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 ZW0A0202602Longeron · crackedDURING CHECK-C MAINT LONGERON 2L WAS CRACKED JUST AFT OF STA 1429. SPLICED IN NEW LONGERON PER SRM 53-02, FIG 18.Mar 4, 2002 · N110HM · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0280059Wire · disconnectedLAS - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WIRING BETWEEN MODULES AT ROW 2. LIGHTS THEN OPERATED PROPERLY. (M)Mar 1, 2002 · N973AS · Doug DC983 · Light System WiringSDR ZW0A0202604Skin · corrodedDURING CHECK-C MAINTENANCE FOUND CORROSION FROM LONGERON 29L TO 29R, STA 160 TO 218. REPLACED SKIN FROM STA 110 TO 229, STRINGER 26L TO 26R, PER SPM.Mar 1, 2002 · N967TW · Doug DC983 · Fuselage Main, Plate/SkinSDR ZW0A0202605Skin · corrodedDURING CHECK-C MAINT THE FWD CARGO COMPT BELLY SKIN HAD CORROSION AT STA 218 TO 229, LONGERON 29L TO 29R. INSTALLED NEW SKIN PER DRAWING 5911401.Feb 28, 2002 · N967TW · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0280057Longeron · corrodedOAK - DURING C-CHECK, FOUND LONGERON 29R IN AFT CARGO BAY TO HAVE CORROSION AROUND FASTENER HOLES AT FS 1022-1025. INSTALLED U-CHANNEL REPAIR PER EA 5310-012066. (M)Feb 26, 2002 · N972AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0280056Bulkhead · crackedOAK - DURING C-CHECK, FOUND CRACK DAMAGE AT THE LEFT LOWER CORNER OF THE FORWARD BULKHEAD AT FS 110 SITUATED IN THE NLG WHEEL WELL. INSTALLED REPAIR DOUBLER PER EA 5310-02068. (M)Feb 24, 2002 · N972AS · Doug DC983 · Fuselage Main, BulkheadSDR ASAA02280055Lanyard · disconnectedSEA - FORWARD GALLEY DOOR LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M)Feb 23, 2002 · N969AS · Doug DC983 · Emergency EquipmentSDR MEX2002047Switch · failedFLT 411 - MIA-CUN - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF LIGHT DISAGREE SLAT TURNED ON. ON REVISION IT WAS FOUND STALL FAILURE LIGHT, TURN ON TOO. PERFORMED BITE TO BOTH COMPUTERS, FAIL ON VANE NR 1, CONNECTOR WAS CLEANED, AND A BITE TO PROXIMITY Feb 22, 2002 · N838AM · Doug DC983 · Leading Edge Slat Position Indicating SystemSDR ASAA0280053Lanyard · disconnectedSEA - DURNIG PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)Feb 22, 2002 · N944AS · Doug DC983 · Escape SlideSDR ZW0A0202403Bracket · crackedDURING CHECK-C FOUND AFT ACCY COMPARTMENT BRACKET CRACKED ABOVE RT VENT BOX FWD OF RUDDER TRIM DRUM. DOUBLER FABRICATED PER SRM 53-01, FIG 3 AND 4, PAGE 18.Feb 22, 2002 · N967TW · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20020175Battery · dischargedDFW - DURING OVERNIGHT MAINTENANCE, EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EXTERIOR OVERWING EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Feb 21, 2002 · N435AA · Doug DC983 · Emergency LightingSDR ZW0A0202202Battery Pack · dischargedTHE FORWARD OVERWING EMERGENCY EXIT LIGHTS, EGRESS LIGHTS AT ROW 17 TO 20, AND FIVE OTHER INDIVIDUAL EGRESS LIGHTS, WERE INOPERATIVE. REPLACED THE BATTERY PACK (P/N 5822-2) FOR THE EMERGENCY LIGHTS, REPLACED THE WIRE HARNESS (P/N 0105606-003SMI) BETWEEN ROW 1Feb 21, 2002 · N9621A · Doug DC983 · Emergency LightingSDR ASAA0280029Lanyard · disconnectedLAX - LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M)Feb 20, 2002 · N944AS · Doug DC983 · Emergency EquipmentSDR ASAA0280052Skin · crackedPAE - DURING 30K CHECK, FOUND MID CARGO BAY DOOR TO BE CRACKED AT INNER SKIN OF LIGHTENING HOLE AT LOWER SIDE NEAR INNER HANDLE MECHANISM. REPAIRED SKIN PER EA 5230-01162. (M)Feb 20, 2002 · N974AS · Doug DC983 · Cargo/Baggage DoorsSDR ASAA0280051Hinge Fitting · corrodedPAE - DURING 30K CHECK, FOUND LEFT OUTBOARD FLAP INBOARD HINGE BEARING RETAINER HOLES AND SCREWS CORRODED. REPAIRED BEARING RETAINER HOLES PER EA 5750-01625, AND REPLACE FASTENERS PER SRM 51-30. (M)Feb 20, 2002 · N974AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0280050Hinge Fitting · corrodedPAE - DURING 30K CHECK, FOUND RIGHT OUTBOARD FLAP CENTER HINGE SUPPORT ON WING REAR SPAR TO BE CORRODED IN TWO BEARINGS RETAINER HOLES. FASTENERS WERE ALSO CORRODED. REPAIRED BEARING RETAINER HOLES PER EA 5750-01625, AND REPLACE FASTENERS PER SRM 51-30. (M)Feb 20, 2002 · N974AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0280049Retainer · corrodedPAE - DURING 30K CHECK, FOUND LEFT OUTBOARD FLAP CENTER HINGE BEARING RETAINER HOLES AND SCREWS CORRODED. REPAIRED BEARING RETAINER AND REPLACED SCREWS PER EA 5750-01625. (M)Feb 20, 2002 · N974AS · Doug DC983 · Trailing Edge FlapsSDR ASAA0280048Channel · corrodedPAE - DURING 30K CHECK, FOUND CORROSION ON HAT CHANNEL AT FS 1106 AND 1155. REPLACED CHANNEL PER SRM 53-01. (M)Feb 20, 2002 · N974AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280046Web · corrodedPAE - DURING 30K CHECK, FOUND CORROSION ON FORWARD PASSENGER (L-1) DOOR WEB FS 1118, 1152, AND 1160. REPLACED WEB PER SRM 51-30-02 AND 51-30-05. (M)Feb 19, 2002 · N974AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280047Frame · corrodedOAK - DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF CIRCUMFERENTIAL FRAME AT FS 1250 FROM LONGERON 29R-28L. (M)Feb 19, 2002 · N972AS · Doug DC983 · Fuselage Main, FrameSDR AALA20020157Battery Pack · dischargedSEA - DURING OVERNIGHT MAINTENANCE, LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Feb 17, 2002 · N435AA · Doug DC983 · Emergency LightingSDR ASAA0280039Door Frame · crackedPAE - DURING 30K CHECK, AFT CARGO DOOR FRAME WEB WAS DETERMINED TO BE CRACKED AT LIGHTNING HOLE, FS STATION 1214. REPAIRED WEB CRACKS PER EA 531-02059. (M)Feb 17, 2002 · N974AS · Doug DC983 · Fuselage Main, StructureSDR ASAA0280038Door Frame · corrodedPAE - DURING 30K CHECK, MID CARGO LOWER BEAM WAS DETERMINED TO BE CORRODED ON VERTICAL AND HORIZONTAL FACES FROM FS 636-693 AND GOUGED FROM 655-689. REPAIRED DOOR BEAM PER EA 5310-02063. (M)Feb 17, 2002 · N974AS · Doug DC983 · Fuselage Main, StructureSDR ASAA0280037Skin · corrodedPAE - DURING 30K CHECK, FUSELAGE EXTERIOR SKIN WAS DETERMINED TO BE CORRODED AT CENTER OF LOWER LOBE, FS 1080, BETWEEN ENDS OF WING BODY FAIRING RUBSTRIPS. REMOVED CORROSION PER EA 5330-01566. (M)Feb 17, 2002 · N974AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0280036Door Frame · corrodedPAE - DURING 30K CHECK, FORWARD CARGO DOOR THRESHOLD LOWER BEAM WAS DETERMINED TO BE CORRODED AT FASTENER HOLES FROM FS 375-420. REMOVED CORROSION AND REPAIRED BEAM PER EA 53-10-02054. (M)Feb 17, 2002 · N974AS · Doug DC983 · Fuselage Main, StructureSDR