Turbomeca ARRIEL-1D1
Service difficulty reports · 933
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 = 'ARRIEL1D1' 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 = 'ARRIEL1D1' 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 CA100806013Starter Gen · inoperative(CAN) PILOT WAS IN A CRUISE AND THE GENERATOR WARNING LIGHT CAME ON. PILOT REDUCED POWER AND CONTINUED CRUISE. PILOT TURNED OFF ALL NON-ESSENTIAL ELECTRONICS AND RETURNED TO BASE. AFTER NORMAL ENGINE SHUT DOWN, IT WAS DISCOVERED THAT AN UNUSUAL AMOUNT OF CARBSDR 2010F00154Crosstube · crackedDURING ROUTINE 100 HR INSPECTION, FOUND MULTIPLE CRACKS IN THE AFT CROSSTUBE: RT SADDLE ATTACHING THE RT SKID TUBE. THE ACFT HAS NO HISTORY OR REPORTED INCIDENT THAT WOULD/COULD OF SUBJECTED THE CROSSTUBE TO DAMAGE.SDR CA100712008Compressor · out of positionTHIS PROBLEM IS WITH THE INSTALLATION OF AN IFS AIR CONDITIONING. VISUAL INSP REVEALED A NICK MID WAY UP THE LT AFT MGB SUSPENSION BAR. THIS IS WHERE THE IFS COMPRESSOR PULLEY AND CLUTCH ROTATES, CURRENTLY WITHIN ABOUT .1875" CLEARANCE TO THE BAR. DAMAGE TOSDR CA101102011Blades · debonded(CAN) AIRCRAFT WAS IN FOR A 100HR INSPECTION. ON INSPECTION AS PER MANUAL FOUND A SMALL AMOUNT OF DEBONDING ON THE LEADING EDGE. NO IMPACT MARKS WHERE FOUND ON EITHER BLADE. MANUFACTURER REPORT FOUND THE BLADES SCRAP DUE TO DIMENSIONAL DIMENSIONS ON ONE BLASDR QMLA2010062710024Starter Gen · malfunctionedGENERATOR LIGHT ILLUMINATED IN FLIGHT. VOLTAGE DROP. COULD NOT DUPLICATE. COULD NOT FIND CAUSE.SDR CA100610006Cap · separatedWHILE CONDUCTING AN INSP ON THE ACCUMULATORS, THE VALVE CAPS WERE REMOVED. UPON DISASSEMBLY IT WAS NOTED THAT THE SEAL AND BRASS CUP HAD SEPARATED FROM THE CAP AND BECAME LODGED IN THE VALVE ASSY. THIS RESULTED IN LOSS OF PRESSURE IN THE ACCUMULATORS. THIS COSDR CA100603005Seal · rotatedUPON REPLACEMENT OF PREVIOUSLY REJECTED NEW BEARING, TECHNICIAN DISCOVERED THAT NEWLY INSTALLED BEARING EXHIBITED THE SAME PROBLEM I.E... THE GREASE SEAL ROTATED WITH BEARING INNER RACE. BEARING REPLACED WITH ANOTHER SERVICEABLE PART.SDR QMLA2010051510013Compressor · failedCREW TOOK OFF ON A MISSION & SMELLED A BURNING ODOR. IMMEDIATELY TURNED OFF AIR CONDITIONING & RETURNED TO BASE. PILOT FOLLOWED ODOR TO LT TRANSMISSION AREA & NOTICED AIR CONDITIONING BELT HAD FAILED. TRIED TO TURN THE AIR CONDITIONING COMPRESSOR & FOUND ITSDR CA100518001Bearing · unsecure(CAN) DURING SCHEDULED INSP OF HYD PUMP DRIVE ASSY, NEW BEARING WAS ABOUT TO BE INSTALLED. TECH NOTICED THAT THE NEW BEARING`S GREASE SEAL ROTATED ALONG WITH THE INNER RACE OF THE BEARING. PART WAS REJECTED AND REPLACED WITH ANOTHER SERVICEABLE BEARING.SDR CA100512003Hose · leakingAFTER A SHORT (0.3 H) FIRST FLIGHT OF THE DAY, THE PILOT LANDS AND SHUTS