Mcdonnell Douglas MD 83
Service difficulty reports · 3,414
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 2WAA2026FA0000318Light · inoperativeDURING PREFLIGHT INSPECTION, FLIGHT CREW REPORTED THAT THE TAIL CONE LIGHT WAS INOPERATIVE. ADDITIONALLY, WHEN THE EMERGENCY LIGHTING SYSTEM WAS ACTIVATED, MULTIPLE CEILING LIGHTS DID NOT ILLUMINATE AS REQUIRED. THE EMERGENCY EXIT LIGHT AT THE L2 DOOR WAS ALSOSDR 2025F00277Warning Light · illuminatedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ON, FLOW LIGHT ON DURING CLIMB AND UNABLE TO MAINTAIN PRESSURIZATION.SDR 2WAA2025091000218A/C Pack · no discrepancyBURNING SMELL REPORTED AFTER FLIGHT BY FLT ATTENDANTS SUSPECTED FROM LEFT PACK PER THEM. PERFORMED INSPECTION WITH L/H AND R/H A/C PACKS AND NO DISCREPANCY FOUND AS PER MD80 AMM 21-00-00: PERFORMED INSPECTION LEFT AND RIGHT ELECTRIC SYSTEMS NO DISCREPANCY FOUNSDR 2025F00212Fire Warning · false activation1.FWD CARGO FIRE INDICATION//2. FWD CARGO FIRE BOTTLE WAS DISCHARGE. AFTER REPLACING FIRE EXTINGUISHER COMPONENTS REF ITEM 2, OPS CHECK FOUND NORMAL IAW MD80AMM 26-18-02. 2. PERFORMED MAINTENANCE PROCEDURES FOLLOWING SYSTEM DISCHARGE. REPLACED COMPONENTS IAW MSDR 2WAA20250820191Skin · corrodedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER CENTER EDGE AREA AND LOWER SECTION. REPAIRED RIGHT HORIZONTAL STABILIZER LEADING EDGE PER E.O.'S WAA-250319, WAA-250623, AND E.O. WAA-250620.SDR 2WAA202508200190Skin · corrodedLEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER EDGE, ALL THRU THE LENGHT ALSO THE HARWARE OF LOWER EDGE IS RUSTY AND HAS CORROSION AROUND THE FASTENER HEAD. REPAIRED LEADING EDGE PER E.O.'S WAA-250220, WAA-250221, WAA-250222, WAA-250223, WAA-2SDR 2WAA20250820192Window Frame · corrodedMAIN CABIN RIGHT SIDE WINDOW # 21 HAS CORROSION AROUND CUT OUT. ACCOMPLISHED REPAIR AT WINDOW # 21 R/H SIDE OF FUSELAGE BETWEEN BS 616 AND BS 636 PER E.O. WAA-250219SDR 2WAA202508190186Window Frame · corrodedMAIN CABIN LEFT SIDE WINDOW CUT OUT HAS SEVERAL CORROSION 4, 5, 13, 29, 43, 51. ACCOMPLISHED CORROSION REMOVAL AT MAIN CABIN LEFT SIDE WINDOW CUT OUT NBR 4,13, 29, 43, 51, FOUND WITHIN LIMITS AND REPAIR WINDOW AT # 5 POSITION PER E.O. WAA-250227, MD-80 SRM 53SDR 2WAA202508190183Angle · corrodedMAIN CABIN L/H SIDE LAVATORY HAS CORROSION ALL AROUND FLOOR BASE ATTACHMENT AREA. ACCOMPLISH L/H SIDE LAVATORY STRUCTURAL REPAIR IAW E.O. WAA 250403.SDR 2WAA202508190182Angle · corrodedFWD LAVATORY L/H SIDE HAS CORROSION ALL AROUND THE FLOOR BASE. ACCOMPLISH FWD LAVATORY L/H SIDE STRUCTURAL REPAIR IAW E.O. WAA-250303SDR 2WAA202508190181Angle · corrodedMAIN CABIN AFT R/H LAVATORY HAS CORROSION ALL AROUND THE FLOOR BASE AND