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 = '206L4' 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 = '206L4' 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 HEEA131128Web · corrodedBAGGAGE COMPARTMENT WEB FOUND TO BE CORRODED. REPAIRED IAW FAA APPROVED DATA.SDR HEEA131085Frame · chafedDURING SCHEDULED MAIN BASE VISIT, PART WAS FOUND TO BE CHAFED.SDR RMXA20110505001Chip Detector · false activationTRASMISSION CHIP LIGHT ILLUMINATED DURING FLIGHT. TECH CHECKED AND CLEANED TRANSMISSION CHIP PLUG. DRAINED AND SERVICED TRANSMISSION OIL AND CHANGED FILTER. PERFORMED 1 HOUR GROUND RUN. DRAINED OIL AND FOUND NO METAL PARTICALS. SERVICED OIL AND GROUND RUN. ACSDR CA110413015Hose · unknown(CAN) PILOT NOTICED THAT WHEN THE FUEL BOOST PUMP CIRCUIT BREAKERS WERE PULLED DURING PREFLIGHT CHECK, THE CAUTION PANEL INDICATION WAS REVERSED, LT BOOST PUMP C/B PULLED, RT CAUTION LIGHT ILLUMINATION & RT BOOST PUMP C/B PULLED, LT CAUTION LIGHT ILLUMINATIONSDR CA110324008Output Seal · leaking(CAN) ON 100HR INSPECTION, FOUND OIL LEAK IN TAIL ROTOR GEARBOX FAIRINGS. AFTER REMOVING OUTPUT SEAL HOUSING, FOUND THE SPRING OF THE SEAL ON THE WEAR SLEEVE, AND WEAR SLEEVE WORN OVER 50 PERCENT THRU. AFTER CALLING REPS AND OTHER COMPANYS WE FOUND THAT THISSDR ALGA031211278ALNut · crackedDURING ROUTINE INSP, MX FOUND 2 NUTS PN MS21042L4 CRACKED. THE NUTS WERE A PART OF THE HARDWARE STACKUP ATTACHING THE TAILROTOR DRIVESHAFT FLEX COUPLINGS TO THE DRIVESHAFT. THE NUTS HAD A VENDOR STAMP MARK RESEMBLING AN "A" OR A "V" TURNED SIDEWAYS ON ONE OFSDR ALGA030211276ALScroll · crackedON DAILY SERVICE CHECK, MX FOUND ENGINE COMPRESSOR SCROLL CRACKED. R & R ENGINE ASSY.SDR ALGAR2241151374Attach Fitting · crackedUPPER LEFT HAND INTERCOSTAL FITTING CRACKED ON FWD. LEFT HAND SIDE OF FITTING.SDR RMXA20110220001Gearbox · failedWHILE IN FLIGHT, PILOT NOTICED SUDDEN VIBRATION IN TAIL ROTOR PEDALS AND CYCLIC. LANDED THE AIRCRAFT AND CALLED TECHNICIAN. TECHNICIAN CHECKED THE TAIL ROTOR AND SURROUNDING AREA. CHECKED TAIL ROTOR GEAR BOX FOR SECURITY AND ALSO THE TAIL ROTOR CHIP DETECTOR ASDR ALGA020211278ALDrive Shaft · shearedIN FLIGHT, ACFT LOST HYDRAULIC POWER. PILOT RETURNED TO BASE. MX FOUND MAIN ROTOR TACH GENERATOR DRIVESHAFT SHEARED.SDR ALGAR1281151434Hanger Assy · mismanufactured3EA HANGER SUPPORTS PN 206-033-412-123S, RADIUS OUTER EDGES RECEIVED NEW FROM MFG DEFORMED AND WILL NOT FIT IN FIXTURE.SDR CA101220011Fuel Cell · leaking(CAN) . ACFT PARKED STATIC INSIDE HANGER. FUEL LEAKS