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 = 'AB139' 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 = 'AB139' 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 KY1R202312220001Stud · fracturedDURING AIRCRAFT RUN, AND RELEASE OF PARKING BRAKE, PILOT'S RIGHT YAW PEDAL STUD BROKEWHICH AFFIXES THE BRAKE CYLINDER TO THE PEDAL ASSEMBLY, WHICH LED TO THE INABILITY FOR THE PILOT IN COMMAND TO USE THE THE RIGHT BRAKE. THE PILOT SECOND IN COMMAND APPLIED BRASDR AC2A2023050213901Boot · tornTHE NEW DESIGN SWASHPLATE BOOT P/N 3G6230L01851 SEPARATED AND TORE AFTER 13.3 HOURS OPERATING TIME. BOOT WAS REMOVED AND SPLIT BOOT P/N 3G6230A06231 WAS INSTALLED.SDR AC2A2021101513902Cooling Fan · contaminatedMAIN GEARBOX OIL COOLER FAN WAS REMOVED AND REPLACED DUE TO MGB FAN QUILL SEAL LEAKING ALLOWING OIL TO MIGRATE TO FAN BEARINGS. SEE SDR AC2A2021101513901 FOR SDR ON SEAL.SDR AC2A2021101513901Seal · leakingMAIN GEARBOX OIL COOLER FAN DRIVE SEAL LEAKINGSDR AC2A2021051713902Clamp · wornCLAMPED ADAPTER P/N 3G6320A16551, S/N DAT197 AND ADAPTER CLAMPS P/N 3G6320A16651, S/N AVI 0406 WERE REMOVED FROM MGB 3G6320A00134, S/N V44 IN PREPARATION FOR SHIPMENT OF MGB IN FOR OVERHAUL. ADAPTER AND CLAMPS DISPLAY EVIDENCE OF SIGNIFICANT WEAR OF 0.010" ON SDR AC2A2021051713901Adapter · wornCLAMPED ADAPTER P/N 3G6320A16551, S/N DAT197 AND ADAPTER CLAMPS P/N 3G6320A16661, S/N AVI 0406 WERE REMOVED FROM MGB 3G6320A001434, S/N V44 IN PREPARATION FOR SHIPMENT OF MGB IN FOR OVERHAUL. ADAPTER AND CLAMPS DISPLAY EVIDENCE OF SIGNIFICANT WEAR OF 0.010" OSDR AC2A2021061013901Cooling Fan · leakingOIL COOLER FAN WAS REMOVED AND REPLACED DUE TO MGB FAN QUILL SEAL LEAKING ALLOWING OIL TO MIGRATE TO FAN BEARINGS. TEARDOWN REPORT INDICATES BEARINGS WORN AND REPLACED WITH ONLY 284.4 HOURS SINCE OVERHAUL.SDR AC2A2021033113901Blade · debondedMAIN ROTOR BLADE TIP CAP ATTACHMENT BOND LINE SEPARATION.SDR AC2A2021061013903Cooling Fan · leakingOIL COOLER FAN WAS REMOVED AND REPLACED DUE TO MGB FAN QUILL SEAL LEAKING ALLOWING OIL TO MIGRATE TO FAN BEARINGS. TEARDOWN REPORT INDICATES BEARINGS WORN AND REPLACED WITH ONLY 13.7HOURS SINCE LAST OVERHAULSDR AC2A2020091813901Boot · tornMAIN ROTOR UPPER SWASHPLATE BOOT TORN, METAL RINGS LOOSE, NO ACCEPT/REJECT CRITERIA PROVIDED BY MANUFACTURER, NO DETAILED INSPECTION CRITERIA AVAILABLE.SDR AC2A2020081013902Check Valve · separatedHEATER WILL NOT BLOW HOT AIR, DURING TROUBLESHOOTING FOUND HIGHT PRESSURE CHECK VALVE FLAPPER HALVES BEING SEPARATED FROM CHECK VALVE BODY ON ONE SIDE.SDR AC2A2020081013901Check Valve · separatedHEATER WILL NOT BLOW HOT AIR; DURING TROUBLESHOOTING FOUND HEATER TEMPERATURE CONTROL VALVE (P/N 3G2140V00751) TO BE DAMAGED FROM HIGHT PRESSURE CHECK VALVE (P/N 3G2140V00651) FLAPPER HALVES BEING SEPARATED FROM CHECK VALVE AND