DOWN NORMALLY THE ENGINE. AFTER GETTING OUT OF THE ACFT, HE DETECTS PRESENCE OF HYD OIL IN THE MAIN TRANSMISSION DECK AREA. OPENING THE COWLINGS, HE DISCOVERS A LOT OF HYD OIL ON THE EQSDR CA100428007Elt · failed(CAN) TSN-INSTALLED 21 APRIL 2008, THE ELT WAS REMOVED FROM AN AS350 FOR ANNUAL RECERTIFICATION. THE UNIT FAILED THE PERFORMANCE TEST AND THE FAULT INDICATES LOW TX POWER OUTPUT.SDR CA100428008Elt · failed(CAN) TSN-INSTALLED 28 MARCH 2008. THE ELT WAS REMOVED FROM AN AS350 AIRCRAFT FOR ANNUAL RECERTIFICATION. THE UNIT FAILED THE PERFORMANCE TEST. SELF TEST INDICATES LOW TX POWER OUTPUT.SDR CA100415005Bearing · failedON REMOVAL OF THE BEVEL REDUCTION GEAR, 2 LARGE CHIPS WHERE FOUND ON THE UPPER INSIDE SURFACE. INSPECTED THE EPICYCLIC AND FOUND ONE OF THE GEARS BEARING HAD FAILED. THIS WAS A SUPRISE TO US AS WE DID NOT HAVE ANY INDICATION THE MGB WAS MAKING METAL. NO CHISDR CA100505005Starter Gen · failedSTARTER FAILED TO ROTATE ENGINE ON STARTUP PHASE. UNIT REMOVED AND SENT TO MFG FOR A TEAR DOWN REPORT AND METAL ANALYSIS.SDR RMXA323103154Line · deterioratedUPON LAUNCHING, TO ANSWER A FLIGHT REQUEST FOR A SCENE CALL, THE MEDIC AND NURSE REPORTED A STRONG ODOR OF FUEL. ADVISED SITUATION AND LANDED THE ACFT TO INVESTIGATE. REQUESTING AGENCY HAD ELECTED TO GROUND TRANSPORT THE PATIENT AND THAT WE WERE CANCELLED ANSDR QMLA031710007Valve · contaminatedFOUND STIFF HEATER VALVE ON A DAILY AIRWORTHINESS CHECK. SPRAYED LPS 1 ON THE U JOINT LINKAGE AND WORKED HANDLE BACK AND FORTH. ON THE NEXT FLIGHT THE CREW ASKED THE PILOT FOR SOME HEAT IN THE BACK OF THE ACFT. HEAT VALVE WAS TURNED ON BY THE PILOT. THE MEDSDR RMXA3877MAR162010Skin · crackedDURING A DAILY INSPECTION BY THE MX, AN APPROXIMATE 1 INCH CRACK WAS FOUND ON THE INBD TOP SIDE OF THE HORIZONTAL STABILIZER PN 355A1305200401, SN TB4750. THE CRACK IS LOCATED ON THE RT SIDE, RADIATING OUT AND FWD FROM UNDER THE CTR SKIN APPROX 10.5 INCHES AFTSDR QMLA2010030110005Rod · bentTHE PILOTS FELT STIFFNESS IN THE FWD QUADRANT OF THE CYCLIC DURING TAKEOFF. TAKEOFF WAS ABORTED LEFT ACFT RUNNING, CHECK FOR BINDING OF THE SERVOS, NONE FOUND. ACFT SHUTDOWN, BELLY PANEL REMOVED FLIGHT CONTROLS WERE INSP AND FOUND BENT PUSH PULL TUBE. NO OTHESDR KBTR 10 0305Starflex · debondedBUSH IN END OF STARFLEX ARM (1 OF 3) FOUND LOOSE AND UNBONDED.SDR KBTR 10 0315Oil Cooler · contaminatedENGINE CHIP LIGHT ILLUMINATED DURING DESCENT FOR LANDING AT MX BASE. INSPECTED ENGINE CHIP PLUGS, FOUND METAL FUZZ ON ALL PLUGS, AND IN OIL FILTER. ALSO FOUND SAND MEDIA DEBRIS IN OIL FILTER. DURING THIS MAINT CYCLE, ENG OIL COOLER WAS REMOVED DUE LEAKAGE AT USDR 2010FA0000209Gearbox · making metalDURING A TOUR FLIGHT THAT DEPARTED AIRPORT, THE MGB CHIP LIGHT ILLUMINATD 3 MINUTES INTO THE FLIGHT. THE