THROUGH FUEL CELL MATERIAL. REPLACED.SDR ALGA12151052057Box Beam · crackedBOX BEAM ASSY WAS FOUND CRACKED AT TIME OF REFURB INSP. DAMAGE FOUND WHERE CTR POST AND BEAM ASSY CONNECT.SDR CA101220010Nut · seized(CAN) UNABLE TO RELEASE THE NUT THAT RETAINED THE BEARING HOUSING TO THE MAST POLE, EXCESSIVE FORCE APPLIED, 2000 FT/LBS.SDR CA101220009Nut · seized(CAN) UNABLE TO RELEASE THE NUT THAT RETAIN THE BEARING HOUSING ON THE MAST POLE AFTER EXCESSIVE FORCE WAS APPLIED, 2000 FT/LBS. A PREVIOUS INCIDENT WAS HANDLE BY MFG ON SN 52351 AND BOTH ASSY WERE RETURNED TO LAB FOR INVESTIGATION.SDR CA101202014Disc Pack · crackedUPON INSP OF THE TAIL ROTOR DRIVESHAFT COUPLINGS, 1 DISK IN THE COUPLING DISK PACK, 2ND FROM THE FRONT, WAS FOUND TO HAVE CRACKED. CRACK DISCOVERED AT AFT 2094.4. DISK PACK CHANGED OUT.SDR HEEA129746Bearing · spalledENGINE REMOVED FOR TURBINE O/H. NR5 BEARING EXHIBITED SPALLING ON OUTER RACE AT SPLIT LINE AREA. SCRAPPED PART AND REPLACED WITH NEW.SDR ALGA10182010192ALEngine · unknownIN HOVER, PILOT HEARD "TWO BIG POPS IN THE ENGINE". INSTRUMENTS INDICATED NO PROBLEMS. NO YAW WAS NOTICED. MX REPLACED ENGINE ASSY ALONG WITH ENGINE FUEL SYSTEM. ENGINE QUARANTINED AWAITING TEST CELL RUN AT TIME OF THIS REPORT.SDR YTRA10265Sprayer · crackedDURING DEPARTURE FROM OFFSHORE PLATFORM PILOT EXPERIENCED A NOISE IN THE ENGINE COMPARTMENT WITH A CORRESPONDING LOSS IN ENGINE POWER. PROCEEDED TO MAKE A PRECAUTIONARY LANDING TO THE WATER.SDR YTRA10258Diffuser · separatedIN CRUISE FLIGHT THE PILOT DESCRIBED A LOUD BANG WHICH COINCIDED WITH A RISE IN TOT AND A DEGRADATION OF ROTOR RPM. THE PILOT MADE A PRECAUTIONARY LANDING IN THE WATER.SDR YTRA1020302Attach Fitting · crackedDURING ROUTINE INSP FOUND UPPER LT TAILBOOM ATTACH FITTING CRACKED. REMOVED CRACKED TAILBOOM ATTACH FITTING AND INSTALLED NEW FITTING.SDR YTRA1019601Bolt · missingTHE PILOT WAS UNABLE TO MAKE ANY COLLECTIVE CONTROL SYS INPUTS. ON INSP IT WAS DISCOVERED THAT BOLT PN 20-057-5-20D HAD BECOME DISCONNECTED FROM LINK ASSY PN 206-001-558-103 AND SWASHPLATE LEVER ASSY PN 206-010-447-109.SDR YTRA1020301Attach Fitting · crackedDURING ROUTINE INSP, FOUND UPPER LT TAILBOOM ATTACH FITTING CRACKED. REMOVED CRACKED TAILBOOM ATTACH FITTING AND INSTALLED NEW FITTING.SDR CA100610004Bearing · spalledDURING FINAL APPROACH TO AIRPORT FREEWHEEL CHIP LIGHT ILLUMINATED. FUTHER INVESTIGATION REVEALED OIL SYS METAL CONTAMINATION. FWD DUPLEX BEARING IN FREEWHEEL ASSY FOUND MAKING METAL FREEWHEEL ASSY REMOVED FROM SERVICE