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 = 'G159' 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 = 'G159' 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 ESPA2015FA0000183Line · rupturedNORMAL TAKEOFF, ABOUT HALFWAY TO DESTINATION STARTED HEARING A LOW RUMBLE IN THE BELLY OF THE PLANE. HAVING BEEN THROUGH THIS BEFORE, HAD THE CO-PILOT CHECK THE HYDRAULIC PRESSURE WHICH WAS NORMAL. ABOUT 15 SECONDS LATER, HE SAID THE HYDRAULIC PRESSURE GUAGE SSDR 2015F00017Line · leakingRT GEARBOX LIGHT ILLUMINATED. SHUTDOWN THE ENGINE IAW THE CHECKLIST, DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. TROUBLESHOT PROBLEM AND FOUND THE FITTING AND LINE FOR THE GEARBOX PRESSURE RETURN LINE LEAKING. R & R FITTING AND LINE WITH A SERVICEABLE UNSDR ESPA2015F00011Line · rupturedPILOT REPORTED A RT ENGINE GEARBOX PRESSURE LIGHT ABOUT 25 MINUTES INTO THE FLIGHT. REDUCED POWER ON THE RT ENGINE AND LIGHT WENT OUT. THE ACFT RETURNED WITHOUT INCIDENT. DECLARE AN EMERGENCY. MAINTENANCE TROUBLESHOT PROBLEM TO A RUPTURED BLOWER OIL FILTERSDR ESPA2014F00107Landing Gear · malfunctionedAFTER PERFORMING ALL LANDING CHECKS DURING A NORMAL LANDING, AT TOUCHDOWN EXPERIENCED A LANDING GEAR WARNING HORN, NOTICED THE NOSE GEAR, GREEN, LIGHT WAS OFF AND RED GEAR HANDLE LIGHT ON. RECYCLED THE GEAR DOWN AND LIGHT FAILED AGAIN. IAW CHECK LIST, PSDR 2013FA0000292Line · rupturedON THE 1430 FLIGHT, AFTER DEPARTURE THE PILOTS FELT A SHUDDER IN THE AIRFRAME. THE HYD PRESSURE GAUGE READ ZERO. THEY DECLARED AN EMERGENCY AND LANDED SAFELY. MX FOUND THE LT OTBD HYD LINE RUPTURED. R & R WITH A SERVICEABLE LINE (PN 159H10007-4C). COMPLIESDR CA120727005Line · chafed(CAN) DURING CLIMB OUT, HYDRAULIC FLUID WAS LOST AND CREW RETURNED TO DEPARTURE AIRPORT SAFELY. MAINTENANCE INSPECTED AND FOUND LT MLG DOWNLOCK ACTUATOR RELEASE HYD PRESSURE LINE CHAFED THROUGH ALLOWING HYDRAULIC FLUID TO BE LOST. LINE WAS REPLACED, AREA CLESDR CA111003001Coupling · swollen(CAN) LT ENGINE WAS SHUTDOWN AFTER LT ENGINE OIL PRESSURE LOST IN FLIGHT DUE TO OIL STARVATION. ACFT LANDED SAFELY ON CLOSEST AIRPORT. GROUND INSPECTION REVEILED THAT OIL STARVATION WAS CAUSED BY ENGINE BREATHER LINE COUPLING SWOLLEN AND CAUSED BREATHER RESTSDR ESPADEA20111Rod End Bearing · brokenAFTER TAKEOFF AND GEAR WAS RETRACTED A VERY LOUD VIBRATION WAS HEARD COMING FROM THE NOSE GEAR WHEEL WELL AREA,THE AIRCRAFT RETURNED. WHEN GEAR WAS SELECTED DOWN,THE GEAR DID NOT COME DOWN THE HYDRAULIC