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 = '407' 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 = '407' 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 IAVA202008040001Drive Shaft · crackedDURING 100 HOUR LUBRICATION OF TAIL ROTOR DRIVE SHAFT SPLINES THE #3 TAIL ROTOR DRIVE SHAFT WAS FOUND CRACKED AT ONE ATTACHMENT EAR. TOTAL TIME OF PART IS UNKNOW AS IT IS AN ON CONDITION PART.SDR QMLA2020072320038Housing · faultyDURING CRUISE FLIGHT WITH NG ABOVE 94%, OIL PRESSURE DROPPED TO 50 PSI. APPROACH WAS INITIATED AND PRECAUTIONARY LANDING WAS MADE WITH A NORMAL SHUTDOWN OF AIRCRAFT. OIL FILTER HOUSING/REGULATOR WAS CHANGED AND OIL PRESSURE RETURNED TO WORKING PROPERLY.SDR QMLA2020071420035Chip Detector · contaminatedPILOT WAS REPOSITIONING THE AIRCRAFT TO THE HOSPITAL FROM THE AIRPORT AND UPON REACHING APPROXIMATELY 300' AGL AFTER TAKEOFF HE RECEIVED A TAIL ROTOR CHIP WARNING INDICATION ON THE PFD. THE PILOT IMMEDIATELY RETURNED BACK TO THE AIRPORT. TWO MECHANICS INSPECSDR QMLA2020071320034Unknown · odorCREW SMELLED FUEL ON DEPARTURE. MAINTENANCE INSPECTED ENGINE DECK AND COMPARTMENT, ENGINE, INSPECTED CABIN AND FUEL CELL AREAS, INSPECTED AND OPERATED CABIN BLOWERS. NO LEAKS, DISCREPANCIES, OR SMELLS WERE FOUND AND COULD NOT DUPLICATE EVENT.SDR QMLA2020061542026Latch · damagedPILOT REPORTED HE WAS UNABLE TO CLOSE THE LITTER AND GET LATCHED DUE TO THE DOOR LATCH WAS OVER CENTER.SDR QMLA2020052920023Belt · out of adjustDURING TAKEOFF, CREW COMPLAINED OF BURNT RUBBER OR PLASTIC SMELL IN THE CABIN. AIR CONDITIONER WAS TURNED ON AND UPON THE SMELL OF THE RUBBER THE A/C WAS TURNED OFF AND SMELL EVENTUALLY WENT AWAY AFTER THE CREW ABORTED THE FLIGHT, AND OPENED WINDOWS TO VENT ASDR QMLA2020052820022Duct · looseDURING CRUISE FLIGHT, CREW AND PATIENT COMPLAINED OF CARBON MONOXIDE POISONING SYMPTOMS INCLUDING LIGHT HEADEDNESS, SLEEPINESS AND HEADACHE. HEATER WAS IN OFF POSITION, BOTH SWITCHES, BUT HEAT AND FUMES WERE COMING FROM HEATER VENT IN AFT COMPARTMENT OF AIRCRASDR QMLA2020052720021Gearbox · making metalON TAKEOFF FROM THE AIRPORT THE PILOT HAD THE MAIN ROTOR GEARBOX CHIP INDICATION ILLUMINATE. THE PILOT LANDED BACK AT THE HANGAR, LESS THAN ONE MINUTE OF FLIGHT PUT ON THE AIRCRAFT. MECHANIC REMOVED CHIP DETECTOR AND FOUND APPROXIMATELY 20 METAL CHIPS ON DETSDR QMLA2020052120020Chip Detector · dirtyTAIL ROTOR GEARBOX CHIP LIGHT INDICATION IN FLIGHT. PRECAUTIONARY LANDING WAS PERFORMED AS PER THE RFM. THE MECHANIC ARRIVED TO INSPECT THE AIRCRAFT AND FOUND ONE HAIR-LIKE PARTICLE ON CHIP DETECTOR. CLEANED AND REINSTALLED DETECTOR. A