Turbomeca ARRIEL-2B
Service difficulty reports · 332
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 = 'ARRIEL2B' 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 = 'ARRIEL2B' 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 HCM2004F00002Servo · intermittentDURING STARTUP, THE PILOT NOTICED THAT THE CYCLIC CONTROL WAS STIFF IN THE FORE/AFT POSITION. HE ATTEMPTED TO ADJUST THE FRICTION AND FOUND IT RELEASED. THE CYCLIC CONTROL JUMPED FORWARD. AS HE PULLED BACK, HE FELT THE CONTROL APPEARED TO BE INTERMITTENT ANSDR Z1RA097452Shield · crackedCONTAINMENT SHIELD CRACKED. REPLACED ITEM IAW TURBOMECA S/B 292722022 TU 22.SDR Z1RA097453Turbine · crackedCONTAINMENT SHIELD CRACKED. REPLACED ITEM I/A/W TURBOMECA S/B 292722022 TU 22.SDR M7K2004F00008Drive Shaft · looseSUBSEQUENT TO THE DISCOVERY OF A VERY LOOSE COUPLING ON ANOTHER COMPANY AIRCRAFT, A SPECIAL INSPECTION OF OUR OTHER LIKE MODEL AIRCRAFT WAS INITIATED. THIS AIRCRAFT HAD TWO (2) OF THE SIX (6) SPECIAL ATTACHMENT RIVETS JUST BEGINNING TO LOOSEN WHEN A LITTLE MOSDR M7K2004F00009Drive Shaft · failedDURING ROUTINE MAINTENANCE INSPECTION OF THE TAIL ROTOR DRIVESHAFT, CENTER SECTION, AFT COUPLING RIVETED ATTACHMENT ONE OF THE SPECIAL RIVET SUPPORT BLOCKS WAS FOUND TO BE NOT SQUARE TO SHAFT CENTERLINE. FURTHER DETAILED EXAMINATION SHOWED ENTIRE COUPLING MOVSDR CA040913002Torquemeter · loose(CAN) THE RESULTS FROM A ROUTINE POWER CHECK ON ENGINE SHOWED A BAD TORQUE MARGIN. OTHER PARAMETERS WERE CONSISTENT WITH PREVIOUS POWER CHECKS. TROUBLESHOOTING REVEALED A MISPLACED OR MISSING PIN ON TORQUEMETER REFERENCE SHAFT. DURING TROUBLESHOOTING, WASHERSDR CA040624004Holder · loose(CAN) AC HAS THREADED TYPE FUSE HOLDERS. IN CRUISE, LOST OIL PRESSURE INDICATION ON NR 2 ENGINE. LOW PRESSURE LIGHT DID NOT COME ON, (IT'S ON A SEPARATE PRESS SWITCH). PILOT REDUCED NR 2 ENG TO IDLE. TEMP REMAINED NORMAL WITH NO OTHER CHANGES IN SYSTEMS. AN SDR CA040521005Warning Light · illuminatedMAY 15TH THE PILOT IN COMMAND NOTED A RED GOV WARNING LIGHT AT 700 FEET ABOVE GROUND. HE ELECTED TO LAND ON A SAND BAR AND NOTED IN THE DESCENT THE MAIN ROTOR RPM EXCEEDED THE MAX LIMIT. A LANDING WAS CARRIED OUT WITH NO INJURIES TO PERSONS. THE HELICOPTER SDR CA040527001Transducer · shortedAFTER MAIN ROTOR GEAR BOX REPLACEMENT GROUND RUN WAS ACCOMPLISHED, HOWEVER NO INDICATION WAS PRESENT. DISCOVERED AFTER CONTINUITY CHECKS THAT THE TRANSDUCER WAS OPEN CIRCUIT. REPLACED PART INDICATION NORMALSDR HXSD2004517Blade · crackedINSPECTOR FOUND CRACK IN TAIL ROTOR PROTRUDING OUT OF RIVET LOCATION ON TRIM TAB. CRACK WAS FOUND DURING INSPECTION IAW AD 2001-26-55. (AL05200402466)SDR CA040504006Wire · severed(CAN) ROUTINE TROUBLESHOOTING FOR INOPERATIVE NAV LIGHT STARBOARD, DISCOVERED POSITIVE WIRE WAS SEVERED FROM CRIMPED PIN BY