PRESSURE WAS ZERO,COMPLIED WITH EMERGENCY GEAR LOWERING PSDR 2011F00041Hose · looseCABIN PRESSURIZATION CONTROL ERRATIC DURING CLIMB. PILOT RETURNED TO DEPARTURE AIRPORT AS A PRECAUTION. INSPECTED PRESSURE CONTROLLER, FOUND LOOSE HOSE ON CONTROLLER, RESECURED HOSE IAW PRESSURE CONTROLLER REMOVAL AND INSTALLATION INSTRUCTION. NO DEFECTIVE SDR 2011F00007Fairing · crackedVISUAL INSP OF NOSE FAIRING, INDICATED CRACKS IN STRUCTURE UNDER THE DOUBLER, WHERE ATTACH RODS ARE MOUNTED. THESE CRACKS EXCEED THE MFG LIMITS. FAIRING WAS REPLACED WITH SERVICABLE REPLACEMENT.SDR 2010FA0001274Skin · corrodedIN COMPLIANCE WITH AD 2006-25-02, X-RAY RESULTS INDICATED SEVERE CORROSION IN AFT FUSELAGE AREA RT OF FUSELAGE, AFT OF PRESSURE BULKHEAD, BETWEEN TAIL ACCESS DOOR AND APU DOOR. CORROSION IS LOCATED BETWEEN STR 11 AND 13. ALL REPAIRS MADE IAW ENGINEERING REPSDR 2010F00077Engine · unknownIN FLIGHT ENGINE SHUTDOWN. AUTO FEATHERING OF PROPELLER. ERRATIC FUEL FLOW. OVERTEMP (POSSIBLE). TURBINE SECTION SEIZED (ON THE GROUND AFTER LANDING). ROOT CAUSE NOT CURRENTLY KNOWN. ACFT RETURNED TO DEPARTURE.SDR ESPADJ20101Fire Loop · out of toleranceAFTER TAKEOFF AND CLIMBING THRU 3000 FT APPROX 15NM NORTH, THE RED FIRE WARNING LIGHT IN THE RT T-HANDLE ILLUMINATED. REDUCED POWER AND CHECKED FOR ADDITIONAL INDICATIONS. ALL OTHER INDICATIONS WERE NORMAL FLIGHT RETURNED TO DEPARTURE WITHOUT SECURING ENGINE.SDR N8UA10102009APump · leakingMX TEST FLIGHT, AFTER REPLACEMENT OF SUSPECT LEAKING RT GEARBOX (THIRD UNIT TO BE INSTALLED IN THE PROBLEM DIAGNOSIS). (2) HOURS OUT, RT ENG GEARBOX LOW OIL PRESSURE WARNING LIGHT. ACFT WAS DIRECTED TO RETURN TO DEPARTURE. PROP WAS FEATHERED AND ENGINE SHUTSDR N8UA10092009AGearbox · leakingMX TEST FLIGHT, AFTER REPLACEMENT OF BLOWER AND ALTERNATOR ON SUSPECT LEAKING RT ENG GEARBOX. (2) HOURS OUT, RT ENGINE GEARBOX LOW OIL PRESSURE WARNING LIGHT. ACFT WAS DIRECTED TO RETURN TO DEPARTURE. PROP WAS FEATHERED AND ENGINE WAS SHUTDOWN. NO PASSENGESDR N8UA10082009AGearbox · leakingRT ENG GEARBOX LOW OIL PRESSURE WARNING LIGHT DURING LANDING. LANDING WAS NORMAL. REPLACEMENT GB WAS INSTALLED AFTER SIMILAR INDICATION PREVIOUS DAY. OPS AND TEST FLIGHT WERE GOOD. NO PASSENGERS WERE ON ACFT DURING FLIGHT.SDR N8UA100720090AGearbox · leakingSCHEDULED FLIGHT, 3.5 HOURS OUT, RT ENGINE GEARBOX LOW OIL PRESSURE WARNING LIGHT INTERMITTENT DURING LANDING. CONTINUED NORMAL LANDING. ACFT GROUNDED UNTIL REPAIRS COMPLETED.SDR N8UA 