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 TWAA0003401Battery Pack · inoperativeTHE COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE WITH THE SWITCH IN THE ON POSITION. REPLACED THE BATTERY PACK. CHECK-C 8-4-99 STL.Feb 29, 2000 · N9622A · Doug DC983 · Emergency LightingSDR CALA0000225Channel · crackedINSPECTION FOUND A 3 INCH CRACK IN LT MLG I/B DOOR UPPER L/E CORNER. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, AND 51-30-08.Feb 29, 2000 · N938MC · Doug DC983 · Landing Gear DoorsSDR CALA0000224Web · corrodedINSPECTION FOUND LOWER VENTRAL DOOR THRESHOLD WEB AFT OF SEAT RETAINER AT FS 1330, RBL 16 CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-03. A DOUBLER WAS INSTALLED IAW SRM 51-10-03 AND 53-05. REMOVED AND REPLACED SEAL IAW SRM 51-30 AND 51-10.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000222Web · corrodedINSPECTION FOUND LOWER CUSP CORRODED AT FS 160-218, LBL 56-62. THE CORRODED AREA WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-03, 51-30-05, AND 51-30-07.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000221Frame · corrodedINSPECTION FOUND AFT CARGO DOOR CUTOUT LOWER FRAME CORRODED AT FS 1136-1193, L27R. THE CORROSION WAS REMOVED IAW SRM 51-10-03. A NEW STRAP WAS INSTALLED IAW SRM 53-05, FIGURE 3, 51-10-04, AND 51-10-03.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Main, FrameSDR CALA0000220Floorbeam · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160-200, RBL 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-04, 53-14-01, AND 51-30-02.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0003806Galley Track · corrodedDURING CHECK-C MAINT, THE NUMBER 4 GALLEY TIE DOWN AREA TRACK HAD CORROSION ON THE OTBD TRACK, FWD AND AFT, STA 1155 TO 1193. REPLACED TRACK PER SRM 53-05, PAGE 10G. PRIMED PER 51-10-03.Feb 28, 2000 · N9406W · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0003805Galley Track · corrodedDURING CHECK-C MAINT, THE NUMBER 3 GALLEY TIE DOWN TRACK AREA HAD CORROSION ON OTBD TRACK, FWD AND AFT OF STA 1117 TO 1155. REPLACED TRACK PER SRM 53-05, PAGE 10G. PRIMED PER SRM 51-10-03.Feb 28, 2000 · N9406W · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0003804Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON SUB FLOOR MEMBRANE AT STA 160 TO 200, LBL 6 IN TO RBL 53 INCHES. REPLACED SUB FLOOR MEMBRANE STA 160 TO 200, LBL 12 TO RBL 59, WITH 0.020 7075-T6, INSTALLED WITH SEALER AND 3 ROWS OF ATTACHMENT FASTENERS PER SRM 53-01,Feb 28, 2000 · N9406W · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0003735Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 1155, BETWEEN NUMBER 3 AND 4 GALLEYS TIE DOWN TRACK. REPLACED FLOOR SUPPORT PER SPM 6-70-01. PRIMED AND PAINTED PER SRM 51-10-03.Feb 28, 2000 · N9406W · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0003734Angle · crackedDURING CHECK-C MAINT, THE LOWER FAIRING ATTACH STRUCTURE CRACKED FWD INBD CORNER OF RT MLG WHEEL WELL, STA 943 RBL 8. REPLACED ATTACHMENT CHANNEL PER SPM 6-70-01 PAGE 3, PARA 4B AND DOUGLAS DRAWING 5930584.Feb 28, 2000 · N9406W · Doug DC983 · Aerodynamic FairingsSDR TWAA0003733Angle · crackedDURING CHECK-C MAINT, FWD FAIRING ATTACH STRUCTURE WAS CRACKED, FWD INBD CORNER, LT MLG WHEEL WELL STA 943, LBL 8. REPLACED ATTACHMENT