LODGED IN HEATER TEMPERATURE CONSDR AC2A2021061013902Cooling Fan · leakingOIL COOLER FAN WAS REMOVED AND REPLACED DUE TO MGB FAN QUILL SEAL LEAKING ALLOWING OIL TO MIGRATE TO FAN BEARINGS. TEARDOWN REPORT INDICATES BEARINGS WORN AND REPLACED WITH ONLY 464.1 HOURS SINCE OVERHAUL.SDR AC2A2020033001Fuel Control · malfunctionedWHEN ADVANCING #1 ENGINE FROM IDLE TO FLIGHT POSITION, #1 ENGINE BEGAN TO "RUN AWAY" AND THE AIRCRAFT SPUN APPROXIMATELY 25-30 DEGREES ON THE PAD AND STARTED TO ROLL OVER. THE PIC WAS STILL ON THE ENGINE MODE KNOB, IMMEDIATELY RETARDED TO #1 ENGINE BACK TO IDSDR AC2A2020012483901Ring · unstakedDURING DAILY INSPECTION, NOTICED RIGHT SIDE MAIN GEARBOX CHIP DETECTOR NOT FULLY ENGAGED. UPON INVESTIGATION, FOUND RETENTION RING FOR CHIP DETECTOR HAD BECOME UN-STAKED FROM CHIP DETECTOR BODY.SDR AC2R2018022001Bolt · brokenHEAD OF BOLT BROKE OFF.SDR AC2R2017071901Wire Harness · chafedTHE MECHANICS HAD THE POWER ON THE AIRCRAFT AND NOTICED SPARKS IN THE OVERHEAD AREA ABOVE CIRCUIT BREAKER PANEL, WHEN THEY MOVED THE ROTOR BRAKE HANDLE FORWARD. THE AREA WAS INSPECTED AND THEY DISCOVERED THAT SOME WIRES HAD BEEN CONTACTING THE ROTOR BRAKE ROD SDR AC2R2018041901Bearing · roughOIL COOLER HAD EXCESSIVE VIBRATION. BEARING ROUGH.SDR AC2R2016070701Ring · damagedDURING REMOVAL OF THE MAIN ROTOR HEAD ASSY, FIVE PRESSURE BOLTS WERE NOTED OF HAVING A LOSS OF TORQUE PRIOR TO REMOVAL. AFTER REMOVAL OF THE MAIN ROTOR HEAD ASSY, AND FURTHER INSPECTION, DAMAGE WAS FOUND TO THE LOWER CONICAL RING AND TO THE LOWER CONICAL RINGSDR PN1R06032016001Nut · defectiveM/R HEAD WAS REMOVED TO INSTALL A NEW SWASHPLATE BOOT, DURING REMOVAL FOUND 3 EA. RING NUT BOLTS EXTREMELY TIGHT AND 1 OF THOSE HAD SEIZED. PROCURED NEW RING NUT AND 3 EA. NEW BOLTS AND PROCEEDED TO INSTALL. NEARING THE FINAL TORQUE OF 55 FT/LBS, THE TORQUE SDR AC2R2016051701Firewall · crackedTHE NR 2 ENGINE FIREWALL HAS A 45MM CRACK AT BS 5700, WL 2670 AND BUTT LINE 780. WE ARE REQUESTING OPTIONS FOR AN REPAIR OF THE CRACKED AREA. THE NR 1 ENGINE FIREWALL HAS AN 78MM CRACK AT BS 5700 AND WL 2670. WE ARE REQUESTING OPTIONS FOR AN REPAIR OF THE CSDR CA151002010Support Bracket · cracked(CAN) DURING A 50 HR INSPECTION, A CRACK WAS FOUND ON THE LT STABILIZER SUPPORT BRACKET, DEFECTIVE PART WAS REMOVED AND UPGRADED PART, PN 3G5351A01433 WAS INSTALLED. ACFT WAS RETURNED TO SERVICE.SDR CA140926003G Switch · malfunctioned(CAN) ACFT HAD GROUND POWERED APPLIED TO IT IN THE HANGAR AND POWER WAS REMOVED AT APPROXIMATELY 16:30. AT AROUND 17:30, SEARCH AND RESCUE COORDINATION CENTER CALLED US TO REPORT ELT ACTIVATION ON THE AIRCRAFT. A TECH WAS DISPATCHED RT AWAY TO THE HANGAR, TO SDR CA140203004Seal · leaking(CAN) DURING FLIGHT, THE CREW OBSERVED RT ENGINE OIL PRESSURE INDICATOR DECREASE. THE ENGINE WAS IMMEDIATELY