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 QMLA2010121010080Bearing Race · debondedMAST BEARING INNER RACE HAS BECOME DEBONDED FROM THE MAIN ROTOR SHAFT. MAIN ROTOR SHAFT WAS REMOVED AND SENT FOR REPAIR. INSTALLED SERVICEABLE SHAFT TO RETURN ACFT TO SERVICE. DO NOT KNOW WHAT HAS CAUSED THE INNER RACE OF THE MAST BEARING TO DE-BOND AND SPISDR RMXA101206110458Unknown · odorA BURNING ODOR WAS DETECTED IN THE COCKPIT DURING AN AIR AMBULANCE FLIGHT 10 MINUTES OUT. CREW MEMBERS CONFIRMED ODOR. ATC CONTACTED AND ADVISED OF THE EVENT AND FLIGHT DIVERTED. MX SEARCHED ACFT FOR EVIDENCE OF BURNING, NOTHING WAS FOUND. PERFORMED A 20 MSDR CA110105004Seal · leaking(CAN) WITHIN LIMITS BUT UNECESSARY THIS SEEMS RELATED TO OIL TYPE MOST OF THE LEAKS START WHEN THE OIL IS CHANGED FROM SUMMER TO WINTER OILS. OUR BEST RESULTS OF NO LEAK IS WITH MOBIL 254 MIL-L-23699 WHICH IS ONLY APPROVED FOR SUMMER OPERATIONS. WHEN WE CHANGSDR QMLDMG1501Structure · chafed(QMLD) DURING INSP OF THE ACFT, FOUND A CHAFE OF THE RT HORIZONTAL STABILIZER OPENING CAUSED BY THE BONDING BRAID. THE MM STATES TO CONTACT ECD OR REPRESENTATIVE FOR REPAIR. AEC HAS BEEN CONTACTED AND WE ARE AWAITING A REPAIR SCHEME.SDR QMLRMD7271Support Angle · burredFLOOR NUTPLATE CAME LOOSE WHILE INSTALLING A SCREW AND DAMAGED THE SUPPORT RIB. DURING THE INSTALLATION OF A LITTER LOADING ATTACHMENT SCREW INTO A NUTPLATE IN FLOOR IN CABIN AREA, LT SIDE OF ACFT, RIVETS RETAINING THE NUTPLATE SHEARED. THE NUTPLATE SUBSEQUESDR 2010FA0001224Compressor · seizedPILOT REPORTED, DURING NORMAL FLIGHT, AIR COND SYS BEGAN TO BLOW WARM AIR FOLLOWED BY HYD SYS WARNING LIGHT ILLUMINATION. DUAL HYD SYS ALLOWED PILOT TO PERFORM PRECAUTIONARY LANDING WITHOUT INCIDENT. POST FLIGHT INVESTIGATION REVEALED THAT BOTH THE A/C COMPRSDR RMXA2010F00240Pitch Link · delaminatedUPON ARRIVING TO CRUISE FLIGHT A LOW FREQUENCY VIBRATION BEGAN AND LASTED APPROX 20 MINUTES AND THEN DISAPPEARED FOR THE REMAINDER OF THE FLIGHT.SDR QMLA2010111110075Bearing Race · debondedMAST BEARING INNER RACE HAS BECOME DEBONDED FROM THE MAIN ROTOR SHAFT.SDR QMLA2010111110076Unknown · smokeTHE PILOT AND MEDICAL CREW BOTH REPORTED SEEING AND SMELLING SMOKE IN THE COCKPIT DIRECTLY AFTER TAKEOFF. THE PILOT THEN CYCLED THE DEMISTER/HEATER VALVES WITH NO CHANGE. HE THEN MADE AN UNSCHEDULED LANDING. MX WAS NOTIFIED AND RESPONDED IMMEDIATELY. THE MESDR 2010F00243Connector · dirtyAMBER GOV CAUTION MESSAGE APPEARED