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 = '369D' 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 = '369D' 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 CA120123005Blade · debonded(CAN) DURING ROUTINE INSPECTION THE MAIN BLADE WAS FOUND DEBONDED BY TAP TEST ON THE BOTTOM SIDE ROOT END DOUBLER. THE MFG WAS CONTACTED AND THIS BLADE CAN BE RETURNED FOR REPAIR.SDR CA111201007Bracket · broken(CAN) BRACKET ASSY CAP WHICH IS A MATCHING PART WAS INSTALLED WITHOUT THE NECESSARY SHIMMING IN PLACE. SO INCORRECT ASSY AND THE POSSIBILITY OF THE COLLECTIVE POLE BEING SNAPPED UP WITH NO BLADES INSTALLED OVER ITS LIFE MAY HAVE LED TO THE BREAKING OF THE BEASDR 2011FA0000784Shaft · seizedGOVERNOR SHAFT SEIZED. OVERHAUL TEARDOWN REVEALED MOST INTERNAL PARTS WORN EXCESSIVELY.SDR CA110923008Gear · broken(CAN) ACFT MAIN ROTOR TRANSMISSION LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT & PILOT PERFORMED AN UNSCHEDULED LANDING. UPON INSPECTION BY A MECHANIC METAL WAS FOUND ON THE M/R TRANSMISSION CHIP PLUGS. CHIP LIGHT DID NOT ILLUMINATE. TRANSMISSION, PN 369D2SDR CA110913002Warning Light · illuminated(CAN) ENGINE CHIP LIGHTS DURING FLIGHT. ACFT LANDED, CHIP PLUGS WERE CLEANED, THE FLIGHT WAS RESUMED, CHIP LIGHTS REOCCURRED, THE ACFT LANDED. THE ACFT WAS RECOVERED BY TRUCK BACK TO THE MAIN MX FACILITY WHERE IT WAITS FOR INVESTIGATION AS TO CAUSE.SDR 2011FA0000554Combustion Case · crackedOUTER COMBUSTION CASE CRACKED IN RT ARMPIT AREA ALONG SPLITLINE WELD. THIS AREA HAD THE BRAZED REINFORCEMENT.SDR CA110810011Bearing · spalledM/R TRANSMISSION CHIP LIGHT ILLUMINATED DURING FLIGHT. EVIDENCE OF METAL FOUND ON CHIP PLUGS. DURING TRANSMISSION DISASSEMBLY, REASON FOR METAL GENERATION WAS FOUND TO BE T/R O/P PINION ROLLER BEARING INNER RACE WHICH WAS CRACKED AND BADLY SPALLED.SDR CA110620011Shaft · shearedPILOT WAS IN A HOVER, NOTICED THAT THE NR/N2 RPM HAD INCREASED BY 3 PERCENT, BEEPED RPM DOWN AND CONTINUED HOVERING OPERATION AND THE RPM INCREASED AGAIN. ELECTED TO LAND AND UPON LANDING THE ENGINE STARTED TO OVERSPEED SO THE PILOT ROLLED THROTTLE OFF IMMEDSDR CA110516022Engine · power loss(CAN) TORQUE FLUCTUATIONS/IFSD DURING FLIGHT AT 1000 FT ALTITUDE THE ENGINE PARAMETER INDICATIONS BEGAN TO FLUCTUATE. THE PILOT TRIED MANUAL MODE AND THE BEEP SWITCH TO NO AVAIL. AFTER A FEW SECONDS THE CAS MESSAGE "ELECTRONIC ENGINE CONTROL FAIL" APPEARED. SDR CA110427017Strut · crackedWHILE PERFORMING THE 12 MONTH INSPECTION, A CRACK WAS NOTED IN THE LT REAR STRUT. THIS CRACK WAS 7" LONG RUNNING ROUGHLY