Douglas 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.
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
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 AALA20130702007Skate Angle · crackedTAIL VERTICAL STABILIZER SKATE ANGLE IS CRACKED ON LT SIDE OF FS 1463. INSTALLED SKATE ANGLE REPAIR DOUBLER IAW EA.SDR WX0A201307121629Battery Pack · inoperativeEMERGENCY EVACUATION LIGHTING SYS FOUND TO BE DEFECTIVE. R & R BATTERIES IN POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECKED WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.SDR YYFA20130701001Interphone · intermittentINTERPHONE INTERMITENT.SDR 2013FA0000380Autothrottle Sys · disengagedMACH TRIM INOPERATIVE LIGHT CAME ON AT ALTITUDE, AUTO THROTTLE AND AUTO PILOT BOTH DISENGAGED, AIR SPEED INDICATORS LEFT .78M RT .71M. ACFT SHUTTERED AND HAD VIBRATION. ALL INDICATIONS RETURNED TO NORMAL AFTER DESCENDING BELOW 28000 FT. PERFORMED NORMAL LANDISDR WX0A2013070800025Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CSDR WX0A2013070800021Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. R & R THE APPROPRIATE BATTERIES IN POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SDR AALA20130629006Computer · inoperativeSLAT DISAGREE LIGHT ILLUMINATED ALONG WITH AUTO SLAT FAIL LIGHT. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. REPLACED NR 1 STALL WARNING COMPUTER. SYSTEM GROUND CHECKED NORMAL.SDR WX0A2013070800028Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMSDR WX0A2013070800027Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHSDR WX0A2013070800026Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK IN THE POWER SUPPLY AND LIGHT RELAY, MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMMSDR WX0A2013070800024Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX R & R BATTERIES IN THE POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECSDR AALA20130628012Electronic Unit · faultedSMOKE & BURNING SMELL IN FORWARD PART OF CABIN AFTER TAKE-OFF. RECIRCULATION FAN WAS OFF & APU WAS OFF. UPON LANDING FOUND AFT CARGO FIRE DETECTION FAULT LIGHT ON. REPLACED CARGO ELECTRONIC UNIT NR THREE THAT HAD FAULTED. SYSTEM GROUND CHECKED NORMAL.SDR YYFA201306280001Smoke Detector · false activationLEFT AFT LAVATORY SMOKE DETECTOR ALARM RINGING.SDR AALA20130628001Fan · malfunctionedSMOKE IN CABIN & FUMES IN CABIN. SMOKE DISAPPEARED AFTER RECIRCULATION FAN TURNED OFF. EMERGENCY DECLARED FLIGHT DIVERTED AUS LANDED WITHOUT INCIDENT. REPLACED AFT CARGO RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL.SDR AALA20130627010Skin · wrinkledOUTER SKIN WRINKLED FROM STATIONS 1202 - 1222 BETWEEN LONGERONS 22 & 23 LT. INSTALLED NEW SECTION OF SKIN IAW SRM 53-04-FIGURE 12 C.SDR AALA20130627009Skin · wrinkledFUSELAGE SKIN WRINKLED FROM STATIONS 1088 - 1183 & LONGERONS 26 TO 18 RIGHT. REPAIRED IAW SRM 53-04 FIGURE 12C.(REPAIR REFERENCE 4A) & EA MD 80-51-029387. INSTALLED FASTENERS IN SKIN & DOUBLER IAW SRM 53-05-00 FIGURE 117 & AARD 51-00-00-1.SDR YYFA20130627001Unknown · odorAFT CABIN SMOKE ALARMS ACTIVATED IMMEDIATELY AFTER TAKEOFF, ACRID ODOR OBSERVED ON FLIGHT DECK AND IN CABIN, F/A NOTIFIED FLIGHT DECK OF SMOKE. EMERGENCY RETURN TO AIRFIELD .SDR AALA20130626011Duct · blownTAIL COMPARTMENT HIGH TEMPERATURE LIGHT & PRESSURIZATION FLOW LIGHT ILLUMINATED, RT & LT PACKS FAILED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. FOUND LT HAND AIR CYCLE MACHINE HOSE DUCT BLOWN & PERI SEALS COMING OFF AT FLOW CONTROL VALSDR YYFA20130625001Warning Light · illuminatedDURING CLIMB 240 TO 280, RECEIVED A "FLOW" ON LIGHT, QRH PROCEDURE WAS COMPLETED, STAYED AT 240, FLOW LIGHT CONTINUED AND THE CABIN ALTITUDE CLIMBING, 100NM FROM DPARTURE, TO AVOID A CABIN PRESSURE PROBLEM, THE CABIN ALTITUDE 7600' AND IN CLIMB, AT 300 FPM, DSDR YYFA201306240001Unknown · smokeSMOKE IN COCKPIT AND CABIN, RIGHT AFTER TAKEOFF.SDR YYFA20130624001Unknown · smokeSMOKE IN COCKPIT CABIN RIGHT AFTER TAKEOFF. OPENSDR WX0A201306240020Skin · chafedRIGHT WING GROUND SPOILER LOWER INBD SURFACE IS CHAFED. REPAIR DAMAGED AREA.SDR WX0A201306240019Skin · chafedLT WING GROUND SPOILER LOWER SURFACE IS CHAFED AT INBD CORNER. REPAIR