FOR APPROX 2-3 SECONDS IN FLIGHT 2 MILES OUT FROM LANDING IN COVENANT MEDICAL CENTER. ON SHUTDOWN ACFT DISPLAYED A (FAILURE DETECTED) MESSAGE. MX WAS NOTIFIED AND A MECHANIC WAS SENT TO THE ACFT. THE ACFT WAS PARKED TO THE FSDR 2010FA0001198Seal · unserviceableSEAL WAS LEAKING - HAVE NOTICED AN INCREASE IN T/R GEARBOX SEAL FAILURES.SDR QMLA2010102110068Anode Terminal · meltedCREW REPORTED SEEING SMOKE COMING FROM CABIN CENTER OVERHEAD LIGHT, ACCOMPANIED BY ELECTRICAL BURNING SMELL. CREW MEMBER TURNED OUT LIGHT IMMEDIATELY, SMOKE AND SMELL WENT AWAY. PILOT NEITHER SMELLED THE ELECTRICAL BURNING SMELL NOR SAW ANY SMOKE. REMOVED OSDR CA101018004Potentiometer · erratic(CAN) A FAILURE CODE ON THE VEMD INDICATED A COLLECTIVE POTENTIOMETER MALFUNCTION ON ONE FLIGHT, ALSO THE PILOT REPORTED THAT DURING CRUISE THE COLLECTIVE INPUT TO THE ENGINE DID NOT RESPOND IMMEDIATELY AND CAUSED THE A/C TO TWITCH.SDR QMLA2010092610063Fire Detector · dirtyTHE PILOT REPORTED AN ENGINE FIRE LIGHT ON ENGINE START. AFTER SHUTDOWN, THE PILOT NOTIFIED THE MECHANIC WHO DETERMINED THAT THE FIRE DETECTOR THAT WAS MOUNTED TO THE M05 HAD A DIRTY CONNECTOR. THE MECHANIC CLEANED THE CONNECTOR AND PERFORMED ANOTHER ENGINE SDR CA100913008Glare Shield · malfunctionedTHE 4 ALPHA PANEL. DURING FLIGHT TRAINING INVOLVING EMERGENCY PROCEDURES IT WAS NOTED THAT SOME PILOTS CANNOT SEE THE CAUTION PANEL LIGHTS ILLUMINATE. SIMULATED EMERGENCIES ARE NOT DETECTED BY SOME TALLER PILOTS. THE INSTRUMENT PANEL HAD BEEN REWORKED AT PRSDR CA101015002Ball Joint · loose(CAN) BALL JOINT P/N EN2023S06E FOUND LOOSE IN CRIMPING RIVET.SDR CA100830003Crosstube · crackedWHILE CARRING OUT A DAILY INSP, THE AME NOTICED A CRACK IN THE PAINT ON THE FWD CROSSTUBE LT SADDLE WHERE IT ATTACHES TO THE SKIDTUBE. PAINT REMOVED AND A CRACK IN THE CROSSTUBE SADDLE WAS VISIBLE.SDR 2010FA0000932Bracket · crackedDURING ALF INSP, MECHANIC DISCOVERED .7500" CRACK IN MRH VIBRATION DAMPENER LOWER FLANGE ASSY SIDE MOUNTING BRACKET.SDR QMLA2010081010050Indicator · failedAFTER DEPARTURE, FLI (FIRST LIMIT INDICATOR) FAILED. RETURNED TO BASE, RESET FLI. MECHANIC CHECKED FLI FOR FAILURE CODE, NONE INDICATED. FLIGHT CONTINUED TO DESTINATION.SDR QMLA2010080910052Support · crackedDURING THE 1ST 600 HR INSP OF THE MAIN ROTOR HEAD AND VIBRATION ABSORBER ASSY FOUND PN 350A 31 2023 04 TO HAVE APPROX .5" CRACK IN THE RADIUS. DISASSEMBLED VIBRATION ABSORBER AND REPLACED BRACKET PN 350A 31 2023 04 