Turbomeca MAKILA-1A
Service difficulty reports · 57
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'MAKILA1A' 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 engine_model_key = 'MAKILA1A' 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 2025F00141Compressor · stalledWHILE CONDUCTING 133 EXTERNAL LOAD OPERATIONS LOCATED ON A NAVY VESSEL, A POSSIBLE COMPRESSOR STALL WAS EXPERIENCED FOLLOWING RELEASE OF AN EXTERNAL LOAD WHILE TRANSITIONING TO FORWARD FLIGHT. A LOUD NOISE WAS NOTED AT THE TIME AND OTHER COCKPIT INDICATIONS FOSDR 2020F00046Swashplate · damagedTHIS SUBMISSION CORRECTS AND EFFECTIVELY REPLACES A PREVIOUS SUBMISSION ON THIS AIRCRAFT AT THE SAME DATE AND TIME.
DURING START UP THE PILOTS RECEIVED A CHIP LIGHT NOTIFICATION ON THE VMS SCREEN CORRESPONDING WITH A CHIP LIGHT IN THE MGB SYSTEM. THE AIRCRAFSDR 9EKA2015042915Fcu · faultyUPON LANDING DIFF NG LIGHT ILLUMINATED ALONG WITH A NG T4 DROP ON ENG 2 FOLLOWED BY AN NR OVER SPEED ALARM & HIGH NG ON ENG 1 & HIGH NR RPM. PILOT REDUCED THROTTLES TO CONTROL NG & NR. NR DID NOT EXCEED 300 RPM. FOUND FAULTY FCU. REPLACED FCU WITH OVERHAULESDR 9EKA20150303010Fcu · failedDURING FLIGHT, NG SPLIT OF 2000 BETWEEN ENGS.SDR 9EKA20150218009Firewall · crackedON A SCHEDULED INSPECTION, NR 2 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.SDR 9EKA02022015008Firewall · crackedON A SCHEDULED INSPECTION, NR 1 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.SDR CA110112007Windscreen · crackedINFLIGHT CRACKING OF OUTER LAYER. RETURN TO BASE.SDR CA110105006Logic Card · failed(CAN) GEAR WAS SELECTED FOR RETRACTION AFTER T/O. AMBER GEAR TRANSIT LIGHT REMAINED ON. EMERGENCY CHECK LIST CONSULTED. GEAR SELECTED DOWN W/NO CHANGE, TRANSIT LIGHT REMAINED ON W/NO GEAR DOWN INDICATION. GEAR SELECTED UP THEN DOWN. GEAR INDICATED DOWN W/SDR CA110105008Phase Relay · failed(CAN) BEFORE TAXIING, THE INLET ANTI ICE WAS TURNED ON, BUT SHOWED THE DEICE LIGHT ON THE 32 ALPHA PANEL AND COULD NOT BE RESET WITH MULTIPLE TRIES AND ENGINE STARTS.SDR CA090522005Spacer · failed(CAN) DURING ROUTINE 500 HR INSP AND AFTER THE REMOVAL OF THE FREQUENCY ADAPTORS, THE FLAPPING HINGE PIN SPACER THAT MATES AGAINST THE FREQUENCY ADAPTER SPHERICAL BEARING WERE FOUND CRACKED. REFERENCES: MET CHP 62.35-00.601, 62.35-00.729.SDR CA080513007Transmission · making metal(CAN) TRANSMISSION CHIP LIGHT ILLUMINATION. FERROUS METAL CHIPS, WHISKERS AND FLAKES FOUND IN FILTER AND SUMP AND ON CHIP DETECTOR.SDR CA070807006Pin · worn(CAN) ON MAIN ROTOR GEARBOX REMOVAL SMALL PIN P/N 332A38-1015-21 FOUND INSTALLED IN LIEU OF LARGE PIN P/N 332A38-1019-21 IN LOWER POSITION OF FORWARD SUSPENSION BAR. RESULTANT, RADIAL PLAY 6 MM APPROXIMATELY. MFG CONTACTED TO DETERMINE FURTHER ACTION. RECORSDR CA070427001Door · separated(CAN) AFTER TAKING OFF FROM AN OFFSHORE RIG AT 300 FT, 70 KNOTS, CREW HEARD A STRONG NOISE AND ONE OF THE PASSENGERS ADVISED THAT DOOR WAS MISSING. P/C NOTICED NO CAUTION LIGHTS. AC RETURNED TO THE RIG AND LANDED WITHOUT FURTHER INCIDENT. AC SUBSEQUENTLY RETURSDR CA060419006Tie Bolt · sheared(CAN) A/C RETURNED FROM AN OFFSHORE TRIP, MAINTENANCE PERSONNEL WERE CARRYING OUT THE TURN AROUND CHECKS AND FOUND THAT ONE OF THE 3 ENGINE TIE BOLTS WAS ONLY HELD IN PLACE BY THE LOCKING