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 ALGA2012012382412Grip · corrodedMAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.SDR ALGA2012012372412Grip · corrodedMAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.SDR ALGA2012012362412Grip · corrodedMAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.SDR ALGA2012012352412Pitch Horn · corrodedMAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.SDR ALGA2012012342412Pitch Horn · corrodedMAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.SDR ALGA2012012332412Pitch Horn · corrodedMAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.SDR ALGA2012012322412Pitch Horn · corrodedMAIN ROTOR HUB PITCH HORN HAS CORROSION BEYOND LIMITS.SDR CA120123007Bearing · failed(CAN) PILOT WAS ON DESCENT DURING HELI SKI OPERATIONS WHEN ENGINE CHIP LIGHT ILLUMINATED. PILOT TURNED ACFT AROUND AND RETURNED TO LODGE. FOUND METALLIC PARTICLES ON ENGINE FORWARD CHIP DETECTOR. PLUG WAS CLEANED AND GROUND RUN CARRIED OUT. NO CHIP LIGHT BSDR CA120120006Nut · worn(CAN) DURING O/H OF THE MAIN TRANSMISSION ASSY DUE TO A CHIP LIGHT IN THE COCKPIT, IT WAS FOUND THAT 3 OF THE NUTS, PN 204-040-131-001 RETAINING BEARING RACE, PN 204-040-130-005 HAD 0 FT/LBS OF TORQUE. THE OTHER 2 NUTS HAD TORQUES OF 25 FT/LBS. OEM TORQUE SPSDR ALGA2012012500022Skin · corrodedCORROSION FOUND ON BELLY SKIN DURING CORROSION INSPECTION. AREA FOUND TO BE OUT OF LIMITS.SDR ALGA2012011611712Tube · corrodedTUBE HAS CORROSION BEYOND REPAIRABLE LIMITS.SDR HEEA201201132925Bearing · spalledENGINE REMOVED DUE TO DEBRIS FOUND ON SCAVENGE FILTER. SPALLING FOUND ON OUTER RACE OF NR 5 BEARING AT SPLIT. REPLACED NR 5 BEARING WITH NEW.SDR ALGA1012421121Tube · corrodedREPLACED TUBE DUE TO CORROSION BEYOND LIMITS.SDR ALGA1311611212Rod End · wornROD END WORN BEYOND REPAIRABLE LIMITS.SDR ALGA7050110121Mount · crackedREAR MOUNT FOUND CRACKED AT BOLT HOLE AT 2:00 POSITION THROUGH VENT TUBE. SCRAPPED REAR MOUNT.SDR HEEA2012010832853Bearing · spalledTURBINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF NR 5 BEARING FOUND SPALLING ON OUTER RACE. REPLACED WITH NEW.SDR HEEA132849Skin · dentedFWD LOWER SKIN WAS FOUND DENTED/CRACKED. OPENSDR HEEA201201052848Skin · corrodedFORWARD ROOF SKIN FOUND CORRODED COMMON TO THE SERVO COWLING HINGE INSTALLATION. THE REPAIR DOCUMENTATION WILL BE SUBMITTED TO A STRUCTURAL FAA-DER FOR APPROVAL. THE FORWARD ROOF SKIN WILL THEN BE REPAIRED IAW THE FAA-APPROVED REPAIR DATA.SDR QMLA2012010412003Fuel Nozzle · separatedON COMPLETION OF A HOVERING AUTOROTATION IN THE COURSE OF A CHECKRIDE, PILOT’S HEARD A NOISE COMING FROM THE ENGINE DURING HOVER FLIGHT. ALL ENGINE INDICATIONS WERE NORMAL DURING HOVER, ACFT WAS TAXIED TO PARK. DURING HOVER TAXI MANEUVER, A LOUD POP WAS HEARSDR HEEA201201032909Bearing · spalledENGINE REMOVED DUE TO FOREIGN OBJECT DAMAGE. NR 5 BEARING EXHIBITED ROUGH ROTATION AND SPALLING OF OUTER RACE. INSTALLED NEW BEARING.SDR HEEA2011123032855Bearing · spalledENGINE WAS REMOVED DUE TO FLUCTUATING OIL PRESSURE. NR 5 BEARING EXHIBITED SPALLING AT OUTER RACE SPLIT. REPLACED WITH SERVICEABLE PART.SDR ALGAR5472122711Pitch