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 engine_model_key = 'CT581402' 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 engine_model_key = 'CT581402' 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 39LA2014031364Warning Light · activatedDURING CRUISE FLIGHT THE NR 1 ENG FIRE WARNING LIGHT ILLUMINATED. THE EMERGENCY CHECKLIST WAS ACCOMPLISHED & THE DECISION WAS MADE TO DIVERT TO FOB WHICH WAS APPROXIMATELY 2 MILES AWAY. THE LANDING AT FOB WAS WITHOUT INCIDENT.SDR 39LA2014031263Fire Loop · chafedDURING CRUISE FLIGHT FROM OAIX TO OASH THE NR 1 ENG FIRE WARNING LIGHT ILLUMINATED. THE EMERGENCY CHECKLIST WAS ACCOMPLISHED & A RETURN TO OAIX WAS ACCOMPLISHED WITHOUT INCIDENT. FOUND FIRE LOOP CHAFFING ENG DECK, REPOSITIONED LOOP ACCOMPLISHED IAW S61N MM SDR 39LA2014021257Generator · failedAFTER DEPARTURE FROM OASH THE DC GEN LIGHT ILLUMINATED. ACCOMPLISHED THE EMERGENCY PROCEDURES, GEN WOULD NOT RESET. R & R DC GEN PN 30E20-97A IAW S61 MM 4045-80, REV 47, 24-20-01.SDR 39LA2014021158Window · departedAFTER DEPARTURE FROM OASH THE RT HAND EMERGENCY EXIT WINDOW DEPARTED THE AIRCRAFT. RETURNED TO OASH WITHOUT INCIDENT. INSTALLED SERVICEABLE EMERGENCY EXIT WINDOW IAW S61N MM SA-4045-83 CH 56-20-00.SDR CA140218005Hose · failed(CAN) PRIMARY HYDRAULIC PRESSURE FLUCTUATING, AND LOW PRESSURE WARNING LIGHT ILLUMINATED IN FLIGHT. PRESSURE HOSE FROM PRIMARY HYDRAULIC PUMP TO MANIFOLD LEAKING AT MIDPOINT OF HOSE. NO INDICATION OF CHAFING OR ANOMALIES THAT MIGHT HAVE CAUSED THE HOSE TO FASDR 39LA2014013056Brake Sys · contaminatedDURING TAXI THE BRAKES BECAME STUCK DURING FWD MOTION, THEN WOULD NOT STOP THE AIRCRAFT WHEN DEPRESSED. BLED MLG BRAKES IAW S61N MM 4045-80 REV 47 CHAPT 32-43-0, OPERATIONS CHECKED OKSDR 39LA2014012254Generator · failedAFTER DEPARTING OAIX DURING CRUISE FLIGHT THE NR 1 FUEL BOOST PUMP LIGHT ILLUMINATED FOLLOWED BY AN AFCS FAILURE. SHORTLY AFTER THE TAIL TAKE-OFF LIGHT ILLUMINATED WITH A NR 1 GEN WARNING LIGHT. THE EMERGENCY PROCEDURE CHECKLIST WAS EXECUTED WITHOUT RESOLUTSDR 39LA2014012053Relay · failedON APPROACH TO OAKN THE GEN FAIL WARNING LIGHT ILLUMINATED WITH A MASTER CAUTION WARNING. THE EMERGENCY PROCEDURE TO TRY & RESTORE POWER WAS ACCOMPLISHED WITH NO RESULT. WE LANDED AIRCRAFT WITHOUT INCIDENT. REMOVED REVERSE CURRENT RELAY PN A-700AW, SN AP98SDR 39LA2013122643Blower Motor · seizedHEATER BLOWER MOTOR SEIZED IN FLIGHT EMITTING SMOKE. REMOVED BLOWER MOTOR ASSEMBLY PN ME-600-1000, SN 1013 & INSTALLED OVERHAULED BLOWER MOTOR ASSEMBLY, FAN AXIVAN PN 500702-4491, SN AA-79463 IAW S-61MM SA4045-80, REV 47 CHAPTER 21 AIR CONDITIONING.SDR 