10012009AGearbox · leakingMX TEST FLIGHT, AFTER REPAIR OF OIL LEAK IN RT ENG GEARBOX. (2) HOURS OUT, RT ENG GEARBOX LOW OIL PRESSURE WARNING LIGHT CONSTANT. RT ENGINE WAS FEATHERS AND SHUTDOWN. ACFT WAS DIRECTED TO RETURN TO DEPARTURE.SDR N8UA09302009AGearbox · leakingSCHEDULED FLIGHT. (2) HOURS OUT, RT ENG GEARBOX LOW OIL PRESSURE WARNING LIGHT INTERMITTENT. ACFT WAS DIRECTED TO RETURN TO DEPARTURE. GEARBOX HAD JUST BEEN INSTALLED AFTER OVERHAUL.SDR 2008FA0000572Actuator · leakingRT MLG SIDE BRACE ACTUATOR LEAKING FROM SWITCH ASSY. SIDE BRACE ACTUATOR REMOVED, REPLACED WITH REPAIRED ACTUATOR ASSY.SDR 110107Warning Light · illuminatedDURING CRUISE FLIGHT MISSION, THE RT GEARBOX LIGHT CAME ON STEADY. THE ENGINE WAS SHUTDOWN IAW AFM PROCEDURES. THE AIRCRAFT LANDED UNEVENTFULLY, AND TAXIED TO THE RAMP. NO EMERGENCY WAS DECLARED.SDR 2007ADP828001Selector Valve · bypassingAIRCRAFT WAS ENROUTE, FLYING THE APPROACH FOR RUNWAY 03. ONCE THE CREW PERFORMED THE APPROACH CHECKLIST, AND GEAR DOWN WAS SELECTED BEFORE LANDING CHECKLIST THEY GOT THE RT MAIN AND NOSE GEAR LIGHT ONLY. CREW TRY THE EMERGENCY PROCEDURES DESCRIBED ON CHECKLISTSDR ESPA20040006Engine · making metalENGINE FLAMED OUT IN FLIGHT WITH NO WARNING OR INDICATION. METAL WAS FOUND IN THE OIL SCREEN. ENGINE WILL BE SENT BACK TO OVERHAUL FACILITY FOR EVALUATION AND WARRANTY CONSIDERATION.SDR ESPA20040005Door · unsecureCARGO DOOR CAME OPEN IN FLIGHT. CREW LANDED SAFELY. IT WAS DETERMINED THAT THE DOOR WAS NOT PROPERLY SECURED BEFORE TAKEOFF.SDR ESPA200400004Structure · bird strikeWHILE ON APPROACH AIRCRAFT WAS STRUCK BY A BIRD ON THE LEFT SIDE OF THE FORWARD FUSELAGE.SDR ESPA200400002Bearing · seizedAFTER TAKEOFF, DISCOVERED THAT THE NR 1 MAIN WHEEL ASSEMBLY HAD DISCONNECTED FROM THE AXLE. THE AXLE NUT WAS STILL IN PLACE. IT WAS DETERMINED THAT A WHEEL BEARING FAILURE WAS PROBABLY THE CAUSE.SDR 2004F00082Control Rod · looseAIRCRAFT RELEASED FROM MAINTENANCE. DEPARTED VPC. CLIMBING OUT FROM 9,000 FT, RIGHT THROTTLE WOULD NOT RESPOND. RETURNED TO VPC WITH UNEVENTFUL LANDING. MAINTENANCE FOUND THE THROTTLE PUSH PULL ROD CAME LOOSE AT THE FIREWALL (ROD END SEPARATED FROM THE BARSDR CA030311002Bearing · disintegrated(CAN) R/H ALTERNATOR WOULD NOT STAY ON LINE. SENT FOR PREMATURE OVERHAUL (1000.0 HR TBO). FOUND REAR BEARING DISINTEGRATED TO THE POINT OF ROTOR RUB. THE OVERHAUL COMPANY IS HOLDING BEARING FOR POSSIBLE T.C. INSPECTION.SDR CA021115010Bearing · shorted(CAN) LT GENERATOR