Boeing 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 TWAA0009401Support Bracket · puncturedDURING CHECK-C MAINT, THE RT WING T/E BUTE DOOR SUPPORT RAIL, INBOARD RIGHT T/E HAD HOLE PUNCTURED IN IT. MADE BEAM (P/N 5936844-7), CLIP (5936844-13), CLIP (5936814-15) AND HEAT TREATED AND PAINTED PER DOUGLAS DRAWING 5936844. MADE CLIP (P/N 5936824-7) PER Jun 9, 2000 · N9409F · Doug DC983 · Wing Miscellaneous StructureSDR TWAA0009314Cargo Track · corrodedDURING CHECK-C MAINT, FOUND AFT CARGO, RT CARGO TIE DOWN TRACK WITH CORROSION PITTING IN CENTER AND ON FLANGES AT STA 1211 TO 1320. REMOVED CORRODED TIE DOWN TRACK AND INSTALLED NEW TIE DOWN TRACK PER SPM 6-70-01, PAGE 3B AND DRAWING 5936663.Jun 9, 2000 · N9409F · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000853Cargo Track · corrodedINSPECTION FOUND FORWARD CARGO LT TIE DOWN TRACK CORRODED ON LOWER SURFACE AT SPLICE, STA 512. THE CORRODED SECTION WAS REMOVED AND NEW TRACK AND SPLICES WERE INSTALLED IAW SRM 51-10-4, 53-05, FIGURE 4G, 51-10-7, 51-30-05, AND 51-30-01.Jun 9, 2000 · N14879 · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000852Panel · crackedINSPECTION FOUND A 1 INCH CRACK IN VERTICAL STABILIZER PANEL NR 6310. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-3, AND 51-30-2.Jun 9, 2000 · N14879 · Doug DC983 · Vertical Stabilizer, Plate/SkinSDR TWAA0009609Seat Track · corrodedDURING CHECK-C MAINT, CABIN STA 1155 LRL 47 HAD CORROSION ON TRACK NUMBER 2. REPLACED TRACK SECTION PER SRM 53-05, FIG 4F.Jun 8, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0009608Floorboard · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOOR PANEL SUPPORT AT STA 200, BL 0 TO RBL 50. REMOVED CORROSION PER SPM 6-80-1. REPLACED SUPPORT EXTRUSION PER DWG 5930545 AND SPM 6-70-01. TREATED PER SRM 51-10-3.Jun 8, 2000 · N9305N · Doug DC983 · Fuselage Floor PanelSDR TWAA0009607Seat Track · corrodedDURING CHECK-C MAINT, NUMBER 3 CHAIR TRACK FROM STA 1031 TO 1309 HAD CORROSION BEYOND LIMITS. REPLACED NUMBER 3 CHAIR TRACK PER IPC 53-40-00 FIG 19B AND SRM 53-05 FIG 4F AND SRM 51-60-0. FIFTEEN FEET 9 INCHES OF TRACK REPLACED WITH TRACK SPLICE AT THE AFT ENJun 8, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA000224Light · inoperativeLGA - E-PATH LIGHT BETWEEN ROW 9-12 INOPERATIVE. FOUND LOOSE CONNECTION. SECURED CONNECTION, OPS CHECK OK. (M)Jun 7, 2000 · N809NK · Doug DC983 · Emergency LightingSDR TWAA0012105Spar · corrodedDURING CHECK-C MAINT ON THE RT WING, CORROSION WAS FOUND ON THE REAR SPAR BETWEEN CENTER AND O/B AILERON HINGE. FABRICATED ACCORDING TO SRM 59-09 FIG 5. FABRICATED, FINISHED, AND INSTALLED FILLER SHIM AND DOUBLER PER SRM 57-09 FIG 5 AND SRM 57-01 PARAGRAPH 3Jun 7, 2000 · N9305N · Doug DC983 · Wing SparSDR TWAA0009604Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOORBEAM, LEFT AFT LAV STA 1338, 20 INCH LBL AND 30 IN LBL. CORROSION REMOVED PER SPM 6-80-01 PAGE 31 TO 42, AND SRM 51-10-3 PARAGRAPH 23. REPAIRED DAMAGED AREA PER SSRM 53-00-101 PAGE 201.Jun 7, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0009310Beam · corrodedDURING CHECK-C MAINT IN THE AFT CARGO, FOUND CORROSION IN THRESHOLD BEAM AREA, BETWEEN BOTTOM CARGO DOOR STOPS. REMOVED CORROSION PER SPM 6-80-01 PAGE 1, ITEM 3A, B, PAGE 2 AND PAGE 3. REMOVED CORRODED BEAM PER SPM 6-70-01 PAGE 3 DRAWING 5930483, SRM 51-60-0Jun 7, 2000 · N9409F · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009309Door Frame · damagedDURING CHECK-C MAINT, THE MID CARGO DOOR JAMB AT APPROX LONGERON 24R HAD IMPACT DAMAGE WITH SHARP CORNER AND