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 M7KA201210171396Bearing Race · wornHYDRAULIC PRESSURE LIGHT ILLUMINATED IN FLIGHT. RETURNED TO BASE. DURING INSPECTION, DETERMINED THE DRIVE BELT HAD DISENGAGED FROM THE HYRAULIC PUMP DRIVE PULLEY. EXAMINATION REVEALED THAT THERE HAD BEEN A LOSS OF INTERFERENCE FIT BETWEEN THE PULLY AND THESDR QMLA2012100912167Filter · missingDURING A ROUTINE 600 HR ENGINE INSPECTION, IT WAS NOTED THAT THE ENGINE INTERNAL OIL FILTER WAS MISSING. DETERMINED THAT THE ENGINE WAS OPERATED FOR THE LAST 600 HRS WITHOUT A FILTER ELEMENT INSTALLED. A NEW FILTER ELEMENT WAS INSTALLED AND THE OIL SYS WSDR QMLA2012091912156Gearbox · making metalWHILE TRANSITIONING OVER AIRPORT, TAIL ROTOR GEAR BOX CHIP LIGHT ILLUMINATED. DECLARED AN EMERGENCY AND LANDED. ON FINAL, CHIP LIGHT EXTINGUISHED. LANDING WAS WITH OUT INCIDENT. FELT NO UNUSUAL PRESSURE OR VIBRATION IN THE CONTROLS. MECHANIC FOUND AN INSISDR QMLA2012090712148Wire · shortedWHEN THE INSTRUMENT LIGHTS WERE TURNED ON SPARKS EMINATED FROM BEHIND AND BELOW THE INSTRUMENT PANEL, LANDED ON THE PILOT'S FEET AND IMMEDIATELY EXTINGUISHED. MECHANIC ADDED. INSPECTED AREA INDICATED BY PILOT FOUND WIRE FROM NVIS GOOSE NECK LIGHT CHAFED AND SDR QMLA2012090712154Bulkhead · crackedRT FWD FLOOR BULKHEAD CRACKED AJACENT TO RT FWD CANOPY FRAME ATTACH WEB.SDR CA120904008Fitting · cracked(CAN) PILOT DISCOVERED CRACKED FITTING DURING PREFLIGHT CHECK. RT UPPER CRACKED. PREVIOUSLY REPLACED SEPT. 29, 2011 AT TTAF 1216 TT ON PART 448.1 HRS.SDR CA120904005Fitting · cracked(CAN) FITTING FOUND CRACKED DURING 100 HOUR INSPECTION.SDR QMLA2012083012142Blade · brokenONE TENSION-TORSION (TT) STRAP ON TAIL ROTOR HUB, HAD ONE BROKEN BLADE FROM THE LAMINATED PACK THAT WAS DISCOVERED DURING AN INSPECTION/CLEANING OF THE TAIL ROTOR HUB. NO DISCREPANCIES WERE NOTED PRIOR TO ITS DISCOVERY DURING FLIGHT OR SHUTDOWN. THE BROKEN BSDR 2012FA0000612Switch · stuckSERVO LIGHT DOES NOT EXTINGUISH WHEN SERVO TEST SWITCH IS PRESSED. . FOUND SWITCH ON SERVO STICKINGSDR QMLA2012081912135Starter Gen · burnedGENERATOR LIGHT ILLUMINATED IN CRUISE FLIGHT FOLLOWED IMMEDIATELY BY A STRONG ODOR OF BURNING AND VISIBLE SMOKE IN THE COCKPIT. ELECTED TO LAND. STARTER GENERATOR WAS ON FIRE.SDR QMLA2012081212127Unknown · odorDURING FLIGHT, AN UNFAMILIAR ODOR WAS PRESENT IN THE COCKPIT. CREW DESCRIBED IT AS A BURNING RUBBER ODOR. ODOR WAS SHORT LIVED AND DISSIPATED SHORTLY AFTER TURNING OFF AC COMPRESSOR SWITCH. ODOR DID NOT RESURFACE AFTER SWITCHING