SLIGHTLY TUGGING ON WIRES FROM THE BACKSHELL. SINCE NO ACCESS AVAILABLE TO REMOVE BROKEN OFF PIN OUT OF LAMP ASSEMBLY, A NEW ASSEMBLY HSDR PG9R117586Starter Gen · failedUNIT FAILED TO START AIRCRAFT. (RMA NR R047877)SDR CA040401007Blade · cracked(CAN) DURING DAILY INSPECTION AND DAILY COMPLIANCE WITH AD 2001-640-089(A), A CHORDWISE CRACK WAS DETECTED APPROXIMATELY 3 INCHES IB OF THE BLADE-TIP.SDR YLYL093965Commutator · failedBRUSHES FAILED PREMATURELY. DAMAGED COMUTATOR.SDR CA040310002Seat Belt · inoperative(CAN) SHOULDER HARNESS INERTIA REEL ON COPILOT'S SEAT WOULD NOT RETRACT AFTER FULL EXTENSION. THE PN SPECIFIED IN 9B APPLIES TO THE 4 POINT HARNESS ON ENERGY ABSORBING STYLE OF SEAT.SDR ALG2004F00011Screw · crackedON DAILY INSPECTION, FOUND THREE SCREW HEADS CRACKED ON THE MAIN ROTOR BLADE TIP CAP INSTALLED ON THE BLUE BLADE. MAINTENANCE REMOVED AND REPLACED THE THREE SCREWS. DURING REPLACEMENT OF THE SCREWS MAINTENANCE FOUND TWO MORE SCREWS WITH CRACKS IN THE WITH NESDR PG9R118897Windshield · crackedWINDSHIELD CRACKED. SCRAPPED (RMA NR R047070)SDR PG9R118895Intake · crackedAIR INTAKE CRACKED WITH ONLY 531.8 HOUR. (RMA NR R046964)SDR PG9R118892Tube · crackedTUBE OIL AIR VENT CRACKED. (RMA NR R046856)SDR PG9R118894Intake · crackedAIR INTAKE HAS A CRACK. (RMA NR R046894)SDR M7K2004F00000Tube · crackedENGINE OIL AIR VENT TUBE POSITIONED ALONG THE RT SIDE OF THE ENGINE WITH THE AFT END CURVED UPWARD INTO THE ENGINE EXHAUST AS TO AID THE VENTURI SECTION OF THE OIL AIR VENTING HAS A WELDED CLAMP SUPPORTED BY A STRAP HANGING FROM THE ENGINE TAILPIPE TO PREVENT SDR M7K2004F00001Fastener · sheared1 OF 4 LATCHES ON THE ENGINE FAIRING, THE LATCH HOOK SHEARED AT THE BASE OR CONTACT POINT IN THE HOOK AND EXAMINATION SHOWED NO APPARENT WEAR JUST A SHEAR BREAK LINE WITH SOME CRYSTALIZATION APPARENT MUCH LIKE A FATIGUE FAILURE. THE HOOK IS OF TITANIUM MATERISDR M7K2004F00004Fastener · shearedON THE ENGINE FAIRING 1 OF 4) LATCHING HOOK OF THE FASTENER SHEARED AT HOOK BASE AND CRYSTALIZATION OF THE METAL AT THE BREAK SEEMED APPARENT. NO SIGNIFICANT WEAR NOTED BEFORE THE BREAK OCCURRED THIS IS A TITAIUM MATERIAL. SUGGEST USING STAINLESS STEEL.SDR PG9R117581Fitting · crackedFITTINGS CRACKED. (RMA NR R046607)SDR PG9R117581AFitting · crackedFORWARD FITTINGS CRACKED. (RMA NR R046607)SDR PG9A117580Fitting · crackedREAR FITTINGS CRACKED. (RMA NR R046607)SDR PG9R117580AFitting · crackedFORWARD FITTINGS CRACKED. (RMA NR R046607)SDR M7K2004F00003Fitting · crackedFITTING, RT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED LARGER RADIUS MACHINING OR TO BE OF GREATER STRESDR M7K2004F00007Fitting · crackedRT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED TO BE OF GREATER STRENGTH AND MACHINED RADIUS INCREASED.SDR M7K2004F00005Fitting · crackedRT CABIN