CHANNEL PER SPM 6-70-01, PAGE 3 PARA 4B AND DOUGLAS DRAWING 5930584.Feb 28, 2000 · N9406W · Doug DC983 · Aerodynamic FairingsSDR TWAA0003732Keelbeam · crackedDURING CHECK-C MAINT, IN RT WHEEL WELL, FWD INBD CORNER AT KEEL BEAM AREA, ATTACHMENT ANGLE CRACKED IN RADIUS .5 INCH LONG. REPLACED ATTACH ANGLE PER SPM 6-70-01, PAGE 3 APRA 4B AND DOUGLAS DRAWING 9936368.Feb 28, 2000 · N9406W · Doug DC983 · Fuselage Main, KeelSDR TWAA0003731Keelbeam · crackedDURING CHECK-C MAINT, THE LT WHEEL WELL, FWD INBD CORNER AT KEEL BEAM AREA, ATTACH ANGLE CRACKED IN RADIUS .375 INCH LONG. REPLACED ATTACH ANGLE PER SPM 6-70-01, PAGE 3, PARA 4B, AND DOUGLAS DRAWING 9936368.Feb 28, 2000 · N9406W · Doug DC983 · Fuselage Main, KeelSDR ASAA0080185Slide · failedPHX - DURING 30K CHECK, THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ASSEMBLY. (M)Feb 27, 2000 · N969AS · Doug DC983 · Escape SlideSDR ASAA0080173Light · inoperativePDX - DURING MAINTENANCE CHECK, THREE CONSECUTIVE TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT GALLEY. REPLACED TWO LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)Feb 27, 2000 · N950AS · Doug DC983 · Emergency LightingSDR 20000329SH040Tire · failedDEFECT: THROWN TREAD FROM CARCASS. CAUSE: UNDETERMINED. TIRE SENT TO MANUFACTURER FOR ANALYSIS. PREVENTIVE ACTION: PENDING COMPLETE INVESTIGATION (INTERIM) ONLY USING NEW TIRES. (X)Feb 27, 2000 · Doug DC983 · TireSDR TWAA0003301Wire · wornTHE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROWS 14 AND 15, ROWS 22 TO 24. REPLACED A CABLE WIRE MODULE AT BOTH LOCATIONS. CHECK-C 7-18-99 STL.Feb 26, 2000 · N9615W · Doug DC983 · Light System WiringSDR AALA20000353Valve · defectiveSEA - FLT 330 - DURING FLIGHT, RED NOSE GEAR LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP. DIVERTED AND LANDED SEA WITHOUT INCIDENT. REPLACED SCHRAEDER VALVE AD O-RING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Feb 26, 2000 · N592AA · Doug DC983 · Nose/Tail Landing GearSDR ASAA9980051Spring · brokenSEA - AFTER ARRIVAL OF FLT 115, CREW REPORTED THE FLIGHT COMPT LEFT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDOW AFT LATCH SPRING BROKEN. REPLACED SPRING AND OPERATED NORMALLY. (M)Feb 25, 2000 · N950AS · Doug DC983 · Flight Compartment WindowsSDR CALA0000206Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STA 1418, LONGERON 2L IN TAIL COMPARTMENT CEILING. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-04, 51-10-03, AND 51-30-05.Feb 25, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000205Floorbeam · crackedINSPECTION FOUND FLOOR SUPPORT WEB CRACKED STA 1287-1301, RBL 2. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Feb 25, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR AALA20000348Wire · shortedORD - FLT 1694 - DURING FLIGHT, ELECTRICAL SPARKS REPORTED FROM TOP AFT GALLEY NUMBER 4 OVEN. CIRCUIT BREAKER POPPED AND SPARKS STOPPED. LEFT CIRCUIT BREAKER OPEN AND LANDED ORD WITHOUT INCIDENT. REPAIRED PINCHED WIRING HARNESS BETWEEN OVEN AND AIRCRAFT STRFeb 25, 2000 · N563AA · Doug DC983 · Equipment/Furnishings WiringSDR CALA0000203Intercostal · crackedINSPECTION FOUND THE LOWER ANTI-COLLISION BEACON PANEL ATTACH STRUCTURE CORRODED AND A 3 CRACK IN INTERCOSTAL. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW SRM 51-10-03 AND 53-01, FIGURE 1. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTFeb 24, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000202Cargo Track · corrodedINSPECTION FOUND AFT CARGO LEFT TIE DOWN TRACK CORRODED AT FS 1200-1320. THE CARGO TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01, 51-30-05, 51-10-04, AND 51-30-03.Feb 24, 2000 · N938MC · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000200Cargo Track · crackedINSPECTION FOUND A 1.5 CRACK IN AFT CARGO PIT RT CARGO TIE DOWN TRACK AT STA 1117. A SECTION OF CARGO TRACK WAS SPLICED IN IAW SRM 53-05, FIGURE 4G.Feb 24, 2000 · N938MC · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000199Angle · corrodedINSPECTION FOUND AFT CARGO BAY GILL LINER SUPPORT Z-ANGLE CORRODED AT RT CARGO TIE DOWN TRACK, STA 1155. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Feb 24, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000198Skin · dentedINSPECTION FOUND SKIN OF HORIZONTAL STABILIZER LE OB SECTION IB END DENTED. A DOUBLER WAS INSTALLED IAW EA 9-5513-2-A0602 AND SRM 51-30-2.Feb 24, 2000 · N938MC · Doug DC983 · Horizontal Stabilizer, Plate/SkinSDR CALA0000197Rib · gougedINSPECTION FOUND LEFT ELEVATOR L/E RIB NR 11 GOUGED AND DENTED. THE RIB WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.Feb 24, 2000 · N938MC · Doug DC983 · Elevator, Spar/RibSDR ASAA0080172Wire · disconnectedSEA - PRIOR TO DEPARTURE OF FLT 274, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)Feb 23, 2000 · N975AS · Doug DC983 · Light System WiringSDR GTIA0000108Light · inoperativeEMERGENCY FLOOR TRACK LIGHTS ARE OUT IN ROWS 1, 2 AND 3 AND 2 IN AFT OF AIRCRAFT. RELAMPED PER MM 33-50-00, OPS CHECKS GOOD. (M)Feb 23, 2000 · N809NK · Doug DC983 · Emergency LightingSDR CALA0000194Splice · corrodedINSPECTION FOUND SPLICES FOR TIE DOWN AT FS 1212 CORRODED. THE SPLICES WERE REMOVED AND NEW SPLICES WERE INSTALLED IAW SRM 51-30-2 AND 51-10-3.Feb 23, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000193Floorbeam · crackedINSPECTION FOUND FLOOR SUPPORT WEB CRACKED AT STA 1287-1301, BL 0. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Feb 23, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR CALA0000192Bracket · brokenINSPECTION FOUND TRANSITION ANGLE ATTACH BRACKET BROKEN AT FS 514, LONGERON 23L. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-04, 51-10-02, 51-10-03, AND 51-30-01.Feb 23, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0003304Skin · damagedDURING CHECK-C MAINT, A 3 INCH DENT, .5 INCH WIDE AND .125 DEEP HAD A SCAB PATCH WITH BLIND FASTENERS, APPROX 3 FEET AFT OF THE FORWARD LEFT CABIN DOOR AND 1.5 FEET BELOW DOOR, ON SIDE OF FUSELAGE. ACCOMP SKIN PANEL REPAIR PER SSRM 53-10-107, PAGE 202 AND SRMFeb 22, 2000 · N9406W · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0080171Wire · disconnectedSEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M)Feb 21, 2000 · N947AS · Doug DC983 · Light System WiringSDR TWAA0003022Floorbeam · corrodedDURING CHECK-C MAINT, MEMBRANE WAS CORRODED ON LT SIDE LONGERON 18, STA 660 TO 665. REMOVED CORROSION PER SPM 6-80-01. ALODINED AND PRIMED PER SRM 51-40-3. FABRICATED DOUBLER FROM TWA SN 55-0261. INSTALLED DOUBLER WITH AD RIVETS. SEALED WITH RRC 1422 PER Feb 