AC SYS BACK ON. DUE TO CLOSESDR QMLA2012081212131Tray · crackedDURING 100 HOUR INSPECTION, FOUND A TOTAL OF 6 CRACKS, CHAFING ON THE LT AND RT AFT BATTERY TRAYS. APPLIED FOR, RECEIVED AND PERFORMED A REPAIR, ISSUED WITH AN 8110-3.SDR QMLA2012080512129Fire Detector · faultyDURING PRESTART CHECK, FIRE LIGHT WAS ILLUMINATED. PRESTART CHECKLIST WAS ABORTED AND MX WAS CALLED. MX TROUBLESHOT THE SWITCH AND FOUND NO DISCREPANCIES. THEY THEN REPLACED ALL 3 FIRE DETECTORS. THE FIRE LIGHT WENT OUT. NO FURTHER ISSUES OR DISCREPANCIES WERSDR QMLA2012080312126Pitch Rod · leakingTEFLON MATERIAL VISIBLE AND COMING OUT AROUND TOP AND BOTTOM CIRCUMFERENCE OF SPHERICAL BEARING OF TAIL ROTOR PITCH CHANGE LINK. DEFECT FOUND DURING ROUTINE AIRWORTHINESS CHECK. MANDATORY REPLACEMENT OF TAIL ROTOR PITCH CHANGE LINK BEFORE FURTHER FLIGHT IAW SDR QMLA2012080212125Connector · contaminatedDURING TAKEOFF, HAD A FLICKERING ENGINE FIRE LIGHT. REMOVED CONNECTOR ON ENGINE DECK, CLEANED WITH CONTACT CLEANER, SUSPECT MOISTURE, APPLIED STABILANT TO CONNECTOR REINSTALLED CONNECTOR. FIRE LIGHT FLICKED 2-3 TIMES AGAIN. APPLIED STABILANT TO CONNECTOR. SDR QMLA2012072312123Horn · crackedTAIL ROTOR PITCH CHANGE HORN CRACKED: VISIBLE FROM THE OTBD FACE OF THE TAIL ROTOR PITCH CHANGE HORN, RUNNING TANGENT FROM THE BOLT HOLE, ALONG THE EDGE THICKNESS, TO THE EDGE OF THE CONICAL INSERT ON THE INBD FACE. WITH THE ROTOR BRAKE SET AND APPLYING FORCESDR QMLA2012072012118Engine · making metalENGINE WAS INSTALLED AT ACFT TT 2647+57 ENGINE TT 3996+36. THIS ENGINE WAS RECENTLY REPAIRED. FIRST CHIP EVENT AT ACFT TT 2660+27 ENG TT 3508+56 FOUND CAT.( A) DUST. PERFORMED DRAIN AND FLUSH OF OIL SYS WITH FILTER CHANGE AT FLUSH AND AGAIN AFTER 15 MINUTES GSDR QMLA2012071012112Fairing · crackedANTI-VIBRATING DOME FAIRING FOUND CRACKED AT 2 OTBD ATTACHMENT SCREWS.SDR M7KA20120711001Starter Gen · shortedDURING A ROUTINE REVENUE FLIGHT, PILOT NOTED THAT THE ACFT VEMD HAD A YELLOW BAR WARNING UNDER THE VOLTAGE INDICATION, INDICATING LOW VOLTAGE OF 24 VOLTS. ON RESET, AN INDICATION OF 250 AMPS WITH THE RED BAR WARNING. FOUND SHORTED GENERATOR WINDINGS AND AN ESDR CA121010009Bracket · misaligned(CAN) LOWER RT PN 350A23-4223-21, 2105.9 TOTAL HOURS. HORIZONTAL FIN WAS REMOVED FROM THE TAILBOOM TO FACILITATE A PROACTIVE INSPECTION OF THE BRACKETS, PN 350A23-4223-20 & -21 AND 350A23-4222-20 & -21. ALL 4 WERE FOUND WITHOUT CRACKS, WHEN THE HORIZONTAL FISDR QMLA2012062312105Skin · crackedCRACK IN HORIZONTAL STABILIZER WITH OVERALL