Horn · corrodedPITCH HORN, CORRODED BEYOND LIMITS.SDR ALGAR5502122711Diffuser · damagedLOW POWER ON TEST CELL. PROBABLE LOW POWER DUE TO O/H VANE DIFFUSER, FWD PLATE SEPARATING FROM VANES.SDR HEEA2011122632795Fitting · crackedDURING 12 MONTH INSPECTION, CRACKS WERE FOUND AT RT AFT UPPER CORNER OF BROOM CLOSET, DURING DISASSEMBLY FOR REPAIR FITTING WAS FOUND COMPLETELY CRACKED THROUGH AT LOWER SUPPORT LEG OF FITTING. REPLACEMENT FITTING ORDERED AND REPAIR REQUEST SENT TO ACFT MFG FSDR CA111219004Bearing · loose(CAN) THE 2.5 BEARING CAGE NUTS WERE FOUND LOOSE AND 1 STUD STARTED TO BACK OUT. THE TORQUEMETER SUPPORT FLANGE, PN 6889191 IS RETAINED BY 4 NUTS. 2 OF THE NUT/STUDS ASSY WERE FOUND LOOSE. 1 NUT WAS LOOSE. ONLY 1 NUT WAS TIGHT. THE 1 NUT THAT WAS FOUND TSDR ALGAR201112080011Bearing · unstakedINBD BEARING UNSTAKED. ALL 4 FEATHER BEARINGS WERE NEVER ROLL STAKED. NEW YOKE FROM MFG WAS INSTALLED.SDR HEEA132858Engine · failedENGINE CHIP LIGHT ILLUMINATED, PILOT TURNED TO LAND AT NEAREST PLATFORM. ON APPROACH TO PLATFORM ENGINE STARTED MAKING A LOUD WHINING NOISE FOLLOWED BY LOUD POPPING NOISE AND AIRCRAFT YAWED. AUTO-ROTATED, DEPLOYED FLOATS AND LANDED IN WATER.SDR HEEA2011121132678Bearing · brokenPILOT REPORTED A CHIP LIGHT AFTER TAKEOFF. AS ACFT WAS TURNING A BASE LEG FOR LANDING AT EC278B. A LOUD WHINING NOISE WAS HEARD FOLLOWED BY A LOUD POPPING NOISE AND A YAW. COMPLETED A SUCCESSFUL WATER LANDING. TEARDOWN INSPECTION REVEALED 25 PERCENT OF NR SDR QMLA2011120111115Transmission · making metalTHE MECHANIC FOUND DURING A ROUTINE INSPECTION, A LARGE AMOUNT OF METAL ON THE TRANSMISSION CHIP DETECTOR. THE ACFT WAS PULLED FROM SERVICE. THERE HAVE BEEN MULTIPLE CHIP EVENTS FOR THIS TRANSMISSION LEADING UP TO THIS CURRENT EVENT. THIS ACFT IS CURRENTLSDR HEEA2011112813268Bearing · spalledIMPELLER BEARING NR 5 EXHIBITED SPALLING OUTER RACE. REPLACED WITH SERVICEABLE BEARING.SDR ZD4R20111201001Bearing Cage · looseDURING INSPECTION OF GEARBOX FOR METAL IN OIL, IT WAS NOTED THAT 5 OF THE 6 STUDS THAT SECURE THE 2.5 BEARING CAGE TO THE GEARBOX COVER ASSY HAD BACKED OUT ALLOWING MOVEMENT OF THE CAGE INSIDE THE GEARBOX. WHILE LOOSENING HARD WEAR THAT RETAINS THE BEARING CASDR CA111104007Ring · cracked(CAN) SWASHPLATE ASSY IN FOR A 2500 HR INSPECTION WHEN THE COMPONENT SHOP NOTICED 2 DISTINCT CRACKS ON THE INSIDE OF THE RING AS VIEWED FROM THE HOLES ON THE BOTTOM OF THE STATIONARY INNER RING.SDR CA111109009Metering Valve · inoperative(CAN) DURING FLIGHT, THE PILOT EXPERIENCED A RESTART FAULT CAUTION LIGHT. HE THEN RETURNED TO BASE, DURING SHUTDOWN A FADEC DEGRADED CAUTION LIGHT CAME ON. HE NOTIFIED MX STAFF. THE FADEC SYS INDICATED THERE WAS A PROBLEM IN THE HMU METERING VALVE WITH A FASDR QML2011102000003Frame · crackedDURING INSP OF THE TAILBOOM AND ATTACH POINT, CRACKING WAS NOTED IN THE UPPER STARBOARD ATTACH BOLT HOLE OF THE TAILBOOM ATTACH FRAME. PN 206-032-308-121, LOCATED AT STA 231.472. AXIAL STRESS EXERTED AT THIS LOCATION BY TAILBOOM FLEX, OVERTIME, CAUSES WEAKENSDR QML2011102000002Frame · crackedDURING INSP OF THE TAILBOOM AND ATTACH POINT, CRACKING WAS NOTED IN THE UPPER