EDGE APPROX 20 INCHES UP FROM THRESHOLD PLATE, STA 693. BLENDED IMPACT DAMAGE ON MID CARGO DOOR JAMB PER SPM 53-05 PAGE 495 FIG 109. ALODINED PER SRMJun 7, 2000 · N9409F · Doug DC983 · Fuselage Main, StructureSDR TWAA0009305Threshold · corrodedDURING CHECK-C MAINT, FOUND CORROSION IN AFT CARGO THRESHOLD PLATE, STA 1212. REMOVED CORROSION PER SPM 6-80-01 PAGE 1 ITEMS 3A AND B, AND PAGE 2 AND 3. REPAIRED PER SRM 53-01 FIG 4 SHEET 3, AND ARA 16728A DATED 5-26-00, SRM 51-60-0 PAGE 36, SRM 51-60-0 PAGEJun 7, 2000 · N9409F · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009606Seat Track · wornDURING CHECK-C MAINT, THE FIRST OFFICER''S RT FWD CHAIR TRACK WAS WORN ON UPPER AND LOWER SURFACES. REPLACED FLOOR TRACK PER MM 53-40-01 PAGE 203.Jun 6, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0009406Frame · corrodedDURING CHECK-C MAINT, THE AFT CARGO BIN HAD CORROSION ON FORMER RING AT STA 1271, LONGERON 30. AT STA 1271 ON FORMER RING AT LONGERON 30 REMOVED CORROSION PER SPM 6-80-01. CUT OUT DAMAGED PORTION OF FORMER RING AND REPAIRED WITH SPLICE PER SRM 53-03, FIG 2A Jun 6, 2000 · N9305N · Doug DC983 · Fuselage Main, FrameSDR TWAA0009405Bracket · crackedDURING CHECK-C MAINT, A FUSELAGE ANGLE BRACKET WAS CRACKED AT STA 946, LBL 7 INSIDE KEEL BEAM LOWER FWD CORNER. FABRICATED PART FROM 7075-T6 PER SPM AND PRINT 9936368, SHEET 1 PART 101.Jun 6, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009308Web · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE ON RT SIDE NEXT TO STA 728 AROUND LIGHTNING HOLE. REMOVED CORROSION PER SPM 6-80-01 PAGE 1 TO 3. MADE REPAIR PER SRM 53-01 FIG 4. INSTALLED RIVETS PER SRM 51-30-03.Jun 6, 2000 · N9409F · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009307Seat Track · wornDURING CHECK-C MAINT, FOUND GROOVES WORN IN NUMBER 3 CHAIR TRACK STA 1041 TO 1072, 1147, 1240 AND 1260. CORROSION WAS AT STA 1058, 1072, 1079 TO 1136, 1200 AND 1226. REMOVED AND REPLACED CHAIR TRACK FROM PRODUCTION SPLICE AT STA 1032 TO STA 1261, PER SRM 53-Jun 6, 2000 · N9409F · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0009605Stiffener · crackedDURING CHECK-C MAINT AT STA 996 BODY FAIRING STIFFENER BOTTOM CORD HAD A 6.5 INCH CRACK AND THE REPAIR ANGLE HAD 1.5 INCH CRACK. STOP DRILLED CRACKS PER SRM 53-00. ACCOMP NDT HIGH FREQ EDDY CURRENT ON STIFFENER PER 51-00-03 PART 6. FABRICATED NEW ANGLE AND Jun 5, 2000 · N9305N · Doug DC983 · Aerodynamic FairingsSDR TWAA0009304Floor Support · corrodedDURING CHECK-C MAINT AT CABIN STA 1155, LBL 33, FOUND CORROSION ON FLOOR SUPPORT BETWEEN NUMBER 2 AND 3 TRACKS. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-14-3, FIG 12 AND SPM 6-70-01 PAGE 3. PROTECTIVE TREATMENT OF SUPPORT PER SRM 51-10-3. INSTALLED WJun 5, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080361Light · defectiveSEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)Jun 4, 2000 · N960AS · Doug DC983 · Emergency LightingSDR TWAA0009005Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CABIN MEMBRANE CORRODED AT STA 503 TO 522, LONGERON 18L. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01, PAGE 9.Jun 4, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0009009Skin · damagedDURING CHECK-C MAINT ON LT WING LOWER SURFACE OF THE TRAILING EDGE, THE I/B FIXED FIBERGLASS PANEL HAD A HOLE IN IT. SANDED AREA AND INSTALLED 3 LAYERS OF FIBERGLASS LAYUPS AND SANDED SMOOTH PER SRM 51-70-1B, FIG 5.Jun 3, 2000 · N9409F · Doug DC983 · Wing, Plate/SkinSDR ASAA0080360Wire · disconnectedONT - PRIOR TO DEPARTURE OF FLIGHT 405, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED LOOSE WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)Jun 2, 2000 · N977AS · Doug DC983 · Light System WiringSDR TWAA0008702Module · wornTHE EGRESS LIGHT AT ROW 33 END LIGHT WAS INOPERATIVE. REPLACED THE LIGHT MODULE.Jun 2, 2000 · N968TW · Doug DC983 · Emergency LightingSDR 20001114SH019Sensor · failedMBJ/ATL - FLT JM 053 - AIRCRAFT RETURNED TO RAMP DUE TO A RECURRENCE OF A SLAT/FLAP DISAGREEMENT LIGHT INDICATION FAULT AT 18,000 FEET. THE AIRCRAFT WAS ACCELERATED TO 280 KNOTS AND THE SLAT OVERSPEED AURAL WARNING CAME ON. QRH PROCEDURE ACCOMPLISHED, ACFT RJun 1, 2000 · N192AJ · Doug DC983 · Leading Edge Slat ActuatorSDR TWAA0009008Floor Support · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT AT STA 148, RBL 59. REMOVED CORROSION PER SPM 6-80-01. TREATED PER SRM 51-10-3 AND REINSTALLED PART PER SRM 51-30-02.Jun 1, 2000 · N9409F · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009007Structure · corrodedDURING CHECK-C MAINT, FOUND CORROSION UNDER WATER LINE PLATE AT STA 160, RBL 50 AT O/B AFT CORNER. REPLACED MEMBRANE WITH NEW PART PER SPM 6-70-01, AND INSTALLED PER SRM 51-30-02. TREATED PER SRM 51-10-3.Jun 1, 2000 · N9409F · Doug DC983 · Fuselage Main, StructureSDR TWAA0009006Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, BETWEEN STA 1022 AND 1002. REPAIRED MEMBRANE PER SRM 53-01, PAGE 9 (TYPICAL DOUBLER REPAIR).Jun 1, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0009004Strap · corrodedDURING CHECK-C MAINT, THE RT WING UPPER O/B SPOILER, O/B END, TRAILING EDGE SUPPORT STRAP HAD CORROSION. REMOVED DAMAGED SUPPORT STRAP AND REPLACED WITH NEW PART PER SRM 51-01 ITEM C.Jun 1, 2000 · N9305N · Doug DC983 · SpoilersSDR ASAA0080352Seat Track · corrodedPHX: DURING 30K CHECK CORROSION WAS FOUND SEAT TRACK, FS 200 TO 237, RBL 45.REMOVED AND REPLACED SEAT TRACK SECTION IAW DC9 SRM 53-05, FIG 4.May 31, 2000 · N960AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0008807Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 750 TO 731, AND STA 712 TO 731. CUT OUT CORRODED AREA AND REPAIRED PER SRM 53-01. TREATED AREA PER SRM 51-10-3.May 31, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR GTIA000213Light · inoperativeDTW - EMERGENCY PATH LIGHTING NOT WORKING FROM ROW 29 AFT. GROUND CHECKED EMERGENCY PATH LIGHTING AND FOUND IT TO BE OPERATIONAL. ALL LIGHTS LIT UP. ALL IAW MD 80 MM SECTION 33-53-01. (M)May 30, 2000 · N808NK · Doug DC983 · Emergency LightingSDR TWAA0008410Light · malfunctionedDURING ROUTINE INSPECTION, FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT VERY DIM. REPLACED LIGHT ASSEMBLY. AC03 5-12-00 JFK.May 29, 2000 · N9404V · Doug DC983 · Emergency LightingSDR GTIA000211Cover · looseMCO - FLT 135 - PLASTIC COVERING ON EMERGENCY TRACK LIGHTING COMING OFF AROUND ROW 8. SECURED PLASTIC COVERING ON EMERGENCY TRACK LIGHTING ON ROW 8 SECTION PER MM 33-50-00. (M)May 28, 2000 · N802NK · Doug DC983 · Emergency LightingSDR ASAA0080350Wire · disconnectedSEA - PRIOR TO FLT 400 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN FIRST CLASS WOULD NOT ILLUMINATE. REPLACED WIRING SECTION AND THE LIGHTS OPERATED NORMALLY. (M)May 27, 2000 · N958AS · Doug DC983 · Light System WiringSDR TWAA0008809Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CABIN CORROSION ON MEMBRANE AT LONGERON 18R, STA 1098 TO 1079 AND STA 1098 TO 1117. CUT OUT CORROSION AND FABRICATED DOUBLER FROM 0.025, 7075-T6 MATERIAL. INSTALLED DOUBLER WITH 1422 SEALANT AND 2 ROWS OF FASTENERS PER SRM 53-01 FMay 26, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0008808Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CABIN CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 560 TO 579 AND STA 541 TO 522. REMOVED CORROSION PER SRM 51-10-3. PRIMED PER 51-10-3. REPAIRED PER SRM 53-01 FIG 4 PAGE 18.May 26, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR CALA0000755Skin · bulgedINSPECTION FOUND LT FUSELAGE EXTERIOR SKIN BULGED AT FASTENER, STA 541 BETWEEN LONGERON 25L AND 26L. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW EA 9-5331-2-A-0684 AND ECRA 5330-02958.May 26, 2000 · N14879 · Doug DC983 · Fuselage Main, Plate/SkinSDR GTIA000208Cover · looseDTW - FLT 606 - EMERGENCY LIGHT COVER FOR FLOOR LIGHTING NEEDS RESECURING. RESECURED EMERGENCY FLOOR LIGHT COVER IAW MD80 MM 33-53-01. (M)May 25, 2000 · N814NK · Doug DC983 · Emergency LightingSDR TWAA0008810Floorbeam · corrodedDURING CHECK-C MAINT, IN LT CABIN FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L STA 655 TO 674. REMOVED CORROSION PER SRM 51-10-3. PRIMED PER SRM 51-10-3B. INSTALLED FASTENERS PER SRM 51-10-05.May 25, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0008804Seat Track · gougedDURING CHECK-C MAINT, CHAIR TRACK HAD GOUGES AT STA 356 TO 389, RBL 22, AND AT STA 243 TO 313 RBL 22. REMOVED AND BLENDED GOUGES PER SRM 53-05, FIG 4B-1, AND SPM 6-80-01. PRIMED, SANDED AREA PER SRM 51-10-3.May 25, 2000 · N9409F · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0008404Lens · brokenDURING LANDING IT WAS NOTED THAT THE EGRESS LIGHT COVER WAS BROKEN AT ROWS 18DEF. REPLACED LENS. AC04 4-12-00 DFW.May 25, 2000 · N968TW · Doug DC983 · Emergency LightingSDR TWAA0008402Symbol Generator · failedDURING CLIMB EXPERIENCED LOSS OF INDICATION ON LEFT EFIS. REPLACED EFIS SYMBOL GENERATOR. AC05 3-25-00 DFW.May 25, 2000 · N9307R · Doug DC983 · Flight Management Computing Hardware SystemSDR ASAA0080349Battery · dischargedSEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)May 24, 2000 · N968AS · Doug DC983 · Emergency LightingSDR TWAA0008811Splice Plate · crackedDURING CHECK-C MAINT, ON RT WING, WING STA 164 L/E SPLICE PLATE WAS CRACKED AT BOLT HOLE. EDDY CURRENT INDICATED CRACK FROM 1 HOLE THRU ANOTHER HOLE TO EDGE PER PART 6-57-00-03 OF NDT MANUAL. FABRICATED AND INSTALLED WING L/E DOUBLER AT WING STA 164, PER SSRMay 24, 2000 · N9409F · Doug DC983 · Wing, Plate/SkinSDR TWAA0008806Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR MEMBRANE AT LONGERON 18L, STA 674 TO 693 AND STA 845 TO 826. REMOVED CORROSION PER SPM 6-80-01. TREATED SURFACES PER SRM 51-10-3.May 24, 2000 · N9409F · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0008401Landing Gear · damagedAFTER TAKEOFF GOT A RED LEFT MAIN LIGHT AND DOOR LIGHT ILLUMINATED. REPLACED LEFT MAIN GEAR ASSEMBLY. 0001 4-10-00 DFW.May 24, 2000 · N939AS · Doug DC983 · Landing Gear SystemSDR TWAA0008805Seat Track · corrodedDURING CHECK-C MAINT, FOUND CORROSION IN CHAIR TRACK AT RBL 22 AT THE FOLLOWING STATIONS: 363 TO 368, 237, 530 TO 460, 427 TO 462, 408 TO 420, 636, 788, AND 484 TO 503. REMOVED CORROSION PER SRM 51-10-3, 53-05 FIG 4B-1, AND SPM 6-80-01. PRIMED PER SRM 51-10-May 23, 2000 · N9409F · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0008803Attach Angle · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON ATTACH ANGLE AT FLOOR LEVEL OF EPC PANEL, AFT SIDE, STA 160L. REMOVED CORROSION PER SPM 6-80-01, PAGE 1 ITEM 2(A).May 23, 2000 · N9409F · Doug DC983 · Fuselage Main, Attach Fittings
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