Boeing DC-9-83

Service difficulty reports · 16,530

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASAA0080475Power Supply · dischargedSEA - DURING MAINTENANCE CHECK, BOTH EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED POWER SUPPLY AND BOTH LIGHTS OPERATED NORMALLY. (M)Jul 22, 2000 · N979AS · Doug DC983 · Emergency LightingSDR ASAA0080474Wire · disconnectedLAS - PRIOR TO FLT 601, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 20-23 WERE FOUND TO BE INOPERATIVE. CONTRACT MAINTENANCE RECONNECTED WIRING/LIGHTS AND THE LIGHTS OPERATED NORMALLY. (M)Jul 21, 2000 · N962AS · Doug DC983 · Light System WiringSDR ASAA0080473Light · inoperativeSEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT SWITCH WAS FOUND BROKEN. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)Jul 20, 2000 · N958AS · Doug DC983 · Emergency LightingSDR TWAA0011401Csd · failedTHE LT CSD OIL TEMPERATURE ROSE INTO THE YELLOW BAND. THE APU WAS PREVIOUSLY DEFERRED INOPERATIVE PER MEL. MAKE AN UNSCHEDULED LANDING AT MCI. FOUND OIL TRANSFERRING FROM THE GEARBOX TO THE CSD. REPLACED THE CSD P/N 696233B. ALSO CORRECTED THE APU BY REPLJul 20, 2000 · N9414W · Doug DC983 · Alternator-Generator DriveSDR ASAA0080472Slide · failedPHX - DURING 30K CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)Jul 19, 2000 · N965AS · Doug DC983 · Escape SlideSDR TWAA0011302Battery · dischargedTHE COCKPIT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY BATTERIES. CHECK-C 2-7-00 JFK.Jul 19, 2000 · N9304C · Doug DC983 · Emergency LightingSDR 20001114SH013Csd · overheatedMBJ/ATL - FLT JM 057 - AFTER TAKEOFF, NR 1 CSD OIL TEMPERATURE APPROACHED RED BAND. THE AIRCRAFT RETURNED TO STATION WHERE TROUBLESHOOTING INCLUDING ENGINE RUN WERE CARRIED OUT. NO ABNORMALITIES DISCOVERED. AIRCRAFT SUBSEQUENTLY HAD THE SAME INDICATION PRIOJul 18, 2000 · N191AJ · Doug DC983 · Alternator-Generator DriveSDR ASAA0080471Wire · brokenSEA - PRIOR TO DEPARTURE OF FLIGHT 584 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED BROKEN WIRE IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (M)Jul 18, 2000 · N977AS · Doug DC983 · Light System WiringSDR ASAA0080470Battery · dischargedSEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 TO 33 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)Jul 18, 2000 · N962AS · Doug DC983 · Emergency LightingSDR ASAA0080468Wire · brokenANC - PRIOR TO DEPARTURE OF FLIGHT 190, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT WIRES AT ROW 24 WERE EXPOSED. REPAIRED BROKEN WIRE IN FLOOR TRACK AT ROW 24 AND OPERTED NORMALLY. (M)Jul 17, 2000 · N982AS · Doug DC983 · Light System WiringSDR ASAA0080467Seal · contaminatedAFTER ARRIVAL OF FLIGHT 405; CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. CLEANED PAINT OVERSPRAY FROM DOOR SEAL AND SEAL MATING SURFACE. ACCOMPLISHED GROUND PRESSURIZATION CHECK TO 3.0 PSID, NO LEAK NOTED. OPERATED DOOR THROUGH SEVERAL CYCLES AND OPERATEDJul 16, 2000 · N961AS · Doug DC983 · Passenger/Crew DoorsSDR ASAA0080466Sign · inoperativeSEA - DURING MAINTENANCE CHECK, THE FORWARD LEFT OVERWING EMERGENCY EXIT IDENTIFIER WAS FOUND TO HAVE ONLY TWO LAMPS ILLUMINATED. REPLACED EMERGENCY EXIT IDENTIFIER AND OPERATED NORMALLY. (M)Jul 16, 2000 · N961AS · Doug DC983 · Emergency LightingSDR ASAA0080465Battery · dischargedOAK - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE MID AND AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLYS AT ROW 22 FORWARD, ROW 22 AFT, AND ROW 24 AND OPERATED NORMALLY. (M)Jul 15, 2000 · N982AS · Doug DC983 · Emergency LightingSDR ASAA0080464Wire · brokenSEA - AFTER ARRIVAL OF FLIGHT 759, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT COVER DAMAGED AND SECTIONS OF THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN INOPERATIVE. REPAIRED BROKEN WIRE IN FLOOR TRACK AT ROW 28 AND OPERATED NORMALLY. (M)Jul 14, 2000 · N968AS · Doug DC983 · Light System WiringSDR ASAA0080463Battery · inoperativeOAK - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POER SUPPLY AND OPERATED NORMALLY. (M)Jul 14, 2000 · N982AS · Doug DC983 · Emergency LightingSDR TWAA0011101Light · inoperativeTHE EMERGENCY LIGHT AT THE FORWARD LT SIDE CABIN DOOR WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. NO CHECK-C.Jul 13, 2000 · N978TW · Doug DC983 · Emergency LightingSDR ASAA0080460Cargo Track · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1211 TO 1309, LONGERON 28R. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30-01. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0080459Cargo Track · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1113 TO 1155, LONGERON 28R. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30-00. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0080457Cargo Track · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON CARGO TRACK, FS 1174-1309, LONGERON 28L. REMOVED AND REPLACED CARGO TRACK SECTION IAW DC9 SRM 51-30-00. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0080438Longeron · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 29L, FS 1200. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1200 TO 1240 IAW DC9 SRM 53-02, FIG 18. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0080437Longeron · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 28L, FS 1200. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1200 TO 1220 IAW DC9 SRM 53-02, FIG 18. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0080454Web · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB, FS 1184, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS 1174 TO 1250 IAW DC9 SRM 51-30. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080453Web · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON FLOOR WEB, FS 570, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS 503 TO 597 IAW DC8 SRM 51-01, PAGE 1. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080450Web · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 503 TO 598, LBL 52. REMOVED DAMGED MATERIAL AND INSTALLED FILLER AND DOUBLER IAW DC9 SRM 51-10-03. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080449Web · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 313 TO 389, LBL 52. REMOVED AND REPLACED WEB IAW DC9 SRM 51-30-01. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080448Web · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON CUSP WEB, FS 217, LBL 6. REMOVED DAMAGED MATERIAL AND INSTALLED NEW SECTION AND DOUBLER FROM FS 214-219 IAW DC9 SRM 53-01, FIG 4, SH 3. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080446Angle · corrodedPHX - DURNG 30K CHECK, FOUND CORROSION ON CUSP ANGLE, FS 1193 TO 1210, LONGERON 18R. REMOVED DAMAGED MATERIAL AND SPLICED IN CUSP ANGLE REPAIR SECTION FROM FS 1185 TO 1240 IAW DC9 SRM 53-05, FIG 25 AND INSTALLED FRAME REPAIR SECTION IAW DC9 SRM 53-03, FIG 32.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080442Shear Tie · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON SHEAR TIE, FS 1220, LONGERON 30 TO 29R. REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-05. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, StructureSDR ASAA0080440Longeron · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 28R, FS 1254. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1254 TO 1280 IAW DC9 SRM 53-02, FIG 18. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0080439Longeron · corrodedPHX - DURING 30K CHECK, FOUND CORROSION ON LONGERON 30, FS 1241. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM FS 1241 TO 1275 IAW DC9 SRM 53-02, FIG 18 AND 53-14-03. (M)Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, Longeron/StringerSDR ASAA0080445Frame · corrodedPHX-DURING 30K CHECK CORROSION WAS FOUND ON FRAME FS 1271 LONGERON 28L TO 28R. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-03, FIG 2A.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0080458Seat Track · gougedDURING 30K CHECK GOUGES WERE FOUND ON SEAT TRACK, FS 1206 TO 1248, LBL 22.REMOVED AND REPLACED SEAT TRACK SECTION FROM FS 1029 TO 1306 IAW DC9 SRM 53-05.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0080461Skin · dentedDURING 30K CHECK DENT WAS FOUND IN FUSELAGE SKIN, FS 240 TO 250, LONGERON 17L TO 18L. REWORKED TO CONTOUR AND INSTALLED TITANIUM DOUBLER IAW DC9 SRM 53-04, FIG. 38, SH 28 THROUGH SH 31.