INCORRECT HOSE INSTALL. ACCOMPLISHED AFT R/H LAVATORY STRUCTURAL REPAIR IAW E.O. WAA-250503.SDR 2WAA202508190185Battery Pack · dischargedMULTIPLES INTERNAL AND EXTERNAL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS AND EMERGENCY LIGHTSPER MD-80 AMM 33-53-00 OPS CKECK OK.SDR 2WAA202508180189Skin · corrodedLEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER EDGE, ALL THRU THE LENGHT ALSO THE HARDWARE OF LOWER EDGE IS RUSTY AND HAS CORROSION AROUND THE FASTENER HEAD. REPAIR DONE BY E.O. WAA-250220, 250221, 250222, 250223, 25024, 250225, 250615.SDR FXGA07302025001Duct · crackedTAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED DURING CLIMB. FOUND RT BLEED AIR SOURCE DUCT WELD BROKEN. REMOVED AND REPLACED 13THSTAGE BLEED AIR SOURCE DUCTING BETWEEN ENGINE AND AUGMENTER VALVE IAW AMM 20-10-11. LEAK CHECK GOOD IAW AMM 71-00-00 CONFIG 4 STEP 4SDR FXGA07292025002Overheat Sensor · activatedTAIL COMPARTMENT TEMP HIGH ILLUMINATED, REPLACED R/H TAIL COMPARTMENT TEMP SENSOR IAW MD-80 AMM 36-20-02. OPERATIONAL CHECK GOODSDR FXGA07292025001Duct Clamp · leakingTAIL COMPARTMENT TEMP HIGH ILLUMINATED, FOUND #2 ENGINE BLEED AIR LEAK IN TAIL SECTION, REPLACED CLAMP IAW MD-80 AMM 20-10-11. GROUND RUN-UP OPERATIONAL CHECK GOOD.SDR 2WAA2025070200158Light · burned outLOW LEVEL EMERGENCY LIGHTS ON SEATS ROWS 21-32 BURNED OUTSDR Y2PA2025061825006Skin Splice · corrodedDISCREPANCY: WHILE AT C-CHECK IN KBQK, STAMBAUGH AVIATION FOUND CORROSION ON THE L/H WING LOWER SURFACE AT STR. 17 (SKIN SPLICE) AND AT XCW 85. BLENDED OUT THE DAMAGED AREA, PERFORMED HFEC OPEN HOLE INSPECTION AND FABRICATED A REPAIR DOUBLER USING 2024T3 .12SDR 2025F00137Lamp · inoperativeDURING DAILY CHECK FOUND SOME EMERGENCY FLOOR PATH LIGHT ARE NOT WORKINGSDR 2WAA20250401086Engine · failedLH ENGINE FAILURE AFTER TAKEOFFSDR 2WAA202503200067Valve · failedAFTER TAKEOFF AND RISING LANDING GEAR, THE LANDING GEAR'S RED NOSE LIGHT WAS NOT EXTINGUISHED.SDR 2025FA0000194Battery Pack · dischargedCABIN DISCREPANCY REPORT (CDR) ROW 3 AND SERVICING EMERGENCY LIGHTS NOT WORKING ROW 21, 23 ISLE PATH LIGHTING NOT WORKING EXIT LIGHT OF L1, R1 AND L2.SDR 2025F00062Skin · dentedTHE L/H UPPER FUSELAGE BETWEEN STA-218 AND STA-237 HAS STRUCTURAL DAMAGE.SDR 2WAA202502270051Light · inoperativeEMERGENCY LIGHTS AT CABIN AFT DOOR INOPSDR 2WAA202502270054Control Module · inoperativeEMERGENCY LIGHTS AT INBOARD OVERWING EXIT DOORS L/H AND R/H ARE INOPSDR 2WAA202502270052Battery Pack · dischargedEMERGENCY LIGHTSAT L1 AND L2DOORS ARE INOP (NOT TESTING)SDR 2025F00042Control Module · failedEMERGENCY LIGHTS FWR EXIT LEFT AND RIGHT WERE FOUND VERY DIM. AFTER TROUBLESHOOTING THE MODULE CONTROL ASSY AB5-1 