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 QMLA2026081320055Blower Motor · burned outODOR OF BURNT ELECTRICAL WIRING. FOUND SMELL COMING FROM AFT AC VENTS. FOUND CONDENSATION/WATER IN ELECTRICAL MOTOR. REPLACED AFT BLOWER MOTORSDR 2A6D20260728001Support Angle · crackedCRACK FOUND ON SUPPORT ANGLE OF UPPER LEFT FUSELAGE TO TAILBOOM ATTACHMENTSDR 2026FA0000304Chip Detector · false indicationENGINE CHIP EVENT - INTERMITTENT ILLUMINATION OF ENGINE CHIP INDICATION DURING CRUISE FLIGHT AFTER MAKING A TURN. DURING DESCENT AND LANDING AT A LOCAL BALL FIELD, THE CHIP LIGHT FLICKERED MULTIPLE TIMES. MAINTENANCE DISPATCHED FROM HONOLULU AND INSPECTED THSDR 2A6D20251125001Crossbeam · chafedVARIOUS DAMAGES AT THE AFT LANDING GEAR LOCATION, THE FIRST DAMAGE (#1) IS AT THE AFT LANDING GEAR CROSS BEAM SHIM (P/N: 350A214344.20) IN THE FORM OF CHAFING. THE CHAFE DAMAGE IS POSSIBLE DUE TO WEAR IN THE SHIM (P/N: 350A410064.20) BETWEEN THE AFT LANDING GESDR 2A6R1124202574604Skin · damagedOVERSIZED FASTENER HOLE DAMAGE WAS FOUND ON THE L/H FUSELAGE SKIN (P/N: 350A210053.BW), FWD FRAME ANGLE (P/N: 350A211036.28), AFT FRAME (P/N: 350A211240.00), LOWER FRAME (P/N: 350A211245.22), AND MAINTENANCE STEP (P/N: 350A21137.20) DURING REMOVAL AND REPLACEMSDR 2A6D20251106001Bulkhead · chafedCHAFING DAMAGE ON THE LT LONGITUDINAL BULKHEAD (X-FRAME) ON THE UPPER INBD FACE MEASURING APPROXIMATELY 0.017" IN DEPTH, 0.10" IN WIDTH, AND 0.210" IN LENGTH. THE DAMAGE WAS REPAIRED WITH A DOUBLER IAW AIR METHODS ENGINEERING AUTHORIZATION 33-5300-EA-5308.SDR 2A6D20251105001Beam · chafedDAMAGE TO THE RH Y398.5 BEAM (P/N: 350A211351.22) AND STOP DOUBLER (P/N: 350A211363.25) IN THE FORM OF A CHAFE. THE CHAFE DAMAGE IS NEAR THE FWD UPPER SIDE OF THE CUTOUT AND WAS MEASURED TO BE APPROXIMATELY 0.4" IN LENGTH AND 0.040" IN DEPTH.SDR 2A6R1024202574601Rail · chafedCHAFING DAMAGE WAS FOUND ON THE TAIL BOOM L/H TRDS SUPPORT RAIL/STIFFENER SHEET (P/N: 350A231028.66) JUST FORWARD OF THE #3 TRDS BEARING SUPPORT. THIS DAMAGE IS A 0.25” IN LENGTH AND 0.1” IN HEIGHT SECTION THAT IS CHAFED THROUGH THE FULL THICKNESS OF THE RAIL.SDR 2A6D20251006001Keelbeam · damagedA MIS-DRILLED HOLE WAS FOUND ON THE FORWARD LH KEEL BEAM (PN: 350A21-1350-20), AFT LH KEEL BEAM (PN: 350A21-1056- 20) AND FWD KNOT ASSEMBLY LH SPLICE (PN: 350A21-1071-20) LOCATED AT Y400 X 1296. TOOL MARK DAMAGE WAS ALSO DISCOVERED ON THE FWD KNOT ASSEMBLY LSDR QMLA2025100420098Display · faultedJUST LIFTED OFF FROM A PR EVENT & HEADING BACK TO BASE, NOTICED UPPER SCREEN OF VEMD HAD REVERTED TO 3-PARAMETERS ENGINE PAGE & NG INDICATION MISSING & YELLOW. A CAUTION MESSAGE OF OVERLIMIT DETECTED SHOWING ON BOTTOM OF VEMD. LOWERED POWER & DIVERTED TO KRVSDR QMLA2025091520094Engine · power lossWE WERE TAKING OFF FROM THE PAD AT PRESCOTT WITH A PATIENT ONBOARD. HAD GOOD POWER IN HOVER AND ON TAKEOFF ABOUT 200-300 FT AND GOT JUST PAST THE STREETLIGHTS IN FRONT OF THE PAD. POWER SETTING BELOW THE YELLOW RANGE, FOR A BRIEF SECOND THE NOSE ROTATING TO LESDR 2A6D20250818001Mount Flange · gougedDAMAGE TO THE LANDING GEAR LH OTBD AFT BEARING IN THE FORM OF GOUGE. THE GOUGE DAMAGE IS AT LOWER FLANGE OF THE BEARING AND WAS MEASURED TO BE APPROXIMATELY 0.3895” X 0.1105” X DEPTH MORE THAN HALF THE THICKNESS OF THE BEARING.SDR QMLA2025071820075Unknown · odorNURSES REPORTED AFTER TAKING OFF FROM GOODYEAR AIRPORT AFTER GETTING FUEL AFTER A PR EVENT THAT THEY NOTICED A STRONG FUEL SMELL. THEY CONTINUED ON TO THE HELIPAD AT ABRAZO WEST AND LANDED SAFELY. I ARRIVED AT THE HELIPAD AND PERFORMED A INSPECTION OF THE HELISDR QMLA2025061620067Vent Line · leakingMAJOR OIL LEAK. DISCOVERED BY NURSE STOWING EQUIPMENT IN REAR COMPARTMENT. HE ADVISED ME OF OIL ALL OVER THE SIDE OF AIRCRAFT. I SHUT DOWN THE AIRCRAFT AND EXITED TO INSPECT. REMOVED AND RE-INSTALLED OIL VENT LINE FROM TANK, GROUND RUN, LEAK CHECK WAS GOOD, RSDR 2A6D20250602001Doubler · chafedCHAFING DAMAGE WAS DISCOVERED ON T/R SERVO GUIDE DOUBLER P/N: 355A23-2000-20SDR 2A6D20250602002Floor Support · chafedCHAFE DAMAGE WAS DISCOVERED ON THE R/H CABIN FLOOR EDGE P/N: 350A21-1359-21SDR QMLA2025052820060Hmu · faultedMULTIPLE ENGINE CHIP CAUTIONS OVER A HANDFUL OF FLIGHTS SINCE MID-APRIL. MOST RECENT EVENT (THIS INCIDENT) OCCURRED LESS THAN ONE DAY AND 0+45 FLIGHT HOURS AFTER PREVIOUS INCIDENT. MULTIPLE CHIPS (IN EXCESS OF 20) FOUND ON CHIP DETECTOR (M01) AND SEVERAL CHSDR QMLA2025051520056Gearbox · warning lightMAIN ROTOR GEAR BOX CHIP INDICATOR LIGHT ILLUMINATED IN FLIGHT. FIRST SET OF FLIGHTS FROM CHANGING OF MBG OIL FILTER YESTERDAY.SDR QMLA2025032420040Motor · shortedELECTRICAL SMOKE ODOR IN CABIN. AFT EVAPORATOR MOTOR HAD INTERNAL SHORT CAUSING SMOKE SMELL AND CAUSING AFT PORTION OF A/C TO BE INOP.SDR 2A6D20250130001Beam · damagedFASTENER HOLE DAMAGE (ELONGATION) WAS DISCOVERED ON THE LH MAINTENANCE FOOTSTEP BEAM (P/N 350A21124520) IN THE FUSELAGE REAR STRUCTURE.SDR 2A6D20241209001Crossbeam · chafedTHE FIRST DAMAGE IS ON THE AFT LANDING GEAR CROSS BEAM (P/N: 350A214311.20). THE AFT CROSS BEAM IS DAMAGED DUE TO MISSING SHIM BETWEEN THE AFT LANDING GEAR LOWER ARM AND LOWER HALF BEARING WHICH CREATED LATERAL MOVEMENT OF LANDING GEAR CROSS TUBE AND CAUSED CHSDR QMLA2024092420125Motor · failedCREW NOTED SMELL OF SOMETHING BURNING IN COCKPIT. A/C WAS TURNED OFF AND THE SMELL BECAME LESS SEVERE.SDR QMLA2024091920118Starter Gen · failedSTAR GEN FAILED