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0080462Skin · corrodedDURING 30K CHECK CORROSION WAS FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN, FS 1220, LONGERON 29R. REPAIRED IAW ASA EA 5330-01439.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0080444Frame · corrodedDURING 30K CHECK CORROSION WAS FOUND ON FRAME, FS 1250, LONGERON 30.REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM LONGERON 27L TO 28R IAW DC9 SRM 53-03, PG 4A.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0080447Frame · corrodedPHX-DURING 30K CHECK CORROSION WAS FOUND ON FRAME, FS 1231, LONGERON 27R TO 28R. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION IAW DC9 SRM 53-03.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0080451Web · corrodedPHX-DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB, FS 427 TO 446, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01, FIG 4.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080452Web · corrodedPHX-DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB, FS 446 TO 465, LONGERON 18R. REMOVED DAMAGED MATERIAL AND INSTALLED DOUBLER IAW DC9 SRM 53-01. FIG 4Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080455Web · corrodedPHX-DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB, FS 1211 TO 1231, LONGERON 18R. REMOVED AND REPLACED WEB FROM FS1174 TO 1250 IAW DC9 SRM 51-30-02 AND 51-30-05.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080456Web · corrodedPHX-DURING 30K CHECK CORROSION AND CRACKS WERE FOUND ON CUSP WEB, FS1250 TO 1309, LONGERON 18R. REMOVED AND REPLACED WEB IAW DC9 SRM 53-01.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080441Shear Tie · corrodedPHX-DURING 30K CHECK CORROSION WAS FOUND ON SHEAR TIE, FS 1211, LONGERON 30 TO 29R.REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-05.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, StructureSDR ASAA0080443Frame · corrodedPHX- DURING 30K CHECK CORROSION WAS FOUND ON FRAME, FS1231, LONGERON 28L TO 27R. REMOVED DAMAGED MATERIAL AND SPLICED IN NEW SECTION FROM LONGERON 26L TO 29R IAW DC9 SEM 53-03, PG 4A.Jul 12, 2000 · N961AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0080436Battery · inoperativeSEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)Jul 12, 2000 · N962AS · Doug DC983 · Emergency LightingSDR ASAA0080435Power Supply · inoperativeSEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROW 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)Jul 12, 2000 · N962AS · Doug DC983 · Emergency LightingSDR ASAA0080433Power Supply · inoperativePHX - DURING 30K CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)Jul 11, 2000 · N961AS · Doug DC983 · Emergency LightingSDR ASAA0080430Slide · failedPHX - DURING 30K CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)Jul 11, 2000 · N965AS · Doug DC983 · Escape SlideSDR TWAA0010901Battery · dischargedTHE AFT GALLEY DOOR EMERGENCY LIGHT AND THE EGRESS LIGHTING AFT OF CABIN ROW 28 WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY FOR ROW 28. CHECK-C 6-30-00 MCI.Jul 11, 2000 · N9409F · Doug DC983 · Emergency LightingSDR GTIA000251Light · inoperativeDTW - EMERGENCY PATH 1ST LIGHT NOT WORKING. RELAMPED 1ST SOCKET OF EMERGENCY PATH LIGHTING IAW MD 80 MM 25-62-05. OPS CHECK GOOT AT THIS TIME. NO DEFECTS NOTED. (M)Jul 10, 2000 · N808NK · Doug DC983 · Emergency LightingSDR 20001114SH012Pump · failedATL/MBJ - FLT JM 052 - PRIOR TO FLIGHT, AT ENGINE START, THE LEFT NR 1 ENGINE HYDRAULIC PUMP INDICATED ZERO PSI. AFTER TROUBLESHOOTING, PUMP REPLACED AND AIRCRAFT DISPATCHED FOR SERVICE. THIS REPORT REMAINS OPEN UNTIL A STRIP REPORT IS AVAILABLE. TOTAL LANDJul 9, 2000 · N191AJ · Doug DC983 · Hydraulic Pump (Electric/Engine), MainSDR 20001114SH002Pump · failedMBJ/ATL - FLT JM 053 - DURING ENGINE START, HYD PRESSURE REMAINED AT ZERO. CAUSE OF THE PUMP''S FAILURE SEEMED TO HAVE BEEN A WEAR-OUT OF ITS COMPONENTS. THIS WAS THE FIRST REMOVAL SINCE IT WAS INSTALLED IN A NEW CONDITION. THIS PART IS MAINTAINED ''ON CONDJul 9, 2000 · N191AJ · Doug DC983 · Hydraulic Pump (Electric/Engine), Main
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