SHUTDOWN. CAPTAIN OBSERVED AN OIL LEAKAGE THROUGH FMM SEAL LEAK DRAIN. THE SEAL WAS REPLACED AND THE ACFT RETURN TO SERVICE. NO OTHER LEAKS WERE REPOSDR CA130508012Seal · leaking(CAN) DURING THE REPLACEMENT OF THE IGB, INTERMEDIATE GEARBOX, SEAL, DUE TO LEAKAGE, THE LIP SPRING WAS FOUND ON THE INPUT SHAFT, INSIDE THE IGB, INSTEAD OF SITTING ON THE SEAL`S LIP ITSELF. NEW SEAL WAS INSTALLED AND INPUT SHAFT REMOVED AND REINSTALLED A FESDR CA120524004Engine · overtemp(CAN) DURING FLIGHT, THE ENGINE TEMPERATURE CLIMBED ABOVE 1000C. THE PILOT SHUT THE ENGINE DOWN AND LANDED SAFELY, SINGLE ENGINE. THE ENGINE WAS REPLACED AND THE HELO WAS RETURNED TO SERVICE. NO DETAILS WERE AVAILABLE ON ENGINE CONDITION OR TROUBLESHOOTING PESDR 2011F00088Attach Fitting · crackedDURING A 300/600 INSP, A FLIGHT CONTROL BRACKET (PN 3G5351A01432) LEFT FITTING WAS FOUND CRACKED FROM THE BOLT HOLE OTBD.SDR AC2A033120119CWHydraulic System · malfunctionedBEFORE LANDING CHECKLIST, TO LAND AND WHEN THE LANDING GEAR HANDLE WENT DOWN, GOT A NR2 SERVO, NR 2 HYD MIN, AND HYD UTIL PRESS CAUTION LIGHTS. THEN WENT TO THE HYD SYNOPTIC PAGE. SAW THE NR 2 HYD FLUID LEVEL GO THROUGH 22 PERCENT AND THEN IT WENT TO ALL AMBSDR AC2R9JP02222011Fitting · crackedDURING ROUTINE 50 HR INSP, FOUND THE SUPPORT FITTING WHERE THE INTERMEDIATE GEARBOX ATTACHES TO THE TAILBOOM WAS CRACKED. REMAINING ACFT IN OUR FLEET WERE INSPECTED AND NO OTHER DESCREPANCIES WERE FOUND.SDR AC2R12062010001Angle · cracked(AC2R) CRACKED FORE AND AFT ANGLE, PN 3P5333A19561, RT SIDE FUEL DRY BAY AREA.SDR 2010FA0000766Pump · leakingAFTER TAKEOFF, AFTER SELECTION OF LANDING GEAR UP, CAS DISPLAYED HYD UTIL PRESS AND MAIN GEAR POSITION INDICATION TURNED TO AMBER. IAW RFM MALFUNCTION PROCEDURE, LANDING GEAR RESELECTED DOWN BUT WOULD NOT LOCK. EMERGENCY LANDING GEAR EXTENSION DEPLOYED & LANDISDR AC2A2009092783295Pressure Switch · failedNR 1 SERVO CAS ILLUMINATED IN FLIGHT. COMPLIED WITH HYD SERVO MALFUNCTION EMERGENCY PROCEDURES AND RETURNED TO BASE. REPLACED 31 HYD SERVO SWITCH.SDR AC2A2009092283308Switch · defectiveIN CRUISE FLIGHT, NR 1 SERVO CAUTION LIGHT CAME ON. CHECKED HYD SCHEMATIC PAGE WHICH SHOWED ALL NT 1 SYS SERVOS IN YELLOW, REFERENCED EMERGENCY PROCEDURES CHECKLIST FOR NR 1 SERVO CAUTION LIGHT. LOWERED LANDING GEAR AND RETURNED TO DEPARTURE. DEFECTIVE SWITCHSDR AC2A2009081482852Pressure Switch · malfunctionedTURNING DOWNWIND AFTER TAKEOFF, NR 2 SERVO LIGHT ILLUMINATED. FOLLOWED ESTABLISHED EMERGENCY PROCEDURE. PRESSURE SWITCH MALFUNCTIONED.SDR ULXR2009070282295Skin · deformedTAIL ASSY LT AND RT SIDES , SKIN DEFORMATION BETWEEN STA 8700.1 TO 9436.1 AND BETWEEN WL 2176.8 TO 2060.8. SKIN IS BUBBLING TBD BETWEEN THE 2 HONEYCOMB AREAS OF THE PANEL ON BOTH SIDES OF BOOM.SDR ULXR2009070282294Skin · deformedTAIL ASSY LT AND RT