ON APPROACH. WOULD NOT RESET.SDR QMLA2024091620116Engine · surgesDURING FLIGHT ON AN AIR AMBULANCE OPERATION. AS THE INCREASE OF COLLECTIVE TO APPROXIMATLEY 9.0 FLI, HEARD THE ENG SURGE WITH A LEFT YAW TO THE ACFT. IMMEDIATELY LOWERED COLLECTIVE & VERIFIED ALL SYS NORMAL. SMOOTHLY AND SLOWLY INCREASED THE COLLECTIVE & AT ASDR QMLA2024091520116Anticipator · faultedREMOVED AND REPLACED ANTICIPATOR. THIS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERVICE. REF# 7481.091524.2054.TTSDR 2A6D20240828001Floor Panel · corrodedTHERE IS CORROSION DAMAGE TO THE CABIN FLOOR EDGING (PN: 350A21-1359-20/21).SDR 2A6D20240828002Structure · gougedDAMAGE TO THE LH UPPER CARGO EDGING (P/N: 350A211041.22) IN THE FORM OF A GOUGE CAUSED WHILE INSTALLING BLIND FASTENER. THE GOUGE DAMAGE NEAR AFT SIDE OF THE LH EDGING AND WAS MEASURED TO BE APPROXIMATELY 0.40” X 0.15” X 0.02”.SDR 2A6D20240828003Bulkhead Web · chafedDAMAGE TO THE 15° BULKHEAD LH WEB (PN: 350A21-1032.86) IN THE FORM OF SEVERAL CHAFES. THE CHAFES WERE REPORTED TO BE 0.20” X 0.10” AND 0.004” DEEP, AS WELL AS 0.20” X 0.30” AND 0.010” DEEPSDR 2A6D20240828004Stiffener · wornDAMAGE TO THE LH STA2700 STIFFENER (LH PN: 350A21-1071.22; RH PN: 350A211071.23) IN THE FORM OF WEAR CAUSED BY A NEARBY BOLT HEAD.SDR 2A6D20240828005Support · damagedDAMAGE TO THE RH BI-DIRECTIONAL SUPPORT FITTING (P/N: 350A211232.23) AND SUPPORT BEAM (P/N: 350A211293.20) IN THE FORM OF CHAFING CAUSED DUE TO CABLE. THE CHAFE DAMAGE AT SUPPORT BEAM MEASURED TO BE APPROXIMATELY 0.30” X 0.20” X 0.015”. THE CHAFE DAMAGE AT BI-SDR 2A6D20240828006Structure · gougedGOUGE AT THE OUTBOARD FLANGE RIVNUT LOCATION IN THE FORM OF SHEAR OUT. THE GOUGE WAS MEASURED TO BE APPROXIMATELY 0.1” X 0.1285”X 0.060”.SDR QMLA2024061720064Unknown · odorDURING FLIGHT AND RETURN TO BASE FROM FLIGHT, CREW NOTIFIED PILOT THAT THEY SMELLED A ELECTRICAL BURNING AROUND THE BACK CABIN WALL. IT WAS DARK INSIDE THE CABIN SO VISUAL IDENTIFICATION WAS DIFFICULT. PILOT AND CREW INSPECTED THE AREA BUT COULD NOT IDENTIFY TSDR QMLA2024042520043Potentiometer · wornTOOK OFF FROM BASE GOT TO LEVEL FLIGHT STARTED POWER CHECK GOT THE SOLID AMBER GOV LIGHT. RETURNED TO BASE.SDR 2A6D20240321001Floor Support · corrodedCORROSION DAMAGE DISCOVERED TO THE L/H CABIN FLOOR EDGING P/N: 350A21-1359-20.SDR 2A6D20240321002Floor Support · corrodedCORROSION DAMAGE DISCOVERED TO THE R/H CABIN FLOOR EDGING P/N: 350A21-1359-21.SDR QMLA202420025Duct · crackedPILOT REPORTED DURING CLIMB OUT FROM BASE AT KDMN EN ROUTE TO SENDING FACILITY HE TURNED ON THE CABIN VENTILATION AND WATER STARTED POURING OUT OF UPPER A/C VENTS. HE THEN TURNED OFF THE A/C VENT SYSTEM AND RETURNED TO BASE AND SHUT THE AIRCRAFT