WIRE. ONCE THE LOCK WIRE WAS CUT THE BOLT WAS PULLED OUT AND FOUND TO BSDR CA060315001Bracket · crackedDURING A ROUTINE DAILY INSPECTION, TWO MAIN ROTOR DEICE BRACKET WERE FOUND TO HAVE CRACKS IN THE SAME AREA. THESE BRACKETS WERE REPLACED AND THE A/C RETURNED TO SERVICE.SDR CA060127007Wire Harness · worn(CAN) A/C RETURNED FROM AN OFFSHORE TRIP, THE MAINTENANCE STAFF WERE CARRING OUT A ROUTINE TURN AROUND CHECK AND FOUND THE M/R DEICE HARNESS BROKEN AT THE CONNECTOR PLUG. MAINTENANCE DEPT REPLACED THE HARNESS AND THE A/C RETURNED TO THE FLYING SCHEDULE. (TC NRSDR CA051123003Bushing · crackedDURING THE DAILY INSPECTION, IT WAS NOTICED BLACK T/R BLADE FLAPPING HINGE HADE A LITTLE MORE RESISTANCE, (SIDE TO SIDE MOTION) THAN THE OTHER BLADES. AFTER FURTHER INVESTIGATION IT WAS FOUND THAT THE BUSHING HAD SOME BRINELLING, WHEN THE BUSHING WAS REMOVED SDR CA051017013Coupling · damagedAFTER LAST FLIGHT OF THE DAY, ENGINEERING REVIEWED THE HUMS DATA AND NOTICED A SPIKE IN THE SHAFT INFORMATION. THE A/C ENGINE WAS REMOVED THE SHAFT REMOVED FROM THE ENGINE AND INSPECTED, AND A CRACK WAS DISCOVERED IN BETWEEN THE TWO FRANGIBLE DISCS. ANOTHER SDR CA050719003Bracket · cracked(CAN) THE DEICE EQUIPMENT WAS BEING REMOVED FOR THE SUMMER SEASON,WHEN THIS CRACK WAS DISCOVERED. NO PREVIOUS EVIDENCE WAS DISCOVERED CONCERNING THIS PART.THIS CRACK WAS DISCOVERED VISUALLY DURING THE REMOVAL.SDR CA040603002Bolt · fractured(CAN) AFTER LAST FLIGHT, DAILY INSPECTION WAS BEING CARRIED OUT ON THE AIRCRAFT, WHEN THE NR 1 ENG LT UPPER TIE BOLT WAS FOUND TO BE FRACTURED. THE OTHER TWO TIE BOLTS WERE REMOVED AND INSPECTED AND FOUND TO BE SERVICEABLE. THIS TIE BOLT ATTACHES THE ENGINESDR CA040504001Adjuster · cracked(CAN) AIRCRAFT REPORTED PEDAL ADJUSTER JAMMED, AFTER INSPECTION THE SUPPORT WAS FOUND TO BE CRACKED. AIRCRAFT IS IN NORWAY FOR A G-CHECK INSPECTION AND WAS ALSO CHECKED FOR THIS PROBLEM , AND WAS FOUND TO ALSO HAVE A CRACK IN THE SAME AREA. FLEET INSPECTION SDR AUS20040315Nut · mismanufactured(AUS) NR 1 ENGINE OUTPUT DRIVESHAFT TO OUTPUT FLANGE ATTACHMENT NUTS FAULTY. MATING SURFACE OF NUTS MISALIGNED. NUTS ARE PART OF BOLT SET PN 332BF6. SUSPECT MANUFACTURING ERROR.SDR CA040202015Tie Rod · sheared(CAN) ONE OF THE THREE BOLTS ATTACHING THE ENGINE TO THE MAIN GEARBOX WAS DISCOVERED SHEARED DURING A TURN AROUND CHECK. THE BOLT WAS SHEARED ABOUT MIDWAY IN THE THREADED PORTION OF THE BOLT. THE ENGINE WAS REMOVED AND AREA INSPECTED IAW WRITTEN PROCEDURES. NOSDR ERAA092665G Switch · sticksG SWITCH STICKS, REPLACED G SWITCH AND TESTED ELT IAW ARTEX PROCEDURES (4090, 1401. 4091) REINSTALLED BATTERY PACK ELT MEETS ALL SPECIFICATIONS.SDR AUS20030952Engine · making metal(AUS) NR 1 ENGINE REAR BEARING CHIP DETECTOR CONTAMINATED WITH METAL.SDR AUS20030871Bearing · broken(AUS) TAIL ROTOR GEARBOX PITCH CHANGE BEARING FAILED. PITCH CHANGESHAFT SERVO END NUT AND LOCKWASHER MISSING. SUSPECT FAILURE OF BEARING DUE TO CONTAMINATION BY H5606 ACTUATOR OIL CAUSING THE LUBRICATING CHARACTERISTICS OF THE SEALED BEARING TO CHANGE.SDR AUS20030357Wire Harness · faulty(AUS) NR 1 ENGINE NH HARNESS INTERNAL FAULT (OPEN CIRCUIT).SDR AUS20020711Control Cable · frayed(AUS) LT REAR TAIL ROTOR CONTROL CABLE CONTAINED BROKEN STRANDS IN AN AREA WHERE