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 MWEA95360Slide · failed testDURING ROUTINE TIME CHANGE OF FWD GALLEY SERVICE DOOR EVACUATION SLIDE, THE DEPLOYMENT TEST FAILED. MAINTENANCE FOUND RELEASE LANYARD ROUTED INCORRECTLY INSIDE SLIDE AT BOTTLE REGULATOR. MAINTENANCE REPLACED GALLEY SERVICE DOOR EVACUATION SLIDE AND RETURNED Oct 21, 1995 · N302ME · Doug DC932 · Escape SlideSDR MWEA95359Eel · inopMAINT REPORTED, THE FWD EMERGENCY ENTRANCE LIGHT WILL NOT ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AND AIRCRAFT RETURNED TO SERVICE.Oct 21, 1995 · N203ME · Doug DC932 · Emergency LightingSDR CAL951055Bulkhead · corrodedHOU - INSPECTION FOUND CORROSION NEAR T-CAP ON RIGHT SIDE OF AFT PRESSURE BULKHEAD. THE CORRODED SECTION WAS CUTOUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 22. (M)Oct 21, 1995 · N17535 · Doug DC932 · Fuselage Main, BulkheadSDR 96ZZZM29Door · not closedON FLT 530 - ATL - AIRCRAFT EXPERIENCED A VIBRATION ON THE LEFT SIDE OF THE AIRCRAFT BY THE COCKPIT. AIRCRAFT RETURNED. CHECKED AROUND THE NOSE GEAR AREA AND FOUND THE EXTERNAL POWER DOOR PANEL LEFT OPEN AND CLOSED DOOR.Oct 21, 1995 · N910VJ · Doug DC932 · Accessory Compartment DoorsSDR ABXA9600137Door · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT BUTE DOOR NR 1502 BROKEN AND DELAMINATED. REPLACED LEFT BUTE DOOR NR 1502 IAW DC-9 SRM 51-30-5.Oct 20, 1995 · N989AX · Doug DC932 · Wing Miscellaneous StructureSDR ABXA9600135Door · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT BUTE DOOR NR 1053 DELAMINATED. REPLACED LEFT BUTE DOOR NR 1503 IAW DC-9 SRM 51-30-5.Oct 20, 1995 · N989AX · Doug DC932 · Wing, Plate/SkinSDR ABXA9500989Skin · corrodedDURING CARGO MOD, OFF WING INSPECTION, FOUND LEVEL 2 CORROSION ON THE INBOARD LOWER SKIN. REPLACED SKIN IAW DC-9 DRAWING 5910039 AND SRM 51-10-3.Oct 20, 1995 · N989AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9500988Spar · corrodedDURING CARGO MOD, OFF WING FLAP INSPECTION, FOUND LEVEL 2 CORROSION ON THE AFT LOWER SPAR. REPLACED LOWER AFT SPAR IAW DC-9 DRAWING 5910039 AND SRM 57-50-1.Oct 20, 1995 · N989AX · Doug DC932 · Trailing Edge FlapsSDR 9516589926Release Cable · frayedDURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR HANDLE FROM THE CLIPS AND TO DROP THE TAILCONE. ALSO, FOUND A FRAYED RELEASE CABLE AND A WORN UPPER LEFT SLIDER BLOCK. REPLACED THE CABLE AND SLIDER BLOCK AND RERIGGED THE RELEASOct 20, 1995 · N926NW · Doug DC932 · Aerodynamic FairingsSDR MWEA95358Eel Socket · inopDURING INSPECTION, FOUND ONE EMERGENCY LIGHT ON FLOOR TRACK INOP. MAINTENANCE REPLACED LIGHT SOCKET AT ROW 17, OPS CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE.Oct 19, 1995 · N602ME · Doug DC932 · Emergency LightingSDR CAL951023Doubler · corrodedHOU - INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 218, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL951022Bracket · corrodedHOU - INSPECTION FOUND CABIN FLOOR SUPPORT BRACKET AT STA 160, AND 8 INCHES - 10 INCHES, LEFT OF CENTERLINE CORRODED. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-0. (X)Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL951021Belt Frame · crackedHOU - INSPECTION FOUND A .25 INCH CRACK COMING FROM HI-LOCK HOLE ON BELT FRAME AT STA 980, LONGERON 16R. THE CRACKED SECTION OF BELT FRAME WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-03, FIGURE 32. (X)Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Main, FrameSDR CAL950993Frame · crackedHOU - INSPECTION FOUND A 2 INCH CRACK EXTENDING FROM FASTENER HOLE ABOVE FLOOR ON FRAME AT STATION 813. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-03. (M)Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Main, FrameSDR CAL950992Floor Supports · corrodedHOU - INSPECTION FOUND CORROSION ON CABIN FLOOR SUPPORTS AT STATION 200. THE CORROSION EXTENDED THE FULL LENGTH FROM LEFT TO RIGHT SIDE OF FUSELAGE. FOUR FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2. (M)Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950988Frame · crackedHOU - INSPECTION FOUND A 3 INCH CRACK EXTENDING FROM FASTENER IN FRAME AT STATION 794, STRINGER 18L. THE FRAME WAS REPAIRED IAW SRM 53-11-3, FIGURE 1. (M)Oct 19, 1995 · N17535 · Doug DC932 · Fuselage Main, FrameSDR ABXA9600144Skin · dentedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT FUSELAGE SKIN DENTED AFT OF FS 965 ABOVE LONGERON 22R. REPAIRED SKIN IAW ABX REA D953-12800-MR.Oct 19, 1995 · N989AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9500885Seat · defectiveFIRST OFFICER'S SEAT LOOSE AND ROCKS ON SEAT RAILS. ALSO, SEAT BACK ROCKS AND SEAT CUSHION WORN OUT. REPLACED FIRST OFFICER'S SEAT ASSEMBLY IAW DC-9 MM.Oct 19, 1995 · N983AX · Doug DC932 · Flight Compartment EquipmentSDR 97ZZZX4197Steering Piston · pin shearedONE EACH OF TWO STEERING PISTON PINS THAT GO THROUGH COLLAR, PN 5920605-503, WAS SHEARED INSIDE THE COLLAR. THE BREAK WAS IN THE BOTTOM THIRD OF THE SHANK. THERE WAS A HEAVY COATING OF RUST ACROSS THE SHEARED SURFACE. THIS DEFECT WAS DISCOVERED DURING THE POct 19, 1995 · N43537 · Doug DC932 · Landing Gear Steering SystemSDR 95ZZZM679Bearing · failedSTL - DURING CLIMB, SHUT DOWN NR 1 ENGINE, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND METAL PARTICLES IN OIL FILTER. REPLACED ENGINE. GROUND OPERATION CHECKED NORMAL. INVESTIGATION OF OIL FILTER BYPASS LIGHT ILLUMINATION AND METAL PARTICLES FOUND IOct 19, 1995 · N931L · Doug DC932 · Turbine Engine Compressor SectionSDR 9522059601Blkhd Web · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE WHEEL WELL BULKHEAD KEEL WEB FS 756. REPAIRED WEB (P/N 9910164-3), PER EA 12-5310-9-C0614.Oct 19, 1995 · N601NW · Doug DC932 · Fuselage Main, BulkheadSDR 9516319603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH FITTING AT FS 237, LBL 54. REPLACED FITTING PER SRM 51-10-3, 51-30 AND 53-01.Oct 19, 1995 · N603NW · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL951057Skin · crackedHOU - INSPECTION FOUND TWO .75 INCH CRACKS AT RIVETS IN SKIN LAP AT STA 1038 ABOVE RIGHT PYLON. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M)Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/SkinSDR CAL951056Skin · crackedHOOU - INSPECTION FOUND A .75 INCH CRACK IN SKIN LAP AT STATION 1038 ABOVE LEFT PYLON. THE SKIN CRACK WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M)Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Plate/SkinSDR CAL951024Longeron · corrodedHOU - INSPECTION FOUND LONGERON 30 AT STA 218 CORRODED IN TWO. A LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02. (X)Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CAL950995Longeron · crackedHOU - INSPECTION FOUND A .25 INCH CRACK IN LONGERON 8L AT STATION 446. THE LONGERON WAS REPAIRED IAW SRM 53-02. (M)Oct 18, 1995 · N17535 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CAL950939Actuator Pin · shearedDHN - INSPECTION FOUND THE NLG RIGHT NOSE STEERING ACTUATOR PIN SHEARED. THE STEERING CONTROL LEVER ASSEMBLY AND RIGHT NOSE STEERING CYLINDER ASSEMBLY WERE REMOVED AND REPLACED. (M)Oct 18, 1995 · N43537 · Doug DC932 · Landing Gear Steering SystemSDR CA951129519Wheel Assembly · seized(CAN)A LOUD RATTLING NOISE WAS HEARD COMING FROM NOSE WHEEL WELL AREA ON TAKEOFF. REJECTED TAKEOFF AT 80 KNOTS. A 180 DEGREE TURN WAS EXECUTED, AIRCRAFT TAXIED 100 FEET AND STOPPED. A LOUD WINDING DOWN NOI SE WAS HEARD IN NOSE WHEEL WELL AREA AS BRAKE SET. UNAOct 18, 1995 · Doug DC932 · Wheel/Ski/FloatSDR ABXA9600184Panel · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT LOWER TRAILING EDGE PANEL INBOARD OF THE MAIN LANDING GEAR DELAMINATED. REPLACED PANEL ASSEMBLY IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 18, 1995 · N989AX · Doug DC932 · Wing Miscellaneous StructureSDR ABXA9600156Blkhd Web · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE APB WEB CORRODED JUST BELOW FLOOR LEVEL AT FS 996 AND BETWEEN LBL 10 AND LBL 20. REPAIRED WEB IAW ABX REA D953-13041-MR.Oct 18, 1995 · N989AX · Doug DC932 · Fuselage Main, BulkheadSDR 95ZZZM645Door · not latchedFLT NR 547 - PHL - AIR RETURN, AFT AIRSTAIR DOOR LIGHT ILLUMINATED. RECYCLED AFT STAIRS, SYSTEM CHECK NORMAL. (M)Oct 18, 1995 · N904VJ · Doug DC932 · Passenger/Crew DoorsSDR 9518599926Angle · corrodedDURING H-CHECK, FOUND CORROSION IN THE UPPER CUSP ANGLE AT THE MAIN CABIN DOOR FS 198 TO 203. REPAIRED