WITH TSN 0.0 REASSEMBLED VIBRATION ABSORBERSDR CA100803001Switch · unserviceableNO START CONDITION, SWITCH REPLACED AND PROBLEM SOLVED.SDR CA100706001Circuit Breaker · unserviceableA REPORT OF NO STROBE LIGHT POWER, INVESTIGATION FOUND THE BREAKER TO BE UNSERVICEABLE, THE BREAKER DID NOT TRIP. NO POWER GOING THRU BREAKER, BREAKER WAS OPENED UP FOR EVALUATION AND FOUND TO HAVE THE BI-METALIC STRIP BROKEN AND OVERHEATED. UNABLE TO ENTER SDR CA100621001Pulley · wornDURING A POST FLIGHT INSP OF THE PULLEY DRIVE ASSY, THE PULLEY DRIVE SYS WAS INSPECTED AND FOUND TO BE LOOSE. FURTHER INSP FOUND THE PULLEY ASSY, INNER BEARING SHAFT OF THE PULLEY WORN, .040", BEARING WOBBLED ON THE SHAFT.SDR CA100611001Compressor Wheel · seizedACFT LANDED AND START WAS ATTEMPTED WITH HIGH T4, START ABORTED, SECOND START WAS ATTEMPED WITH SAME RESULT ACFT REMAINED OVERNIGHT. DURING START ATTEMP THE FOLLOWING MORNING THE AXIAL COMPRESSOR WHEEL WAS FOUND SEIZED. ENGINE WAS REMOVED AND SENT FOR INVESTISDR CA100426011Pump · defective(CAN) WHILE CARRYING OUT A BRIDGING INSPECTION ON A NEW AIRCRAFT IT WAS FOUND THE HYDRAULIC PUMP SPLINES ON THE FORWARD HYDRAULIC PUMP HAD NO LUBRICATION. IT WAS ALSO MISSING THE ORING ON THE SHAFT TO HELP RETAIN THE GREASE ON THE SPLINES. REFERENCE MET 29.10SDR HCMA601EDisplay · inoperativeAT APPROXIMATELY 1.5 HOURS INTO A TOUR FLIGHT, THE PILOT NOTICED THAT LANE 1 AND LANE 2 OF THE VEMD WERE BLANK. THE PILOT ATTEMPTED TO REST THE VEMD AND IT DID NOT RESET. THE PILOT LANDED AT THE HELIPORT WITHOUT INTERRUPTING HIS TOUR. THE VEMD WAS CHANGED AND SDR QMLA2010032210009Potentiometer · unsecurePILOT REPORTED THAT, IN CRUISE FLIGHT, WHEN SLOWLY INCREASING POWER FROM 93 PERCENT NG, PILOT PERCEIVED THAT ACFT EXPERIENCED A YAW/TORQUE KICK. DURING OCCURRENCE, NO GOV LIGHTS ILLUMINATED, NOR WERE ANY GOV LIGHTS ILLUMINATED DURING SHUTDOWN, DURING NORMAL LSDR QMLA2010029010002Wire · failedELECTRICAL ODOR IN COCKPIT FOLLOWED BY A SMALL PUFF OF SMOKE FROM FWD CTR RT OF GLARESHIELD TOP. ALL ACFT SYS APPEARED NORMAL WITH NO WARNING/ CAUTION LIGHTS. ODOR AND SMOKE DIMINISHED WHEN OUTSIDE AIR VENT KNOB WAS PULLED. SUSPECT FAULTY CLOCK BACKLIGHTISDR CA100106009Bearing · worn(CAN) MAIN ROTOR HEAD BEARING WORN- NOT EXPECTED TO LAST NEXT INSP INTERVAL.SDR HCM2009F00001Gearbox · making metalACFT DEPARTED AIRPORT ON A SIGHT SEEING FLIGHT AT 11:54 AM, SHORTLY BEFORE RETURNING, AT APPROX 12:40 PM AT 1,000 FT AGL THE ENGINE "CHIP" LIGHT ILLUMINATED, THE PILOT REDUCED POWER AND WITHIN 4 TO 5 SECONDS ADDITIONAL CAUTION LIGHTS ILLUMINATED AND THE AURAL SDR CA090716004Clamp · fracturedCLAMP THAT ATTACHED REAR CROSSTUBE FAIRING FRACTURED ALLOWING FAIRING END PLATE TO WEAR A GROOVE INTO THE REAR CROSSTUBE. 