WAS REPLACED. THE OPERATIONAL TEST WAS FOUND NORMAL IAW MD-80 AMM 33-53-00.SDR 2WAA20250205036Light · inoperativeEMERGENCY EXIT LIGHT INOPSDR 2024F00139Clamp · looseDURING CRUISE FLOW LIGHT ON AND DURING DESCENT CABIN ALTITUDE LIGHT ON, CABIN OXYGEN LIGHT ON , OXYGEN MASKS DEPLOYED. THE CORRECTIVE ACTION RESECURED CLAMPS OF A/C COMPONENTES AT AFTER PRESSURE BULKHEAD, FUNCTIONAL TEST OF CABIN PRESSURE CONTROL SYSTEM I.A.W SDR 2024F00137Battery · inoperativeON THE L1 DOOR JAMB THE EMERGENCY LIGHT LOCATED ON THE FRAME OF THE DOOR FAIL TEST PERFORMED DURING C-CHECK. REF. TASK CARD 53-200-05-01, WO 6549 CORRECTIVE ACION: REMOVED NAD REPLACE BATTERIES PACK L1 DOOR LAP EMERGENCY LIGHT I.A.W. MD80 AMM 33-53-00. PN: 10-SDR FXGA20240426001Unlock Cylinder · leakingNOSE LANDING GEAR FAILED TO EXTEND WITH NORMAL MEANS, CYCLED GEAR AND NOSE GEAR EXTENDED NORMALLY. LANDED WITH NO FURTHER INCEDENTSDR FXGA20240417001Hinge · wornBIG VIBRATION FELT AFTER TAKEOFF IN AIRCRAFT AND YOKE. NOSE GEAR FORWARD DOORS CLOSING LINKAGE FOUND TO BE WORNSDR 2024F00015Oven · odorCREW DISCREPANCY REPORT (CDR) #1 FWD CABIN GALLEY OVEN SMELL OF BURNED PLASTIC WHEN IN USE (LEFT SIDE) LP27780. OEM: BUDERUS SELL GMBH GERMANYSDR 2023F00218Window · detachedDURING A CRUISE AT FL 300, THE FLIGHT MECHANIC REPORTED TO THE FIRST OFFICER AND CAPTAIN THAT A PASSENGER WINDOW WAS BLOWN OUT. THE FIRST OFFICER CHECKED THE PRESSURIZATION WHICH WAS STABILIZED AND INDICATED NORMAL. THE FIRST OFFICER ASKED FOR THE ROW LOCATIONSDR 2023FA0000306Unknown · unknownLEFT WINGTIP MADE CONTACT WITH AN ALUMINUM GATE. DAMAGE TO LEFT WINGTIPSDR FXGA202301142301None · noneMAIN CARGO DOOR AFT SEAL DEPRESSOR PERMANENT REPAIR REFERENCE AEI TICKET 21004 R00 (002) STEP 1.2. TO REPAIR DAMAGE TO MAIN CARGO DOOR AFT SEAL DEPRESSOR. CUTOUT EXISTING SEAL DEPRESSOR DAMAGES SECTION AT AEO PROPOSED CUTOUT LINES AS PER ATTACHED (967 MCD #3)SDR FXGA202211172230None · noneFUSELAGE SKIN GOUGED AT F/STA 463, STR 21L. TO REPAIR A DEEP GOUGE ON FUSELAGE SKIN. PERFORM SKIN REPAIR PER AEI EO 20455.SDR FXGA202211112229None · noneMAIN CARGO DOOR LATCHES REPAIR. DURING TORQUE TUBE ISSUES ON ABOVE AIRCRAFT, ALL LATCHES RESULTED WITH GOUGES CAUSED BY THE LOCK PINS. IN ORDER TO CONTINUE WITH LATCHES EVALUATION, IT WILL BE REQUIRED TO BLEND OUT THE LATCHES AND PROVIDE THE THICKNESS OF REMSDR FXGA202210102224None · noneDENT ON FUESELAGE SKIN AT F/STA 393, STR 15L. TO REPAIR DENT DAMAGE ON THE FUSELAGE SKIN AT F/STA 393, STR 15L. PERFORM FUSELAGE SKIN REPAIR PER STS EA 81-2022-122. RE-INSPECTION INSTRUCTIONS TO BE PROVIDED WITH DTA NO LATER THAN 12 MONTHS FROM REPAIR COMPLETISDR Y2PA2022090622047Skin · corrodedDISCREPANCY: DURING