Boeing DC-9-83

Service difficulty reports · 16,530

Newest first. General aviation reporting is voluntary.

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 ASAA0280697Insert · corrodedOKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS CORRODED INSERTS AT FS 1071-1155. REPLACED FLOOR PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280696Floor Support · corrodedOKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED AT FS 180-192. REPLACED FLOOR SUPPORT PER SRM 51-10-2, 51-10-4, 51-30-1, 51-30-2, AND DAC DWG 9936534. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280695Fitting · corrodedOKC - FOUND DURING 30K CHECK, FORWARD SERVICE (R-1) DOOR EMERGENCY SLIDE GIRT BAR FLOOR FITTING IS CORRODED AT FS 160. REPLACED FITTING PER SRM 51-30-1. (M)Dec 28, 2002 · N972AS · Doug DC983 · Emergency EquipmentSDR ASAA0280694Rib · wornOKC - FOUND DURING 30K CHECK, FLOOR PANEL RIB WORN IN 6 PLACES AT FS 1003-1098. REPLACED DAMAGED SECTION PER SRM 51-70-5, 53-24-0, AND 51-60-0. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280693Rib · crackedOKC - FOUND 30K CHECK, FLOOR PANEL HAS A CRACKED RIB AT FS 465-541. CUT OUT AND REPLACED DAMAGED SECTION PER SRM 51-70-5, 53-24-0, AND 51-60-0. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280692Seat Track · corrodedOKC - FOUND DURING 30K CHECK, SEAT TRACK CORRODED AT FS 1148-1164. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-05, 51-10-4, 51-30-1, 51-30-2 AND 51-30-5. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0280691Insert · corrodedOKC - FOUND DURING 30K CHECK, FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280690Web · corrodedOKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 1022-1071. REPLACED CUSP SECTION AND INSTALLED DOUBLER PER SRM 51-30-2, 51-30-5, AND 51-70-4. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280689Insert · corrodedOKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 200-256. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280688Insert · corrodedOKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 180-200. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280687Insert · corrodedOKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 160-180. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280686Insert · corrodedOKC - FOUND DURING 30K CHECK, FLOOR PANEL INSERTS ARE CORRODED AT FS 160-200. REPLACED PANEL WITH NEW INSERTS PER SRM 53-24-0 AND 53-05. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280685Insert · corrodedOKC - FOUND DURING 30K CHECK, AFT SERVICE L-2 DOOR EMERGENCY SLIDE GIRT BAR FITTING INSERTS ARE CORRODED. REPLACED FOUR INSERTS PER SRM 51-30-1. (M)Dec 28, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ZW0A0213003Wire · damagedTHE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPAIRED WIRE AT SPLICE.Dec 27, 2002 · N963TW · Doug DC983 · Light System WiringSDR ZW0A0213002BatteryTHE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 7-7-02 STL. --CLOSED--Dec 27, 2002 · N9615W · Doug DC983 · Emergency LightingSDR ZW0A0212902Valve · defectiveNOSE GEAR STRUT FLAT NOT ALLOWING GEAR TO RETRACT. REMOVED AND REPLACED SCHRADER VALVE AND RESERVICED STRUT.Dec 26, 2002 · N9305N · Doug DC983 · Nose/Tail Landing Gear Strut/AxleSDR GTIA021394Engine · failedDEN - FLT 980 - IN FLIGHT ENGINE FAILURE OF LEFT ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M)Dec 24, 2002 · N808NK · Doug DC983 · Engine (Turbine/Turboprop)SDR ASAA0280684Web · corrodedOKC - FOUND DURING 30K CHECK, LEFT CUSP WEB CORRODED AT FS 313-370. INSTALLED DOUBLER ON WEB PER SRM 53-14-2, 53-01, 51-70-4, AND 51-30-1. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280683Floorboard · damagedOKC - FOUND DURING 30K CHECK, FLOORBOARD HAS ONE PUNCTURE, ONE DENT, AND DISBONDING AT ENDS OF LOWER STIFFENER AT FS 826-927. INSTALLED DOUBLERS ON LOWER STIFFENER AND REBONDED ENDS PER SRM 51-70-2 AND 53-05. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280682Floorboard · damagedOKC - FOUND DURING 30K CHECK, FLOORBOARD HAS ONE PUNCTURE, 50 DENTS, AND DISBONDING AT BOTH ENDS OF LOWER STIFFENERS AT FS 825. INSTALLED DOUBLERS ON LOWER STIFFENER PER SRM 51-70-2 AND 53-05. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280681Frame · corrodedOKC - FOUND DURING 30K CHECK, SHEAR TIE FRAME CORRODED AT FS 1155. REPLACED FRAME PER SRM 51-30-5. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0280680Cargo Track · corrodedOKC - FOUND DURING 30K CHECK, SIX CLIP NUT HOLES ARE CORRODED ON MID CARGO BAY TRACK AT FS 522-561. REPLACED DAMAGED SECTION PER SRM 53-24-0 AND 53-05. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0280679Access Panel · crackedOKC - FOUND DURING 30K CHECK, LEFT INBOARD FLIGHT SPOILER ACCESS PANEL 1526 IS CRACKED. REPLACED PANEL PER SRM 51-30-1. (M)Dec 24, 2002 · N972AS · Doug DC983 · SpoilersSDR ASAA0280678Panel · chafedOKC - FOUND DURING 30K CHECK, LEFT WING FORWARD ROCK DEFLECTOR PANEL IS WORN/CHAFED AT EDGES. REPAIRED WITH DOUBLER PER SRM 51-30-2 AND 51-70-4. (M)Dec 24, 2002 · N972AS · Doug DC983 · Wing, Plate/SkinSDR ASAA0280677Frame · corrodedOKC - FOUND DURING 30K CHECK, FRAME CORRODED AT FS 1155, LONGERON 27L-27R. REPLACED FRAME PER SRM 51-30-5. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Main, FrameSDR ASAA0280676Floorboard · tornOKC - FOUND DURING 20K CHECK, FLOORBOARD HAS TORN METAL AT 'W' SANDWICH EXTRUSION AT FS 826-886. REPLACED SUPPORT SECTION PER SRM 51-30-8, 51-20-0, AND 51-10-4. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280675Floorboard · tornOKC - FOUND DURING 30K CHECK, FLOORBOARD HAS TORN METAL AT 'W' SANDWICH EXTRUSION AT FS 886-946. REPLACED SUPPORT SECTION PER SRM 51-30-8, 51-20-0, AND 51-10-4. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280674Intercostal · gougedOKC - FOUND DURING 30K CHECK, INTERCOSTAL BETWEEN LONGERON 26L-27L GOUGED AT FS 1322. REPLACED INTERCOSTAL PER SRM 51-10-2, 51-10-4, 51-30-2, AND DAC DWG 5936667. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280673Floor Panel · crackedOKC - FOUND DURING 30K CHECK, FLOOR PANEL IS PUNCTURED AT FS 1003-1071. REPLACED FLOOR PANEL PER SRM 53-05. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280672Floor Panel · crackedOKC - FOUND DURING 20K CHECK, FLOOR PANEL CRACKED AT OUTBOARD SIDE FS 465-541. REPLACED FLOOR PANEL PER SRM 51-70-5, 51-60-0 AND 53-24-0. (M)Dec 24, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASAA0280671Floorboard · crackedOKC - FOUND DURING 30K CHECK, FLOORBOARD SKIN CRACKED AT FS 212. REPLACED FLOORBOARD SECTION PER SRM 53-05. (M)Dec 23, 2002 · N972AS · Doug DC983 · Fuselage Floor PanelSDR ASA0280670Attach Fitting · crackedOKC - FOUND DURING 30K CHECK, UPPER LEFT TAILCONE ATTACH BRACKETS TWO CRACKED. REPLACED BRACKETS PER SRM 51-10-2, 51-10-4, 51-30-1, AND DAC DWG 9911957. (M)Dec 23, 2002 · N972AS · Doug DC983 · Fuselage Main, Attach FittingsSDR ASAA0280669Floor Support · corrodedOKC - FOUND DURING 30K CHECK, FLOOR SUPPORT CORRODED IN CABIN AT FS 200. REPLACED SUPPORT PER SRM 53-14-1, 51-10-2, 51-10-4, AND 51-30-2. (M)Dec 23, 2002 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ASAA0280668Rod · crackedOKC - FOUND DURING 30K CHECK, AFT CARGO COMPARTMENT BARRIER DOOR ASSEMBLY AFT HOLDUP SPEAR IS CRACKED. REPLACED SPEAR PER SRM 51-30-2. (M)Dec 23, 2002 · N972AS · Doug DC983 · Cargo/Baggage DoorsSDR ASAA0280667Bracket · crackedOKC - FOUND DURING 30K CHECK, BRACKET BELOW 'Y' DUCT IN ACCY COMPARTMENT IS CRACKED. REPLACED BRACKET PER SRM 51-10-3, 51-30-1 AND DAC DWG 5937954. (M)Dec 23, 2002 · N972AS · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0212801Seal · looseBOTH HEAT