TEN MINUTE GROUND RUN WASDR QMLA2020051820019Cooling Fan · seizedWHILE RETURNING TO THE BASE, THE PILOT REPORTED AN ELECTRICAL SMELL IN THE COCKPIT AND SAW A SLIGHT AMOUNT OF SMOKE FWD OF INSTRUMENT PANEL. ONCE ON THE GROUND, THE MECHANIC ARRIVED TO TROUBLESHOOT THE CAUSE OF THIS SMELL AND FOUND THE AVIONICS COOLING FAN ON SDR M3XA20200511004Engine · unknownPILOT REPORTED DURING CRUISE FLIGHT A SUDDEN LOUD BUZZING/GRINDING NOISE THAT DROWNED OUT THE CABIN NOISE. IT FOLLOWED POWER APPLICATION.SDR QMLA2020050520017Unknown · odorFUEL SMELL WAS REPORTED BY THE NURSE AND PARAMEDIC DURING CRUISE FLIGHT. THE NURSE STATED THAT THE SMELL IS STRONGER THEN HE'S SMELLED IN THE PAST. WE TURNED OFF THE AIR-CONDITIONER AND OPENED THE WINDOWS TO VENT THE A/C AND LANDED AT OUR BASE. AFTER SHUTTING SDR QMLA2020042320016Attach Fitting · crackedDURING AIRWORTHINESS CHECK BY THE MECHANIC, HE FOUND A 1.75" CRACK IN LH UPPER HORIZONTAL STABILIZER ATTACH FITTING. *** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION WHILE A BELL APPROVED CUSTOMER SERVICE FACILITY COMPLETES THE PART REPLSDR K2DA53101Transmission · making metalSHORTLY AFTER TAKEOFF THE MAIN ROTOR TRANSMISSION CHIP LIGHT ILLUMINATED. THE AIRCRAFT TURNED AROUND AND LANDED BACK AT THE AIRPORT & MX WAS DISPATCHED TO THE AIRCRAFT. UPON INSPECTION OF THE MAIN ROTOR TRANSMISSION CHIP DETECTORS, MAINTENANCE PERSONNEL FOUNSDR QMLA2020031320011Structure · crackedWHILE CONDUCTING SCHEDULED MAINTENANCE, THE MECHANIC FOUND A CRACK ON THE VERTICAL FIN FLANGE THAT MOUNTS THE TAIL ROTOR GEAR BOX COVER TO VERTICAL FIN TOP AFT CORNER. ** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION PENDING REPAIR. **SDR EVCA2020030600000Freewheel Unit · crackedDURING PERIODIC INSPECTION, THE FREEWHEELING UNIT HOUSING WAS VISUALLY DISCOVERED TO BE CRACKED ON THE MATING SURFACE TO THE ENGINE. THE CRACK EXTENDED APPROXIMATELY 0.5 INCHES FROM THE ATTACHMENT HOLE.SDR QMLA2020022752010Blade · crackedWHILE PERFORMING THE A 1640 600 HOUR/12 MONTH HUB AND BLADE INSPECTION THE MECHANIC FOUND TWO SMALL CRACKS ON THE TOP OF THE TRIM TAB WHERE IT MEETS THE TRAILING EDGE OF THE BLADE. P/N 407-015-001-117FM1 S/N A-133. THIS IS ONLY REPAIRABLE BY AUTHORIZED MECHANISDR M3XA20200130002Unknown · odorPILOT REPORTED A FUEL SMELL IN THE CABIN. MECHANIC TROUBLESHOT THE SMELL. REPLACED FUEL CAP AND REAPPLIED SEALANT TO FUEL CAP COMPONENTS. SMELL STILL PRESENT.SDR HEER20200129626Combustion Case · crackedENGINE REMOVED 12/31/2019 DUE TO SCHEDULE CHANGE FOR TURBINE OVERHAUL (WHEEL RETIREMENTS). FOUND OUTER COMBUSTION CASE CRACKED AROUND FUEL NOZZLE