AND FREEWHEEL REPLACED NEW. OIL SYS FLUSSDR EVCA1821Bearing · flakingINTERMITTENT TRANSMISSION CHIP LIGHT IN FLIGHT, DISASSEMBLED TRANSMISSION AND FOUND SEVERAL PLANETARY ROLLER BEARINGS FLAKING AND PITTING.SDR PBV2010F00000Engine · power lossENGINE LOSS POWER DURING HOVER TO PAD AND LANDED SHORT IN GRASS. ACFT SHUTDOWN. AFTER STOPPED, FUEL SYS WAS CKD, OK. ACFT START AND HOVERED TO PAD. FUEL ONT SYS REMOVED AND SENT TO MFG . NO DEFECTS FOUND. A/F FUEL SYS INS, ACCORDING TO BHT-206L-4-MM-1, ESDR ALGA39105908Blade · debondedFOUND MAIN ROTOR BLADE LOWER SURFACE NR 1 GRIP FINGER DOUBLER CORRODED AND DEBONDED APPROX 2.25".SDR ALGA39106254Blade · debondedFOUND MAIN ROTOR BLADE UPPER SURFACE NR 4 GRIP FINGER DOUBLER CORRODED AND DEBONDED APPROX 3.5".SDR ALGA391098605Fireshield · mismanufacturedCOULD NOT FIT VERTICAL FIRE SHIELD ON ENGINE GEARBOX DUE TO ALL FIRE SHIELD MOUNTING PADS WELDED OFF CENTER FROM SHEET METAL.SDR ALGA0111105694Mount · crackedFWD FLANGE ON COMPRESSOR REAR MOUNT CRACKED.SDR YTRA1000701Fitting · crackedCRACKED UPPER LT FWD FITTING ON TAILBOOM ASSY.SDR 2009FA0001038Support Fitting · crackedDURING INSPECTION OF ACFT, IDENTIFIED A CRACK IN THE TAIL ROTOR GEAR BOX SUPPORT FITTING PN 206-033-426-001 AT APPROX THE 7 O'CLOCK POSITION. SHIP IS FITTED WITH A HIGH ALTITUDE TAIL ROTOR KIT.SDR ALGA111309895436Fireshield · mismanufacturedCOULD NOT FIT VERTICAL FIRESHIELD ON ENG GEARBOX. ALL FIRESHIELD MOUNT PADS WELDED OFF CENTER.SDR CA091109001Nut · cracked(CAN) DURING REMOVAL OF T/R PITCH CHANGE CROSS HEAD NUT, THE NUT WAS FOUND TO BE CRACKED IN 2 OF THE RELIEF SLOTS. THE NUT WAS COMPLETELY SEPARATED AFTER REMOVAL. NUT WAS DISCARDED AND REPLACED WITH NEW.SDR ALGA10150990546Combustion Liner · mismanufacturedENGINE FLAME OUT ON TEST CELL ON NUMEROUS RUNS. SOLVED FLAME OUT PROBLEM BY REPLACING LINER.SDR ALGA145920990242Fireshield · misalignedUNABLE TO FIT FIRESHIELD TO GEARBOX, 6 PADS OFF CENTER TO GEARBOX.SDR HEEA125620Fuel Control · malfunctionedLOWERED THE COLLECTIVE TO SLOW DOWN, DESCEND AND TURN INTO THE WIND FOR LANDING. WHEN INCREASED THE COLLECTIVE TO SLOW DESCENT, THE LOW ROTOR HORN SOUNDED. LOWERED COLLECTIVE ESTABLISHED 60 KNOTS, CHECKED ALL GAUGES AND THROTTLE AND ALL WAS GOOD. MADE RADIOSDR CA090923004Line · chafed(CAN) BHTCL WAS MADE AWARE SHIP 52394 HAD A HYDRAULIC FAILURE, IN FLIGHT, ON APPROACH TO HELIPAD. THE REPORT STATES THE HYDRAULIC FLEX LINE P/N 70-061H000T134A SHOWED DAMAGE BY CHAFING. THE CHAFING APPEARED TO BE FROM CONTACT WITH AN