Douglas 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 AALA20160811001Battery Pack · no testOVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 22 AND 26 FAIL TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-53-00. OPS CHECKED NORMAL.Aug 10, 2016 · N964TW · Doug DC983 · Emergency LightingSDR AALA20160810001Battery Pack · no testWHILE ACCOMPLISHING WORK CARD 5403, EMERGENCY POWER SUPPLY BATTERY AB5-1 FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-60-98. OPS CHECKED NORMALAug 9, 2016 · N979TW · Doug DC983 · Emergency LightingSDR WX0A2016081073182Structure · damagedFWD CARGO DOOR AND LOWER BELLY SKIN DAMAGE. ACCOMPLISHED VISUAL INSPECTION OF DAMAGE AREA IAW EA 40-2016-258. FWD CARGO DOOR PUNCTURED ON LOWER FWD SECTION AT BS 389. DOOR SILL AT BS 389 CRACKED AND BENT. SKIN AT BS 389 CRACKED AT STRINGER 29 -30R. SKIN Aug 9, 2016 · N409NV · Doug DC983 · Fuselage Structure (General)SDR AALA20160812005Stringer · crackedAIRCRAFT WAS GROUNDED. IN ACCESSORY COMPARTMENT, RT STR AFT OF FIRE BOTTLES IS CRACKED. R & R STR IAW AARD 51-00-00-1.Aug 8, 2016 · N9629H · Doug DC983 · Fuselage Main, Longeron/StringerSDR AALA20160808005Warning Message · false activationDURING CRUISE AT FL 320, NR 2 CSD OIL PRESSURE LIGHT ILLUMINATED WITH NO RISE IN TEMPERATUR, CSD WAS DISCONNECTED. CREW REPORTED AN ELECTRICAL ODOR. EMERGENCY DECLARED, LANDING UNEVENTFUL, AND AIRCRAFT GROUNDED. MAINTENANCE INSPECTED THE NR 2 CSD PRESSURE SAug 8, 2016 · N983TW · Doug DC983 · AC Generator-AlternatorSDR AALA20160809003Battery Pack · inoperativeDURING ACCOMPLISHMENT OF WORK CARD 0801, THE FORWARD INTERIOR OVERWING EMERGENCY EXIT LIGHTS FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY ASSEMBLY B5-103 IAW AMM 33-53-00. SYSYTEM TESTED NORMALAug 8, 2016 · N565AA · Doug DC983 · Emergency LightingSDR AALA20160809002Battery Pack · inoperativeDURING ACCOMPLISHMENT OF WORK CARD 0801, THE FIRST CLASS EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY ASSEMBLY B5-100 IAW AMM 33-53-00. SYSYTEM TESTED NORMAL.Aug 8, 2016 · N565AA · Doug DC983 · Emergency LightingSDR AALA20160808004Filter · cloggedDURING FLIGHT, THE NR 1 ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED. ALL ENGINE PARAMETERS REMAINED NORMAL. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE ACCOMPLISHED MCM CARD 71-91-14 AND 71-91-11. REMOVED AND REPLACED NR 1 ENGAug 8, 2016 · N9615W · Doug DC983 · Turbine Engine Oil SystemSDR AALA20160809004Switch · leakingAT GATE AN ACRID ODOR WAS REPORTED WITH APU SUPPLYING THE LEFT PACK. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE APU OIL SEQUENCING SWITCH LEAKING. REMOVED AND REPLACED SWITCH. SYSTEM CHECKED NORMAL.Aug 3, 2016 · N964TW · Doug DC983 · APU Oil SystemSDR AALA20160801009Wire · brokenDURING CRUISE, THE NR 1 ENGINE OIL TEMPERATURE REACHED 184 DEGREEES. IAW THE APPLICABLE CHECKLIST. NR 1 ENGINE WAS SHUT DOWN. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND A WIRE PULLED FROM THE P1-812 CONNECTOR FOR THE OIL TAug 1, 2016 · N9619V · Doug DC983 · Engine Oil System WiringSDR AALA20160731005Bearing · failedDURING FLIGHT THE LT ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. POWER REDUCED TO IDLE AND LIGHT REMAINED ILLUMINATED. ENGINE REMAINED AT IDLE THROUGH LANDING AND SHUT DOWN. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND Jul 31, 2016 · N9409F · Doug DC983 · Engine (Turbine/Turboprop)SDR AALA20160730006Proximity Sensor · out of adjustDURING CLIMB THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE ADJUSTED THE RIGHT MAIN LANDING GEAR PROXIMITY SENSOR IAW AMM 32-60-05. OPS CHECKED NORMAL.Jul 29, 2016 · N566AA · Doug DC983 · Landing Gear Position and WarningSDR AALA20160727006Angle · corrodedRIGHT MAIN LANDING GEAR WHEEL WELL ANGLE LOCATED UNDER THE OUTBOARD FORWARD CORNER ABOVE ACCUMULATOR IS CORRODED. REMOVED AND REPLACED ANGLE IAW AARD 51-00-05, DRAWING 5930516, AND SRM 51-30-01.Jul 27, 2016 · N972TW · Doug DC983 · Fuselage Miscellaneous StructureSDR AALA20160726008Proximity Switch · out of adjustDURING TAKE OFF ROLL, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. THE TAKE OFF WAS ABORTED AT APPROXIMATELY 100 KNOTS. MAINTENANCE ACCOMPLISHED ADJUSTMENT AND TEST OF THE FORWARD CARGO DOOR PROXIMITY SWITCH IAW AMM 52-70-02. SYSTEM CHECKED NORMALJul 25, 2016 · N970TW · Doug DC983 · Door Warning SystemSDR AALA20160724001Bottle · low pressureR1 DOOR SLIDE BOTTLE PRESSURE READS OUTSIDE OF THE GREEN BAND. REMOVED AND REPLACED R1 DOOR SLIDE IAW IAW WORK CARD 25-94-20.Jul 23, 2016 · N980TW · Doug DC983 · Escape SlideSDR AALA20160722004Warning Light · illuminatedDURING DESCENT RECEIVED A NR 1 BRAKE HIGH TEMPERATURE INDICATION. EMERGENCY DECLARED. LANDING UNEVENTFUL. MAINTENANCE OBSERVED NR 1 BRAKE TEMPERATURE READING THE SAME AS OTHER BRAKES DURING TAXI FROM GATE TO HANGAR. CHECKED SECURITY OF NR 1 BRAKE TEMPERATUREJul 22, 2016 · N436AA · Doug DC983 · Landing Gear Brake SystemSDR AALA20160727003Fuel Control · contaminatedWHEN TAKE OFF THRUST WAS APPLIED, NR 1 ENGINE FAILED TO ACCELERATE ABOVE IDLE. MAINTENANCE DRAINED NR 1 ENGINE FUEL CONTROL MOISTURE TRAP AND ACCOMPLISHED AN OPS CHECK IAW AMM 73-20-01. SYSTEM CHECKED NORMAL.Jul 20, 2016 · N972TW · Doug DC983 · Fuel Control/Turbine EnginesSDR AALA20160720001Lavatory · underservicedDURING CLIMB FLIGHT ATTDENDANTS REPORTED ALL LAVATORIES INOPERATIVE. EMERGENCY DECLARED. LANDING UNEVENTFUL. LAVATORIES SERVICED. SYSTEM CHECKED NORMAL.Jul 19, 2016 · N564AA · Doug DC983 · Waste Disposal SystemSDR AALA20160719002Beam · crackedL1 DOOR NR 6 BEAM CENTER SECTION IS CRACKED AT BOLT HOLE. REPAIRED THE BEAM IAW AARD 52-10-00-3.Jul 19, 2016 · N9624T · Doug DC983 · Passenger/Crew DoorsSDR 2WAA201608090001Sensing Element · out of positionFIRE DETECTOR LOOP-B FAULT, FIRE DETECTOR LOOP-A NORMAL. TS ENGINE FIRE DETECTION SYSTEM IAW AMM 26-10-00. FOUND SENSING ELEMENT ON ENGINE NR 2 GROUNDED, SPACED ELEMENT AND PERFORMED OPS TEST IAW AMM 26-10-00. OPERATIONAL TEST NORMAL.Jul 15, 2016 · N802WA · Doug DC983 · Fire DetectionSDR AALA20160715006Blades · damagedDURING CLIMB, CREW REPORTED A BIRDSTRIKE ACCOMPANIED BY A BURNING ODOR IN AIRCRAFT. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. NR 2 ENGINE INSPECTION REVEALED DAMAGED FAN BLADES. REMOVED AND REPLACED 2 PAIRS OF FAN BLADES IAW WORKCARD 72-91Jul 15, 2016 · N964TW · Doug DC983 · Turbine Engine Compressor SectionSDR WX0A20160802176Computer · failedSLAT FLAP DISAG LIGHT ILLUMINATED DURING FLIGHT WITH CLEAN WINGS WITH EQRH PAGE 27.8 DISAGREE LIGHT EXTINGUSHED WHEN FLAPS 11 AT 10,000' RETRACTED SLATS RAN CHECK LIST. INDICATIONS NORMAL PASSING 15,000', SLAT CAWS WARNING SOUNDED. WITH DISAGREE LIGHT ILLUMIJul 14, 2016 · N863GA · Doug DC983 · Stall Warning SystemSDR AALA20160714016Frame · crackedFUSELAGE FRAME AT BS 1418 IS CRACKED AT L2R. REPAIRED THE FRAME IAW SRM 53-03-00 FIGURE 31A.Jul 14, 2016 · N9403W · Doug DC983 · Fuselage Main, FrameSDR AALA20160714015Frame · crackedFUSELAGE FRAME AT BS 1418 IS CRACKED AT L2L. REPAIRED FRAME IAW SRM 53-03-00 FIGURE 31A.Jul 14, 2016 · N9403W · Doug DC983 · Fuselage Main, FrameSDR AALA20160714011Shear Tie · crackedSHEAR TIE AT BS 1437 AND L3L IS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-01-00 AND 53-05-00.Jul 14, 2016 · N9403W · Doug DC983 · Fuselage Internal Mounting StructureSDR AALA20160714010Shear Tie · crackedSHEAR TIE AT BS 1437 AND L3R IS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-01-00 AND 53-05-00.Jul 14, 2016 · N9403W · Doug DC983 · Fuselage Internal Mounting StructureSDR AALA20160714008Attach Angle · crackedLEFT VERTICAL STABILIZER LOWER ATTACH ANGLE IS CRACKED AT AFT END. REMOVED AND REPLACED ANGLE IAW SRM 51-01-00 AND BOEING DRAWING 5912188.Jul 14, 2016 · N9403W · Doug DC983 · Vertical Stabilizer, Attach FittingsSDR WX0A201607193177Control Valve · crackedDURING CLIMB OUT, PASSING 9000 FT, TAIL COMPARTMENT HIGH LIGHT AND MASTER WARNING RED LIGHTS ILLUMINATED. PRFORMED MEMORY ITEMS PER QRH 21.4 PERFORMED QRH 21.4 AND LIGHT EXTINGUISHED WITH RIGHT THROTTLE RETARTED. FOLLOWED 21.4 7A-B EMERGENCY DECLARED, RETURJul 14, 2016 · N406NV · Doug DC983 · Pneumatic Indicating SystemSDR AALA20160718003Generator · faultyDURING CRUISE, THE NR 1 CONSTANT SPEED DRIVE TEMPERATURE ROSE ABOVE AN ACCEPTABLE LEVELS AND WAS DISCONNECTED BY FLIGHT CREW. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. REMOVED AND REPLACED THE NR 1 CONSTANT SPEED DRIVE TRANSMISSION AND GENERJul 14, 2016 · N972TW · Doug DC983 · AC Generator-AlternatorSDR AALA20160714018Transmission · faultyDURING CRUISE THE NR 1 CONSTANT SPEED DRIVE TEMPERATURE ROSE ABOVE AN ACCEPTABLE LEVEL HIGH AND WAS DISCONNECTED BY FLIGHT CREW. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. REMOVED AND REPLACED NR 1 CONSTATNT SPEED DRIVE TRANSMISSION AND GENEJul 14, 2016 · N972TW · Doug DC983 · AC Generator-AlternatorSDR WX0A201607153176Warning Message · illuminatedSLAT FLAP DISAGREE LIGHT ILLUMINATED DURING FLIGHT WITH CLEAN WINGS WITH EQRH PAGE 27.8 DISAGREE LIGHT EXTINGUSHED WHEN FLAPS 11 AT 10,000' RETRACTED SLATS RAN CHECK LIST (CLIMB) INDICATIONS NORMAL PASSING 15,000'. SLAT CAWS WARN SOUNDED. WITH DISAGREE LIGHTJul 14, 2016 · N863GA · Doug DC983 · Leading Edge Slat Position Indicating SystemSDR WX0A20160713175Outflow Valve · failedDURING CLIMBOUT PASSING FL 330 FLOW LIGHT ILLUMINATED WITH RAPID RISE IN CABIN PRESSURE. SWITCHED AUTO CONTROLLER BUT COULD NOT ARREST PRESSURE LOSS. ACCOMPLISHED RAPID DEPRESSURIZATION CHECKLIST AND DID EMERGENCY DESCENT. MANUAL PRESSURIZATION CONTROL JAMMED,Jul 12, 2016 · N417NV · Doug DC983 · Pressure Regulator/Outflow ValveSDR AALA20160712001Lens · missingFORWARD GALLEY WALL MOUNTED EMERGENCY LIGHT EXIT COVER IS MISSING. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY AND ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-53-01.Jul 11, 2016 · N571AA · Doug DC983 · Emergency LightingSDR AALA20160711004Skin · crackedFUSELAGE SKIN AT BS 1418 AND L2L IS CRACKED. REPAIRED SKIN IAW SRM 53-04-00.Jul 11, 2016 · N9403W · Doug DC983 · Fuselage Main, Plate/SkinSDR AALA20160711003Skin · crackedFUSELAGE SKIN AT BS 1418 AND L2R IS CRACKED. REPAIRED SKIN IAW SRM 53-04-00.Jul 11, 2016 · N9403W · Doug DC983 · Fuselage Main, Plate/SkinSDR AALA20160707004Lamp · inoperativeAFTER GEAR EXTENSION, NO NOSE GEAR GREEN DOWN AND LOCKED LIGHT. FOLLOWED QRH, DID FLY BY--TOWER VERIFIED NOSE GEAR DOWN. LANDING NORMALLY. RELAMPED BOTH NLG GREEN DOWN AND LOCK LAMPS. OPS CK"D NORMAL. REMOVED GEAR PINS THAT WERE INSTALLED TO TAXI TO THE GATE. Jul 7, 2016 · N9617R · Doug DC983 · Landing Gear Position and WarningSDR WX0A2016070873174Holder · looseREAR F/A REPORTS BURNING, PLASTIC ODOR, BURNING POPCORN ODOR. PULLED C/B, ALL F/A REPORTED ODOR MOVING FORWARD FROM REAR CABIN PROGRESSIVELY GETTING HEAVIER. DESCENDED WHILE PERFORMING ON PACK OFF 1 ON. NO CHANGES, DIVERTED. ON GROUND ODOR STILL EVIDENT, FJul 6, 2016 · N876GA · Doug DC983 · Passenger Compartment LightingSDR JR2R20160705353Fairing · crackedVERTICAL STABILIZER UPPER FORWARD FAIRING AFT ATTACH FLANGE IS CRACKED. REPAIRED VERTICAL STABILIZER UPPER FORWARD FAIRING AFT FLANGE IAW SRM 55-01, FIGURE 2, SHEET 3.Jul 5, 2016 · N419NV · Doug DC983 · Vertical Stabilizer, Plate/SkinSDR AALA20160705002Warning Light · false activationABORTED TO AT 80 KTS ACCT WHEEL NOT TURNING LIGHT ILLUMINATED. ACCOMPLISHED REJECTED TAKE OFF INSPECTION IAW MCM 05-91-27, AND PERFORMED TRANSDUCER FUNCTION CHECK IAW AMM 32-43-02-201. OPERATIONS CHECK NORMAL AND PERFORMED ANTI-SKID BITE TEST IAW AMM 32-43-00Jul 4, 2016 · N967TW · Doug DC983 · Landing Gear Position and WarningSDR AALA20160718008Switch · out of adjustDURING TAKE OFF ROLL, THE AUTO BRAKE HORN ACTIVATED. TAKE OFF WAS REJECTED. MAINTENANCE ADJUSTED THE REJECTED TAKE OFF SWITCHES IAW AMM 27-60-00. OPS CHECKED NORMAL.Jul 3, 2016 · N564AA · Doug DC983 · Landing Gear Brake SystemSDR AALA20160701003Battery Pack · no testOVERHEAD EMERGENCY LIGHTS BY AFT CBIN DOOR WILL NOT TEST. REMOVED AND