Mcdonnell Douglas MD 83

Service difficulty reports · 3,415

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 = 'MD83'
  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 ASAA0580517Shear Tie · corrodedOKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Internal Mounting StructureSDR ASAA0580516Shear Tie · corrodedOKC - DURING HV CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Internal Mounting StructureSDR ASAA0580525Panel · gougedOKC - DURING HV-CHECK, LEFT INBOARD SPOILER PANEL GOUGED ON UPPER SURFACE AT TRAILING EDGE. REPLACED DAMAGED PLIES. (M)Sep 26, 2005 · N982AS · Doug MD83 · SpoilersSDR ASAA0580524Wedge · crackedOKC - DURING HV-CHECK, FOUND RIGHT INBOARD FLAP INBOARD WEDGE TRAILING EDGE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED VACUUM CURED SPLICE. (M)Sep 26, 2005 · N982AS · Doug MD83 · Trailing Edge FlapsSDR ASAA0580523Angle · crackedOKC - DURING HV CHECK, FOUND VERTICAL STABILIZER TO FUSELAGE LEFT ATTACH ANGLE IS CRACKED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR ANGLE. (M)Sep 26, 2005 · N982AS · Doug MD83 · Vertical StabilizerSDR ASAA0580522Tab · delaminatedOKC - DURING HV CHECK, FOUND RIGHT ELEVATOR ANTI-FLOAT TAB LOWER SURFACE IS DELAMINATED. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Elevator, Tab StructureSDR ASAA0580521Tab · delaminatedOKC - FOUND DURING HV-CHECK, RIGHT ELEVATOR GEAR TAB UPPER SURFACE HAS DELAMINATION. REMOVED DAMAGED SECTION. INSTALLED SKIN FILLER AND REPAIR DOUBLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Elevator, Tab StructureSDR ASAA0580520Doubler · corrodedOKC - DURING HV-CHECK, FOUND ANTENNA DOUBLER CORRODED IN AFT CARGO BAY. REPLACED DOUBLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Main, Plate/SkinSDR ASAA0580519Skin · lightning strikeOKC - DURING HV-CHECK, FOUND FUSELAGE HAS LIGHTNING DAMAGE. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND INTERNAL DOUBLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Main, Plate/SkinSDR ASAA0580518Skin · dentedOKC - DURING HV CHECK, FOUND DENT IN FUSELAGE. COLD-FORMED SKIN TO ORIGINAL CONTOUR. INSTALLED INTERNAL REPAIR DOUBLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Main, Plate/SkinSDR ASAA0580515Shear Tie · corrodedOKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REMOVED DAMGAED SECTION. INSTALLED REPLACEMENT SECTION WITH TWO REPAIR SPLICES. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Internal Mounting StructureSDR ASAA0580514Cusp Web · corrodedOKC - DURING HV CHECK, FOUND CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580513Frame · corrodedOKC - DURING HV-CHECK, FOUND FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER, TWO REPAIR ANGLES AND TWO REPAIR PLATES. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Main, FrameSDR ASAA0580512Shear Tie · corrodedOKC - DURING HV-CHECK, FOUND SHEAR TIE CORRODED. REPLACED SHEAR TIE. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Internal Mounting StructureSDR ASAA0580511Frame · corrodedOKC - DURING HV-CHECK, FOUND FRAME CORRODED. REMOVED DAMAGED SECTION. INSTALLED TWO REPAIR DOUBLERS, TWO REPAIR PLATES, AND ONE REPAIR FILLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Main, FrameSDR ASAA0580510Cusp Web · corrodedOKC - FOUND HV CHECK, CUSP WEB CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580509Intercostal · corrodedOKC - DURING HV CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580508Intercostal · corrodedOKC - FOUND DURING HV-CHECK, INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580507Intercostal · corrodedOKC - DURING HV-CHECK, FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580506Channel · crackedOKC - FOUND HV-CHECK, PASSENGER CABIN FLOOR PANEL HAS CRACKED HAT CHANNEL. REPLACED DAMAGED CHANNEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580505Floor Panel · delaminatedOKC - FOUND HV-CHECK, PASSENGER CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580504Floor Panel · delaminatedOKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED. REPLACED PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580503Web · corrodedOKC - DURING HV CHECK, FOUND PAX CABIN FLOOR WEB CORRODED. REPLACED DAMAGED SECTION. INSTALLED WEB REPAIR AND TWO DOUBLERS. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580502Floor Support · corrodedOKC - DURING HV CHECK, PAX CABIN FLOOR TRACK CORRODED. REPLACED TRACK. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580501Floor Support · corrodedOKC - DURING HV CHECK, FOUND PAX CABIN FLOOR TRACK CORRODED. REPLACED TRACK. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Miscellaneous StructureSDR ASAA0580499Floor Panel · delaminatedOKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580498Floor Panel · corrodedOKC - DURING HV-CHECK, PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580497Floor Panel · delaminatedOKC - FOUND HV CHECK, PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580496Floor Panel · delaminatedOKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580495Floor Panel · corrodedOKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL HAS CORRODED INSERTS WITH DELAMINATION AROUND INSERTS. