Turbomeca MAKILA-1A

Service difficulty reports · 57

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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.

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 FOJun 9, 2025 · N569AC · Urocop EC225LP · Turbine Engine Compressor SectionSDR 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 AIRCRAFSep 12, 2019 · N252EV · Urocop EC225LP · Main Rotor Mast/SwashplateSDR 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 OVERHAULEApr 17, 2015 · N368EV · Snias AS332L · Fuel Control/Turbine EnginesSDR 9EKA20150303010Fcu · failedDURING FLIGHT, NG SPLIT OF 2000 BETWEEN ENGS.Mar 3, 2015 · N216VA · Snias AS332L · Fuel Control/Turbine EnginesSDR 9EKA20150218009Firewall · crackedON A SCHEDULED INSPECTION, NR 2 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.Feb 18, 2015 · N368EV · Snias AS332L · Engine (Turbine/Turboprop)SDR 9EKA02022015008Firewall · crackedON A SCHEDULED INSPECTION, NR 1 ENG TO MGB FIREWALL FEED THROUGH FOUND CRACKED.Feb 2, 2015 · N708LH · Snias AS332L · Fuselage Main, BulkheadSDR CA110112007Windscreen · crackedINFLIGHT CRACKING OF OUTER LAYER. RETURN TO BASE.Jan 9, 2011 · Snias AS332L · Flight Compartment WindowsSDR 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/Dec 9, 2010 · Snias AS332L · Landing Gear Retraction/Extension SystemSDR 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.Dec 7, 2010 · Snias AS332L · Turbine Engine Air Inlet SectionSDR 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.May 19, 2009 · Snias AS332L · Main Rotor HeadSDR CA080513007Transmission · making metal(CAN) TRANSMISSION CHIP LIGHT ILLUMINATION. FERROUS METAL CHIPS, WHISKERS AND FLAKES FOUND IN FILTER AND SUMP AND ON CHIP DETECTOR.May 6, 2008 · Snias AS332L · Main Rotor GearboxSDR 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. RECORJul 14, 2007 · Snias AS332C · Main Rotor GearboxSDR 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 RETURApr 16, 2007 · Snias AS332L · Passenger/Crew DoorsSDR 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 BApr 18, 2006 · Snias AS332L · Engine Mount SectionSDR 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.Mar 14, 2006 · Snias AS332L · Main Rotor Drive SystemSDR 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 NRJan 27, 2006 · Snias AS332L · Ice/Rain Protection System WiringSDR 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 Nov 22, 2005 · Snias AS332L · Tail Rotor HeadSDR 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 Oct 16, 2005 · Snias AS332L · Engine/Transmission CouplingSDR 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.Jul 2, 2005 · Snias AS332L · Main Rotor HeadSDR 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 ENGINEJun 2, 2004 · Snias AS332L · Engine Mount SectionSDR 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 Apr 30, 2004 · Snias AS332L · Tail Rotor Control SystemSDR 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.Apr 29, 2004 · Snias AS332L · Turbine Engine Reduction GearSDR 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. NOJan 30, 2004 · Snias AS332L · Main Rotor GearboxSDR ERAA092665G Switch · sticksG SWITCH STICKS, REPLACED G SWITCH AND TESTED ELT IAW ARTEX PROCEDURES (4090, 1401. 