39LA2013121329Blower · failedDURING FLIGHT AT CRUISE ALTITUDE WITH CABIN HEAT ON, SMOKE WAS NOTICED COMING FROM THE HEATER AREA. REMOVED HEATER BLOWER PN ME-600-1000, SN 1632. INSTALLED SERVICEABLE HEATER BLOWER PN 500702-4491, SN AA6117 IAW SA4045-80, CH 21-40-0.SDR 39LA2013121228Bearing · damagedDURING LANDING CREW FELT VIBRATION & ON SHORT FINAL MASTER CAUTION LIGHT ILLUMINATED WITH CORRESPONDING INTERMEDIATE GEARBOX CHIP DETECTOR LIGHT. REMOVED INTERMEDIATE GEARBOX PN S6135-66300-002, SN A15-887 & INSTALLED PN S6135-66300-2, SN A15-1045 IAW S-61 MMSDR 39LA2013120727Cable Assy · damagedNR 1 ENG FIRE WARNING LIGHT ILLUMINATED IN FLIGHT. TROUBLE SHOT SYS, FOUND DAMAGED LEAD, REPLACED WITH SERVICEABLE LEAD PN 35302-62, SN NA, WORK PERFORMED IAW S61N MM SA4045-80, CHP 26-00-00, OPERATIONS CHECKED GOOD 12/07/13.SDR 39LA2013120226Door · openDURING TAKEOFF FROM FOB SHANK THE PASSENGER AIRSTAIR DOOR OPENED. THE TAKEOFF WAS ABORTED & AIRCRAFT RETURNED TO PARKING.SDR 39LA2013111415Indicator · failedDURING CRUISE FLIGHT, ENROUTE, THE AFT FUEL CELL LOW LIGHT ILLUMINATED. TRANSFERRED KNOWN QUANTITY OF FUEL INTO AFT FUEL CELL WITH NO RISE IN AFT TANK INDICATION. ACFT DIVERTED WITHOUT INCIDENT. R & R AFT FUEL CELL INDICATOR GAUGE AND CALIBRATED TO AFT TANKSDR 39LA201311066Connector · dirtyNR 2 ENGINE FIRE LIGHT INTERMITTENTLY ILLUMINATED IN FLIGHT. DISCONNECTED NR 2 ENG FIRE LOOP CONNECTORS, CLEANED AND CONNECTED FIRE LOOP CONNECTORS IAW MM 26-10 AS APPLICABLE. OPS CHECKED GOOD, LIGHT NO LONGER ILLUMINATED.SDR CA131105014Blades · wrong part(CAN) THE ENGINE WAS SENT TO THE SHOP FOR SCHEDULED O/H. AFTER DISASSEMBLY, INSPECTION INDICATES THAT THERE WERE A NR OF STAGE 1, 3, 4, AND 9 COMPRESSOR BLADES THAT DO NOT CONFORM, AS THEY DID NOT HAVE THE CODE NR STAMPED INTO THE ROOT END AS IS STANDARD FOR SDR 39LA201311045Blanking Plate · departedAFTER DEPARTURE, ENROUTE, A WINDOW PLUG DEPARTED THE ACFT FROM THE LT EMERGENCY EXIT DOOR. AFTER LANDING IT WAS DISCOVERED THAT A TAIL ROTOR BLADE HAD BEEN DAMAGED AS A RESULT OF THE INCIDENT.SDR 39LA201310314Generator · failedAFTER NR 2 ENGINE START CREW REPORTED STRANGE ODOR AND SMOKE IN THE CABIN. ENGINE SHUTDOWN WAS ACCOMPLISHED. REMOVED NR 2 AC GENERATOR, INSTALLED OVERHAULED NR 2 AC GENERATOR WORK PERFORMED IAW MM SA4045-80, CHSP 24-00-00 & 65.00.00 AS APPLICABLE, OPS CHECSDR 39LA201310283Fire Loop · failedDURING CRUISE FLIGHT NR 2, ENGINE FIRE WARNING ILLUMINATED. R & R NR 2 ENGINE FIRE LOOP IAW MM CH26-10-3.SDR 39LA201310182Fan · failedWHILE IN CRUISE, BOTH PILOTS NOTICED SMOKE COMING INTO THE COCKPIT FROM VENTS. BEGAN EMERGENCY