P2EA2002M008Inlet Guide Vane · crackedON INSPECTION OF THE NR 2 ENGINE INLET FOUND THE IGV AT 4 O'CLOCK WITH CRACK. UPON FURTHER INSPECTION FOUND THE NR 2 ENGINE BEARING HUB CRACKED. REPLACED THE NR 2 ENGINE INLET GUIDE VANE ASSY AND REPLACED THE NR 2 ENGINE BEARING HUB IAW 72-23-01 AND 72-23-02Feb 17, 2002 · N131NJ · Doug DC983 · Turbine Engine Air Inlet SectionSDR ASAA0280044Battery · dischargedOAK - PREFLIGHT CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT BATTERY. LIGHT THEN OPERATED NORMALLY. (M)Feb 16, 2002 · N960AS · Doug DC983 · Emergency LightingSDR ASAA0280043Wire · disconnectedSEA - DURING PREFLIGHT CHECK, FIRST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WIRING BETWEEN MODULES. LIGHTS THEN OPERATED PROPERLY. (M)Feb 16, 2002 · N958AS · Doug DC983 · Light System WiringSDR ASAA0280042Wire · disconnectedSEA - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. RECONNECTED WIRING BETWEEN MODULES. LIGHTS THEN OPERATED PROPERLY. (M)Feb 16, 2002 · N958AS · Doug DC983 · Light System WiringSDR ASAA0280041Light · inoperativePAE - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M)Feb 16, 2002 · N974AS · Doug DC983 · Emergency LightingSDR ASAA0280040Wire · damagedSEA - DURING PREFLIGHT CHECK, 1ST CLASS EMERGENCY FLOOR TRACK LIGHTING WAS DETERMINED TO BE INOPERATIVE. REPLACED DAMAGED SECTION OF WIRING AND TWO LENS. LIGHTS THEN OPERATED PROPERLY. (M)Feb 15, 2002 · N973AS · Doug DC983 · Light System WiringSDR ZW0A0202203Tie Clip · brokenDURING CHECK-C MAINT THE LT SIDE VENT BOX UPPER FORWARD STRUCTURAL TIE CLIP WAS FOUND BROKEN.Feb 15, 2002 · N967TW · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280035Door Frame · crackedPAE - DURING 30K CHECK, AFT CARGO DOOR FRAME WEB WAS DETERMINED TO BE CRACKED AT LIGHTNING HOLE AT FS 1214, WL 16, AND BUTTOCK LINE 46. REPAIRED CRACK PER EA 5310-02059. (M)Feb 14, 2002 · N974AS · Doug DC983 · Fuselage Main, StructureSDR ASAA0280034Web · corrodedPAE - DURING 30K CHECK, FOUND CORROSION ON OUTBOARD WEB FROM FS 522-541. REPLACED WEB SECTION FROM FS 503-600 PER SRM 51-30-02 AND 51-30-05. (M)Feb 14, 2002 · N974AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280033Lanyard · disconnectedSEA - DURING PREFLIGHT CHECK, L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED FROM SLIDE COVER LATCH. REATTACHED LANYARD BETWEEN GIRT BAR AND DOOR SLIDE COVER LATCH. (M)Feb 13, 2002 · N958AS · Doug DC983 · Emergency EquipmentSDR ZW0A0202004Tie Clip · brokenDURING CHECK-C MAINT THE UPPER FWD CORNER OF THE RT VENT BOX STRUCTURAL TIE CLIP WAS BROKEN. FABRICATED NEW CLIP AND INSTALLED PER SRM 51-30-6 AND SPM 6-30-07.Feb 13, 2002 · N967TW · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0202003Skin · gougedDURING CHECK-C MAINT FOUND 8 INCH LONG GOUGE WITH SHARP EDGES IN FUSELAGE STA 323 BETWEEN LONGERON 17L AND 18L. INSTALLED REPAIR PER SRM 53-04, FIG 38.Feb 10, 2002 · N9304C · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0280028Wire · disconnectedPDX - DURING LINE CHECK, FIRST CLASS EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED EMERGENCY TRACK LIGHT MODULE. LIGHTS THEN OPERATED PROPERLY. (M)Feb 9, 2002 · N947AS · Doug DC983 · Light System WiringSDR