MIDPOINT AND UP UNDER THE STEP. THE CRACK DID NOT START OR END AT ANY BOLT HOLES. THE CRACK WAS PERPENDICULAR TO THE BOLT HOLES AND RAN PASDR CA110106008Clamp · wornFOR STC SR01062LA, IT WAS DISCOVERED DURING INSPECTION THAT THERE THE HEAD OF THE TEE BOLT RESTS IN THE BAND CLAMP HAD WORN THROUGH TO THE POINT THAT THE TEE BOLT COULD BECOME DISENGAGED RESULTING POTENTIALLY IN EXHAUST CLAMP PARTS DEPARTING THE AIRCRAFT INTO SDR CA101214007Bracket · broken(CAN) THE BEARING CAP THAT IS ATTACHED TO BRACKET ASSEMBLY WAS FOUND BROKEN AT ATTACHMENT POINT OF BEARING CAP. REMOVED FROM SERVICE (TC# 20101214007)SDR CA101105006Swashplate · sheared(CAN) INSPECTION FOUND DRIVE SPLINES SHEARED OFF. HELICOPTER HAS NO HISTORY OF TAIL ROTOR STRIKE. INVESTIGATION INCLUDING ENGINEERING FAILURE ANALYSIS OF PART. OPERATORS FLEET INFORMED AND INSPECTED FOR SIMILAR PROBLEM. WILL FORWARD RESULTS.SDR CA100916006Strut · crackedAFTER CHANGING A LANDING GEAR DAMPER FOR LOW PRESSURE, THE ACFT WAS PLACED BACK ON THE GROUND. AFTER IT WAS SITTING ON THE GROUND THE SAME ACFT ORIENTATION PRIOR TO CHANGING THE DAMPER WAS NOTED, TAIL LOW AND LEANING TOWARD THE LT. UPON INSP OF THE LANDING GSDR HXF2010F00000Skid · crackedDURING A 100 HR INSP, A CRACK WAS FOUND ON THE RT FWD LANDING GEAR FOOT. THE CRACK LOOKS TO HAVE ORIGINATED AT THE LOWER END, OTBD SIDE AT THE TOP OF THE BOSS AREA JUST ABOVE THE SKID TUBE MOUNT HOLES. THE CRACK EXTENDS UP ABUT 1" AND SPIDERS FWD AND AFT. TSDR CA100527004Pin · worn(CAN) BLADE PIN FOUND TO BE CRACKED BY PILOT ON A VISUAL INSPECTION. IT IS AN EXPANDABLE PIN WITH A NUT TO ADJUST TENSION. PIN FOUND TO BE CRACKED AT THE END OF THE THREADS, PIN HAD 779.4 HOURS REMAINING ON IT.SDR CA100520002Longeron · crackedUPPER LONGERON, PN 369D23072-3, CRACKED 2.5 AFT OF STA 131.0 BULKHEAD, CRACK ORIGINATED FROM A FASTENER HOLE AND ENDED AT THE EDGE OF THE HORIZ LEG OF THE EXTRUSION.SDR 2010FA0000401Collective Stick · crackedFOUND A CRACK IN THE PILOT'S COLLECTIVE STICK. THE CRACK RADIATES.SDR 2009FA0000509Turbine · seizedDURING EXTERNAL LOAD OPERATIONS AT A HOVER, THE ENGINE STOPPED SUDDENLY CAUSING THE PILOT TO AUTO ROTATE FROM APPROX 80 FEET AGL. THE PROBABLE CAUSE OF THE ENGINE STOPPAGE IS A MALFUNCTION IN THE TURBINE MODULE. RECENT OCCURRENCE, NO PRELIMINARY REPORT PUBLISDR CA090402007Bearing · seized(CAN) NEW PMA ROD END FOR M/R PITCH LINK WAS INSTALLED AND BEARING WAS VERY TIGHT. AFTER 2.1 HRS OF OPERATION THE SWAGE LOST IT EFFECTIVENESS AND THE OUTER RACE OF THE BEARING STARTED TO ROTATE IN THE ROD END. THE ACFT WAS