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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DU4R2006608Skin · gougedLT I/B FLAP LOWER SKIN GROUP OF NICKS AT 16 INCHES FROM I/B EDGE. BLENDED GOUGES OUT OF LT I/B FLAP LOWER SKIN. REMOVED AND REPLACED SKIN 22-3/4" BY 1-3/8", 24-7/8" BY 4" FROM 7075-T6 .063 AND 42-1/4" BY 25" FROM 7075-T6 .040" AND LOWER TEE REPAIR 41" BY 12.SDR DU4R2006609Bulkhead · corrodedCORROSION ON AFT PRESSURE BULKHEAD LWR T-CHORD AND SURROUNDING AREAS IN AFT CARGO AT FS 1338 AND BETWEEN LONGERONS 24L AND 24R. REMOVED AND REPLACED WEB DOUBLER FABRICATED 6.0" BY 4.90" FROM 7075-T6 CLAD .080" IAW DELTA DC-9/MD-80 SRM 51-30-2, 51-10-2.SDR GTIA200600083Power Supply · inoperativeEMERGENCY LIGHTS AT AFT SERVICE DOOR AND CATWALK INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY AT ROW 31DEF.SDR ASMF200608008Generator · failedAIRCRAFT RETURNED TO PLATFORM AFTER ENGINE START, THE LT GENERATOR WAS OUT OF SERVICE, THE CORRESPONDING SWITCH WAS RESEATED AND FREQUENCY AND VOLTAGE WERE WITHOUT INDICATION. LT GCU, CSD AND CHIP DETECTOR WERE CHECKED AND NO FAILURE WAS DETECTED, THEREFORE, GSDR GTIA200600081Battery Pack · dischargedSEVERAL CABIN LIGHTS APPEAR TO BE INOP. REPLACED POWER SUPPLY BATTERIES B5-28 & B5-200.SDR GTIA200600080Battery · dischargedL1 AND R1 DOOR EMERGENCY EXIT SIGNS INOP. REPLACED BATTERY AT B5-205.SDR ASMF200608002Gyro · failedAIRCRAFT RETURNED TO PLATFORM (ATT) FLAG WAS SHOWN IN FIRST OFFICER ADI. RT VERTICAL GYRO WAS REPLACED IAW MM 34-23-02, TESTED CORRECT.SDR ASMF200607018Actuator · failedCAPTAIN REPORTED THAT DURING CRUISE, NOSE LANDING GEAR RED LIGHT TURNED ON AND AFT CENTER FUEL PUMP WAS OUT OF SERVICE. DURING OVERNIGHT CHECK, NOSE LANDING GEAR ACTUATOR AND AFT CENTRAL FUEL PUMP WERE REPLACED IAW MM 32-32-00 AND 28-20-07, TESTED CORRECT.SDR ASMD200607018Actuator · failedCAPTAIN REPORTED THAT DURING CRUISE, NOSE LANDING GEAR RED LIGHT TURNED ON AND AFT CENTER FUEL PUMP WAS OUT OF SERVICE. DURING OVERNIGHT CHECK, NOSE LANDING GEAR ACTUATOR AND AFT CENTRAL FUEL PUMP WERE REPLACED IAW MM 32-32-00 AND 28-20-07, TESTED CORRECT.SDR GTIA200600072Battery Pack · inoperativeEMERGENCY LIGHT IN COCKPIT INOP. REPLACED BATTERIES IN BATTERY PACK.SDR ASMF200607007Fcu · failedAIRCRAFT RETURNED TO PLATFORM, LOW OIL PRESSURE AND HIGH TEMPERATURE ON RT ENGINE. FCU AND FUEL PUMP WERE REPLACED IAW MM 73-12-00 AND 73-12-02, TESTED CORRECT IAW MM 71-00-00.SDR DU4R2006537Skin · gougedC-3 CARGO DOOR FWD INSIDE EDGE GOUGED. BLENDED GOUGES, ORIGINAL THICKNESS .050", .032" MATERIAL REMAINING, NDT VERIFIED OUT OF LIMITS. INSTALLED DELTA GENERIC 383 REPAIR DOUBLER IAW MD-80 SRM 52-33-0 FIG 1, 52-01 FIG 1, 51-30-5, 52-03D FIG 8.SDR ASMF200607004Manifold · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING FLIGHT CONTROL TEST, WHEN PUSHING THE CONTROL COLUMN FORWARD, VIBRATION WAS FELT IN THE WHOLE AIRCRAFT. DURING CHECK LOAD FEEL, DAMPER, ELEVATOR VALVE, CYLINDER ELEVATOR AND HORIZONTAL STABILIZER MANIFOLD WERE REPLACSDR 2006FA0000640Carrier Assy · crackedCARRIER PN 3500693-1 FOUND CRACKED DURING PENERANT INSPECTION OF PART. PART WAS BEING INSPECTED FOR OVERHAUL REPAIR, CRACK IS BEYOND REPAIR LIMITS.SDR ANCF200600023Clamp · looseAFTER SETTING TAKEOFF THRUST, LT