Turbomeca ARRIEL-2B1
Service difficulty reports · 757
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 = 'ARRIEL2B1' 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 = 'ARRIEL2B1' 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 HDNA2016F00137Mount Fitting · crackedCRACK FOUND ON THE RT HORIZONTAL STABILIZER LOWER MOUNT FITTING.SDR 2016FA0000177Shutoff Valve · rotatedDURING OPS CHECK OF EMERGENCY FUEL SHUTOFF VALVE, DISCOVERED THE SHUTOFF VALVE LEVER CONTACTED THE LT MGB SUSPENSION BAR. RE-CLOCKING THE FUEL SHUTOFF VALVE PROVIDED SUFFICIENT CLEARANCE FOR NORMAL OPERATION.SDR QMLA2016032316028Belt · overheatedAIR CONDITIONER COMPRESSOR BELT OVER HEATED & BROKEN.SDR QMLA2016032116025Support Frame · chafedTHE TRANSMISSION SUPPORT FRAME, PN 350A21-1041-143, HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE, PN 704A34-1302-23. PN 350A38-1040-20 ATTACHES TO PN 350A21-1041-143.SDR QMLA2016030916024Support Frame · chafedTHE TRANSMISSION SUPPORT FRAME, PN 350A21-1041-143, HAS CHAFING DAMAGE ON THE LOWER FLANGE, FROM AN UNSECURED CABLE, PN 704A34-1302-23. PN 350A38-1040-20 ATTACHES TO PN 350A21-1041-143.SDR QMLA2016030316017Frame · crackedA CRACK WAS FOUND DURING A 1660.22.1, 600 HR IN 24 MONTH, INSPECTION ON THE 22 DEGREE FRAME APPROX 65 MM IN LENGTH.SDR QMLA2016030116016Panel · burnedPILOT WAS PERFORMING GND RUN FOR ENG COMPRESSOR WASH, PILOT NOTICED SOME SMOKE FROM PEDESTAL SWITCH AREA & A BURNING SMELL, BLUE LIGHTS ON FUEL PUMP, TAXI & LANDING LIGHTS FLICKERED ACCORDING TO THE PILOT. ACFT WAS SHUT DOWN & DISCONNECTED THE BATTERY. REMOVSDR QMLA2016022916013Connector · dirtyTHE PILOT REPORTED THAT UPON TAKEOFF WITH CREW & PATIENT ONBOARD HE HEARD A WARNING TONE AS HE WAS CLIMBING & TRANSITIONING TO FWD FLIGHT. HE IMMEDIATELY REDUCED POWER & GLANCED AT THE CAUTION & WARNING PANEL & VEMD. THERE WAS AN EXCEEDANCE DETECTED INDICATISDR QMLA2016022316008Unknown · odorSMELL OF AN UNIDENTIFIED BURNING ODOR IN COCKPIT.SDR H4QA20160223001Servo · malfunctionedDURING FLIGHT THE PILOT REPORTED THAT HIS RT TAIL ROTOR PEDAL WOULD PRESS FWD BUT HIS LT PEDAL COULD ONLY TRAVEL TO NEUTRAL POSITION. TOWER WAS CONTACTED & A REQUEST TO PERFORM A STUCK PEDAL LANDING WAS MADE. THE ACFT LANDED SAFELY & THE ENSUING MX INVESTIGASDR CA160217003Servo · leaking(CAN) THIS IS THE 4TH SERVO TO LEAK OUT OF THE LIMIT SWITCH AREA IN THE LAST 2 MONTHS WITH VERY LITTLE TIME SINCE REPAIR.SDR QMLA2016021016023Support Frame · chafedTHE TRANSMISSION SUPPORT FRAME, PN 350A21-1041-143 HAS CHAFING DAMAGE ON THE LOWER FLANGE, FROM AN UNSECURED CABLE, PN 704A34-1302-23. PN 350A38-1040-20 ATTACHES TO PN 350A21-1041-143.SDR QMLA2015123015112Unknown · odorPILOT & CREW REPORTED STRONG BURNING RUBBER SMELL IN COCKPIT AT ENG RUN UP TO IDLE. PILOT ABORTED FLIGHT & CALLED MECHANIC. CHECKED ACFT SYS, FINDING NO OBVIOUS DEFECTS. HAD PILOT RUN ENG AT IDLE & FULL POWER WHILE CHECKING VARIOUS SYSTEMS INCLUDING BLEED ASDR