CHECKLIST, THE SMOKE SOURCE WAS ISOLATED TO THE HEATER BLOWER MOTOR AND WAS SECURED. REMOVED FAN BLOWER, PN ME-630-10001-10, SN 1037, INSTALLED OVERHAULED FAN BLOWESDR 39LA2013100400004Line · burstNR 2 ENGINE FLAMED OUT DURING TAKEOFF. R & R FUEL LINE FROM STATIC FILTER TO FUEL FLOW DIVIDER. PRIMED SYS LEAKED CHECKED, NO LEAKS NOTED.SDR 39LA2013090300004Engine · malfunctionedSUSPECTED COMPRESSOR STALL ON NR 1 ENGINE DURING CLIMBOUT. COMPLETED NR 1 ENG COMPRESSOR WASH AND INSPECTED FRONT FRAME. NO DAMAGE NOTED WORK DONE IAW SEI -182, CHAPTER 72-00, DATE 8/27/13.SDR 39LA2013082000004Compressor · stalledAT HOVER, MULTIPLE COMPRESSOR STALLS.SDR CHIR20131608001Engine · inoperativePILOTS REPORTED THAT DURING A DESCENT, NR 1 ENGINE TORQUE WAS AT 25 PERCENT AND NR 2 ENGINE TORQUE WAS AT 7 PERCENT. PULLED IN POWER TO INCREASE TORQUE ON THE NR 2 ENGINE. DURING PULL IN OF POWER, NR 2 ENGINE TORQUE DECREASED TO 1 PERCENT MOMENTARILY PRIOR SDR 39LA2013062700004Fire Detector · false activationINTERMITTENT FIRE LIGHT ILLUMINATES, NR 1 ENGINE WITH NO EVIDENCE OF FIRE. INSPECTED NR 1 ENGINE FIRE DETECTOR SENSING ELEMENTS IAW MM 26-10-2. NO DEFECTS NOTED. REPOSITIONED FIRE DETECTOR SENSING ELEMENT IAW MM 26-10-2, PAR 1. PERFORMED MOC, NO DEFECTS SDR CHIR201306250058Sprag Clutch · brokenON STARTUP, AFTER ADVANCING THE ENGINES TO FLIGHT IDLE, DISCOVERED THAT NR 2 ENGINE NF WAS HIGHER THAN NR AND NR 2 ENGINE TORQUE WAS CLOSE TO 0 PERCENT. WHEN NR 1 ENGINE WAS RETARDED TO GROUND IDLE, WITH NR 2 ENGINE STILL AT FLIGHT IDLE, NR DROPPED AND NR 2 ESDR CA131022008Support · damaged(CAN) ACFT EXPERIENCED A LOW OIL PRESSURE EVENT WHILE IN FLIGHT. TWIN ENGINE, FLIGHT CREW SHUTDOWN THE ENGINE AND LANDED THE ACFT. ENGINE WAS REMOVED AND SENT TO FOR REPAIR. ENGINE WAS DISASSEMBLED AND FOUND TO HAVE SUFFERED OIL STARVATION DUE TO A SHEAREDSDR CHIR201306060002Bolt · wornDURING OPPORTUNITY INSPECTION, MX CREW NOTICED EXCESSIVE STEP WEAR ON AFT ROTOR PITCH CHANGE LINK (GREEN POSITION) UPPER BOLT. PITCH CHANGE LINK BOLT WAS SUBSEQUENTLY REPLACED.SDR CA130527005Purifier · chafed(CAN) ENGINE NR 2 WAS REMOVED FROM THE ACFT FOR A ROUTINE FUEL CONTROL & FUEL PUMP REPLACEMENT, DUE O/H. AT THIS TIME THE CFP WAS INSPECTED AND FOUND TO HAVE AN INTERNAL RUB BETWEEN THE CENTRIFUGE ASSY AND THE DRIVE HSG. METALLIC PARTICLES WERE ALSO FOUND INSDR 39LA2013030800004Engine · malfunctionedIMMEDIATLY AFTER TAKEOFF AT APPROX 97 PERCENT NG THE NR 1 NG BEGAN TO FLUCTUATE 3-4 PERCENT. NOTICED THE NR 1 NF BEGIN TO FLUCTUATE AS WELL NR 1 FUEL PRESSURE AND T5. ALL INDICATIONS ON NR 2 ENGINE WERE NORMAL. APPROXIMATE 40 