ANTI-VIBRATOR TUNING HAMMER. SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORE AND AFT FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS SHOULD BE STRONGER AND MACHINING OF THE PARTS SHOULD INCLUDE A MSDR M7K2004F00006Fitting · crackedRT CABIN ANTI VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME, THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS SHOULD BE STRONGER AND MACHING OF THE PARTS SHOULD INCLUDE A MUSDR I05R092763Clamp · crackedCRACKED CLAMP, REPLACED PART.SDR M7K2004F00002Windscreen · crackedWINDSCREEN DEVELOPED 3 INCH CRACK IN LT UPPER CORNER NOTICED UPON LANDING DURING POST FLIGHT CHECK. MFG METHOD OF BONDING OF WINDSCREEN TO AIRFRAME CAUSES EXPANSION AND CONTRACTION TO DEVELOP STRESS IN THE LEXAN MATERIAL LENDING TO CRACKING DEFECTS.SDR AUS20031132Pin · failed(AUS) ENGINE TORQUEMETER PIN FAILED. PIN COULD NOT BE FOUND AND IT WAS SUSPECTED THAT THE PIN WAS SOMEWHERE IN THE ENGINE. ENGINE WAS REMOVED FOR REPAIR.SDR Z1R2003F00000Screw · corrodedYELLOW BLADE(COLOR CODE) TIP CAP M/R SCREWS. FORWARD PAR OF ALL SCREWS HAVE A .002 INCH GAP BETWEEN THE HEAD OF SCREW AND MATING SURFACE. (AS MEASURED) SCREW IS NOT CONTACTING COMPLETELY AROUND THE HEAD OF SCREW. CORROSION IS APPEARING AT THE FIRST THREE THSDR I05R091299Latch · failedDOOR SPRING FAILURE REMOVED DOOR INNER PANEL AND FOUND BROKEN SPRING AT THE LATCH ARM. REPLACED SPRING.SDR PG9A118870Starter Gen · failed(STARTER GENERATOR) UNIT FAILED, REMOVED AND REPLACED.(K)SDR PG9A118869Fuel Filter · failedFUEL FILTER FAILED AND CAUSED ENGINE TO FLAMED OUT, (K)SDR KBT2004F00000Bearing · failedDURING INSPECTION OF TAIL ROTOR CONTROL ROD, FOUND ELASTOMERIC BEARING HAD FAILED. INNER BUSHING HAD BECOME UNBONDED, SHIFTED FULLY TO ONE SIDE (NOT CENTERED).SDR I05R089182Indicator · inaccurateFUEL INDICATOR GIVEING ERRONEOUS READINGS, REPLACED PART.SDR 36020820Blade · debondedTRIM TAB DISBONDED ON RED TAIL ROTOR BLADE. RESULTING IN APPROXIMATELY 1.25 INCH LONG SEPARATION.SDR XG3R088675Light · brokenANTI-COLLSION LIGHT INOPERATIVE. REPLACE ANTI-COLLISION LIGHT ASSEMBLY.SDR 3602081003Blower Motor · damagedAIR CONDITIONING BLOWER POPS CIRCUIT BREAKER.SDR 9015081003Belt · deterioratedAIR CONDITIONER COMPRESSOR BELT BURNED/DETERIATED DUE TO COMPRESSOR FAILURE.SDR HEEA088652Igniter · wornIGNITER WORN TO LIMITS. TO BE SENT TO VENDOR.SDR 3602072103Bellcrank · wornT/R PITCH BELLCRANK WORN BEYOND ACCEPTABLE LIMITSSDR PG9A118859Strobe · failed(STROBE UNIT) UNIT FAILED WITH 37 HOURS TOTAL TIME.(K)SDR HEEA088364Metering Valve · out of adjustRED GOVERNOR LIGHT ON GROUND RUN UP. FAULT CODE 129. FAIL2 CODE 4002.SDR 3144070703Servo · leakingMAIN ROTOR SERVO LEAKING.SDR 9015070403Battery · inoperativeAIRCRAFT BATTERY, UNSERVICEABLE.
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