UNDERGOING TRACKING AND BALANCING WHESDR CA090313009Blades · broken(CAN) ENGINE EXPERIENCED A COMPRESSOR STALL IN CRUISE. PILOT RETURNED TO BASE, AS THE ENGINE WAS LOADED UP FOR LANDING 2 MORE COMPRESSOR STALLS OCCURRED. ACFT WAS LANDED AND SHUTDOWN WITHOUT FURTHER INCIDENT. COMPRESSOR WAS SENT TO REPAIR SHOP WHERE IT WAS NOTSDR CA090115008Sprag Assy · unserviceableSPRAG ASSY FAILED 300 HR INSPECTION DUE TO 2 BROKEN CORNERS OF 2 DIFFERENT TEETH (SPRAGS). NO OTHER DAMAGE WAS FOUND TO THE ASSEMBLY AS A RESULT OF THIS INCIDENT. CLUTCH ASSY WAS WORKING FINE PRIOR TO INSPECTION. NEW SPRAG ASSY INSTALLED AND CLUTCH RETURNEDSDR CA090112011Bellcrank · crackedA CRACK WAS FOUND ON THIS FLIGHT CONTROL BELLCRANK DURING ANNUAL INSPECTION.SDR 2008FA0000902Tube · unserviceableTHIS DEFECT WAS DETECTED DURING TROUBLESHOOTING FOR AN ENGINE PWR PROBLEM. THIS FLEX TYPE TUBE ASSY WAS INSTALLED IN CONJUCTION WITH AN STC FROM ENG PWR PROBLEM. THIS FLEX TYPE TUBE ASSY WAS INSTALLED IN CONJUNCTION WITH AN STC, PC SAFETY VALVE KIT SE5511NM.SDR 2009FA0000508Turbine · seizedDURING EXTERNAL LOAD OPERATIONS AT A HOVER, THE ENGINE STOPPED SUDDENLY CAUSING THE PILOT TO AUTOROTATE FROM APPROXIMATELY 120-150 FEET AGL. THE PROBABLE CAUSE OF THE ENGINE STOPPAGE WAS A MALFUNCTION IN THE TURBINE MODULE. NO FINAL REPORT HAS BEEN PUBLISHEDSDR CA081021005Governor · malfunctioned(CAN) PILOT REPORTED ROTOR SPEED HUNTING IN CRUISE SO THE GOVERNOR WAS REMOVED TO CLEAN THE ORIFICES. ONCE REMOVED IT WAS NOTICED THAT THE EPOXY BOND ON THE END OF THE DRIVESHAFT WAS MISSING AND THE SPLINE DRIVE WAS LOOSE ON THE GOVERNOR DRIVESHAFT. IF LEFT THSDR WVX2008F00000Turbine · destroyedAIRCRAFT WAS IN A 70 FOOT HOVER AND HAD JUST PLACED A SLING LOAD ON THE GROUND WHEN A LOUD BANG OCCURRED THE LOUD BANG WAS THE TURBINE EXPLODING. AT THIS TIME, THE PILOT LOWERED THE COLLECTIVE AND ENTERED AN AUTO ROTATION. AIRCRAFT TOUCHED DOWN IN A LEVEL ATTISDR CA080610002Starflex · wornM/R SWASHPLATE RECEIVED FOR O/H. AFTER DISASSEMBLY AND PAINT STRIPPING ROTATING STAR PN 369D27611-503 WAS FOUND WITH FORK INNER EAR SURFACE WEAR BEYOND LIMITS. THIS WEAR WAS FOUND FILLED WITH SOME SORT OF ADHESIVE ONCE THE ADHESIVE WAS REMOVED THE WEAR WAS BSDR CA080121008Sprag Clutch · corroded(CAN) DURING 300 HOUR INSPECTION PART WAS FOUND TO HAVE PITTING ON SEVERAL ELEMENTS. SPRAG CLUTCH REPLACED. (TC NR 20080121008)SDR CA071227007Cap · cracked(CAN) DURING ROUTINE INSPECTION AND FILTER CHANGE, A CRACK AROUND THE EAR OF THE CAP WAS NOTED. THE STUD WAS ALSO STRIPPED. MFG COVERED THIS TOPIC IN THEIR