THE CABLE PASSES THROUGH FAIRLEAD. FAIRLEAD INSPECTED AND FOUND SERVICEABLE.SDR CA020125007Adjuster · cracked(CAN) PEDAL ADJUSTER LOCATION PIN SUPPORT CRACKED CAUSING THE PEDAL ADJUSTER LEVER TO BE UNMOVEABLE AND THE PEDALS UNADJUSTABLE.SDR AUS20020004Rib · cracked(AUS) HORIZONTAL STABILISER ROOT RIB ASSEMBLY CRACKED BEYOND LIMITS.SDR AUS20011292Blade · cracked(AUS) BLUE MAIN ROTOR BLADE CRACKED AT THE ROOT END TRAILING EDGE.SDR CA011210001Panel · inoperative(CAN) PRESSURE REFUELING CONTROL PANEL WILL NOT PERMIT SINGLE POINT REFUELING TO BE CARRIED OUT.SDR AUS20011267Actuator · leaking(AUS) RT MAIN LANDING GEAR ACTUATOR HYDRAULIC UNIT FAULTY.SDR AUS20011001Engine · malfunctioned(AUS) NR 1 ENGINE AUTOMATICALLY REDUCED POWER TO IDLE. INVESTIGATION COULD FIND NO FAULTS. ENGINE WAS GROUND RUN AND TEST FLOWN WITH ALL SYSTEMS OPERATING CORRECTLY. AIRCRAFT RETURNED TO SERVICE.SDR AU010124Fuel Control · faulty(AUS) NR 2 ENGINE FUEL CONTROL UNIT FAULTY.SDR AU010140Structure · cracked(AUS) TAIL BOOM CRACKED IN AREA OF PYLON DECK.SDR AU010226Stator · cracked(AUS) ENGINE FIRST STAGE TURBINE NOZZLE GUIDE VANE INNER RING CRACKED.CRACK RAN FOR APPROXIMATELY 270 DEGREES OF CIRCUMFERENCE.SDR AU010009Fuel Control · malfunctioned(AUS) NR 1 ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND THE PPNG OF THE FCU INTERNAL CIRCUIT TO BE OPEN CIRCUITED.SDR AU001245Smoke Detector · faulty(AUS) BAGGAGE BAY SMOKE DETECTOR FAULTY. HEATER HOT AIR VALVE STUCK INOPEN'' POSITION.SDR AU001181Warning System · faulty(AUS) LANDING GEAR WARNING LIGHTS ILLUMINATED DURING DESCENT. THE LANDING GEAR WAS CONFIRMED DOWN. INVESTIGATION OF THE WARNING SYSTEM COULD FIND NO FAULTS. AIRCRAFT RETURNED TO SERVICE.SDR AU001182Landing Gear · failed(AUS) LANDING GEAR WOULD NOT EXTEND. THE GEAR WAS EXTENDED USING THEEMERGENCY SYSTEM. INVESTIGATION COULD FIND NO FAULTS BUT THELANDING GEAR CONTROL PRINTED CIRCUIT BOARD WAS CHANGED AS A PRECAUTION.SDR AU001180Transmission · making metal(AUS) MAIN TRANSMISSION MAGNETIC PLUG AND OIL FILTER CONTAMINATED WITHMETAL.SDR AU000303Harness · faulty(AUS) NR 1 ENGINE N1 HARNESS FAULTY.SDR AU000114Transmission · contaminated(AUS) MAIN TRANSMISSION MAGNETIC PLUG AND OIL FILTER CONTAMINATED WITH METAL.SDR AU000138Transmission · contaminated(AUS) MAIN ROTOR GEARBOX CHIP DETECTOR METAL CONTAMINATION. THERE WAS NO METAL IN THE OIL FILTER. INVESTIGATION FOUND THE CONTAMINATION TO BE WITHIN LIMITS AND FOLLOWING A GROUND RUN AND HOVER CHECKS, THE AIRCRAFT WAS RETURNED TO SERVICE.SDR AU000100Windshield · cracked(AUS) RIGHT HEATED WINDSHIELD CRACKED WITH A BURNING SMELL COMING FROM THE BASE OF THE WINDSHIELD. INVESTIGATION FOUND THAT THE RESISTORS IN THE WINDSHIELD WERE DEFECTIVE.SDR AU000085Gearbox · corroded(AUS) MAIN ROTOR GEARBOX LEAKING OIL FROM THE AREA OF THE ROTOR BRAKE ATTACHMENT LUGS. INVESTIGATION FOUND CORROSION AROUND THE STAINLESS STEEL SLEEVE.SDR AU990545Circuit Board · faulty(AUS) NR 2 ENGINE ELECTRONIC CONTROL UNIT (ECU) CHANNEL SELECTOR PRINTED CIRCUIT BOARD FAULTY.SDR AU990151Transmission · making metal(AUS) MAIN ROTOR GEARBOX METAL CONTAMINATION. PART TC: 1,704.SDR AU981162Harness · failed(AUS) NR 1 ENGINE NTL HARNESS FAULTY. PART TC: 6,171.
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