TRIPPED, PILOTS REPORTED AN UNDER VOLTAGE CONDITION.ACTION: LT GENERATOR REMOVED, UPON INSPECTION OF COMPONENT, GEARING ASSEMBLY PARTS HAD MIGRATED TO, AND SHORTED OUT A BRUSH HOLDDOWN SPRING TO THE GENERATOR CASE.SDR CA020226004Fitting · fractured(CAN) GEARBOX LOW OIL PRESSURE LIGHT CAME ON, ENGINE SHUTDOWN AND AIRCRAFT LANDED. GEARBOX OIL LEVEL FOUND LOW BUT STILL ON DIP STICK. OIL LEAK TRACED TO FAILED FITTING ON SUPERCHARGER. UNIT HAS OVERHAUL LIFE OF 2,500 HOURS. LINE IS PRESSURE CHECKED (LOW PRESSSDR CA010504015Fairing · cracked(CAN) WHEN DOING THE POST FLIGHT INSPECTION A CRACK WAS FOUND IN THE NOSE GEAR DRAG BRACE FAIRING ASSEMBLY. THE CRACK WAS ON THE L/H SIDE FORMER WHICH WAS CRACKED COMPLETELY THROUGH. IF LEFT UNREPAIRED A FAILURE OF THE FAIRING ASSEMBLY WAS POSSIBLE. THE CRACK SDR CA001128016Element · broken(CAN) CREW REPORTED NR 1 FIRE TEE HANDLE LIGHT FLICKED. MAINTENANCE FOUND ALSO WOULD NOT TEST. FIREWALL FIRE ELEMENT FOUND BROKEN. ELEMENT REPLACED CHECKED SERVICEABLE.SDR CA001128015Coupling · intermittent(CAN) CREW REPORTED INTERMITTENT NR 1 ENGINE FIRE WARN. MAINTENANCE FOUND FIRE WIRE COUPLING AT FIREWALL (LT UPPER) INTERMITTENT POOR CONNECTION CLEANED RE-ASSEMBLIED CHECKED SERVICEABLE..SDR 20001101SH023Coupling · excess playWHILE DOING ROUTINE MAINT, FOUND EXCESSIVE PLAY IN ACCESSORY DRIVESHAFT, AND THE ACCESSORY DRIVE COUPLING AT THE ENGINE WAS THE CAUSE OF THE EXCESSIVE PLAY. THERE WERE NO PUBLISHED LIMITS FOR THIS COMPONENT. ROLLS ROYCE WAS CONTACTED AND THEIR ENGINEERING SUSDR CA000926010Rotor · cracked(CAN) ON PREFLIGHT, FIBERGLASS DUCT MATERIAL AND METAL FRAGMENTS WERE DISCOVERED IN ENGINE NACELLE/WHEEL WELL AREA.SUPERCHARGER ROTOR FAILED SENDING METAL FRAGMENTS THROUGH FIBERGLASS INLET DUCT.SUPERCHARGER AND DUCT WERE REPLACED, DEBRIS REMOVED FROM INLET PASDR CA000926009Rotor · cracked(CAN) CABIN SUPERCHARGER ROTOR FAILED IN FLIGHT.FLIGHT CREW ACTIVATED APU AS ALTERNATE SOURCE OF PRESSURIZATION AND AIR CONDITIONING.SDR CA000516019Rod · corroded(CAN) X-RAY INSPECTION OF AILERON PUSH ROD REVEALED SEVERE INTERNAL CORROSION.SDR CA991004032Disc · broken(CAN) CREW TAXIED FROM RAMP THEN HEARD NOISE FROM RIGHT SIDE OF AIRCRAFT. INCREASED POWER TO MOVE AIRCRAFT - WOULD NOT MOVE. FOUND NR 4 BRAKE DISC BROKEN AND JAMMED IN WHEEL RIM. WHEEL, BRAKE, AND DISC REPLACED.SDR 99ZZZX3960Fire Loop · shortedEWR/TXKF - EN ROUTE, WHEN LEFT FIRE LIGHT CAME ON. CREW DID VISUAL INSPECTION OF ENGINE AND ENGINE