WELD. M250-C47 SERIES CEB A-72-6085 REV 3 ENGINE, COMBUSTION ASSEMBLY - INSPECTION OF OUTER COMBUSTION CASE P/N SDR QMLA2020011320001Transmission · making metalJUST AFTER TAKE OFF FROM THE HOSPITAL HELIPAD, DURING THE INITIAL CLIMB TO CRUISE ALTITUDE, THE XSMN CHIP CAUTION LIGHT ILLUMINATED. ALTITUDE WAS APPROXIMATELY 700 FEET, AIRSPEED OF 90 KTS WITH CLIMB-OUT POWER APPLIED. FORTUNATELY, WE WERE JUST PASSING THE APPSDR QMLA201912198099Hose · leakingFUEL SMELL IN CABIN DURING FLIGHT. UPON INVESTIGATION BY MECHANIC, IT WAS DETERMINED THAT A STEAL BRAIDED HOSE WAS FOUND TO BE LEAKING DURING A PRESSURE TEST OF THE FUEL SYSTEM. *** THIS AIRCRAFT REMAINS OOS AT THE TIME OF THIS SUBMISSION AWAITING THE REPLACEMSDR QMLA2019112299087Engine · making metalDURING ROUTINE INSPECTION OF ENGINE CHIP DETECTORS FOUND NUMEROUS CHIPS AND DEBRIS ON BOTH UPPER AND LOWER CHIP PLUGS. AMOUNT AND SIZE EXCEEDED ALLOWABLE PER ROLLS ROYCE C47-250 EMM. *** THIS AIRCRAFT REMAINS OOS AT THE TIME OF THIS SUBMISSION TO REPLACE THIS SDR QMLA2019110749082Vhf Comm · malfunctionedPILOTS REPORT: AT TAKE OFF, THE NUMBER 2 VHF RADIO/GPS SHUT OFF. I WAS UNABLE TO GET IT TO COME BACK ON. BEING FAMILIAR WITH THE MEL (2312-01) I KNEW THAT I ONLY HAD TO HAVE ONE VHF RADIO OPERATIONAL TO CONTINUE MY FLIGHT. AFTER A SHORT DISCUSSION WITH THE CRESDR QMLA2019102291981Fuel Cap · leakingFOLLOWING A RECENT SIMILAR EVENT, THE SAME CREW MEMBER SMELLED FUEL IN FLIGHT ONCE THE AIRCRAFT REACHED APPROXIMATELY 100 KIAS STRAIGHT AND LEVEL. THIS TIME THE SMELL APPEARED TO BE MUCH STRONGER. THE PILOT IMMEDIATELY RETURNED TO BASE AND CONTACTED THE MECHANSDR QMLA2019101719080Unknown · odorMED CREW REPORTED SMELLING FUEL IN CABIN DURING THE SECOND LEG OF A PATIENT TRANSPORT FLIGHT. THE AIRCRAFT WAS LANDED, AND MECHANIC WAS CALLED TO INSPECT THE AIRCRAFT. THE BAGGAGE COMPARTMENT MEDICAL SERVICES PANEL WAS REMOVED TO EXPOSE A FUEL VALVE THAT WAS TSDR QMLA201910119079Evaporator · inoperativeAIRCRAFT WAS IN ROUTE WITH PATIENT ON BOARD. CREW NOTICED BURNING ODOR. PILOT MADE PRECAUTIONARY LANDING IN A PASTURE AND NOTIFIED DISPATCH. PILOT CALLED MECHANIC WHO ARRIVED AND DETERMINED THE AFT AIRCONDITION EVAPORATOR MOTOR OVERHEATED. MECHANIC INSPECTED FSDR HEER20191010343Skin · corrodedFORWARD SHELL ASSEMBLY FOUND TO BE CORRODED - THREE PLACES: BOTH FORWARD CORNERS AND AT AN EXISTING INSERT. FORWARD SHELL ASSEMBLY WILL BE REPAIRED.SDR QMLA2019100741977Control Head · overheatedTHE RADIO CONTROL HEAD IN THE CREW COMPARTMENT BEGAN VERY RAPIDLY CYCLING SEARCH MODE WHILE DEVELOPING EXCESSIVE HEAT AND FUMES. THE HELICOPTER