REPLACED AFT CABIN EMERGENCY BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL.Jun 30, 2016 · N590AA · Doug DC983 · Emergency LightingSDR AALA20160701002Light · faultyL1 PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK NORMAL.Jun 30, 2016 · N590AA · Doug DC983 · Emergency LightingSDR AALA20160701009Bulkhead Web · crackedDAMAGE ON INNER ALUMINUM BULKHEAD, APPROXIMATELY 4" FORWARD OF THE LT SIDE GEAR TRUNNION. DAMAGE RESULTED IN A 2.75" BY 4" LOSS OF MATERIAL TO THE INNER ALUMINUM WEB AND A 0.090" DENT IN THE STEEL WEB. REPAIRED PER SRM 53-05-00-001, FIG 36 AND EA 261750. AIRCRJun 29, 2016 · N969TW · Doug DC983 · Fuselage Main, BulkheadSDR AALA20160630002Pin · shearedDURING TAKE OFF ROLL THE AMBER WHEEL NOT TURNING LIGHT ILLUMINATED. TAKE OFF ABORTED AT APPROXIMATELY 60 KNOTS. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE NR 1 WHEEL TRANSDUCER PINS SHEARED. REMOVED AND REPLACED TRANSDUCER IAW AMM 32-43-02.Jun 29, 2016 · N9625W · Doug DC983 · Brake Anti-Skid SectionSDR 2WAA201629003Duct · failedRIGHT FIRE INDICATION AND BOTH LOOP LIGHTS ILLUMINATED DURING CLIMB OUT. ALL LIGHTS EXTINGUISHED AFTER REDUCING THRUST. OPENED NR 2 ENGINE FOUND UPPER INBD ANTI-ICE AIR TUBE RUPTURED UP TO STAGE 8 IAW AMM 75-10-02.REMOVED AND INSTALLED NR 2 ENGINE INBD UPPER Jun 29, 2016 · N807WA · Doug DC983 · Airfoil Anti/De-ice SystemSDR AALA20160628004Shutoff Valve · faultyAIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY NOT DECLARED, LANDING UNEVENTFUL, AIRCRAFT OVERWEIGHT. DURING CLIMB F/A`S REPORTED A BURNING ODOR. R & R THE RT PRSOV IAW AMM 21-31-12. ACCOMPLISHED PACK BURN OUT IAW CARD 21-92-12. NO ODORS NOTED. SYSTEM CJun 28, 2016 · N9629H · Doug DC983 · Cabin Pressure Control SystemSDR AALA20160627011Trim Switch · wornAIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL. DURING CLIMB THE HORIZONTAL STABILIZER PRIMARY TRIM FAILED. ALTERNATE TRIM OPERATED NORMALLY. R & R THE CAPTAIN"S PRIMARY TRIM YOKE SWITCH IAW AMM 27-40-02. RESET PRIMARY TRIM DJun 27, 2016 · N9403W · Doug DC983 · Stabilizer Control SystemSDR AALA20160627005Frame · wornAIRCRAFT WAS IN BASE MAINTENANCE. CANT FRAME AT FUSELAGE STA 1510 IS WORN FROM TAIL CONE RUBBING. REPAIRED FRAME IAW SRM 51-70-05, FIGURE 1, EA 261574 AND EA 261591.Jun 27, 2016 · N9615W · Doug DC983 · Fuselage Main, FrameSDR AALA20160627004Battery · dischargedAIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS IN FORWARD ENTRANCE AREA ARE INOPERATIVE. R & R THE FORWARD EMERGENCY BATTERY ASSY IAW AMM 33-53-00. OPS CHECK GOOD.Jun 27, 2016 · N9621A · Doug DC983 · Emergency LightingSDR AALA20160627003Battery Pack · dischargedAIRCRAFT WAS NOT GROUNDED. AFT EMERGENCY ESCAPE PATH LIGHTING IS INOPERATIVE. EMERGENCY PATH MARKING SYS FAILS DUAL FEED TEST IN AFT PORTION OF CABIN. R & R POWER SUPPLY AND BATTERY PACK AT FUSELAGE STA 1260 IAW AMM 33-60-98. OPS CHECK GOOD, ALSO, AALA2016Jun 27, 2016 · N9621A · Doug DC983 · Emergency Lighting
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