INSTRUMENTS. NO INDICATION OF ANYTHING UNUSUAL. FIRE LIGHT WENT OUT, CREW TRIED TO TEST SYSTEM FIRE LOOP LOCATED IN ENGINE COMPARTMENT. WOULD NOT TEST. CREWSDR CA981230009Actuator · failed(CAN) FUEL TRIM ACTUATOR FAILED AFTER TAKEOFF, UNABLE TO CHANGE FUEL TRIM SETTING. AIRCRAFT RETURNED TO BASE. THE UNIT WAS REPLACED.SDR CA990202006Line · cracked(CAN) ON GEAR EXTENSION, THE CREW OBSERVED FLUCTUATING HYDRAULIC PRESSURE. GEAR EXTENDED SLOWLY. AFTER LANDING, COMPLETE LOSS OF HYDRAULIC PRESSURE AND FLUID. TWO LEFT MAIN TIRES BLEW. MAINTENANCE FOUND A CRACKED LINE FLARE ON THE AUX/MAIN HYDRAULIC SELECTSDR CA981209007Fitting · broken(CAN) UPLOCK FRAME ATTACH FITTING FOR MAIN LANDING GEAR FOUND BROKEN AT FRONT SPAR.SDR CA981116003Gyro · failed(CAN) RIGHT HAND ADI GYRO FLAGGING NUMEROUS TIMES.SDR CA981116002Gyro · failed(CAN) LEFT ADI TOPPLED.SDR CA980825009Bellcrank · cracked(CAN) DEFLECTION CRANK FOUND CRACKED USING NDT TECHNIQUE. PART TC: 19,718.SDR 99ZZZX173Uplock · failedAIRCRAFT ARRIVED WITH DISCREPANCY, 'RIGHT MAIN LANDING GEAR FORWARD DOORS DO NOT CLOSE ALL THE TIME'. PERFORMED RETRACTION TESTS, FOUND UPLOCK BOOK ASSY, P/N 159LM10124-1, STRIKING PISTON/AXLE ASSY CASTING, P/N 173527, IN RETRACTED POSITION NOT COMPLETING CYCSDR 98ZZZX1388Riser · corrodedGULFSTREAM CUSTOMER BULLETIN NR CB 337 REQUIRES X-RAY INSPECTION OF INBOARD LOWER PLANK SPLICES AND ULTRASONIC INSPECTION OF THE ADJACENT RISERS. SUBSEQUENT DISASSEMBLY FOR REPAIRS REVEALED EXTENSIVE CORROSION IN SPLICES AND RISERS NOT DETECTABLE BY THE SPECISDR 98ZZZX1066Bracket · crackedWHILE INSPECTING THE RUDDER CONTROL SYSTEM REFERENCING CUSTOMER BULLETIN NR 235A DATED 5-21-73, DISCOVERED A CRACK IN THE RUDDER CONTROL BELLCRANK SUPPORT BRACKET AND ITS ATTACHMENT ANGLE. THE BRACKET IS MOUNTED TO THE TOP OF THE TAIL COMPARTMENT BETWEEN FRAMSDR 98ZZZX535Driveshaft · looseTHE BOLT SECURING THE FORWARD U-JOINT ONTO THE DRIVESHAFT HAD BACKED ALL THE WAY OUT. THE BOLT SECURING THE AFT U-JOINT TO THE DRIVESHAFT WAS LOOSE EVEN WITH THE LOCKING TAB WASHER INSTALLED. UPON INVESTIGATION, IT APPEARED THE WRONG LOCKING TAB WAS USED DURSDR 98ZZZX216Wing Plank · corrodedGULFSTREAM CUSTOMER BULLETIN NR CB 337 REQUIRES X-RAY INSPECTION OF INBOARD LOWER PLANK SPLICES AND ULTRASONIC INSPECTION OF THE ADJACENT RISERS. SUBSEQUENT DISASSEMBLY FOR REPAIRS REVEALED EXTENSIVE CORROSION IN SPLICES AND RISERS NOT DETECTABLE BY THE SPECI
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