LENTH OF 1.49". THIS CRACK IS ON THE UPPER LT SIDE OF THE STABILIZER. IT BEGINS AT A MEASUREMENT OF 10.3125" AFT OF THE LT STABILIZER ATTACHMENT PIN AND CONTINUES AT AN APPROX 45 DEGREE ANGLE OF THE GENERAL ORIENTASDR 2012FA0000390Control Cable · dirtyPEDALS STIFF DURING FLIGHT. FOUND PEDAL CONTROL CABLES DIRTY.SDR CA120622002Guide · damaged(CAN) THE SELF-LUBRICATING TAPE ON THE SWASH PLATE GUIDE, STOVE PIPE, PN 350A37-1181-01 WAS FOUND TORN & BALLED UP INSIDE THE JOINT BALL, UNIBALL, PN 350A37-1D74-21. THE STOVE PIPE WAS FOUND TO HAVE WORN FROM CONTACT WITH THE UNIBALL TO A MAXIMUM DEPTH OF 0.0SDR HDNA201206220001Switch · failedSWITCH IS MADE OF PLASTIC AND BREAKS VERY EASY, WHERE THE LEVER ATTACHES TO THE SWITCH BODY.SDR QMLA2012042812071Warning Light · malfunctionedTHE OVER LIMIT LIGHT ILLUMINATED ON LANDING. ACCORDING TO PILOT, WAS ON ROUTE, 1 MILE OUT, IN SEMI-WINDY CONDITIONS. DID NOT PUT ACFT IN ANY ABRUPT MOVEMENTS TO CAUSE OVERSPEED CONDITION & NEVER EXPERIENCED A GONG IN HEADSET. AFTER LANDING, AT SHUTDOWN, VEMSDR 2012FA0000241Shaft · mismanufacturedCHROME SURFACE ON TAIL ROTOR OUTPUT SHAFT COMPROMISED. SURFACE AREA OF DAMAGE EXCEEDS MFG SPECIFIED LIMITS. PITTING IN THE METAL SUGGESTS THAT CORROSIVE ELEMENTS WERE PRESENT BEFORE THE CHROME PROCESS OCCURRED. THIS CORROSION CAUSED THE CHROME FINISH TO NOTSDR QMLA2012040712049Engine · odorSHORTLY AFTER TAKEOFF, AN ODOR DESCRIBED AS "BURNING CRAYONS" WAS DETECTED. SECONDS LATER, HAZE WAS VISIBLE IN THE CABIN. A PRECAUTIONARY LANDING WAS EXECUTED AND A NORMAL SHUTDOWN CONDUCTED. THERE WERE NO OBVIOUS INDICATIONS AS TO THE ORIGIN OF THE SMELL SDR 2012FA0000263Sending Unit · looseWHEN PERFORMING A 600 HR INSPECTION, THE MECHANIC NOTED, NO SAFETY WIRE PRESENT ON THE SCREWS SECURING THE SENDING UNIT TO THE TANK. THIS IS THE ACFT FIRST SCHEDULED 600 HR INSP. THIS DEFECT WOULD HAVE HAD TO OCCUR DURING THE ASSEMBLY PROCESS. A MORE COMPRESDR 2012FA0000191Control Panel · unserviceableON OTBD FLIGHT 30 ALPHA PANEL PRODUCED AN ELECTRICAL CHEMICAL SMELL, PERFORMED INSP ON PANEL, SN PO29433 AND FOUND ANTI-COLLISION CIRCUIT INOPERTIVE. REPLACED 30 ALPHA PANEL WITH SN PO15420.SDR 2012FA0000259Flange · damagedWHEN PERFORMING A 600 HR INSPECTION OF THE ACFT, THE MECHANIC PERFORMING THE INSP OF THE TAIL ROTOR FLANGES AND FLEXIBLE COUPLINGS NOTICED A SCORE ON THE FLANGE IN THE ATTACHMENT AREA. ACCORDING TO OEM CRITERIA, SCORES ARE CAUSE FOR REJECTION IN THIS AREA. ASDR CA120416006Starter Gen · failed(CAN) DURING A START ON THE