ASAA0280030Light · inoperativePDX - DURING PREFLIGHT CHECK, EMERGENCY FLOOR TRACK LIGHTS IN 1ST CLASS SECTION WERE FOUND TO BE INOPERATIVE. REPLACED DAMAGED SECTION OF WIRING. LIGHTS THEN OPERATED NORMALLY. (M)Feb 8, 2002 · N958AS · Doug DC983 · Emergency LightingSDR ASAA0280025Light · inoperativeSEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPRERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M_Feb 8, 2002 · N944AS · Doug DC983 · Emergency LightingSDR ASAA0280027Light · inoperativeSEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M)Feb 8, 2002 · N949AS · Doug DC983 · Emergency LightingSDR ASAA0280026Seat Track · corrodedPAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FUSELAGE STATION 1212-1296, BUTTOCK LINE PLUS 22. REPLACED SEAT TRACK PER SRM 53-05. (M)Feb 8, 2002 · N974AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0280024Connector · looseSEA - DURING FLIGHT, LEFT HYDRAULIC SYSTEM 'PRESS LOW' LIGHT ILLUMINATED AND PRESSURE FLUCTUATED BETWEEN 0 AND 100 PSI. LEFT SYSTEM AND THE POWER TRANSFER UNIT (PTU) WERE TURNED OFF. TIGHTENED LEAKING HYDRAULIC LINE CONNECTION TO THRUST REVERSER CONTROL VALVFeb 8, 2002 · N949AS · Doug DC983 · Hydraulic System, MainSDR ZW0A0201701Battery · dischargedTHE AFT LEFT AND RT OVERWING EMERGENCY OVERHEAD LIGHTS, AND THE ROW 13 EGRESS LIGHT, WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK FOR THE OVERWING LIGHTS, AND THE LAMP P/N 7732 FOR THE EGRESS LIGHT.Feb 8, 2002 · N971TW · Doug DC983 · Emergency LightingSDR ASAA0280019Light · inoperativeOAK - DURING LINE CHECK, EMERGENCY FLOOR TRACK LIGHTS CONTROLLED BY POWER SUPPLY B5-27 WERE FOUND TO BE INOPERATIVE. REPAIRED CHAFED WIRING. LIGHTS THEN OPERATED PROPERLY. (M)Feb 7, 2002 · N968AS · Doug DC983 · Emergency LightingSDR ASAA0280020Seat Track · corrodedPAE - DURING 30K CHECK, FOUND CORROSION ON SEAT TRACK AT FUSELAGE STATIONS, 1118, 1152, AND 1160, AT BUTTOCK STATION X PLUS 54, AND WATERLINE 2-2. REPAIRED SEAT TRACK PER SRM 53-05, FIG 4F. (M)Feb 7, 2002 · N974AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0280022Web · corrodedPAE - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB BETWEEN FS 608 AND 693. EXTEND WAS DETERMINED TO BE BEYOND LIMITS. REPLACED CORRODED WEB PER SRM'S 51-10-04 AND 51-30-02. (M)Feb 7, 2002 · N974AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0201603Angle · corrodedDURING CHECK-C FOUND CORROSION ON HORIZONTAL ANGLE ATTACHED TO TRAPEZOIDAL PANEL RBL 58, 7 INCHES AFT OF CENTER SECTION UPPER SPAR CAP; JUST AFT OF LT MLG SIDE STRUT UPPER MOUNT, 9 INCHES BELOW PRESSURE DECK. REMOVED AND REPLACED ANGLE PER SRM 6-7-01 PG 3, ANFeb 7, 2002 · N948TW · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280017Light · inoperativeSEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M)Feb 5, 2002 · N943AS · Doug DC983 · Emergency LightingSDR ASAA0280018Fuel Line · leakingFAI - INTERMITTENT FUEL ODOR IN COCKPIT AND CABIN NOTED DURING FLIGHT. RESECURED LOOSE FUEL LINE CONNECTION TO APU BURNER. ALSO, TIGHTENED BURNER CAN CLAMP. RAN APU. NO FUEL ODOR WAS NOTED. (M)Feb 4, 2002 · N949AS · Doug DC983 · APU Engine Fuel and Control
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