-57-17, REVISION 2. AIRCRAFT TT, 54,495 HRS.Mar 24, 1995 · N650UG · Doug DC931 · Trailing Edge FlapsSDR 95ZZZX1753Eel Sign · failed testFORWARD SERVICE DOOR SELF-ILLUMINATING EMERGENCY EXIT SIGN FAILED LUMINOSITY CHECK. REPLACED SIGN PER SRM 51-30-1. AIRCRAFT TT, 54,495 HRS.Mar 24, 1995 · N650UG · Doug DC931 · Emergency LightingSDR 9504779956Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN FORWARD CARGO DOOR END FITTING VISIBLE THROUGH OPENING NR 21. REPLACED FITTING.Mar 24, 1995 · N923RW · Doug DC931 · Cargo/Baggage DoorsSDR USAA950488Skin · crackedPIT - DURING ACCOMPLISHMENT OF SCHEDULED PRODUCTION CONTROL ITEM NR 105, FOUND 13/16 INCH CRACK AT TOP FORWARD CORNER OF FWD CARGO DOOR FRAME AT STA 370 BELOW LONGERON 19. VISUAL INSPECTION AND HFEC. INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-05 FIG 68. Mar 23, 1995 · N950VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500311Door · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE HALF WORN. REPLACED LEFT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 M.M. 32-10-0.Mar 23, 1995 · N948AX · Doug DC931 · Landing Gear DoorsSDR 95ZZZW581Torque Tube · sheared rivetFLT 9831 - ON APPROACH TO PIE, RIGHT MAIN GEAR DOOR WOULD NOT CLOSE ON GEAR EXTENSION. LANDED WITH GEAR DOOR OPEN. INSPECTION OF AREA NOTED DAMAGE TO RIGHT MLG DOOR. DAMAGE DID NOT PREVENT GEAR DOOR FROM LOCKING IN CLOSED POSITION. AIRCRAFT MADE GEAR DOWN Mar 21, 1995 · N8931E · Doug DC931 · Landing Gear Door Retract SectionSDR 9504869959Stall Warning · malfunctionedSTALL WARNING INDICATION FAILURE LIGHT ILLUMINATED UPON APPLICATION OF TAKEOFF POWER. TAKEOFF WAS ABORTED. A SUCCESSFUL TAKEOFF WAS ACCOMPLISHED ON SECOND ATTEMPT. RECYCLED SYSTEM ON GROUND. ALL CHECKED OK. AIRCRAFT RETURNED TO SERVICE.Mar 21, 1995 · N919RW · Doug DC931 · Stall Warning SystemSDR 9504879959Radar · failedRADAR BEGAN SPOKING ON LOWER RIGHT SIDE OF SCREEN EN ROUTE DTW-BNA. THIS CAUSED ERRONEOUS DISPLAY OF KNOWN WEATHER. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR INDICATOR AND TRANSCEIVER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SEMar 20, 1995 · N919RW · Doug DC931 · Weather Radar SystemSDR 9504599960Skin · oil cannedDURING PERIODIC CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN BELOW THE ELEVATOR HYDRAULIC ACCUMULATOR ACCESS DOOR. REPAIRED PER EA 99-097154.Mar 20, 1995 · N920RW · Doug DC931 · Fuselage Main, Plate/SkinSDR 9504589960Floor Beam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON AFT CARGO FS 996 FLOOR BEAM RIGHT SIDE INBOARD OF VERTICAL SIDE PANELS. REPAIRED PER EA 99-097166.Mar 20, 1995 · N920RW · Doug DC931 · Fuselage Main, Floor BeamSDR 9504459978T Ducts · lack of lubeSLAT DISAGREEMENT LIGHT ILLUMINATED DURING SLAT EXTENSION. AIRCRAFT ROLLED SLIGHTLY TO THE LEFT. VISUAL INSPECTION INDICATED LEFT SLAT TO BE FULLY EXTENDED AND RIGHT SLAT APPROXIMATELY .75 EXTENDED. INDICATED AIRSPEED WAS 200-220 KNOTS. FLIGHT CONTINUED ANMar 20, 1995 · N9342 · Doug DC931 · Leading Edge Slat Control SystemSDR ABXA9500262Cap · crackedDURING C-CHECK INSPECTION, FOUND THE NR 1 ENGINE PYLON CLOSING RIB CAP CRACKED AT STA. YN-174. REPAIRED IAW ABX REA D954-11218-MR.Mar 18, 1995 · N942AX · Doug DC931 · Nacelle/Pylon, Longeron/StringerSDR ABXA9500249Channel · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON A FLOOR SUPPORT BETWEEN STA.'S 897 THROUGH 937. REPAIRED IAW ABX REA D953-11215.Mar 18, 1995 · N942AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 95ZZZW338Cylinder · crackedSTL - AFTER TAKEOFF LEFT MAIN LANDING GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS REMAINED ILLUMINATED WITH GEAR HANDLE IN THE UP POSITION. FOUND LEFT MAIN LANDING GEAR BUNGEE CYLINDER, MFG P/N 3914016-5503 CRACKED. REPLACED LEFT MAIN LANDING GEAR BUNGEE CYLINDER.Mar 18, 1995 · N989Z · Doug DC931 · Landing Gear Retraction/Extension SystemSDR 9504559908Skin · corrodedDURING LINE CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 451 BETWEEN LONGERONS 29R - 30. REPAIRED PER EA 99-097065.Mar 18, 1995 · N958N · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9500252Cusp · crackedDURING C-CHECK INSPECTION, THE RIGHT CUSP TEE WAS FOUND CRACKED AT STA. 994. REPAIRED IAW ABX REA D953-11118-MR.Mar 17, 1995 · N942AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 9504549960Floor Beam · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON AFT CARGO FLOOR BEAM FS 980 INBOARD OF VERTICAL SIDE PANELS. REPAIRED PER EA 99-097152.Mar 17, 1995 · N920RW · Doug DC931 · Fuselage Main, Floor BeamSDR USAA950245Eel Wire · brokenCLT - THE FLOOR LEVEL LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE FIRST SEGMENT OF FLOOR TRACK LIGHTING. OPERATIONS CHECKED GOOD. (W)Mar 16, 1995 · N932VJ · Doug DC931 · Emergency Lighting
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