ABORTED THE REVENUE FLIGHT AND RETURNED TO BASE. MAINTENANCE REPLACED THE FAULTY RADIO CONTROL HEAD AND THE AIRCRAFTSDR HEER20190917266Skin · corrodedFORWARD SHELL ASSEMBLY WAS FOUND TO BE CORRODED (TWO PLACES AT EXISTING INSERTS). THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THE FAA-APPROVED REPAIR DATA.SDR EVCA2019091200000O-Ring · wornSTRONG FUEL SMELL NOTED DURING FLIGHT. UPON MAINTENANCE INSPECTION, FOUND FUEL FILLER CAP O-RING WORN, WHICH ALLOWED THE CAP TO LEAK FUEL.SDR M3XA2019090902Blower Motor · noisyPILOT MADE A PL FOR AN UNUSUAL NOISE IN THE CABIN AND NO PATIENT ON BOARD. MECHANIC INSPECTED AIRCRAFT AND FROM DESCRIPTION OF THE NOISE SUSPECTED AIR CONDITIONER BLOWER. PERFORMED RUN UP OF AIRCRAFT AND COUL NOT DUPLICATE NOISE. ACFT RETURNED TO SERVICE.SDR EVCA2019090900000Fuel Nozzle · corrodedDURING 300 HOUR MAINTENANCE, AMT NOTED CORROSION AND PITTING ON ENGINE FUEL NOZZLE TIP.SDR HEER20190830230Skin · corrodedFORWARD SHELL ASSEMBLY WAS FOUND TO BE CORRODED - OUTER SKIN AND OUTER CORNER SKIN. THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THE FAA-APPROVED REPAIR DATA.SDR HEER201908143161Skin · corrodedFORWARD ROOF SKIN WAS FOUND TO BE CORRODED - ONE PLACE, STATION 61.88, LBL 5.27. THE REPAIR DOCUMENTATION WILL BE SUBMITTED TO A STRUCTURAL FAA-DER FOR APPROVAL. THE FORWARD ROOF SKIN WILL THEN BE REPAIREDSDR 2020FA0000039Oil Cooler · unknownDURING A ROUTINE 150 HOUR INSPECTION IT WAS DISCOVERED THAT THE COMPOSITE PANEL BELOW THE OIL COOLER BLOWER, AS WELL AS AN AIRFRAME LONGERON AND STRINGER BELOW THE PANEL EXHIBITED STRUCTUAL CRACKING. THE DEFECT OCCURRED DURING UTILITY FIRE FIGHTING OPERATIONSSDR HDNA2019080154341Blade · erodedA SMALL HOLE WAS DISCOVERED AT THE OUTBOARD EDGE OF THE TIP CAP APPROX. ONE INCH ABOVE AND ONE INCH AFT OF BLADE TIE DOWN.SDR CA191210010Link · failed(CAN) DURING REGULAR 2500HRS INSPECTION. INSERT FAILED PROOF LOADING PREMATURELY (APPROX 100IN-LBS) (TC# 20191210010)SDR CA190719011Closeout Panel · damaged(CAN) EAGLE COPTERS IS CURRENTLY INVESTIGATING A CUSTOMER REPORTED MARKING THAT WAS OBSERVED ON THE MAIN ENGINE TO TRANSMISSION DRIVESHAFT (PN 407-340-310-101). IT APPEARS THE DRIVESHAFT BRIEFLY TOUCHED THE 0789-03-132 LOWER CLOSE OUT, PART OF THE AIRCRAFT ENGSDR HEER20190710093Skin · corrodedFORWARD SHELL ASSEMBLY OUTER SKIN WAS FOUND TO BE CORRODED -LOCAL TO AN EXISTING INSERT LOCATION. THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THE FAA-APPROVED REPAIR DATA.SDR CA190705010Resistor · discolored(CAN) EAGLE COPTERS IS CURRENTLY INVESTIGATING THE DISCOLORATION AND POSSIBLE OVERLOADING OF