PILOT RETURNED TO DEPARTURE WITHOUT INCIDENT. THE MECHANIC INSPECTED THE CHIP PLUGS AND FOUND METAL ON LOWER PLUG. THE OIL WAS CHANGED AND THE CHIP PLUGSDR CA100127011Fcu · malfunctioned(CAN) WHEN ACFT WAS ATTEMPTING TO START, THE INITIAL LIGHT OFF WAS ABSENT. THIS OCCURENCE HAPPENED ONLY WHEN ACFT WAS COLD SOAKED, AND NOT ALL THE TIME. IT SEEMS TO HAVE HAPPENED WHEN THE OAT DROPPED TO AT LEAST `0 DEGREES CELSIUS. AFTER MANY TRIES OF ACCESSOSDR RMXA350R122309Belt · melted8 MILES NORTH OF HOSPITAL, PILOT AND CREW EXPERIENCED SMOKE AND FUMES INSIDE COCKPIT WHILE TRANSFERRING PATIENT. PILOT IMMEDIATELY EXECUTED EMERGENCY PROCEDURES AND LANDED THE ACFT AT THE NEAREST CLEAR AREA, WHICH WAS A GOLF COURSE FAIRWAY. THE MED CREW IMMEDISDR CA091201002Switch · unserviceable(CAN) THE HYDRAULIC SYSTEM INCORPORATES A CUT OFF SWITCH ON THE COLLECTIVE, THE HYDRAULIC TEST PUSH BUTTON DID NOT ACTIVATE THE T/R SOLENOID TO CENTER THE T/R PEDALS, THE CIRCUIT BREAKER HAD BLOWN, AND WAS REPLACED, AFTER REPLACEMENT THE CUTOFF COLLECTIVE SWITSDR CA091116011Turbine Blades · deformed(CAN) THE ENG WAS REMOVED AND INSP WAS BEING CARRIED OUT. DURING THE BOROSCOPE INSP OF THE 1 STAGE TURBINE BLADES A DEFECT WAS FOUND, LOCATED ON THE SURFACE COATING SWELLING BUT RATHER APPEARS THAT THE BLADE STRUCTURE IS DEFORMED ON THE PLATFORM OR NEAR THE ROSDR QMLA2009102509035Engine · making metalENGINE CHIP LIGHT AFTER TAKEOFF. WARNING LIGHT DID NOT EXTINGUISH, LANDED AT DOWNTOWN STL BASE, CALLED MECHANIC. MECHANIC FOUND METAL FLAKES ON LOWER ELECTRIC CHIP PLUG, AND NUMEROUS CHIPS/FLAKES IN OIL FILTER. TROUBLE SHOOTING FLOW CHART INDICATED MOCULE REPLSDR CA091021015Pressure Switch · inoperative(CAN) A/C HAD JUST CLEARED CONTROL ZONE , WHEN THE HYDRAULIC HORN AND HYDR. LIGHT ACTIVATED, HYD ISOLATION SWITCHED OFF PROCEEDED BACK TO BASE [6 MILES] LANDED WITH HYDRAULICS OFF, WITHOUT INCIDENT. MAINTENANCE CARRIED OUT. TROUBLE SHOOTING, FOUND TO BE AN INSDR QMLA0911200909030Wheel · loosePHONOLIC WHEEL FOR TORQUE SENSING FOUND LOOSE ON ENGINE POWER SHAFT DURING TROUBLESHOOTING OF AMBER GOVERNOR LIGHT ON CAUTION PANEL. POWER SHAFT IS POST TU 81A, PRE TU 122A.SDR QMLA2009090909029Unknown · odorON CLIMBOUT FROM BASE, PILOT AND CREW NOTICED AN ODOR SIMILAR TO BURNING RUBBER. ODOR WAS NOT STRONG BUT APPEARED SUDDENLY. NOTHING ON THE GROUND IN THE VICINITY OF THE ACFT WAS OBSERVED BURNING. ABORTED MISSION AT 1-2 MILES OF BASE. ODOR DISAPPEARED DURINGSDR CA090908010Yoke · crackedDURING STARFLEX CHANGE, ONE OF THE 3 YOKES WAS FOUND CRACKED. RECORDS INDICATE THAT THIS PART WAS AN ORIGINAL INSTALLATION. CLOSER INSP WILL TAKE PLACE AT 500 HR SCHEDULED INSP INTERVAL.SDR CA090910005Magnetic Seal · leakingAFTER RE-INSTALLING ENG, FOLLOWING 5 MODULES REPLACEMENT, GROUND