6 OTHER UPPER FAIRING ATTACHMENT RIBS ALSO CRACKED.SDR CA090716005Elec Connector · out of limitsNR INDICATOR FAILURE AND NR OVER LIMIT DETECTED BY VEMD. 5 PREVIOUS INCIDENTS OF NR OVER-LIMIT OR NO INTERMITTENT LOW ROTOR AUDIBLE TONE.SDR 2009FA0000597Starflex · debondedDURING A DAILY INSP, CRACKS WERE NOTED ON MAIN ROTOR STARFLEX IN THE ADHESIVE BOND FILLET THAT BONDS BUSH ONTO THE STARFLEX ARM. THERE WAS NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN THE BUSH AND STARFLEX. UTILIZING THE PROCEDURE FROM THE MM IN CHAPTER SDR CA090703003Nut · loose(CAN) WHILE CARRYING OUT 600 HR INSP ON ACFT, WAS NOTED THAT THE MAIN ROTOR GEARBOX INPUT BEVEL NUT WAS LOOSE. THERE WAS SIGN OF FRETTING AND THE ADAPTER WAS LOOSE. THE NUT WAS REMOVED AND PINION INSPECTED NO DAMAGE. MFG WAS CONTACTED AND THE PINION WAS INSSDR 2009FA0000606Starflex · debondedDURING A DAILY INSP, CRACKS WERE NOTED ON THE MAIN ROTOR STARFLEX IN ADHESIVE BOND FILLET THAT BONDS BUSH ONTO THE STARFLEX ARM. THERE WAS NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN BUSH AND STARFLEX. UTILIZING PROCEDURE FROM THE MM IN CHAPTER 62.20.0SDR 2009FA0000605Starflex · debondedDURING A DAILY INSP, CRACKS WERE NOTED ON MAIN ROTOR STARFLEX IN ADHESIVE BOND FILLET THAT BONDS BUSH ONTO STARFLEX ARM. THERE WAS NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN BUSH AND STARFLEX. UTILIZING PROCEDURE FROM MM IN CHAPTER 62.20.00.601 PARAGSDR RMXAN5431551409Wire Harness · arcedACFT WAS ON APPROACHAND APPROX 1 MINUTE PRIOR, ENGINE YELLOW GOV LIGHT ILLUMINATED. ACFT LANDED WITHOUT INCIDENT. UPON SHUTDOWN, THE PILOT COULD NOT REDUCE ROTOR RPM BY USE OF THROTTLE SO HE OPTED TO USE THE SHUTDOWN SWITCH TO COMPLETE ENGINE SHUTDOWN. PILOT CSDR 2009FA0000364Resistor · blownA/C KIT, WITH TWO SPEED SWITCH FOR PAX COMPARTMENT, BALLAST RESISTOR BLEW, ALLOWING FOR A PRECAUTIONARY LANDING, (DUE TO BURNED ELECTRICAL ODOR) THIS RESISTOR IS THE SECOND ONE INSTALLED IN 164.8 HRS, RECOMMEND COMPLETING A LOAD ANALYSIS ON THE ENTIRE SYSTEM, SDR CA090420002Stop · brokenWHILE PILOT WAS DOING HIS POST FLIGHT INSPECTION, FOUND THAT THE STATIC STOP HAD BROKEN OFF AT THE FORGE LINE. THE PART WAS BEING