SIDES , SKIN DEFORMATION BETWEEN STA 8700.1 TO 9436.1 AND BETWEEN WL 2176.8 TO 2060.8. SKIN IS BUBBLING OTBD BETWEEN THE 2 HONEYCOMB AREAS OF THE PANEL ON BOTH SIDES OF BOOM.SDR AC2A2009062382120Pressure Switch · malfunctionedNR 2 SERVO CAS ILLUMINATED IN FLIGHT. EMERGENCY CHECK LIST USED. LANDING GEAR WAS LOWERED NORMALLY IAW THE CHECKLIST AND ACFT LANDED UNEVENTFULLY AS SOON AS PRACTICAL. REPLACED NR 2 RT SERVO PRESSURE SWITCH.SDR AC2A2009062282113Warning Light · illuminatedNR 2 SERVO CAS ILLUMINATED IN FLIGHT. EMERGENCY CHECK LIST USED. LANDING GEAR WAS LOWERED NORMALLY IAW THE CHECKLIST AND ACFT LANDED UNEVENTFULLY AS SOON AS PRACTICAL. PROBLEM COULD NOT BE DUPLICATED AND ACFT WAS RETURNED TO SERVICE.SDR ULXR2009061882082Probe · inoperativeFUEL QUANTITY READS ZERO. NO SIGNAL FROM PROBE. REPLACEMENT PROBE FIXED DISCREPANCY.SDR ULXR2009042481807Bearing · wornLAG DAMPER ROD END BEARING HAS PLAY .017.SDR ULXR2009040881808Warning System · inoperativeRT MAIN GEAR GREEN DOWN ARROW SEGMENT WILL NOT ILLUMINATE. REPLACED CONTROL UNIT.SDR U0GA2009030780996Oil System · leakingDURING THE INITIAL DESCENT FROM 4500 FT, CRUISING ALTITUDE, ACFT SUFFERED A PRESSURE LOSS TO NR 1 ENGINE OIL SUPPLY, APPROX 8 MINUTES FROM LANDING. OIL PRESSURE INDICATION FLICKERED TO A YELLOW CAUTION MOMENTARILY. POST FLIGHT INSP CONFIRMED MASS OIL LOSS FRSDR U0G2009F00000Seal · failedDURING THE INITIAL DESCENT FROM 4500 FT CRUISING ALTITUDE, ACFT SUFFERED A PRESSURE LOSS TO THE OIL SUPPLY IN ENGINE NR 1. WE WERE APPROX EIGHT MINUTES FROM LANDING. THE OIL PRESSURE INDICATION FLICKERED TO A YELLOW CAUTION MOMENTARILY. THE NFP CHECKED THE SDR AC2A2008093078342Rod End · brokenDURING TRANSITION FROM CLIMB TO CRUISE FLIGHT THE ACFT DEVELOPED A SEVERE VIBRATION. FOUND TAIL ROTOR DAMPER ROD END BROKEN. REPLACED TAIL ROTOR BLADE AND DAMPER.SDR U0GA2008092378215Fire Warning · illuminatedIN LEVEL FLIGHT WHILE CONDUCTING A PT91 FERRY FLIGHT A NR 1 ENGINE FIRE CAS MESSAGE AND AURAL WARNING OCCURED WITHIN 30 SECONDS THE NR 2 ENGINE FIRE CAS MESSAGE AND AURAL WARNING SOUNDED THERE WAS NO OTHER INDICATION OF A FIRE THE ECL'S FIRE BOTTLE SELECTORS SDR U0GA120982Fire Warning · activatedIN LEVEL FLIGHT, WHILE CONDUCTING A PT91 FERRY FLIGHT, A NR1 ENGINE FIRE CAS MESSAGE AND AURAL WARNING OCCURRED WITHIN 30 SECONDS. THE NR 2 ENGINE FIRE CAS MESSAGE AND AURAL WARNING SOUNDED, THERE WAS NO OTHER INDICATION OF A FIRE. THE ECL`S FIRE BOTTLE SELESDR AC2A2008081677771Bolt · scoredBOLTS ARE SCORED.SDR U0GA2008080877721Warning Message · multiple indMULTIPLE CAS MESSAGES TO INCLUDE ENG FIRE, BAG FIRE, EEC FAI AND NUMEROUS OTHERS. CAPTAINS A/S, VSI AND ALTIMETER AND NR2 PI INDICATION FAILEDSDR AC2A119534Fireseal · tornFIRESEAL, TORN AND DETERIORATED.SDR AC2A119533Bolt · brokenBOLT BROKEN.
Back to Agusta AB139