CSL-1251. TORQUEING IS THE POSSIBLE CAUSE FOR THIS DEFECT, THE LETTER RECOMMENDS 30-40 LBS-IN. IT IS IMPSDR CA071210005Housing · cracked(CAN) CLUTCH HOUSING RECEIVED FOR OVERHAUL AFTER PAINT STRIPPING HOUSING SENT OUT FOR NDT INSPECTION AND CAME BACK FOUND CRACKED ON ENGINE SIDE OF HOUSING. (TC NR 20071210005)SDR CA071112002Bracket · broken(CAN) RUDDER PEDALS WERE FOUND TO BE LOOSE IN MOUNTS ON FURTHER INVESTIGATION IT WAS FOUND THE BRACKET THAT THE RUDDER PEDALS MOUNT IN WAS BROKEN ON (3) OF THE (4) MOUNTING BOLT EARS. (TC NR 20071112002)SDR CA071015004Spline · failed(CAN) PILOT COMPLAINED OF EXCESSIVE (ROTOR) DROOPING. CHECKED AIRCRAFT RIGGING AND LOOSE ENGINE AIR LINES. REMOVED GOVERNOR FOR BLEED CLEANING AND THE DRIVE ASSY ON THE GOVERNOR WAS COMPLETELY DISCONNECTED FROM THE PT GOVERNOR. COMPONENT WAS SHIPPED FOR FURTHESDR CA070928004Belt · worn(CAN) ON LANDING, THE PILOT FELT A STRANGE VIBRATION. AFTER LANDING, THE AC WAS GROUNDED PENDING MAINTENANCE TROUBLESHOOTING. A CLOSE INSP WAS COMPLETED AND DETERMINED TO BE A LOOSE COOLER BELT CAUSING EXCESSIVE VIBRATION AT 100 PERCENT. THE BELT WAS REPLACESDR CA070924002Drive Gear · broken(CAN) MAIN ROTOR TRANSMISSION REMOVED DUE TO CHIP LIGHT ILLUMINATION. TRANSMISSION RETURNED TO HELICOPTERS COMPONENT OVERHAUL SHOP FOR REPAIR. UPON DISMANTLE IT WAS DISCOVERED THAT THE I/P GEAR HAD FAILED AND EXHIBITED ONE COMPLETE TOOTH BROKEN OFF FROM THE GESDR CA070927007Stator Vane · failed(CAN) NR 6 STATOR VANE FAILURE (1 VANE ONLY). NO EROSION TO NEIGHBORING VANES OR PLASTIC COATING. FOUND BY HELICOPTER OPERATOR. (TC NR 20070927007)SDR CA070928001Stator Vane · failed(CAN) PILOT REPORTS UNUSUAL NOISE COMING FROM AIRCRAFT DURING GROUND RUN. AIRCRAFT IS GROUNDED UNTIL ENGINEER INVESTIGATES THE UNUSUAL NOISE. NOISE IS DESCRIBED AS A (KNOCKING NOISE COMING FROM THE ENGINE) AND TOT HOTTER THAN USUAL. DURING THE GROUND RUN THE SDR 2007FA0000829Control System · roughDURING 100 HR INSPECTION, PLAY WAS NOTICED BETWEEN THE ROTATING AND NOT-ROTATING SWASH PLATES OF THE TAIL ROTOR PITCH CONTROL AFTER REMOVAL, IT WAS NOTED THAT THE BEARING WAS DRY AND ROUGH. RECORDS INDICATE IT WAS REGREASED IN DEC OF 2006. (K)SDR CA070508003Pin · bent(CAN) DURING AN INSPECTION THE ENGINEER NOTICED THE THE M/R BLADE FOLDING PIN LOOKED BENT. UPON TAKING THE UNIT APART HE NOTICED THAT THE THREADS OF THE PIN WERE NOT ON THE PIN STRAIGHT, KIND OF LOPSIDED. (TC NR 20070508003)SDR 2007FA0000400Bearing · failedDURING FLIGHT THE UPPER CHIP PULL ILLUMINATED, IT WAS CLEANED IAW MM AND RETURNED TO SERVICE. A