QMLA2015121115110Unknown · odorDURING STARTUP AT GND IDLE, CREW REPORTED BURNING RUBBER SMELL IN COCKPIT. ACFT WAS SHUT DOWN. MECHANIC POWERED ON ALL SYSTEMS USING A POWER CART FOR APPROX 30 MINUTES. ALL COWLINGS & DOORS WERE OPENED WITH NO DEFECTS NOTED. A/C BELT SHOWED NO VISUAL EVIDESDR CA151207008Servo · leaking(CAN) ON DAILY INSPECTION CREWS NOTICED OIL FORMING ON COWLING HINGE UPON REVIEW FOUND SERVO LEAKING FROM THE TOP CAP. ALL THE SERVO`S THAT WE HAVE THAT HAVE LEAKED, ALL LEAKED FROM TOP CAP AND WERE THIS PN SERVO.SDR QMLA2015110215102Bushing · bindingAFTER INSTALLING DUAL CONTROLS & READY TO DEPART TO RETURN TO BASE FOR PILOT TRAINING, THE ACFT WAS STARTED & BROUGHT TO GND IDLE IAW EC130B4, NORMAL PROCEDURES CHECKLIST. FLIGHT CONTROLS CHECKED GOOD & FREE OF MAJOR BINDING, EXCEPT FOR SLIGHT ADDED FRICTION SDR M7KA20151102001Bearing · failedDURING CRUISE FLIGHT PILOT OBSERVED AN ENG CHIP LIGHT INDICATION ON THE CENTRAL WARNING PANEL & IAW FLIGHT MANUAL MANDATED PROCEDURES COMPLETED A ROUTINE LANDING AT THE FIRST SUITABLE LANDING SITE. THE HELICOPTER LANDED ON A SECONDARY DIRT ROAD. UPON EXAMINASDR CA151116005Elt · no test(CAN) ELT FAILED SELF TEST, LOW RF.SDR QMLA2015100615091Adapter · crackedDURING AIRWORTHINESS CHECK, FOUND MAIN ROTOR HEAD BLUE FREQUENCY ADAPTER WITH A CUT & CRACK IN THE RUBBER, AREA B, OUT OF LIMITS IAW AMM.SDR QMLA2015100115090Unknown · smokePILOT & CREW NOTICED ODORLESS SMOKE IN COCKPIT ON DEPARTURE. ACFT ELEC, AVIONICS, AIR CONDITIONING SYS, MEDICAL EQUIPMENT WERE INSPECTED & NO DEFECTS WERE FOUND. PERFORMED OPERATIONAL GND RUN OF ALL SYSTEMS & NO DEFECTS WERE FOUND. PERFORMED OPERATIONAL CHESDR QMLA2015093015089Compressor · seizedAFTER DEPARTURE, THE WHOLE CREW SMELLED A RUBBER & ELEC BURN TYPE SMELL. THE PILOT ISOLATED THE SMELL TO THE AIR CONDITIONER & TURNED OFF THE AIR CONDITIONER SYS & THE SMELL WENT AWAY. WE CONTINUED THE FLIGHT BACK TO THE BASE WITH NO OTHER INCIDENTS & COMPLESDR CA150914006Frame · damaged(CAN) PERFORMING A 1000 HOUR / 5 YEAR INSPECTION ON CARGO HOOK SWING FRAME ASSY. THE CARGO HOOK AND LOAD CELL WERE SENT OUT FOR O/H TO THE MFG. WE SENT THE FRAME AND OTHER PARTS FOR NDT INSPECTION WHICH WAS NOT A REQUIREMENT IN THE ICA DOCUMENTATION BUT WE WSDR CA150826004Pulley · worn(CAN) ON SHUTDOWN HEARD LOUD CLUNK FROM REAR OF CABIN AT APPROXIMATELY 100 RPM, PULLED ROTOR BRAKE. UPON INSPECTION NOTICED THAT THE PULLEY SYS TO HYDRAULIC PUMP WAS MISSING. LOCATED PULLEY AT REAR OF FIREWALL AS NOTED IN PICTURES. NO EFFECTS, ABNORMALITIESDR QMLA2015081001506Compressor · seizedPILOT REPORTED SMELLING SOMETHING HOT IN THE COCKPIT, NO SMOKE PRESENT. INSPECTED THE ACFT, FOUND THE AIR CONDITIONER BELT BROKEN & THE COMPRESSOR SEIZED. BELT WAS REMOVED, DRIVE LINE INSPECTED, ACFT SYS MEL'D & ACFT RETURNED TO SERVICE.SDR QMLA2015080515067Unknown · odorIN CRUISE FLIGHT TO PICK UP A PATIENT. ABOUT 5 MINUTES PRIOR TO OUR PRECAUTIONARY LANDING, THE CREW STATED THAT THEY