21, 2000 · N9406W · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0002903Cover · missingTHE RED EGRESS LIGHT COVER WAS MISSING AT CABIN ROW 30. REPLACED THE RED COVER. CHECK-C 8-11-99 MCI.Feb 21, 2000 · N9413T · Doug DC983 · Emergency LightingSDR CALA0000179Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN LEFT MLG I/B DOOR AT LOWER FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW EA 5281-2-A064 AND ECRA 5280-01220.Feb 21, 2000 · N938MC · Doug DC983 · Landing Gear DoorsSDR ASAA0080505Shear Tie · corrodedPHX - DURING SCHEDULED 30K CHECK, THE AFT CARGO COMPARTMENT STATION 1287 BETWEEN LONGERON 29L TO 30L SHEAR TIE WAS FOUND TO BE CORRODED. REPAIRED PER SRM. (M)Feb 20, 2000 · N969AS · Doug DC983 · Fuselage Main, StructureSDR TWAA0002901Unknown · smokeTHERE WAS SMOKE IN THE COCKPIT AND CABIN DURING TAKEOFF. CLEARED UP IN 5 MINUTES. FOUND OIL IN THE ENGINE END CAPS. REPLACED THE ENGINE. CHECK-C 10-28-99 STL.Feb 20, 2000 · N9307R · Doug DC983 · Air Distribution SystemSDR ASAA0080141Floor Support · corrodedPHX - DURING 30K CHECK, THE MAIN CABIN FLOOR SUPPORT AT FS 180, RBL 25 WAS FOUND CORRODED. REPAIRED PER SRM 53-14-1, FIG 11. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080170Seat Track · corrodedPHX - DURING 30K CHECK, THE RIGHT MAIN CABIN SEAT TRACK AT FS 400 TO 474, RBL 22 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-05, FIG 4B. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0080169Web · corrodedPHX - DURING 30K CHECK, THE CUSP MEMBRANE AT FS 1142, LBL 58 ON THE TOP SURFACE WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080168Web · corrodedPHX - DURING 30K CHECK, THE WEB IN THE AFT CARGO COMPARTMENT WAS FOUND CORRODED ON THE UPPER FLANGE AROUND NUTPLATE HOLES AT FS 1307 AND 1320 BETWEEN LONGERON 27R AND 28R. REMOVED CORROSION AND REPAIRED PER SRM 51-30-2 AND 51-30-5. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080167Web · corrodedPHX - DURING 30K CHECK, THE WEB IN THE AFT CARGO COMPARTMENT WAS FOUND CORRODED ON THE UPPER FLANGE AT FS 1307 AND 1320 BETWEEN LONGERON 27L AND 28L. REMOVED CORROSION AND REPAIRED PER SRM 53-01, FIG 4 AND 51-30-5. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080166Floorbeam · corrodedPHX - DURING 30K CHECK, THE LEFT MAIN CABIN FLOOR CUSP BEAM WEB AT FS 1231 TO 1250, LBL 56 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-14-3, FIG 12. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Main, Floor BeamSDR ASAA0080165Floorbeam · corrodedPHX - DURNG 30K CHECK, THE LEFT MAIN CABIN FLOOR CUSP BEAM WEB AT FS 1174 TO 1193, LBL 56 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01, FIG 1 AND FIG 4. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Main, Floor BeamSDR ASAA0080164Floor Support · corrodedPHX - DURING 30K CHECK, THE AFT CARGO COMPARTMENT FLOORBOARD SUPPORT AT FS 1155, LONGERON 28L TO 29R WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 51-30-1. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0080163Floorbeam · corrodedPHX - DURING 30K CHECK, THE MAIN CABIN FLOOR CUSP BEAM WEB AT FS 1041, RBL 56 WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 53-01, FIG 4. (M)Feb 18, 2000 · N969AS · Doug DC983 · Fuselage Main, Floor Beam
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