Douglas DC-9-83

Service difficulty reports · 16,530

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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 = 'DC983'
  ORDER BY difficulty_date DESC"

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SDR ZW0A0200603Web · corrodedDURING CHECK-C MAINT FOUND CORROSION ON FWD BOTTOM OF DOOR JAMB, LBL 57 AT STA 160. REPAIRED WEBBING PER SRM 53-01, FIG 2, AND REPAIRED ANGLE PER SRM 53-01, FIG 2.Jan 11, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200602Floor Support · crackedDURING CHECK-C MAINT CABIN FLOOR SUPPORT AT STA 864 HAD A CRACK AT LBL 10. REMOVED CRACKED SUPPORT AND REPLACED PER SPM 6-70-01.Jan 11, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200601Skin · corrodedDURING CHECK-C MAINT ON THE RT WING LOWER SURFACE, CORROSION WAS FOUND AROUND THE FASTENER AT WING STATION 511, TR LOWER MID SPAR SKIN. ACCOMPLISHED UT INSPECTION PER NDT 51-00-03 AND FOUND 47 PERCENT MATERIAL LOSS. INSTALLED FILLER AND DOUBLER PER SRM 57-03Jan 11, 2002 · N948TW · Doug DC983 · Wing, Plate/SkinSDR ANCF200200001Csd · malfunctionedDURING CLIMB LT CSD OIL OUTLET TEMP.REACHED RED DANGER ZONE AND CONTINUED INCREASING. CSD WAS DISCONNECTED. APU WAS STARTED AT FL.260 BUT AT FL.305 APU HAD AUTO SHUT DOWN. DESCENT WAS DOWN TO FL.290 WE TRIED TO START APU AGAIN BUT START WAS UNSUCCESSFUL. CREW Jan 11, 2002 · N190AN · Doug DC983 · Alternator-Generator DriveSDR AALA20020100Seat Track · corrodedTUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1233-1235. ROUTED OUT CORROSION BY ROUTER, TREATED AND PRIMED, INSTALLED PLUG REPAIR. (M)Jan 10, 2002 · N591AA · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR AALA20020099Seat Track · corrodedTUL - FOUND NR 1 SEAT TRACK CORRODED STATION 1205-1210. ROUTED OUT CORRODED AREA, TREATED AND PRIMED. INSTALLED PLUG REPAIR. (M)Jan 10, 2002 · N591AA · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0200513Web · brokenDURING CHECK-C MAINT IN TAIL COMPT RT SIDE BETWEEN STA 1474 AND 1486 STRUCTURAL WEB WAS BROKEN OUTBOARD OF STAIR HYD ACTUATOR. INSTALLED NEW STANDARD STRUCTURAL WEB PER SPM 6-70-01 AND DOUGLAS DRAWING 9911946.Jan 10, 2002 · N948TW · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200510Web · corrodedDURING CHECK-C MAINT FOUND CABIN FLOOR TO FUSELAGE MEMBRANE CORRODED AT APPROXIMATELY 6 INCHES FWD OF STA 636 THROUGH STA 712, RIGHT SIDE. REMOVED CORROSION PER SPM 6-80-01. REPAIRED PER SRM 51-70-4 PAGE 6, STA 636 TO 680.Jan 10, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200509Web · corrodedDURING CHECK-C MAINT IN AFT CABIN, LT FLOOR, FOUND CORROSION IN SHEET METAL MEMBRANE AT REAR CABIN FORMER RING, 1287 LT, LBL 42 INCHES. REMOVED CORROSION PER SPM 6-80-01. INSTALLED DOUBLER PER SRM 51-70-4.Jan 10, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200508Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM CAP STA 1155, LBL 22 TO 44. REPLACED SUPPORT ASSEMBLY PER SPM 6-70-01 AND SRM 51-30-5.Jan 10, 2002 · N9304C · Doug DC983 · Fuselage Main, Floor BeamSDR ZW0A0200512Cargo Track · corrodedDURING CHECK-C MAINT IN AFT CARGO COMPARTMENT FOUND CORROSION ON FLOOR TRACK BETWEEN STA 1136 THROUGH 1155 AT LONGERON 28R. REMOVED SURFACE CORROSION PER SPM 6-80-01. REMOVED AND REPLACED 2 ANGLES PER SRM 6-70-01.Jan 9, 2002 · N948TW · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0200507Seat Track · corrodedDURING CHECK-C MAINT IN THE AFT CABIN FOUND CHAIR TRACK CORROSION AT STA 1205, LBL 44, AND STA 1262 LBL 46. REPAIRED CHAIR TRACK PER SRM 53-05, FIG 4, FROM STA 1183 THROUGH 1308.Jan 9, 2002 · N9304C · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0200506Web · corrodedDURING CHECK-C MAINT IN CABIN FOUND CORROSION AT STA 1125 TO 1127, MEMBRANE ON RT SIDE. REMOVED CORROSION PER SRM 51-10-03 PAGE 27. REPAIRED AREA PER SRM 51-70-4 PAGE 4 AND 5.Jan 9, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200503Seat Track · corrodedDURING CHECK-C MAINT IN THE CABIN THE AFT FLOOR HAD CORROSION IN TRACK AT STA 1136 TO 1308, LBL 22. REMOVED AND REPLACED TRACK. SPLICED TRACK PER SRM 53-05.Jan 9, 2002 · N9304C · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0280003Longeron · corrodedOAK - DURING C-CHECK, FOUND CORROSION AROUND FASTENERS ON LONGERON 30 FROM FUSELAGE STATION 1003 TO 1070 IN AFT CARGO BAY. REMOVED DAMAGED SECTION. SPLICED IN NEW SECTION PER EA 5310-02049. (M)Jan 8, 2002 · N947AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ZW0A0200511Skin · dentedDURING CHECK-C MAINT ON FUSELAGE EXTERIOR, STA 1293, FOUND DENT BETWEEN LONGERON 16L AND 15L. ACCOMP INSP PER NDT 51-00-03 AND NO CRACK. UT INSPECTION INDICATED 50 PERCENT MATERIAL LOSS. CUT OUT PLUG TO REMOVE DAMAGED AREA AND INSTALLED AN EXTERIOR AND INTEJan 8, 2002 · N948TW · Doug DC983 · Fuselage Main, Plate/SkinSDR ZW0A0200505Web · corrodedDURING CHECK-C MAINT THE FWD CABIN HAD CORROSION ON FLOOR MEMBRANE AT STA 198, RBL 9. REMOVED LIGHT CORROSION. CUT OUT BROKEN AREA. INSTALLED AND FILLED WITH TOP AND BOTTOM DOUBLER PER SRM 51-70-4, 51-10-3, 51-20-0, AND SPM 6-80-01.Jan 8, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200504Bracket · crackedDURING CHECK-C MAINT THE FWD SERVICE DOOR HAD A BRACKET BELOW LOWER HINGE ARM THAT WAS CRACKED. REPLACED FRAME PER SPM 6-70-01.Jan 8, 2002 · N9304C · Doug DC983 · Service DoorsSDR ZW0A0200407Web · corrodedDURING CHECK-C MAINT FOUND IN CABIN SIDE WALL, CORROSION ON FLOOR MEMBRANE STA 1091 TO 1093, LONGERON 18L. INSTALLED REPAIR DOUBLER PER SRM 51-70-4, FIG 2.Jan 8, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200406Seat Track · corrodedDURING CHECK-C MAINT FOUND CABIN CHAIR TRACK CORRODED, STA 1127 TO 1136, LBL 36. REMOVED CORRODED TRACK AND REPLACED TRACK PER SPM 6-70-01.Jan 7, 2002 · N9304C · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0200409Doubler · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPT AT LONGERON 25L, THE STIFFENER HAD DOUBLER WITH CORROSION AT STA 1271, STA 1283, 1250, 1240 AND 1231. THE DOUBLERS WERE ON TOP OF THE STIFFENERS AND FORMERS. REMOVED CORROSION PER SRM 51-10-3. MADE NEW DOUBLER AS Jan 4, 2002 · N948TW · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200408Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 180, LBL 56. REMOVED OLD SUPPORT AND FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-30-2.Jan 4, 2002 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA030020Pump · inoperativeORD - FLT 1225 - AFT CENTER BOOST PUMP INOPERATIVE. LOW PRESSURE LIGHT ILLUMINATES WTH AFT CENTER PUMP ONLY RUNNING. PULLED AND RESET CIRCUIT BREAKER. LIGHT GOES OUT FOR 25 SECONDS THE ILLUMINATES. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)Jan 3, 2002 · N802NK · Doug DC983 · Fuel Boost PumpSDR ZW0A0201403Power Supply · dischargedTHE CABIN EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 1 TO 20. REPLACED THE POWER SUPPLY, AND THE EMERGENCY SWITCH.Jan 3, 2002 · N966TW · Doug DC983 · Emergency LightingSDR AALA2002054Beam · corrodedTUL - FOUND AFT CARGO DOOR BEAM HAS CORROSION FROM 1160 TO 1207. BLENDED OUT CORROSION PER ESO 80559. (M)Jan 2, 2002 · N589AA · Doug DC983 · Fuselage Main, StructureSDR GTIA012167Throttle · lack of lubeTPA - FLT 639 - FOUND LEFT AUTO THROTTLE STICKING. LUBE LEFT THROTTLE IN PEDESTAL, PERFORM AUTO THROTTLE SYSTEM CHECK. SYSTEM CHECKS GOOD IAW MD80 MM 22-31-00. (M)Dec 31, 2001 · N809NK · Doug DC983 · Auto Throttle SystemSDR AALA20012187Landing Gear · malfunctionedDFW - FLT 1658 - EN ROUTE DFW-TUL - SHORTLY AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED GEAR RETRACTION PER THE MM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Dec 31, 2001 · N596AA · Doug DC983 · Landing Gear Retraction/Extension SystemSDR ZW0A0200203Skin · corrodedDURING CHECK-C MAINT ON THE FUSELAGE EXTERIOR, STA 1293, FOUND BULGE IN SKIN AT LONGERON 16L. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 51-00-03 AND NO CRACK. ULTRA SOUND INSPECTION INDICATES NO MATERIAL LOOSE DUE TO CORROSION. SHIM BETWEEN SKIN AND STRIDec 28, 2001 · N948TW · Doug DC983 · Fuselage Main, Plate/SkinSDR ZW0A0200202Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 180, RBL 14 TO 36. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-02.Dec 28, 2001 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0200201Skin · corrodedDURING CHECK-C MAINT THE FUSELAGE EXTERIOR HAD A BULGE IN THE SKIN AT LONGERON 17L, STA 1293. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 51-00-03 AND NO CRACK. ULTRA SOUND INSPECTION INDICATES NO MATERIAL LOOSE DUE TO CORROSION. SHIM BETWEEN SKIN AND STRIDec 28, 2001 · N948TW · Doug DC983 · Fuselage Main, Plate/SkinSDR ZW0A0200107Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 1280, RBL 14 TO 36. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-02.Dec 28, 2001 · N9304C · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0112401Battery PackTHE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-25-01 STL. --CLOSED--Dec 28, 2001 · N9622A · Doug DC983 · Emergency LightingSDR ZW0A0200106Skin · dentedDURING CHECK-C MAINT FOUND 2 DENTS IN FUSELAGE SKIN , STA 237, LONGERON 17L. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR PER SRM 53-10-107, FIG 207.Dec 27, 2001 · N9304C · Doug DC983 · Fuselage Main, Plate/SkinSDR ZW0A0200104Skin · dentedDURING CHECK-C MAINT FOUND NUMEROUS DENTS AT STA 216 TO 218, LONGERON 15L TO 17L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SSRM 53-10-107, FIG 201.Dec 27, 2001 · N9304C · Doug DC983 · Fuselage Main, Plate/SkinSDR GTIA012085Accelerometer · faultyDFGS DOES NOT WORK EITHER AP 1 OR 2, WILL NOT CAPTURE ALTITUDE, HOLD ALTITUDE IN A TURN THERE IS IMMEDIATE DESCENT, DOES NOT WORK IN PERF ON EITHER SIDE BOTH COMMAND BARS DISAPPEAR FROM VIEW WHEN TO GO BUTTONS ARE PUSHED PRIOR TO TAKEOFF THE IAS MACH BUTTON DODec 21, 2001 · N802NK · Doug DC983 · Autopilot SystemSDR ZW0A0112303Longeron · crackedDURING CHECK-C MAINT LONGERON 2 LT HAD A 1 