4091) REINSTALLED BATTERY PACK ELT MEETS ALL SPECIFICATIONS.Dec 8, 2003 · N171EH · Snias AS332C · Emergency Locator BeaconSDR AUS20030952Engine · making metal(AUS) NR 1 ENGINE REAR BEARING CHIP DETECTOR CONTAMINATED WITH METAL.Sep 12, 2003 · Snias AS332L · Engine (Turbine/Turboprop)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.Aug 29, 2003 · Snias AS332L · Tail Rotor GearboxSDR AUS20030357Wire Harness · faulty(AUS) NR 1 ENGINE NH HARNESS INTERNAL FAULT (OPEN CIRCUIT).Mar 20, 2003 · Snias AS332L · Engine Indicating System WiringSDR 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.Jul 10, 2002 · Snias AS332L · Tail Rotor Control SystemSDR CA020125007Adjuster · cracked(CAN) PEDAL ADJUSTER LOCATION PIN SUPPORT CRACKED CAUSING THE PEDAL ADJUSTER LEVER TO BE UNMOVEABLE AND THE PEDALS UNADJUSTABLE.Jan 25, 2002 · Snias AS332L · Tail Rotor Control SystemSDR AUS20020004Rib · cracked(AUS) HORIZONTAL STABILISER ROOT RIB ASSEMBLY CRACKED BEYOND LIMITS.Jan 2, 2002 · Snias AS332L · Horizontal Stabilizer, Spar/RibSDR AUS20011292Blade · cracked(AUS) BLUE MAIN ROTOR BLADE CRACKED AT THE ROOT END TRAILING EDGE.Nov 30, 2001 · Snias AS332L · Main Rotor BladesSDR CA011210001Panel · inoperative(CAN) PRESSURE REFUELING CONTROL PANEL WILL NOT PERMIT SINGLE POINT REFUELING TO BE CARRIED OUT.Nov 27, 2001 · Snias AS332L · Fuel StorageSDR AUS20011267Actuator · leaking(AUS) RT MAIN LANDING GEAR ACTUATOR HYDRAULIC UNIT FAULTY.Nov 23, 2001 · Snias AS332L · Landing Gear ActuatorSDR 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.Sep 7, 2001 · Snias AS332L · Engine (Turbine/Turboprop)SDR AU010124Fuel Control · faulty(AUS) NR 2 ENGINE FUEL CONTROL UNIT FAULTY.Feb 6, 2001 · Snias AS332L · Fuel Control/Turbine EnginesSDR AU010140Structure · cracked(AUS) TAIL BOOM CRACKED IN AREA OF PYLON DECK.Jan 19, 2001 · Snias AS332L · Rotorcraft Tail BoomSDR AU010226Stator · cracked(AUS) ENGINE FIRST STAGE TURBINE NOZZLE GUIDE VANE INNER RING CRACKED.CRACK RAN FOR APPROXIMATELY 270 DEGREES OF CIRCUMFERENCE.Jan 13, 2001 · Snias AS332L · Turbine SectionSDR AU010009Fuel Control · malfunctioned(AUS) NR 1 ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND THE PPNG OF THE FCU INTERNAL CIRCUIT TO BE OPEN CIRCUITED.Jan 4, 2001 · Snias AS332L · Fuel Control/Turbine EnginesSDR AU001245Smoke Detector · faulty(AUS) BAGGAGE BAY SMOKE DETECTOR FAULTY. HEATER HOT AIR VALVE STUCK INOPEN'' POSITION.Dec 28, 2000 · Snias AS332L · Smoke DetectionSDR 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.Dec 9, 2000 · Snias AS332L · Landing Gear Position and WarningSDR 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.Dec 9, 2000 · Snias AS332L · Landing Gear Retraction/Extension SystemSDR AU001180Transmission · making metal(AUS) MAIN TRANSMISSION MAGNETIC PLUG AND OIL FILTER CONTAMINATED WITHMETAL.Dec 8, 2000 · Snias AS332L · Main Rotor GearboxSDR AU000303Harness · faulty(AUS) NR 1 ENGINE N1 HARNESS FAULTY.Apr 14, 2000 · Snias AS332L · Engine RPM Indicating SystemSDR AU000114Transmission · contaminated(AUS) MAIN TRANSMISSION MAGNETIC PLUG AND OIL FILTER CONTAMINATED WITH METAL.Apr 13, 2000 · Snias AS332L · Main Rotor GearboxSDR 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.Feb 27, 2000 · Snias AS332L · Main Rotor GearboxSDR 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.Feb 10, 2000 · Snias AS332L · Flight Compartment WindowsSDR 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.Jan 20, 2000 · Snias AS332L · Main Rotor GearboxSDR AU990545Circuit Board · faulty(AUS) NR 2 ENGINE ELECTRONIC CONTROL UNIT (ECU) CHANNEL SELECTOR PRINTED CIRCUIT BOARD FAULTY.Apr 24, 1999 · Fuel Control/Turbine EnginesSDR AU990151Transmission · making metal(AUS) MAIN ROTOR GEARBOX METAL CONTAMINATION. PART TC: 1,704.Feb 14, 1999 · Snias AS332L · Main Rotor GearboxSDR AU981162Harness · failed(AUS) NR 1 ENGINE NTL HARNESS FAULTY. PART TC: 6,171.Sep 11, 1998 · Snias AS332L · Turbine Section
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