GROUND, THE STARTER GENERATOR PRODUCED A LARGE AMPERAGE DRAW, AND STARTED SMOKING. THE START WAS ABORTED BY THE PILOT. UPON DISASSEMBLY, IT WAS FOUND THAT THERE WAS CONTINUITY BETWEEN ALL THE TERMINALS ON THE STARTER, HOWEVER, THE SDR 2012FA0000226Sensor · misinstalledINTERMITTENT FLUCTUATIONS ON NR GAUGE DURING OPERATION. FOLLOWED TROUBLESHOOTING STEPS AND FOUND NR TACH SENSOR TO BE IMPROPERLY SHIMMED BY MFG CAUSING CONTACT OF THE SENSOR AND THE PICK UP TEETH ON THE MAIN ROTOR MAST, DAMAGING THE NR TACH SENSOR AND MAIN ROSDR UNFR20120100003Attach Fitting · brokenDURING AN INSPECTION, HORIZONTAL STAB WAS REQUIRED TO BE REMOVED. UPON REMOVAL, THE UPPER LT MOUNT FITTING WAS FOUND BROKEN COMPLETELY IN HALF. AN EDDY CURRENT INSPECTION OF THE AREA RESULTED IN THE DISCOVERY OF THE UPPER RT FITTING BEING CRACKED ALSO.SDR CA120221013Nut · backed out(CAN) FLANGE ROCKING ON SPLINES. RETAINING NUT APPEARS TO BE BACKED OFF ENOUGH TO ALLOW FLANGE MOVEMENT.SDR CA120127006Link Assy · misinstalled(CAN) DURING 600 HR INSPECTION, YAW PETENSIOMETER LINK FOUND IMPROPELY INSTALLED, AMM 76-11-04, REMOVAL, INSTALLATION, ADJUSTMENT INSTRUCTIONS DOES NOT ILLUSTRATE THE PROPER ASSEMBLY OF LINK, ITEM 7, WHETHER OT IS ASSEMBLIES ABOVE OR BELOW THE LEVER ASSY, ITEMSDR 2012FA0000073Magnetic Seal · leakingOIL FOUND ON ENGINE DECK DURING ALF CHECK. LEAK WAS DETERMINED TO COME FROM THE FRONT MAGNETIC SEAL OF THE FREEWHEEL SHAFT. LEAK RATE WAS MEASURED AT 11.94 ML/H. MAX LEAK RATE ALLOWED IS 10 ML/H AS SPECIFIED IN MFG TROUBLESHOOTING BOOK 71-00-06-816-804-B01.SDR 2012FA0000074Ground Wire · brokenPITOT LIGHT ON CAUTION PANEL NOT FUNCTIONING. FOUND GROUND WIRE FOR THE PITOT LIGHT CIRCUIT TO BE BROKEN. WIRE DID NOT HAVE THE SLACK REQUIRED WHEN INSTALLED, PLACING A STRAIN ON THE WIRE WHICH BROKE DURING OPERATION OF THE ACFT. RECOMMEDN IMPROVEMENTS IN QSDR QMLA2012011212004Module · defectiveDURING ROUTINE ENGINE INSPECTION OF THE MAGNETIC CHIP DETECTORS, THE OIL CHECK VALVE FOR THE MAGENETIC CHIP DETECTOR FOR THE M05 MODULE WOULD NOT CLOSE. REMOVED THE HSG ASSY AND FOUND A METAL TAB STUCK TO THE CHIP DETECTOR. THIS ACFT IS CURRENTLY OUT OF SERVSDR QMLD201112284761Blade · brokenHP TURBINE BLADE LOCK BROKEN.SDR QMLA2011121711120Switch · failedPILOT UPON LANDING, PROCEDED W/ NORMAL ENGINE SHUTDOWN. AFTER ROLLING TWIST GRIP TO IDLE POSITION, AMBER GOV LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN. FAILURE DETECTED ON VEMD, TEST REF 121 W/ LRU ENG START SWITCH LISTED AS FAILED. SWITCH WAS