COUPLE OF HOURS LATER, A SECOND LIGHT ILLUMINATED. FOUND LOTS OF FINE CHIPS. REPLACED ENGINE. FOUND NR 1 BEARING BAD. (K)SDR 2009FA0000507Spring · defectiveDURING LEVEL FORWARD FLIGHT, A SPRING INSIDE THE PT GOVERNOR FAILED, CAUSING THE ENGINE TO GO TO IDLE. AN AUTOROTATION WAS REQUIRED AND WAS DONE SO INTO A SOFT PLOWED FIELD. THE HELICOPTER TURNED OVER AFTER SKIDDING A SHORT DISTANCE.SDR PHA2007F00000Support · crackedAFTER A REFUELING STOP ON A PART 91 FLIGHT, THE PILOT PLACED HIS FEET ON THE TAIL ROTOR PEDALS AND FELT THEM MOVE. HIS INSPECTION REVEALED THAT 3 OF THE 4 MOUNT LOCATIONS FOR THE LT TAIL ROTOR PEDAL SUPPORT WERE BROKEN OFF OF THE SUPPORT. THE UPPER LT, LOWERSDR 2007FA0000390Bracket · damagedDURING A PREFLIGHT, THE PILOT NOTICED THE GOVENOR BELCRANK HAD SOME SLOP SUBSEQUENT INSPECTION DISCLOSED THAT THE BELCRANK PIVOT BOLT WAS MOVING IN THE BRACKET BECAUSE THE HOLE WAS ELONGATED, REPLACED BRACKET. (K)SDR 2007FA0000330Combustion Case · crackedPILOT NOTICED CRACK IN COMBUSTION CAN ON PREFLIGHT CHECK REPLACED UNIT. (K)SDR 2007FA0000321Exciter · inoperativePILOT WENT TO START THE AIRCRAFT AND THERE WAS NO IGNITION. FOUND IGNITION EXCITER INOPERATIVE, REPLACED. (K)SDR 2007FA0000285Governor · frozenDURING AN INSPECTION IT WAS NOTED THAT THE BEAING RETAINING WASHER FOR THE ROD END WAS INCORRECT. AFTER THE BOLT WAS REMOVED IT WAS THEN DISCOVERED THAT THE THROTTLE ARM WAS SEIZED UP ON THE GOVERNOR, REPLACED GOVERNOR. (K)SDR CA070309003Blade · cracked(CAN) PILOT FELT A VIBRATION AND UPON LANDING CHECKED MAIN ROTOR BLADES. A CRACK APPROXIMATELY 18 INCHES FROM THE ROOT, RUNNING PERPENDICULAR TO THE TRAILING EDGE WAS DISCOVERED. IT APPEARS AS IF THE BLADE DEBONDED AT A RIB, AS THE CRACK FOLLOWS STRAIGHT FROM SDR CA070118006Blade · cracked(CAN) THE UPPER BLADE SURFACE IS CRACKED CHORDWISE FROM LEADING EDGE TO TRAILING EDGE BETWEEN BLADE STATION 120 AND 124. THE LOWER BLADE SURFACE IS ALSO CRACKED IN THE MID CORD AREA BETWEEN STATION 120 AND 124 BUT DOES NOT EXTENT TO THE LEADING EDGE OR TRAILINSDR EOO2006F00001Snap Ring · damagedREMOVED COMPRESSOR FOR INSPECTION, FOUND DAMAGED SNAP RING GROOVE IN IMPELLER SPUR GEAR ADAPTOR SHAFT. SENT UNIT OUT FOR REPAIRS. (K)SDR 2006FA0001087Shaft · spalledFOUND SPALLING ON BEARING RACE AT 2.5 BEARING CONTACT POINT. FOUND VISIBLE LINE ON 2.5 BEARING ROLLERS MATCCHING SPALL LINE ON SAG SHAFT. COMPRESSOR ASSY INSTALLED ON AC 6/SEPT/2006, TIME IN SERVICE SINCE INSTALLATION OF COMPRESSOR ASSY 105.1 HOURS, 220 CYCL
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