ADJACENT FLEX LINE`S "B" NSDR ALGR051609N69ALUnknown · smoke30 SECONDS INTO START SEQUENCE, PILOT REPORTED COCKPIT BEGAN TO FILL WITH SMOKE. APPEARED TO BE COMING FROM CO-PILOT FOOT AREA. MX INSPECTED UNDER CO-PILOT SEAT, RADIO RACK, AND BEHIND AND UNDER INSTRUMENT PANEL. NO SMOKE SMELL, BURNED WIRES, OR DISCREPANCIES SDR ALGRN269AL022609Indicator · inoperativePILOT REPORTED A BURNING SMELL IN CRUISE FLIGHT. MX FOUND ATTITUDE INDICATOR INOP. MEL'D ATTITUDE INDICATOR. NO FURTHER WIRING DEFECTS NOTED. OPS CHECK FLIGHT PERFORMED WITH NO FURTHER DEFECTS NOTED.SDR CA090213003Fuel Cell · leaking(CAN) ACFT PARKED STATIC IN HANGER. FUEL LEAKS THOUGH CELL MATERIAL. REQUIRES REPLACEMENT.SDR CA090213002Fuel Cell · leaking(CAN) ACFT PARKED STATIC INSIDE HANGER. FUEL LEAKS THOUGH CELL MATERIAL. REQUIRES REPLACEMENT.SDR 2009FA0000078Collar · crackedON SHUTDOWN AT AN OFFSHORE PLATFORM THE PILOT HEARD A POP. ON INSP, HE DISCOVERED THE COLLAR SET LOOSE ON THE MAST ASSY.SDR 2009FA0000092Bearing · failedSPOOL BEARING ASSY FAILED INTERNALLY. BEARING ASSY NO LONGER ROTATES. THE UPPER BEARING LOWER SHIELD AND RETAINER HAS COME OFF, BEARING BALLS ARE LOOSE. THE LWR BEARING IS INTACT BUT NO LONGER ROTATES. (K)SDR 2008FA0000610Bearing · failedSPOOL BEARING ASSY FAILED INTERNALLY. BEARING ASSY NO LONGER ROTATES AND CAUSED DRIVE SHAFT GUIDE POST AND FORK IN GOVERNOR LEVER ASSY TO BEND. THE UPPER BEARING LOWER SHIELD AND RETAINER HAS COME OFF. THE LOWER BEARING IS INTACT BUT NO LONGER ROTATES. (K)SDR HEF2008F00000Bearing · failedUPPER BEARING, (PN 2525465) INSIDE OF SPOOL BEARING ASSY FAILED (CAME APART). LOWER SPOOL BEARING, (PN 2525468) IS STILL INTACT, BUT NO LONGER ROTATES FREELY. (K)SDR CA080821008Frame · chafed(CAN) HYDR SERVO PILOT VALVE SUPPORT RUBBING AGAINST MAIN FRAME. WEAR MARK IS APPARENT ON LT SUPPORT. PICTURES AVAILABLE ON REQUEST AND INFO FWD TO MFG CUSTOMER SUPPORT FOR ACTION.SDR 2008FA0000460Meter · malfunctionedAC MAINT HOBBS METER FOUND RUNNING SLOW. THIS PROBLEM CAUSES THE ACTUAL TT OF THE AC TO BE INCORRECT. THIS PROBLEM CAUSED THE AC TO OVER RUN INSPECTIONS, AND TIME LIFE ITEM. PROBABLE CAUSE OF THIS PROBLEM, HOBBS METERS GETTING OLD AND WORN OUT. RECOMMENDASDR RMX2008F00001Fitting · crackedDURING ROUTINE INSPECTION TECHNICIAN DISCOVERED UPPER LEFT TAILBOOM ATTACH FITTING CRACKED. (K)SDR RMX2008F00000Fitting · crackedDURING ROUTINE INSPECTION TECHNICIAN DISCOVERED UPPER LEFT TAILBOOM ATTACH FITTING CRACKED. (K)
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