WERE SMELLING SOMETHING THAT MIGHT BE ELEC BURNING. THE ODOR SEEMED TO FADE IN & OUT, WERE NOT SURE IF IT WAS COMING FROM THE ACFT. IT STARTSDR QMLA2015080415066Firewall · crackedDURING AAIP A1660 600 HR SCHEDULED INSPECTION, IT WAS DISCOVERED THAT THE FWD ENG FIREWALL HAD A TOTAL OF 5 CRACKS IN 4 LOCATIONS. TWO OF THE LOCATIONS ARE ON THE UPPER LT & RT BEND ADJACENT TO THE END OF THE ENG COWLING HINGE CONSISTING OF 1 CRACK EACH APPROSDR QMLA2015072715063Webbing · crackedWHILE DIAGNOSING WIRING ISSUE, LEFT FRONT BELLY PANEL WAS REMOVED & A CANOPY WEB CRACK WAS DISCOVERED.SDR CA151015011Power Supply · inoperative(CAN) POWER SUPPLY WOULD STOP WORKING AFTER 15-20 MINUTES INTO FLIGHT, THE PULSE WOULD STOP BEING GENERATED AND THE ANTI COLLISION LIGHT WOULD STAY DIMLY LIT. REPLICATED SCENARIO IN HANGAR WITH GROUND POWER ON FOR 15 MINUTES, LIGHTLY TAPPED POWER SUPPLY BOX ASDR QMLA2015072115062Skin · crackedCRACK FOUND, DURING 600 HR AIRFRAME INSPECTION, ON THE TAIL BOOM INNER SKIN AT THE AFT, LOWER CORNER OF THE RT SIDE STABILIZER OPENING, X-8610.0, Y-150.0, Z- 1847.13.SDR CA150717003Brushes · unsecure(CAN) CLIP, ATTACHING THE WIRE TO THE BRUSH SET IS HELD TOGETHER WITH A RIVET. THE RIVET HEAD BROKE CAUSING A BAD CONTACT CREATING NOISE IN THE PILOTS HEADSET.SDR CA150713008Detector · failed(CAN) ATTEMPTED TO START THE ACFT FOR A LEAK CHECK AND RUN UP AFTER THE INSPECTION, THE START SWITCH WAS SELECTED AND 1 SNAP OF THE IGNITORS WAS HEARD AND THE STARTER BARELY MADE AN ENGAGEMENT NOISE. THE VEMD SCREENS WENT OFF LINE AND THE START WAS ABORTED. SDR CA150709002Plug · cracked(CAN) ACFT SITTING IN HANGAR. CAME IN TO FIND LARGE PUDDLE OF FUEL ON FLOOR. FOUND RUBBER CAP COVERING LOWER FWD PORTION OF FUEL TANK CRACKED AND DRIPPING FUEL. FUEL TANK HOLDS 940 LBS OF FUEL AND RUBBER CAP COVERS A 1" DIAMETER OPENING. RUBBER CAP WAS 9.5 YESDR QMLA2015070215052Structure · crackedON PREFLIGHT THE PILOT REPORTED A SOFT SPOT ON THE NOSE DIRECTLY UNDER THE AIR VENT & SOME CRACKS IN THE PAINT. THE ACFT WAS GNDED & THE MECHANIC CALLED. REMOVED THE PAINT IN THE VISIBLE AREAS WHERE THE PAINT WAS CRACKING & FOUND THE CRACK TO BE THROUGH THE SDR QMLA2015061215049Unknown · odorAC IS OUT OF SERVICE FOR A PRECAUTION LANDING. DURING THE PRECAUTION LANDING FOR FUEL SMELL IN COCKPIT, THE PILOT PULLED THE EMER FUEL SHUT OFF HANDLE. ACFT REQUIRED AN INITIAL INSPECTION & REPLACEMENT OF THE BREAKAWAY EMER FUEL SHUT OFF GUARD. AFTER INSPECSDR QMLA2015052915044Fire Detector · false activation5 MILES SOUTH OF AIRPORT, THE ENG FIRE LIGHT ILLUMINATED FOR 2 - 3 SECONDS. CONTINUED & LANDED WITHOUT INCIDENT. THE AREA SOUTH HAD NO SUITABLE LANDING AREAS & THE ENG FIRE REMAINED OFF FOR THE DURATION OF THE FLIGHT. NO FURTHER ISSUES WITH THE ACFT WERE NSDR CA150601003Bushing · damaged(CAN) NEW RUBBER BUSHING THAT HOUSES THE TAILROTOR DRIVESHAFT BEARING HAS A SERIES OF MECHANICAL CUTS AROUND FLANGE. THEY ARE ONLY NOTICED WHEN BUSHING IS