REPLACED. GROUNDSDR QMLD201112054591Guide Vane · crackedWHILE DISASSEMBLING ENGINE TO PERFORM MODIFICATION TU 166 FOUND THE POWER TURBINE NOZZLE GUIDE VANE CRACKED. MODULE 3 MUST BE RETURNED TO MFG FOR REPAIR.SDR CA120904004Fitting · cracked(CAN) UPPER ATTACH FITTING LT SIDE REPLACED WITH NEW PART, PN350A23422221.SDR QMLA2011102611106Tube · blockedDURING CLIMB, NOTIFIED OF SOME SMOKE TO THE LT SIDE OF THE COCKPIT NEAR THE DEMISTING VENT. SMOKE SLIGHT & APPEARED TO BE CONTINUOUS. VERIFIED NO VISIBLE FIRE OR SPARKS, & ALL ENGINE PARAMETERS NORMAL. CONFIRMED THE HEATING & DEMISTING KNOBS WERE CLOSED. SDR QMLA2011101211098Clutch · brokenDURING FLIGHT OPERATIONS FLIGHT CREW STATED THAT WHEN THEY ENGAGED THE AIR CONDITIONING THERE WAS AN ELECTRICAL TYPE SMELL AND WHEN THE AIR CONDITIONING WAS DISENGAGED THE SMELL WOULD DISIPATE . THE ACFT DID NOT HAVE ANY WARNINGS OR CAUTIONS SO THEY PROCEEDED SDR VY1R201110120710Seal · misinstalledFUEL LEAKING FROM HP PUMP OVERBOARD DRAIN. FUEL AMOUNT BEYOND SPECIFIC LIMIT. REPLACEMENT OF THE VARLIP SEAL WAS NECESSARY. THE SEAL HOUSING APPEARED TO BE INCORRECTLY SEATED IN THE HMU WHICH RESULTED IN THE SEAL BEING DESTROYED BY THE PRESSURE ON THE SHAFTSDR VY1R201110120711Bushing · leakingFOUND FRONT AND REAR MAGNETIC SEAL OF THE FREEWHEEL SHAFT LEAKING. FRONT SEAL WAS LEAKING BEYOND LIMITS. BELIEVED TO BE CAUSED BY M/R AND T/R IMBALANCE.SDR 2011FA0000712Seal · leakingFOUND FRONT AND REAR MAGNETIC SEAL OF THE FREEWHEEL SHAFT LEAKING. FRONT SEAL WAS LEAKING BEYOND LIMITS. BELIEVED TO BE CAUSED BY M/R AN T/R IMBALANCE.SDR 2011FA0000713Shaft · mismanufacturedAFTER INSTALLATION OF REPAIRED TAIL ROTOR ASSY, A VIBRATION CHECK AND BALANCE CHECK OF THE "SHORT SHAFT" IS REQUIRED. THE BALANCE WAS OUT BY A CONSIDERABLE AMOUNT AND AS THESE PART WERE NEVER REMOVED OR ALTERED DURING THE REPLACEMENT OF THE TAIL ROTOR ASSY, ISDR 2011FA0000714Rotor · out of balanceAFTER INSTALLATION OF REPAIRED TAIL ROTOR, A MAIN ROTOR TRACK AND BALANCE WAS REQUIRED AND CONDUCTED. BOTH THE TRACK AND THE BALANCE OF THE MAIN ROTOR SYS WAS FOUND TO BE OUT OF LIMITS. THE ONLY MX PERFORMED ON THIS SYS WAS THE RE-TORQUE REQURIED AFTER THE ASDR 2011FA0000715Blades · defectiveMECHANIC CONDUCTING DAILY INSPECTION OF THE TAIL ROTOR ASSY HEARD "CRUNCHING" SOUNDS WHEN FLEXING THE BLADES. A BOROSCOPE INSP OF THE INTERNAL CUFFS REVEALED FIBERGLASS FIBERS PROTRUDING FROM THE SPAR AND A CRACK THROUGH THE RUBBER BLOCK AND INTO THE BLADE IN
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