AC SUPPLY IND REACH 55PSI , SUPPLY SWITCH WAS MOVED TO OFF POS, REMAINED INDICATING 10 PSI. AFTER LIFTOFF, (TAIL COMPT TEMP HI) LIGHT CAME ON AND STAYED ON UNTIL FIRST THRUST REDUCTION. FOUND PNEUMATIC LEAK AT AUGMENTATION VASDR AALA20060438Wire · shortedTUL - EMERGENCY ESCAPE PATH LIGHTING SYSTEM FROM SEATS 3EF TO 20DEF INOPERATIVE. FOUND SHORTED WIRE AT SEAT 9DEF. REPAIRED WIRING FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM FROM SEATS 3EF TO 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR GTIA200600070Battery Pack · dischargedEMERGENCY EXIT IDENTIFIER ON LT AFT OVERWING EXIT DOORS ARE INOP. REPLACED BATTERY PACK.SDR AALA20060369Battery Pack · dischargedLGA - OVERHEAD EMERGENCY LIGHTS AT ROW 24DEF INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR OVERHEAD EMERGENCY LIGHTS AT ROW 24DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASMF200605016Igniter Box · failedAIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORTED THAT DURING TAXIING AND AFTER TWO RIGHT ENGINE STARTING ATTEMPTS, EGT'S DID NOT INCREASE, PERCEIVING STRONG FUEL ODOR. AT PLATFORM, IGNITER BOX WAS REPLACED IAW MM 74-10-01, TESTED CORRECT IAW MM 74-00-00.SDR GTIA200600052Longeron · corrodedIN FWD PIT, LONGERON 29L STA 235 HAS CORROSION. REMOVED CORROSION. INSTALLED SPLICE REPAIR.SDR GTIA200600051Support · crackedFWD CARGO PIT LINING SUPPORT CRACKED AT STA 522, CENTERLINE. INSTALLED STIFFENER.SDR AALA20060305Battery Pack · inoperativeBOS - EMERGENCY LIGHTS AT EMERGENCY EXIT CEILING AND OVER DOOR AT SEAT ROW 9 INOPERATIVE. REPLACED BATTERY PACKS AT SEAT ROWS 9 AND 18 AND 19 FOR EMERGENCY LIGHTS AT EMERGENCY EXIT CEILING AND OVER DOOR AT SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR GTIA200600012Wire · brokenONE OVERHEAD EMERGENCY IS INOP IN AFT CABIN BY AFT RIGHT LAV. BROKEN WIRE AT L2-694 LAMP 1. ALSO, REPLACED FWD AND AFT BATTERY POWER SUPPLYS FOR TROUBLESHOOTING.SDR ANCF200600019Control Unit · failedDURING CLIMB AT FLIGHT LEVEL 210 AC CROSS DURING CLIMB AT FLIGHT LEVEL 210 AC CROSS TIE LOCK OUT LIGHT TURNED ON WITH NO ADDITIONAL LIGHTS IN THE EOAP. FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL ODOR. FOUND BURNT GCU APU IN ACCORDANCE TO AMM 24-20-07 PAG 4SDR ANCF200600017Fuel Control · out of trimDURING T/O, A DIFFERENCE BETWEEN LT AND RT OF EPR 0.5 PERCENT. DURING FLIGHT AT FL 320 MACH 076 LT EPR 1.98 AND RT EPR 1.82. THEN USING ENG ANTI ICE AUTO THROTTLE DISCONNECT AND LT EPR 1.28 & RT EPR 1.72. WITH THIS PROBLEM IS UNABLE TO FLY IN IT CONDITIONS ISDR ASMF200604014Fairing · damagedDURING TRANSIT CHECK, IT WAS DETECTED THAT THE RT AILERON FAIRING WAS DELAMINATED ON THE TRAILING EDGE. THE AILERON FAIRING WAS REPLACED AND THE SYSTEM WAS TESTED IAW M/M 27-10-01, BEING ALL CORRECT. DURING OVERNIGHT CHECK THE SYSTEM WAS TESTED IAW M/M 27-10SDR GTIA200600050Seat Track · corrodedCORROSION IN OUTER RT SEAT TRACK CHANNEL STA 513 THRU STA 517. REPAIRED SEAT TRACK.SDR GTIA200600049Seat Track · corrodedCORROSION IN OUTER RT SEAT TRACK CHANNEL STA 1204 THRU STA 1206. REPAIRED SEAT TRACK.SDR GTIA200600048Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT RBL 7 FS 148 THRU FS 200. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600044Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT LBL 44 FS 160 THRU FS 196. REMOVED CORROSION. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600043Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT LBL 7 FS 148 THRU FS 200. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600040Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT LBL 16 THRU LBL 42 FS 196. REMOVED CORROSION. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600037Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT LBL 55 FS 180. REMOVED CORROSION. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600036Finger Doubler · corrodedCORROSION ON INNER FINGER DOUBLER ON LONGERON 26L, JUST AFT OF PRODUCTION SPLICE AT STA 588. CLEANED SKIN. FINGER DOUBLER REPAIRED. INSTALLED SPLICE DOUBLER.SDR GTIA200600047Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT RBL 9 THRU RBL 43 AT FS 185. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600046Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT RBL 44 FS 160 THRU FS 200. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600045Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT RBL 9 THRU RBL 46 AT FS 200. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600041Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT LBL 5 THRU RBL 5 FS 200. REMOVED CORROSION. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600039Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT LBL 44 FS 196. REMOVED CORROSION. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600038Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT LBL 50 FS 196. REMOVED CORROSION. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600042Floor Support · corrodedCABIN FLOOR SUPPORT CORROSION AT BL 0 FS 218. REMOVED CORROSION. INSTALLED NEW FLOOR SUPPORT.SDR ANCF200600015Switch · malfunctionedAFTER TAKEOFF, TAIL CONE UNSAFE ANNUNCIATION ILLUMINATED. IN ACCORDANCE WITH AMM 52-70-11 PAGE 201-202. THE TAIL CONE EXTERNAL WARNING SWITCH WAS REPLACED AND AMM 53-53-00 PAGE 501 ADJUSTMENT/ TEST TAILCONE WAS PERFORMED SWITCH PART NUMBER H20-28B.SDR GTIA200600074Floor Support · corrodedFORWARD FLOOR SUPPORT BRACKET ADJACENT TO L-1 DOOR IS CORRODED. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600029Floorbeam · corrodedFWD PIT CEILING FLOORBEAM CORRODED STA 256 RBL 4-12. REMOVED CORRODED FLOOR SUPPORT AND MADE NEW SUPPORT.SDR GTIA200600033Floor Support · corrodedCABIN FLOOR SUPPORT LBL 45 CORRODED FS 180. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600032Floor Support · corrodedFOUND CABIN FLOOR SUPPORT LBL 55 CORRODED FS 160-200. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600031Floor Support · corrodedFOUND CABIN FLOOR SUPPORT RBL 7 CORRODED FS 150-200. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200600030Floor Support · corrodedFOUND CABIN FLOOR SUPPORT LBL-7 CORRODED FS 150-200. INSTALLED NEW FLOOR SUPPORT.SDR ANCF200600014Pump · inoperativeDURING CLIMB, RIGHT HYD PRESS (R HYD PRESS) ANNUNCIATION CAME ON. RIGHT HYD PRESS DROPPED TO ZERO. RT ENGINE DRIVEN PUMP IS INOP. IN ACCORDING WITH AMM 29-10-05 ENGINE DRIVEN HYDRAULIC PUMP WAS REPLACED.SDR GTIA200600079Floor Support · corrodedCABIN FLOOR SUPPORT LBL 15 CORRODED. INSTALLED NEW FLOOR SUPPORT.
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