DAMAGED AREA.SDR YYFA20130621001Pa System · intermittentPA SYSTEM FROM COCKPIT TO CABIN WORKS INTERMITTENTLY USING BOTH THE HANDSET PHONE AND THE MIKE.SDR AALA20130617013Mount Fitting · corrodedCORROSION ON FORWARD GALLEY MOUNT AT STATION 160 & RIGHT BUTTLINES 43 & 51. REPLACED GALLEY TIEDOWN FITTINGS IAW SRM 51-30-05.SDR WX0A201306240016Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX R & R BATTERY PACK IN THE POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK ACCOMPLISHED IAW AMM 33-50-00, SSDR AALA20130618020Battery Pack · dischargedROWS 12 THRU 23 EMERGENCY LIGHTS ON LT SIDE INOPERATIVE. REPLACED BATTERY PACK B5-100. OPS CHECK NORMAL.SDR AALA20130617005Battery Pack · dischargedROWS 12 THRU 23 EMERGENCY LIGHTS ON LT SIDE INOPERATIVE. REPLACED BATTERY PACK B5-103, OPS CHECK NORMALSDR YYFA20130617001Interphone · inoperativeCOCKPIT INTERPHONE NOT TRANSMITTING.SDR YYFA20130616001Pa System · inoperativeP/A AFT NOT AUDIBLE ON GROUND, P/A AFT INTER CREW NO VOLUME.SDR YYFA201306150001Pa System · inoperativeF/A PA SYS INOPERATIVESDR YYFA201306150002Handset · lowFWD CABIN HANDSET VOLUME LOW FROM L1 TO FLT DECK.SDR AALA20130614019Cusp Web · corrodedLT CUSP AT STATION 698 CORRODED. INSTALLED DOUBLER AT STA 698 IAW AARD 53-20-00-16.SDR YYFA20130614002Unknown · odorSLIGHT ODOR OF SMOKE IN COCKPIT CONFIRMED BY CAPTAIN, F/O AND THE REST OF THE CREW PRECAUTIONARY RETURN.SDR YYFA20130614001Pa System · inoperativeFWD P/A DOES NOT RESET AFTER USE.SDR AALA20130613004Generator · failedCREW REPORTED HIGH TEMPERATURE INDICATION ON LT ENGINE AND LT ENGINE GENERATOR FAILED. FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENGINE CONSTANT SPEED DRIVE AND GENERATOR. SYS GROUND CHECK NORMAL OPS.SDR AALA20130613003Door Frame · gougedFORWARD SERVICE DOOR, GOUGES ON BOTTOM MAIN DOOR FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER IAW EA COMP 52-030157.SDR YYFA20130613002Interphone · inoperativeFLIGHT DECK TO CABIN INTERCOM IS BARELY AUDIBLE.SDR YYFA20130613001Engine · malfunctionedNR 2 ENGINE START VALVE OPEN LIGHT ON, NO ENGINE ROTATION.SDR AALA20130626004Cusp Web · corrodedCORROSION ON BOTTOM OF LT HAND CUSP FROM STATIONS 712 - 731. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.SDR WX0A201306270018Vane · chafedRT WING OTBD FLAP INBD VANE L/E DOUBLER CHAFED THROUGH 8" FROM INBD END STA X05 164. REMOVED DAMAGED AREA. FABRICATED DOUBLER, HOT BOND REPAIR AND PERMANENT REPAIR ACCOMPLISHED.SDR WX0A201306240017Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX R & R BATTERY PACK IN POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK ACCOMPLISHED IAW AMM 33-50-00SDR AALA20130612005Beam · crackedFORWARD SERVICE DOOR, DOOR BEAM CRACKED AT LOWER DOOR HINGE MOUNT FITTING. INSTALLED DOUBLER IAW SRM 52-05-00, FIGURE 25.SDR AALA20130612003Seat Track · corrodedSEAT TRACK NR 6 FROM STA 855 TO 856 CORRODED. SEAT TRACK NR 6 FROM STA 855 TO 856 REPAIRED BY ROUTING OUT DAMAGED AREA AND INSTALLING SEAT TRACK PLUG IAW AARD 53-20-00-10 AND SRM 53-05-00, FIG 4A.SDR AALA20130612002Cusp Web · corrodedCORROSION ON CUSP UNDER NR 1 SEAT TRACK AT STA 1174. INSTALLED CUSP DOUBLER ON SEAT TRACK NR 1 FROM STATIONS 1174 TO 1177 IAW AARD 53-20-00-16.SDR AALA20130611017Cusp Web · corrodedRT CUSP SHEET CORRODED FROM STA 503 TO 579. REPLACED RT CUSP FROM STATIONS 503 TO 579 IAW AARD 53-20-00-16.SDR AALA20130611010Longeron · crackedNR 2 RT LONGERON CRACKED AT STA 1429. INSTALLED NEW LONGERON AND SPLICE IAW SRM 53-02-00.SDR AALA20130611008Skin · wrinkledFUSELAGE SKIN WRINKLED FROM STATIONS 512 TO 588 AND LONGERONS 18 TO 26 LT. INSTALLED NEW SERVICABLE SKIN FROM STATIONS 512 TO 588 IAW SRM 53-04-00, FIG 12C.SDR AALA20130611006Skin · wrinkledFUSELAGE SKIN WRINKLED FROM STATIONS 1088 TO 1202 BETWEEN LONGERONS 21 AND 22 LEFT. INSTALLED NEW SKIN SECTION AND INTERNAL DOUBLERS FROM STATIONS 1088 TO 1202 IAW SRM 53-04-00, FIG 12C.SDR YYFA20130611001Warning Light · illuminatedAFTER TAKE OFF, LEFT MAIN GEAR RED LIGHT REMAINED ON AND GEAR DOOR LIGHT ON. FOLLOWED QRH PROCEDURE AND CYCLED ONE TIME LIGHTS REMAINED ON. RETURNED TO DEPARTURE.
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