INCH CRACK AT STA 1418. REPAIRED PER SRM 53-02.Dec 21, 2001 · N931TW · Doug DC983 · Fuselage Main, Longeron/StringerSDR ZW0A0112302Longeron · crackedDURING CHECK-C MAINT LONGERON 2 RT WAS FOUND CRACKED AT STA 1418, 1 INCH LONG. REPAIRED 2R LONGERON PER SRM 53-02, FIG 18.Dec 21, 2001 · N931TW · Doug DC983 · Fuselage Main, Longeron/StringerSDR GTIA012084Wire · damagedDTW - FOUND EMERGENCY FLOOR PATH LIGHTING NOT ILLUMINATING SEAT ROWS 6-10. REPAIRED WIRE AT ROWS 10 AND OPS CHECK GOOD IAW MM 33-53-00. (M)Dec 20, 2001 · Doug DC983 · Light System WiringSDR AALA20020030Skin · dentedTUL - FOUND SKIN DENTED RIGHT SIDE OF FUSELAGE, JUST AFT OF RADOME AND JUST BELOW SKIN BREAK. INSTALLED INTERNAL REPAIR DOUBLER PER SRM 53-04 PAGE 38. (M)Dec 18, 2001 · N589AA · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0180314Battery Pack · dischargedSEA - DURING LINE CHECK, LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. (M)Dec 16, 2001 · N973AS · Doug DC983 · Emergency LightingSDR AALA20012157Light · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Dec 11, 2001 · N570AA · Doug DC983 · Emergency LightingSDR ZW0A0112107Skin · bentDURING CHECK-C MAINT THE MID CARGO DOOR SKIN BELOW THE DOOR HANDLE WAS BENT INWARD. INSTALLED DOUBLER PER SRM 52-05, FIG 30.Dec 11, 2001 · N984TW · Doug DC983 · Cargo/Baggage DoorsSDR ZW0A0112106Skin · bentDURING CHECK-C MAINT THE FWD CARGO DOOR SKIN BELOW THE DOOR HANDLE WAS BENT INWARD. INSTALLED DOUBLER PER SRM 52-05, FIG 30.Dec 11, 2001 · N984TW · Doug DC983 · Cargo/Baggage DoorsSDR AALA20020036Seat Track · corrodedTUL - FOUND NR 1 SEAT TRACK CORRODED AT CLIP NUT HOLE INBOARD LEG STATION 1303. INSTALLED STRAP PER AARD 53-20-00-13. (M)Dec 10, 2001 · N589AA · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR AALA20020031Seat Track · corrodedTUL - FOUND NR 1 SEAT TRACK CORRODED, UPPER SURFACE, OUTBOARD LEG AT STATION 1301. INSTALLED STRAP ON SEAT TRACK IAW AARD 53-20-00-13, TREATED AND PRIMED, BLENDED AREA IAW 51-10-3. (M)Dec 10, 2001 · N589AA · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0112104Skin · gougedDURING CHECK-C MAINT THE FWD LT PASSENGER DOOR, OUTER SKIN AND INTERNAL STRUCTURE WAS GOUGED AND WORN BELOW THE GUST LOCK RECESS. INSTALLED NEW GUST LOCK HOUSING AND REPAIRED DOOR SKIN PER SRM 52-05, FIG 20A.Dec 10, 2001 · N931TW · Doug DC983 · Passenger/Crew DoorsSDR AALA20020035Web · crackedTUL - FOUND CRACK IN FLOOR CUSP AT STATION 498 LEFT. ROUTED OUT CRACK, INSTALLED DOUBLER PER SRM 53-00-00. (M)Dec 9, 2001 · N589AA · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20020033Web · crackedTUL - FOUND CRACK IN FLOOR CUSP STATION 218 RIGHT .75 INCH. CUT OUT DAMAGE. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4-3. (M)Dec 8, 2001 · N589AA · Doug DC983 · Fuselage Miscellaneous StructureSDR GTIA012086Annunciator · failedFLL - FLT 774 - FMA DOES NOT DISPLAY IN ANY MODE. FAILED EN ROUTE. REMOVED AND REPLACED F/O'S FMA'S IAW 34-24-00. OPS CHECK NORMAL. (M)Dec 8, 2001 · N808NK · Doug DC983 · Instrument PanelSDR ASAA0180309Lanyard · disconnectedLAX - DURING PREFLIGHT CHECK, L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DETACHED FROM SLIDE COVER. REATTACHED LANYARD TO SLIDE COVER. (M)Dec 8, 2001 · N975AS · Doug DC983 · Escape Slide
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