SQUEEZED, BEFORE INSTALLATION.SDR CA150601004Bushing · damaged(CAN) SYMETRICAL MECHANICAL CUTS ON FLANGE OF NEW RUBBER BUSHING THAT HOUSES THE T/R DRIVE SHAFT BEARING. ONLY SEEN WHEN RUBBER BUSHING IS SQUEEZED TO CHECKED FOR RUBBER FOR PLIABILITY.SDR QMLA2015052015040Stabilizer · crackedFOUND APPROX 2.5" CRACK ON UPPER RT SIDE OF HORIZONTAL STABILIZER. APPROX 4" AFT OF THE STABILIZER MOUNT.SDR HCMA2015051700001Circuit Board · defectivePILOT WAS CONDUCTING A HELICOPTER TOUR FLIGHT ON THE BIG ISLAND, AT APPROX 1325 HOURS THE PILOT HEARD A LOUD ELEC BUZZING SOUND IN HIS HEADSET THAT MADE THE RADIO COMMUNICATIONS VERY DIFFICULT, PILOT ALSO NOTICED A MOMENTARY INTERMITTENT ILLUMINATION OF THE ENSDR CA150608005Bracket · broken(CAN) DURING DAILY INSPECTION BROKEN BRACKET WAS DISCOVERED.SDR QMLA2015050515035Door · delaminatedRIGHT LATERAL CARGO HOLD DOOR HAS DELAMINATION.SDR CA150617016Bracket · cracked(CAN) BRACKET FOUND CRACKED DURING COMPLIANCE INSPECTION, PN 350A23-0762-00. ONCE ASSEMBLY 350A23-0761-00 WAS REMOVED & PRIMER REMOVED FROM THE INSIDE OF BRACKET 350A23-0763-00 ADDITIONAL CRACKS WERE FOUND. FLEET INSPECTION IS IN PROGRESS. WITHIN CURRENT FLSDR QMLA2015050315034Door · delaminatedLEFT LATERAL CARGO HOLD DOOR HAS TWO DENTS WITH DELAMINATION.SDR CA150416001Shaft · sheared(CAN) WHEN STARTER BUTTON WAS PUSHED TO INITIATE START, THE STARTER SPOOLED UP BUT THE ENGINE DID NOT TURN. THE STARTER WAS THEN REMOVED AND IT WAS DISCOVERED THE SHAFT HAD SHEARED.SDR QMLA2015040415023Test Switch · faultyTHE PILOT REPORTED A FIRE LIGHT ILLUMINATION WHILE ON APPROACH TO THE BASE. LANDED THE ACFT & VERIFIED THERE WAS NO EVIDENCE OF FIRE OR SMOKE IN ENG BAY AREA. THE MECHANIC ALSO VERIFIED THE PILOTS FINDINGS. CYCLED THE FIRE TEST SWITCH NUMEROUS TIMES & FOUNDSDR QMLA2015040515025Light · contaminatedBURNING PLASTIC SMELL IN CABIN COMING FROM OVERHEAD LIGHTING, NO SMOKE OR FIRE IN CABIN. LIGHTS TURNED OFF, CABIN VENTILATED & SMELLS DISSIPATED. GRASS WAS FOUND IMBEDDED IN OVERHEAD LIGHT FROM THE FRESH AIR VENT.SDR HDNA20150325001Indicator · faultyTRIPLE TACH INDICATOR FAILS SELF-TEST WHEN IT GETS HOT DUE TO OUTSIDE AIR TEMP BEING WARM.SDR CA150415012Cable Cutter · damaged(CAN) REPEATED DELAMINATION AND/OR CRACKING OF THE CABIN ROOF STRUCTURE REINFORCEMENT FOR UPPER CABLE CUTTER.SDR QMLA2015031415017Wire · chafedDURING TAKEOFF, THE PILOT & CREW REPORTED SMELLING & SEEING WHITE SMOKE IN CABIN. THE PILOT ABORTED THE TAKEOFF & LANDED WITHOUT DELAY. THE MECHANICS PERFORMED VISUAL SEARCHES FOR ANY EVIDENCE OF THAT WOULD CAUSE WHITE SMOKE. THE MECHANICS PERFORMED GND TESSDR QMLA201503111502Stringer · gougedDURING PREFLIGHT OF ACFT, PILOT OPENED TAIL BOOM BATTERY COMPARTMENT DOOR TO EXAMINE CONTENTS. PILOT NOTICED A SMALL GAP BETWEEN THE TWO HALVES OF THE CLOSE OUT PLATES FWD OF THE BATTERY THAT ARE VELCRO'D TO THE BULKHEAD RING. EXAMINED MORE CLOSELY & NOTICED
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