ANGLE (P/N 9910078-9), PER EA99-103303.Oct 18, 1995 · N926NW · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL951053Splice · crackedHOU - INSPECTION FOUND A 4 INCH CRACK IN LEADING EDGE SPLICE BETWEEN NR 6 AND NR 7 SLAT TRACK. THE LEADING EDGE SPLICE WAS REPAIRED IAW ECRA 5710-01701. (M)Oct 17, 1995 · N17535 · Doug DC932 · Wing Miscellaneous StructureSDR CAL950990Le Splice · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN LEADING EDGE SPLICE BETWEEN THE NR 3 AND NR 4 SLAT TRACK. A DOUBLER WAS INSTALLED IAW ECRA 5710-01697. (M)Oct 17, 1995 · N17535 · Doug DC932 · Wing Miscellaneous StructureSDR CAL950989Spar Cap · corrodedHOU - INSPECTION FOUND INTERGRANULAR CORROSION ON LOWER SPAR CAP AT FXLS 325. THE SPAR CAP WAS REPAIRED IAW SRM 57-01, FIGURE 2. (M)Oct 17, 1995 · N17535 · Doug DC932 · Wing SparSDR ABXA9600177Longeron · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED AT FS 237. REPLACED LONGERON 30 IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 17, 1995 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9600133Longeron · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON NR 30 CRACKED AT FS 237. REPLACED IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 17, 1995 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9516229608Fitting · corrodedDURING D-CHECK, FOUND CORROSION ON THE JACK SUPPORT FITTING. REPLACED FITTING PER SRM 51-01 AND DWG 59-17491. DUE TO INCORRECT AIRCRAFT NUMBER, ALL OTHER REFERENCES; MODEL NUMBER, SERIAL NUMBER, ETC HAVE BEEN CHANGED RESPECTIVELY.Oct 17, 1995 · N608NW · Doug DC932 · Fuselage Main, StructureSDR 9516219921Striker · wornDURING CLIMB, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR STRIKEROct 17, 1995 · N943N · Doug DC932 · Landing Gear Position and WarningSDR ABXA9600158Trap Panel · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT TRAPEZIODAL PANEL HAD CORROSION INSIDE THE BOLT HOLES ABOVE THE FIXED SIDE BRACE. REPAIRED PANEL IAW ABX REA D953-13155-MR.Oct 16, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9600130Blkhd Web · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 CRACKED AT LONGERON 11R. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2.Oct 16, 1995 · N989AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9600129Blkhd Web · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 HAD A SMALL CRACK RADIATING FROM LIGHTENING HOLE BETWEEN LONGERON 12R AND 13R. REPAIRED CRACK IAW DC-9 SRM 53-01 FIGURE 2.Oct 16, 1995 · N989AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9600091Angle · crackedDURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 16, 1995 · N986AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9600090Angle · crackedDURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 16, 1995 · N986AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9600089Angle · crackedDURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 16, 1995 · N986AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9600088Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE OF AD 92-22-08, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 16, 1995 · N986AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9500983Te Skin · corrodedDURING CARGO MOD OFF WING INSPECTION, FOUND LEVEL 2 CORROSION IN TWO AREAS ON THE LOWER SKIN DOUBLER ALONG THE TRAILING EDGE. REPLACED CENTER SKIN IAW DC-9 DRAWING 5910411.Oct 16, 1995 · N989AX · Doug DC932 · Wing, Plate/SkinSDR 95ZZZM682Door Beam · crackedSTL - DURING C-CHECK, FOUND TWO INCH CRACK IN NR 2 DOOR BEAM FORWARD END. REPAIRED PER SRM 51-30 AND STANDARD PRACTICES.Oct 16, 1995 · N922L · Doug DC932 · DoorsSDR 9518589926Web · corrodedDURING H-CHECK, FOUND CORROSION IN THE LEFT MAIN LANDING GEAR WHEEL WELL FORWARD SLANT PRESSURE PANEL WEB. REPAIRED WEB (P/N 5956065-41), PER EA 99-102597.Oct 16, 1995 · N926NW · Doug DC932 · Fuselage Miscellaneous StructureSDR 9518579926Floorbeam · corrodedDURING H-CHECK, FOUND CORROSION IN THE BL 0 FLOOR CAP BETWEEN FS 689 TO 699. REPAIRED CAP (P/N 5910347-25), PER EA 99-103291.Oct 16, 1995 · N926NW · Doug DC932 · Fuselage Main, Floor Beam
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