THE MANUAL MODE RESISTORS (P/N RS02B330R0FE70) THAT ARE PART OF THE 0789-17-003 4962-J196 HARNESS ASSEMBLY MANUFACTURED BY EAGLE COPTERS. CURRENTLY THE MANUAL MODE RESSDR EVCA201906250001Fitting · crackedCRACK IN UPPER R/H AFT VERTICAL TUNNEL FITTING AND SKIN.SDR QMLA2019062649056Filter · leakingPILOT LANDED AND COMPLAINED OF STRONG ODOR IN AIRCRAFT. FOUND BARRIER FILTER OIL POOLED IN INTAKE PLENUM. CLEANED POOOLED OIL AND RAN UP AIRCRAFT. FUNCTION CHECK GOOD AT THIS TIMESDR BHHR20190621002Adapter · contaminatedFADEC DEGRADED AND FADEC FAULT LIGHT ILLUMINATED IN-FLIGHT. DISCONNECTED FOST ADAPTER LOCATED IN ENGINE HARNESS AT (P3) AND VISUALLY INSPECTED FOR CORROSION. NO OBVIOUS DEFECTS WERE NOTED. WE CLEANED ALL THE CONTACTS OF HARNESS AT (P3). WE APPLIED ACF-50 TO SDR H44R2019061000009Float · malfunctionedDURING ACCOMPLISHMENT OF THE APICAL LIGHTWEIGHT EMERGENCY FLOAT KIT (STC# SR01450LA) 3 YEAR INSPECTION THE SYSTEM IS ACTUATED AND THE EMERGENCY FLOATS ARE DEPLOYED. IT REQUIRED 3 ATTEMPTS TO ACTUATE THE SYSTEM. WE WERE UNABLE TO DETERMINE IF IT WAS A RIGGING ISDR HEER20190520958Skin · corrodedFORWARD SHELL OUTER SKIN WAS FOUND TO BE CORRODED NEAR TWO EXISTING INSERTS AND AN OEM DOUBLER INSTALLATION.SDR CA190514011Skin · cracked(CAN) IT WAS REPORTED TO BELL: WE FOUND A CRACK IN OUR TAIL BOOM AT APPROX.F.S 120.75 ON THE L/H SIDE WHERE THE LOWER PLATE FOR THE HORIZONTAL PASSES THROUGH. (TC# 20190514011)SDR HEER20190507882Skin · puncturedFORWARD SHELL ASSEMBLY INNER SKIN WAS FOUND TO BE DAMAGED - PUNCTURED UNDER THE EXISTING RT PASSENGER DOOR STRUT INSTALLATION. THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THSDR CA190507001Bushing · cracked(CAN) IN BELL FACILITY: AIRCRAFT COMMERCIAL UNDER EXPERIMENTAL PERMIT: DURING CLEARANCE CHECK, WITH THE HYDRAULIC SYSTEM INSTALLED, WE STARTED ROTATION MOVEMENT OF CYCLIC AND UP/DOWN COLLECTIVE. WHILE COLLECTIVE DOWN, A CLUNK NOISE WAS DETECTED COMING FROM THESDR QMLA2019050519045Chip Detector · contaminatedAFTER MAIN GEARBOX TIME CHANGE. AIRCRAFT HAD CHIP LIGHT INDICATION AND DID A PRECAUTIONARY LANDING. PULLED, 3 EACH, CHIP DETECTORS PER MAINTENANCE MANUAL. INSPECTION REVEALED, 1 EACH, SMALL SLIVER PARTICLE. CLEANED AND PERFORMED GROUND RUN. AIRCRAFT RETURNED TSDR QMLA2019050319045Unknown · odorAFTER TAKE OFF, THE CREW AND PILOT NOTICED AN INEXPLICABLE HEAT RADIATING THROUGH THE AIRCRAFT ACCOMPANIED BY A SMELL OF BURNING PLASTIC. HEATER, AIR CONDITIONER AND DEMISTER WERE IN THE OFF POSITION. WE WERE ONLY A FEW MILES AWAY FROM BASE AND RETURNED TO BAS
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