STARBOARD ATTACH BOLT HOLE OF THE TAILBOOM ATTACH FRAME, PN 206-032-308-121, LOCATED AT STA 231.472. AXIAL STRESS EXERTED AT THIS LOCATION BY TAILBOOM FLEX, OVERTIME, CAUSES WEAKENISDR QML201110201111Frame · crackedDURING INSP OF THE TAILBOOM AND ATTACH POINT, CRACKING WAS NOTED IN THE UPPER STARBOARD ATTACH BOLT HOLE OF THE TAILBOOM ATTACH FRAME. PN:206-032-308-121, LOCATED AT STA 231.472. AXIAL STRESS EXERTED AT THIS LOCATION BY TAILBOOM FLEX, OVERTIME, CAUSES WEAKENSDR ALGAR101811532471Seat Track · crackedFWD SEAT TRACK CRACKED.SDR CA111026003Bearing · debonded(CAN) WHILE CARRING OUT A DAILY CHECK, A LITTLE RUBBER AROUND THE SPINDLE OF THE SHEAR BEARING. FURTHER INVESTIGATION LEAD TO THE DEBONDING OF THE RUBBER COMPOUND TO THE CENTER SPINDLE.SDR CA111013007Blade · delaminatedWHILE DOING A 600 HR INSPECTION TAP TEST OF THE M/R BLADE, IT NOTICED THAT THERE WAS A DULL SOUND NEAR STATION 183 TO 185 ON THE UNDER SIDE OF THE BLADE. THE APPROXIMATE CHORD WISE LENGTH 2".SDR ALGAR101311A307Spline · corrodedSPLINES WORN AND PITTING CORROSION BEYOND LIMITS.SDR 2011F00208Skin · crackedWHILE PERFORMING MX, A CRACK WAS DISCOVERED IN THE OUTER SKIN OF THE TAILBOOM ON THE LT SIDE AT THE FORWARD ROW OF RIVETS THAT SECURED THE TAIL ROTOR GEARBOX HOUSING. THE CRACK APPEARS TO HAVE STARTED AT ONE OF THE RIVETS, EXTENDED TO ANOTHER AND WAS CONTINUSDR 2011FA0000653Bearing · failedWHILE IN CRUISE FLIGHT, ENGINE CHIP LIGHT ILLUMINATED, PILOT LANDED IN FIELD. INSP OF BOTH ENGINE CHIP DETECTORS REVEALED MULTIPLE CHIPS. THE SOURCE OF THE METAL WAS DUE TO FAILURE OF THE PTO BEARING, PN (M250-10121) THE ENGINE GEARBOX IS AN "ON CONDITION" ISDR HEEA2011927132675Bearing · spalledENGINE REMOVED DUE TO METAL IN OIL. NR 5 BEARING EXHIBITED SPALLING AT OUTER RACE SPLIT.SDR CA110929013Blade · cracked(CAN) THE ENGINEER WAS TRYING TO TRACK AND BALANCE THE MAIN ROTOR AFTER DOING MANY RUNS AND IT WAS NOTICED THAT THERE WAS A CRACK ON THE TAB.)SDR ALGAR919115682Crosstube · corrodedCROSS TUBE CORRDED BEYOND LIMITS IAW AA00061 PAGE 19, FIG 2, TABLE 8.SDR IAVA201109140001Structure · crackedPILOT REPORTED THAT THERE WAS A VIBRATION IN THE ACFT. INVESTIGATION FOUND THE RIVETS WORKING AT TAILBOOM TO TAIL ROTOR GEARBOX CASTING MOUNT. FURTHER INVESTIGATION FOUND A CRACK IN THE TAIL BOOM AT THE 11:00 POSITION, APPROX 1.5 INCHES LONG AT THE ROW OF RISDR CA110916008Bearing · delaminated(CAN) THE ENGINEER WAS TROUBLESHOOTING A MAIN ROTOR VIBRATION WHEN IT WAS DISCOVERED VISUALLY, A DELAMINATION OF THE RUBBER COMPOUND OF THE SHEAR BEARING, S/N LK14771, TO SPINDLE.SDR ALGAR911153264Skid · corrodedSKID TUBE CORRODED BEYOND MANUFACTURER'S LIMITS.SDR HEEA132169Bearing · spalledENGINE WAS REMOVED DUE TO N2 LOCKUP. NR 5 BEARING REVEALED SPALLING IN SEAM OF OUTER RACE. REPLACED NR 5 BEARING.SDR ALGAR8291153069Longeron · crackedDURING 50 HR, LT UPPER AFT LONGERON CRACKED AT STA 204.92. INSPECTED AND REPLACED LT UPPER AFT LONGERON PN 206-031-314-237, C/W ASB 407-11-95 PART III, INSTALLATION OF 3 EXTERNAL STRAP DOUBLERS, PART V, TERMINATING ACTION TO RECURRING INSPECTION.
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