TESTS C/O AND FOUND SATISFACTORY. TEST FLIGHT REQUIRED. AFTER START, IMPORTANT OIL LEAK AT THE AIRFRAME LT DRAIN. TAKE-OFF CANCELLED. INVESTIGATIONS SHOW LEAK COMES FROM FRONT ENG SUPPORT DRAINSDR CA090910004Engine · making metalCHIP ENGINE LIGHT BEFORE LANDING. LANDING C/O NORMALLY. CONTAMINATION ON CHIP DETECTORS. CLEANED DETECTORS. HOVER FLIGHT REQUIRED TO CHECK FOR RE-OCCURENCES. CHIP LIGHT ON AGAIN JUST AFTER TAKEOFF (IN HOVER). LANDING C/O NORMALLY. CONTAMINATION AGAIN ON TU 208SDR CA090910007Connector · failedAFTER SHUTDOWN PILOT NOTICED BURNING ODOR AND OBSERVED SMOKE COMING OUT OF RT BAGGAGE COMPARTMENT. CLOSER EXAMINATION REVEALED ELT TO BE SOURCE OF SMOKE. CARGO RESTRAINT NETTING FRAME INTERFERED WITH ELT CONNECTOR CAUSING CHAFING. FUNCTIONAL TEST OF ELT WAS SDR CA090903003Engine · flamed outENGINE FLAMED OUT DURING SURVEY FLIGHT, CONTROLLED AUTOROTATION FROM 1000 ` TO GROUND, LANDED IN A CLEAR LAKE WITHOUT ANY INCIDENT, WATER WAS ABOUT 3 FEET DEEP. MANUFACTURERS ADVISED IMMEDIATELY. ACFT TRANSPORTED TO BASE FOR FURTHER INVESTIGATION.SDR CA090813015Line · burstPART OF INCIDENT REPORT SUBMITTED BY PILOT. LINE WAS REPLACED AND ACFT GROUND RUN WITH NO FURTHER ACTION. "3 MINUTES AFTER TAKEOFF FROM AIRSTRIP, DURING CRUISE FLIGHT, AT APPROX 100KTS AND 500FT AGL THE HYD LIGHT ILLUMINATED WITH THE CORRESPONDING HORN. REDUSDR CA090810002Battery · failedDURING START THE BATTERY HOT CAUTION LIGHT ILLUMINATED, PILOT ABORTED START AND FELT THE BATTERY. THE BATTERY WAS EXTREMELY HOT TO THE TOUCH. A REPLACEMENT BATTERY WAS INSTALLED. ACFT WAS GROUND RUN. ALL ACFT SYS SEEMED TO BE OPERATING CORRECTLY AND CHARGE SDR CA090806002Wire · brokenPOSITION LIGHT FOUND UNSERVICEABLE. TROUBLESHOOTING REVEALED BROKEN WIRE TOUCHING GROUND. POSITION LIGHT SYS BREAKER DID NOT FUNCTION. POSITION LIGHT SWITCH NO LONGER SERVICEABLE.SDR CA090730010Pressure Switch · false indication(CAN) PILOT WOULD GET A HYD LIGHT OF A HYD PROBLEM. PILOT WOULD LAND AND ENGINEER WOULD TROUBLESHOOT PROBLEM. FLUID LEVEL WAS CHECKED AND HYD BELT WAS CHECKED FOR PROPER ADJUSTMENT, AND NUMEROUS OTHER POSSIBILITIES WERE CHECKED OUT. FALSE INDICATION WAS THESDR CA090723011Switch · inoperative(CAN) HYD PRESSURE WARNING SWITCH STOPPED INDICATING CHANGES IN HYD PRESSURE. DISCOVERED DURING PRE-TAKEOFF CHECKS AND THE FLIGHT WAS ABORTED AS THERE WOULD BE NO INDICATION OF HYD FAILURE IN FLIGHT.SDR CA090720002Turbine Blades · broken(CAN) DURING A ROUTINE 30 HR INSP, N2 TURBINE BLADE IS INSP IAW ALERT LETTER 2726/09/ARID/82 AND TIP AREA OF BLADE WAS FOUND MISSING. ENG WAS SENT TO FOR INSP AND REPORT TO FOLLOW.SDR 2009FA0000621Starflex · chippedDURING A DAILY INSP CRACKS WERE NOTED ON THE MAIN ROTOR STARFLEX IN THE ADHESIVE BOND FILLET THAT BONDS BUSH ONTO