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580494Floor Panel · delaminatedOKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580493Floor Panel · delaminatedOKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLAED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580492Floor Panel · delaminatedOKC - DURING HV-CHECK, PASSENGER CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580491Floor Panel · delaminatedOKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580490Floor Panel · delaminatedOKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580489Floor Panel · delaminatedOKC - DURING HV C-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580488Floor Panel · delaminatedOKC - FOUND HV-CHECK, PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580487Floor Panel · delaminatedOKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580486Floor Panel · delaminatedOKC - FOUND HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0580485Floor Panel · delaminatedOKC - DURING HV-CHECK, FOUND PAX CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)Sep 26, 2005 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASMF200509014Valve · failedCAPTAIN REPORTED, DURING FLIGHT, THE F/O RMI CHANGED HEADING, BEING NECESSARY TO ADJUST CONTINUOUSLY. DURING REVISION, DETECTED A DIFFERENCE OF 20 GRADES BETWEEN COURSES. THE LT FLUX VALVE NR 1 WAS REPLACED IAW MM, SYNCHRONY TEST WAS PERFORMED IAW MM, BEING SASep 24, 2005 · N831LF · Doug MD83 · Attitude Gyro and Indicating SystemSDR ASMF200509012Actuator · failedCAPTAIN REPORTED THAT AFTER LANDING RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON. AIRCRAFT WAS SENT TO THE HANGAR; THE RUDDER THROW LIMITER AND PUSHROD NR 5 WERE REPLACED AND SYSTEM WAS ADJUSTED IAW MM 27-20-06, PAGE 201, TESTED CORRECT.Sep 21, 2005 · N881LF · Doug MD83 · Rudder Control SystemSDR ASMF200509010Actuator · malfunctionedCAPTAIN REPORTED THAT RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON. THE RUDDER POSITION SENSOR WAS CHECKED AND CLEANED IAW MM 27-20-00. NON ROUTINE CARD NR A0082196 TO RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON WAS GENERATED TO REPLACE RUDDER THROW LIMITER. THESep 18, 2005 · N881LF · Doug MD83 · Rudder Control SystemSDR ASMF200509009Wheel · damagedDURING TRANSIT CHECK THE MAIN LANDING GEAR WHEELS WERE DETECTED CONTAMINATED WITH RUNWAY RE-COVER MATERIAL. THE WHEELS WERE CHECKED; THE WHEEL POSITION 2 WAS REPLACED AND A GENERAL REVISION WAS PERFORMED AT ENGINES AND FLIGHT CONTROL SURFACES IAW MM 32-40-01, Sep 18, 2005 · N831LF · Doug MD83 · Wheel/Ski/FloatSDR ASMF200509008Pressure Switch · inoperativeAIRCRAFT RETURNED TO PLATFORM, LT ENGINE OIL PRESSURE WAS 38 PSI NEAR YELLOW RANGE. THE PARAMETERS IN FLIGHT CABIN WAS CHECKED AND OIL PRESSURE ADJUST WAS PERFORMED IAW MM 79-20-03. AFTER, TO ACCELERATE THE ENGINE, THE ENGINE PRESSURE WAS INCREASED TO 90 PSI. Sep 17, 2005 · N831LF · Doug MD83 · Engine Oil Distribution (Airframe Furnished)SDR AALA20050581Valve · inoperativeDEN INFLT T887/09 SEPT SEVERAL MINUTES AFTER ENGINE WAS ON WING ICE, SMOKE WAS PRESENT IN COCKPIT AND CABIN. DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. TURNED ANTI ICE ON AGAIN AND SMOKE REAPPEARED. PRESSURE ABNORMAL LIGHT ILLUMINATED. REPLACED ANTI ICESep 9, 2005 · N9630A · Doug MD83 · APU Bleed Air SystemSDR ASMF200508017Ignition Unit · malfunctionedDURING RIGHT ENGINE STARTED, THE IGNITION FAILED. ONCE THE ENGINE STOPPED TURN, A SECOND START WAS PERFORMED IAW 74-20-02, BEING CORRECT. DURING OVERNIGHT CHECK, THE CABLES, SPARK PLUGS AND IGNITION SYSTEM OF BOTH ENGINES WERE CHECKED IAW MM 74-10-02 AND MM Aug 29, 2005 · N861LF · Doug MD83 · Ignition SystemSDR FE5F200500002Housing · crackedTHE A/C, LOST BOTH HYD PRESS (BOTH PRESS 0) WHILE TOUCH DOWN AND USE REVERSE THRUST(BOTH SIDE HYD QTY NORMAL.L:15, R:17 PROCEED QRH(L/R)HYD PRESS LOW PROCEDURE:TRANS PUMP SW OFF CHECK PRESSURE AND QTY NORMAL.TAXI BACK TO GATE. ENGINEERS VISUAL CHECKED, FOUND Aug 26, 2005 · Doug MD83 · Hydraulic Pump (Electric/Engine), MainSDR ASMF200508006Computer · failedAIRCRAFT RETURNED OF FLIGHT, BOTH DFGC OUT OF SERVICE. THE DFGC RTC BITE WERE PERFORMED IAW MM 22-01-05, TESTED CORRECT. THE OVERWEIGHT LANDING CHECK WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. DURING OVERNIGHT CHECK, BOTH DFGC TESTS WERE PERFORMED IAW MM 22-0Aug 15, 2005 · N945AS · Doug MD83 · Autopilot SystemSDR AALA20050518Battery Pack · inoperativeLGA - EMERGENCY SEAT MOUNTED ESCAPE PATH LIGHTING BATTERIES INOPERATIVE. REPLACED BATTERIES AT POSITION AB51 AND AB54 FOR EMERGENCY SEAT MOUNTED ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.Aug 10, 2005 · N951TW · Doug MD83 · Emergency Lighting
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