C-CHECK AT COMMERCIAL JET IN KDHN, CORROSION FOUND ON FUSELAGE SKIN INTERNAL DOUBLER AT DRAIN VALVE MOUNTING SURFACE AT STATION 157 SDR Y2PA2022090622046Flap · corrodedDISCREPANCY: : DURING C-CHECK AT COMMERCIAL JET IN KDHN, EXFOLIATION CORROSION FOUND ON RH WING INBOARD FLAP AT APPROXIMATELY XRS 69 INNER SURFACE EMANATING FROM UNDER RIB JUST BELOW 3RD FROM INBOARD FLAP VANE MOUNT SDR Y2PA2022090622045Latch · crackedDISCREPANCY: DURING C-CHECK AT COMMERCIAL JET IN KDHN, THE MAIN CARGO DOOR LATCH BASE LUG FITTINGS 3,4,5,6 AND 7 WERE FOUND TO BE CRACKED AT FASTENER HOLES DURING THE ACCOMPLISHMENT OF AD 2004-11-07 (PSE 52.80.FC3) HFEC INSPECTION OF THE MAIN CARGO DOOR LATCH SDR FXGA202206212218Retainer · damagedSEAL RETAINER INSTALLATION - DEVIATION. DAMAGED SEAL RETAINER PN: AE5660-11 MUST BE REPLACED WITH ALTERNATE PN: AE5738-16. DURING A VISUAL INSPECTION AROUND THE DOOR, IT WAS FOUND A CRACKED SEAL RETAINER PN: AE5660-11 (SEE FIGURE 1). THUS, A SECTION OF EXISTINSDR FXGA202205252213Longeron Splice · corrodedCORRODED LONGERON AND SPLICES FROM F/STA 1211 TO 1259. TO REMOVE AND REPLACE A CORRODED LONGERON SECTION (29L) AND ITS TWO CORRODED SPLICES AT F/STA 1211 AND 1259. REMOVED CORRODED SPLICES AND STRINGER SECTION, REPLACE WITH NEW. PERFORM ALL WORK FROM DC-9/MD-SDR FXGA202112282139None · noneFUSELAGE SKIN DAMAGED AT CANT STA 1497. TO REPAIR A DENT IN THE FUSELAGE SKIN AT CANT STATION 1497. FUSELAGE SKIN @ CANT/STA 1497 R/H DAMAGED. SEE ATTACHED REPORT NO. NR-0155SA REV IR FOR ACCOMPLISHMENT INSTRUCTION AND 8110-3 APPROVAL.SDR FXGA2021102001None · noneLEFT PAC SUPPLY PRESSURE DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURIZATION WHILE IN CRUISE TO ANC. FOUND LOOSE CLAMP AND DUCTING FROM ACM OUTPUT.SDR FXGA20210721001Pump · faultedCENTER FUEL PRESSURE LOW LIGHT ILLUMINATED/CENTER TANK FAILS TO FEED IN FLIGHT. RAN QRH PROCEDURE.(FOUND AFT CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKER OPEN)SDR FXGA20210328Fire Detector · false activationCARGO FIRE MASTER WARNING ILLUMINATED WITH LOWER AFT COMPARTMENT FIRE INDICATION. NO FIRE DETECTED AFTER LANDING.SDR 2WAA202104220084Instrument Panel · multiple failDURING ADVERSE WEATHER LOST MULTIPLE NAV GUIDANCE INSTRUMENTS, AUTO THROTLE AND AUTO PILOT, DECLARED EMERGENCY DIVERTED TO KIAH. UPON LANDING EVERTHING RETORNED TO NORMAL.SDR FXGA20201026Control Cable · bindingGEAR HANDLE STUCK IN UP POSITION, UNABLE TO LOWER THE GEAR IN BET ON FINAL APPROACH RWY 19. RETURN TO ANC, UNABLE TO LOWER THE FLAPS IN LANDING IN ANC, UNTIL 5 MILE FINAL, THEN THEY STARTED WORKING AGAIN. DECLARED EMERGENCY IN ANC PERFORMED EMERGENCY GEAR E
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