STARFLEX ARM AND PIECES OF THE ADHESIVE FILLET WERE MISSING. THERE WAS NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN BUSH AND STARFLEX. UTILSDR 2009FA0000607Starflex · debondedDURING A DAILY INSP, CRACKS NOTED ON MAIN ROTOR STARFLEX IN ADHESIVE BOND FILLET THAT BONDS BUSHING ONTO STARFLEX ARM. NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN BUSHING & STARFLEX. UTILIZING PROCEDURE FROM MM 62.20.00.601 PARA 7, TEST PERFORMED TO CHSDR CA090703002Bearing · crackedDURING A SCHEDULED TAIL ROTOR GEARBOX CHANGE THE PITCH LINKS WERE INSPECTED. PITCH LINK WAS FOUND TO HAVE CRACKS IN THE INNER RACE OF THE INBD ELASTAMERIC BEARING. THE RUBBER PORTION OF THE BEARING APPEARED NORMAL. THE PART IS TO BE SENT TO MFG FOR O/H.SDR 2009FA0000619Starflex · debondedDURING A DAILY INSP, CRACKS WERE NOTED ON THE MAIN ROTOR STARFLEX IN
ADHESIVE BOND FILLET THAT BONDS THE BUSH ONTO STARFLEX ARM. THERE WAS NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN BUSH AND STARFLEX. UTILIZING THE PROCEDURE FROM MM 62.20.00.601 PARSDR 2009FA0000620Starflex · debondedDURING A DAILY INSP, CRACKS WERE NOTED ON MAIN ROTOR STARFLEX IN ADHESIVE BOND FILLET THAT BONDS THE BUSH ONTO THE STARFLEX ARM. THERE WAS NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN THE BUSH AND STARFLEX. UTILIZING THE PROCEDURE FROM MM 62.20.00.601 PASDR ULXR2009061882081Duct · leakingMODULE 5 INCORPORATED TU332. LUBRICATION DUCT SEALING PROCEDURE CONTAINED IN SB A292 72 0825 (AD 2009-12-51) WAS PERFORMED AT ENGINE TOTAL TIME OF 12631.7. LUBRICATION DUCT BEGAN TO LEAK OIL AT 12699.9. MO5 REMOVED FROM SERVICE. LUBRICATION DUCT TO BE REPLSDR CA090630004Line · cut(CAN) DURING ACFT START, WHILE PERFORMING A LEAK CHECK ON THE ACFT THE AME DISCOVER A FUEL LEAK COMING FROM THE FUEL CAP LOCATION, TO DISCOVER THAT THE LEAK WAS FROM THE TRANSMISSION DECK, THE FUEL LINE HOSE WAS CUT FROM THE INSIDE AT FITTING AND SPRAYING FUESDR CA090610006Starter Gen · arced(CAN) PILOT REPORTED LOSS OF GEN IN FLIGHT AND ELECTRICAL NOISES IN THE RADIOS. GEN LIGHT DID NOT ILLUMINATE. PILOT ATTEMPTED TO RESET GEN TWICE WITH NO SUCCESS. THEN TURNED GEN SWITCH OFF AT WHICH TIME LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH WHEN ATTEMPSDR CA090423005Release Cable · damaged(CAN) NOTED DURING PAST FLIGHT INSP THAT THE "LOCK" INDICATOR WAS NOT FULLY IN THE INDEX WINDOW. AFTER REMOVING THE MANUAL RELEASE COVER IT WAS POSTED THAT THE SWAGED END OF THE MANUAL RELEASE CABLE WAS BINDING ON THE CARGO HOOK COVER. THIS INTERMITTENTLY PREVSDR CA090401014Pump · leaking(CAN) FUEL LEAK FOUND ON DAILY INSP FROM FUEL PUMP . THAT PUMP AS BEEN INSPECTED FOR 600HRS INSP. TIME SINCE INSPECTION 20.7 HRS . PUMP SENT BACK TO MFG FOR REPAIR .
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