HELD BY THE BONDING STAP. AIRCRAFT WAS RETURNED TO SERVICE AFTER PART WAS REPLACED.SDR 2009FA0000263Starflex · debondedDURING PRE-FLIGHT INSPECTION PILOT WAS INSPECTING STARFLEX IAW AD 2002-03-52. SEPARATION OF THE ARM END BUSHES WAS FOUND ON ALL (3) ARM ENDS. FURTHER INVESTIGATION REVEALED THAT ONE BUSHING HAD BECOME COMPLETELY DETACHED FROM THE STARFLEX.SDR 2009FA0000266Nut · misinstalledWHILE PERFORMING AN AFTER LAST FLIGHT (ALF) OF THE DAY INSP OF THE DESCRIBED HELICOPTER, IT WAS DISCOVERED THAT THE RING NUTS, (PN 350A37-1164-21, QTY 12 ) OF THE MAIN ROTOR (M/R) HEAD BOLTS WERE INSTALLED INCORRECTLY, THEY HAD BEEN INSTALLED UPSIDE DOWN AND TSDR CA090225002Hose · leaking(CAN) HYDRAULIC HOSE REPLACED 89.0 HRS PRIOR TO OTHER HOSE WITH 650.0 HRS. BOTH HOSE ASSEMBLIES HAD PIN HOLE LEAKS.SDR HCM2009F00000Windshield · brokenACFT DEPARTED AIRPORT ON A TOUR FLIGHT AT APPROX 3:20 PM, WHILE FLYING AT 2500 FT, APPROX 100 KNOTS IAS A BIRD STRUCK THE CENTER WINDSHIELD OF THE ACFT, SHATTERING THE UPPER SECTION OF THE WINDSHIELD, THE DEAD BIRD CAME INTO THE CABIN. THE PILOT IMMEDIATELY SSDR CA081212012Magnetic Seal · leaking(CAN) MAG SEAL LEAK AT INPUT SEAL OF TGB.SDR M7KA1030084134Freq Adapter · crackedDURING ROUTINE MX INSPECTION 1 OF THE 3 FRQUENCY ADAPTERS FOUND TO HAVE A CRACK IN THE ELASTOMER NEARING ITS MAXIMUM ALLOWABLE LIMITATION OF 10MM. A NEW KIT OF 3 MATCHED ADAPTERS WERE INSTALLED.SDR M7KA1026083949Freq Adapter · crackedDURING ROUTINE INSPECTION 1 OF 3 FREQUENCY ADAPTERS FOUND TO HAVE A CRACK IN THE ELASTOMER NEARING ITS MAXIMUM ALLOWABLE LIMITATION OF 10MM. A NEW KIT OF 3 MATCHED ADAPTERS WERE INSTALLED.SDR M7KA0908084266Mount Flange · crackedDURING ROUTINE INSPECTION THE MOST AFT OTBD CORNER OF THE MOUNTING FLANGE ASSEMBLY WHICH INCLUDES THE UPPER LOCKING PIN MECHANISM WAS CRACKED. A NEW ASSEMBLY WAS INSTALLED.SDR M7KA1006084142Actuator · intermittentGOVENOR LIGHT ILLUMINATES INTERMITTENTLY WITH THIS EMERGENCY BACKUP CONTROL. ACTUATOR INSTALLED.SDR M7KA1031083949Spar · crackedDURING ROUTINE 500 HOUR INSPECTION A CRACK WAS FOUND RADIATING FROM AN ATTACHMENT FITTING SCREW BORE TO THE EDGE OF THE SPAR. A NEW SPAR WAS MATCH DRILLED AND INSTALLED IAW EUROCOPTER REPAIR SCHEME.SDR M7KA1028084248Latch · wornDURING ROUTINE INSPECTION LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. HINGE ATTACHMENT BORE HAD A 1` LONG CRACK RADIATING. INSTALLED NEW LATCHES AS REQUIRED.
Back to Turbomeca ARRIEL-2B1