EXCHANGERS LEAKING NOT ALLOWING AIRCRAFT TO PRESSURIZE. TIGHTENED SEALS ON BOTH HEAT EXCHANGERS.Dec 23, 2002 · N9305N · Doug DC983 · Cabin Cooling SystemSDR ASAA0280666Lanyard · disconnectedLAS - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)Dec 22, 2002 · N944AS · Doug DC983 · Escape SlideSDR AALA20021837Battery · dischargedORD - FLT 1592 - EN ROUTE SEA-ORD, AFT EMERGENCY EXIT FLOOR LIGHTS FLICKERED. LANDED ORD WITHOUT INCIDENT. REPLACED TWO EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Dec 22, 2002 · N437AA · Doug DC983 · Emergency LightingSDR ZW0A0212702Battery Pack · dischargedTHE EMERGENCY EXIT LIGHT ABOVE THE OVERWING EXIT DOOR ROW 21 LEFT AND RT SIDE, WERE INOPERATIVE. REPLACED THE BATTERY PACK.Dec 22, 2002 · N9304C · Doug DC983 · Emergency LightingSDR ZW0A0212701Light · inoperativeTHE L1 DOOR EMERGENCY PORTABLE LIGHT, THE AFT FLIGHT ATTENDANT SEAT CEILING LIGHT JUST FWD OF RT LAV, AND THE FLOOR EGRESS LAMP AT SEAT ROWS 6 AND 9, WERE ALL INOPERATIVE. REPLACED THE PORTABLE LIGHT, REPLACED THE BATTERY PACK AT AFT LAV, AND REPLACED BOTH EGDec 22, 2002 · N9409F · Doug DC983 · Emergency LightingSDR CA030107017Blade · damaged(CAN) ON ROUTE TO YVR FROM YYZ AT 130 NM FROM YYC HEARD LOUD BANG, FOLLOWED BY NR 1 ENGINE EPR DROP TO ZERO N1-N2 SPEED DECREASING. ENGINE RETARDED TO IDLE. PARAMETERS WITHIN LIMITS. DIVERTED TO YYC. PRELIMINARY INSPECTION REVEALS DAMAGED TURBINE BLADES. ENGDec 21, 2002 · Doug DC983 · Turbine SectionSDR ASAA0280665Lanyard · disconnectedSJC - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)Dec 20, 2002 · N969AS · Doug DC983 · Escape SlideSDR AALA20021838Battery · not seatedDFW - DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Dec 20, 2002 · N597AA · Doug DC983 · Emergency LightingSDR CA030108013Tube · fractured(CAN) 13 STAGE BLEED MANIFOLD TRANSFER TUBE FRACTURED. ENGINE REMOVED AND SENT TO SHOP FOR REPAIR AND PREVENTIVE MOD SB6369 SB6393 INCORPORATION.Dec 19, 2002 · Doug DC983 · Turbine Engine Compressor SectionSDR GTIA021285Wire · looseMCO - FOUND ONE EMERGENCY LIGHT ON LEFT SIDEWALL IN TAIL COMPARTMENT INOPERATIVE. REMOVED LIGHT ASSEMBLY OF TAIL COMPARTMENT EMERGENCY LIGHT, SECURED LOOSE WIRE AND RELAMPED LIGHT. OPS CHECK OK. (M)Dec 18, 2002 · N824NK · Doug DC983 · Light System WiringSDR AALA20021840Skin · crackedTUL - FOUND SKIN CRACKED AT STATION 1380, LONGERON 14L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M)Dec 18, 2002 · N562AA · Doug DC983 · Fuselage Main, Plate/SkinSDR ZW0A0213102Skin · damagedDURING CHECK-C FOUND ON THE FWD LT FUSELAGE ALL BLIND FASTENERS IN A LARGE REPAIR AT STA 218, LONGERON 18L TO 19L. REMOVED EXISTING REPAIR. CUTOUT DAMAGED SKIN AND INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 12B, SHEET 34.Dec 18, 2002 · N983TW · Doug DC983 · Fuselage Main, Plate/SkinSDR ASAA0280663Light · inoperativeSEA - DURING LINE CHECK, THE EMERGENCY TRACK LIGHTING AT ROWS 29-33 AND IN THE TAIL SECTION ALONG CATWALK WERE FOUND TO BE INOPERATIVE. REPLACED SHORTED TAILCONE EJECT HANDLE LIGHT ASSEMBLY AND EMERGENCY TRACK LIGHTS. LIGHTS THEN OPERATED PROPERLY. (M)Dec 17, 2002 · N977AS · Doug DC983 · Emergency LightingSDR AALA20021836Attach Angle · crackedTUL - FOUND FUSE TO VERTICAL STABILIZER ATTACH ANGLE CRACKED IN RADIUS STATION 1463 RIGHT SIDE AND CRACKED IN LOWER LEG BETWEEN FASTENERS. STOP DRILLED CRACK IN RADIUS AND CUTOUT CRACKED AREA BETWEEN FASTENERS AND INSTALLED DOUBLER AND FILLER PER AARD 53-10-0Dec 17, 2002 · N76200 · Doug DC983 · Fuselage, Stabilizer Attach FittingsSDR AALA20021835Door Frame · crackedTUL - FOUND RIGHT FORWARD OVER WING EXIT JAMB CRACKED TOP CENTER. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-05-00 FIG 32. (M)Dec 17, 2002 · N76200 · Doug DC983 · Fuselage Main, Structure
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