PERCENT TORQUE SPLIT WAS NOTED SDR 39LA201301150023Chip Detector · contaminatedAT CRUISE ALTITUDE, THE NR 1 ENGINE CHIP LIGHT ILLUMINATED. A RESET WAS ATTEMPTED WITH NO AFFECT. ACFT DIVERTED FOR MX. MX REMOVED THE CHIP DETECTOR AND CLEANED IT. AFTER REINSTALLATION NO LIGHTS WERE INDICATED DURING OR AFTER RUN UP.SDR P4YA2012121500001Blade · damagedAFTER TAKEOFF, NR 1 ENGINE LOST POWER, LOUD REPORT FROM ENGINE AND LANDED IMMEDIATELY. MX INSPECTED NR 1 ENGINE AND FOUND 1ST AND 2ND STAGE COMPRESSOR BLADE DAMAGE DUE TO FOD. R & R NR1 ENGINE.SDR CHIR201208281020Engine · leakingAIRCRAFT WAS ON AN ACTIVE FIRE MISSION WHEN FLYING BACK TO THE WATER DIP SIGHT CO-PILOT NOTICED THE NR 2 ENGINE OIL PRESSURE DROP TO ZERO, SECONDS LATER THE NG DROPPED TO ZERO THEN THE NR 2 CHIP LIGHT ILLUM PILOT RELEASED THE LONGLINE AND WATER BUCKET (THEY HESDR P4YA2012081000001Thermostat · failedAFTER TAKEOFF, CREW NOTICED TRANSMISSION OIL PRESSURE WAS BELOW THE MINIMUM CONTINUOUS LIMIT IAW THE RFM (35 PSI). CREW RETURNED TO BASE AND SHUTDOWN. MAINTENANCE REMOVED, DISSASSEMBLED, CLEANED AND REINSTALLED SNUBBER. ALSO, R & R THERMOSTAT. PERFORMED GSDR CHIA20122001001Generator · failedNR 1 GENERATOR LIGHT ILLUMINATED WHILE CIRCLING AND HOLDING WAITING FOR LANDING SPACE. A BRIEF PUNGENT ODOR WAS NOTICE AND ACFT DIVERTED TO ALTERNATE LANDING ZONE. THE ODOR DISAPPEARED UNTIL LANDING. AFTER LANDING AND SHUTDOWN IT WAS NOTICED THAT THE NR 1 GSDR CA111219006Engine · making metal(CAN) NR 1 ENGINE CHIP WARNING LIGHT ILLUMINATED DURING TAXI. MAGNETIC PARTICAL PLUG INSPECTED AND PARTICLE EXCEEDING LIMITS WAS FOUND. ENGINE WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR 3S8R201110150001Switch · inoperativeNR 1 ENGINE FAILED DURING FLIGHT. R & R THE FUEL VALVE SWITCH WITH THE SAME. OPS CHECKED GOOD. NO DEFECTS NOTED.SDR CA120221001Safety Wire · unsecure(CAN) DURING LONG LINE OPERATIONS, AN UNCOMMANDED LOSS OF AN EXTERNAL LOAD WAS EXPERIENCED. POST EVENT INVESTIGATION REVEALED THAT THE POSITION OF THE SAFETY WIRE USED TO SECURE THE CABLE IN THE RELEASE ARM HAD SNAGGED THE MANUAL RELEASE CABLE, CAUSING IT TO SDR P4YA2011022400001Case · crackedON POST FLIGHT INSPECTION FOUND THE NR 1 ENGINE POWER TURBINE EXHAUST CASING CRACKED BEYOND LIMITS. ENGINE SN 285-063RC IN PROCESS OF BEING REMOVED AND REPLACED.SDR CA101019019Bolt · brokenDURING NORMAL OPERATIONS A "SNAP" IN THE CYCLIC WAS NOTICED BY THE PIC. AS POWER WAS APPLIED THE PIC NOTED ABNORMAL BEHAVIOR IN THE ACFT THAT REQUIRED A FULL RT AND FWD CYCLIC INPUT TO MAINTAIN STRAIGHT AND LEVEL ATTITUDE. ACFT WAS STABILIZED AND LANDED IMMESDR CA101103003Mount · cracked(CAN) POST FLIGHT INSPECTION FOUND SMALL CRACK IN GEARBOX MOUNT RADIUS THIS WAS THE SECOND OCCURENCE.SDR 2010F00159Insulator · wornTHE NR 1 ENGINE FIRE LIGHT ILLUMNIATED IN FLIGHT. GROUND CHECKS WERE BEING PERFORMED FOR FIRE LIGHT ON PREVIOUS DAY. ACFT WAS IN HOVER WHEN LIGHT ILLUMINATED AFTER REPLACING FIRE LOOP ON PREVIOUS DAY. MX PERFORMED ADDITIONAL TROUBLESHOOTING AND DISCOVERED TSDR KHS2010F00001Insulator · wornNR 1 ENG FIRE LIGHT ILLUMINATED IN FLIGHT. GROUND CHECKS WERE BEING PERFORMED FOR FIRE LIGHT ON PREVIOUS DAY. ACFT WAS IN HOVER WHEN LIGHT ILLUMINATED AFTER REPLACING FIRE LOOP ON PREVIOUS DAY. MX PERFORMED ADDITIONAL TROUBLESHOOTING AND DISCOVERED THE INSUSDR 2010F00156Fire Loop · false activationTHE NR 1ENGINE FIRE LIGHT ILLUMINATED UPON LANDING. ACFT COMPLETED ITS NORMAL LANDING WITH NO SECONDARY INDICATIONS, SHUTDOWN AND NOTIFIED MX. MX INSPECTED ACFT NOTING NO DAMAGE TO SYS. DURING TROUBLESHOOTING REPLACED DENTED FIRE LOOP, TESTED FIRE DETECTIONSDR CA100702007Bushing · worn(CAN) ON JUNE 15 20 NR 1 & 2 ENGINES. EMERGENCY PROCEDURES WERE CARRIED OUT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. A DETAILED VISUAL INSPECTION OF THE APPLICABLE ENGINE WAS CARRIED OUT WITH NO FAULT FOUND. THE MAINTENANCE STAFF ARRANGED FOR A GROSDR CA090911001Limit Switch · failed(CAN) DURING THE DAILY FUNCTIONAL TEST OF THE SPEED TRIM LIMIT SWITCHES THE RETRACT LIMIT SWITCH FAILED TO STOP THE MOTOR. THIS SPEED TRIM ACTUATOR WAS IN SERVICE FOR 30 HOURS AFTER REPAIR FOR THE SAME FAILURE. (TC# 20090911001)SDR CA090324013Arm · cracked(CAN) A CRACK APPEARED ON A TORQUE ARM EMANATING FROM THE LUBRICATION FITTING HOLE. THE CRACK RUNS ALONG THE AXIS OF THE BOLT THAT WOULD GO THROUGH THE PIVOT JOINT.SDR C4N2008F00000Connector · disconnectedMAIN TRANSMISSION CHIP DETECTOR ILLUMINATED IN FLIGHT. (K) AFTER LANDING, INSPECTION FOUND CHIP PLUG LEAD HAD FALLEN OFF CHIP DETECTOR. LEAD WAS REINSTALLED, ACFT WAS RETURNED TO SERVICE.SDR CA071204008Bearing · overheated(CAN) ON FIRST FLIGHT OF THE DAY, AIRCRAFT WAS GROUND TAXIING TO TAKE OFF AREA WHEN GROUND CREW NOTICED SMOKE FROM TAIL ROTOR DRIVE INTERMEDIATE GEAR BOX AREA. AIRCRAFT WAS SHUT DOWN, AND INSPECTION REVEALED OVERHEATING IN THE INPUT BEARING AREA. SIKORSKY AND SDR CA071126010Gearbox · making metal(CAN) INTERMEDIATE GEAR BOX CHIP LIGHT ILLUMINATED IN FLIGHT. AFTER LANDING CHIP PLUG INSPECTION CONFIRMED METAL CONTAMINATION, AS WELL AS PAINT DISCOLORATION WAS NOTED IN THE INPUT BRG AREA. ASSY WILL BE SENT TO OH SHOP FOR INVESTIGATION. (TC NR 20071126010)
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