DOWN WITHOUT SDR 2A6D20240229001Bulkhead · crackedA CRACK WAS DISCOVERED ON THE AFT BULKHEAD CENTER STRUCTURE. THE CRACK MEASURES APPROXIMATELY 1.0 INCH LONGSDR 2A6D20240201001Angle · corrodedDAMAGE TO THE LH VERTICAL ANGLE (PN: 350A62-1148.21) ON THE AFT SECTION FWD LOWER FRAME IN THE FORM OF CORROSION. THE CORRODED AREA IS LOCATED AT THE BOTTOM END OF THE ANGLE, AND WAS MEASURED TO BE APPROXIMATELY 0.875” X 0.875” IN SIZE THROUGH THE FULL THICKNESDR 2A6D20240201002Web · corrodedDAMAGE TO THE LOWER CENTER WEB (P/N: 350A21-4300.20) IN THE FORM OF CORROSION. THE CORROSION DAMAGE IS TOWARDS THE AFT SIDE OF THE WEB NEAR LIGHTENING HOLES AND MEASURED TO BE THROUGH THICKNESS IN DEPTH.SDR QMLA2024012920009Unknown · odorSMELL OF FUEL IN CABIN. FLIGHT LEG ABORTED AND RETURNED TO AIRPORT. MECHANIC NOTIFIED AND RESPONDED. CHECKED ALL COMPONENTS AND AREAS OF HELICOPTER FOR SOURCE. NO FUEL LOCATED IN OR AROUND AIRCRAFT OR STRUCTURES, CABINS, COMPARTMENTS. PERFORMED ENGINE RUN-UP WSDR QMLA2023112820110Bulkhead · damagedCRACK DAMAGE WAS NOTED ON THE 22 DEGREE BULKHEAD WEB P/N 350A21-4002 UNDER THE RH FLOOR AT STA 845, RBL 673.3 WL 2806.2.SDR QMLA2023112720108Outlet · odorCREW REPORTED UNUSUAL ODOR IN CABIN AFTER LIFTOFF.SDR 2A6D20231102001Floor Support · corrodedCORROSION WAS FOUND ON THE CABIN FLOOR EDGING ON THE LH AND RH SIDE (P/N: 350A21-1359-20/21)SDR QMLA2023110220099Unknown · unknownAFTER AMBER AND RED GOV LIGHT ILLUMINATED, MYSELF AND THE CREW COULD SMELL AN ELECTRICAL SMOKE ODOR. AFTER LANDING AND SHUTDOWN. ARRIVED AT AIRCRAFT, CLEANED ELECTRICAL CONNECTORS ON FADEC AND NF SENSOR. GOV LIGHT WENT OUT.SDR QMLA2023100420081Compressor · odorPILOT REPORTED SMOKE SMELL IN CABIN, TURNED OFF THE A/C SYSTEM AND SMELL WENT AWAY. LANDED AT BASE WITH NO FURTHER ISSUES. MECHANIC ON SITE FOUND WHERE A/C COMPRESSOR CLUTCH WAS INOP.SDR QMLA2023060420043Unknown · unknownUPON DEPARTURE FROM KPDK, ENG CHIP LIGHT ILLUMINATED ON THE WARNING PANEL. IT WENT OUT AFTER A FEW SECONDS. LANDED AS SOON AS POSSIBLE BACK TO KPDK AND SHUT DOWN ENGINE, CHECKED THE CHIP PLUGS AND THERE WAS NOTHING ON THEM. GROUND RUN THE AIRCRAFT WITH NO LISDR 2A6D20230525001Floorbeam · damagedDURING INSPECTION, TWO NUTPLATES WERE FOUND TO BE INCORRECTLY INSTALLED CAUSING DAMAGE TO THE FLOOR BEAM AT APPROXIMATELY STA 1510 AND RBL 398.SDR 2A6D20230523001Support Beam · elongatedDAMAGE WAS DISCOVERED ON THE L/H BEAM UNDER THE ENGINE DECK (P/N: 355A21-2110.25) IN THE FORM OF AN ELONGATED HOLE IN THE LOWER FLANGE, NEAR THE AFT END OF THE PARTSDR 2A6D20230523002Floorbeam · corrodedDURING INSPECTION, CORROSION DAMAGE WAS DISCOVERED TO THE R/H CABIN FLOOR EDGING P/N: 350A21-1359-21.SDR 2A6D20230510001Deck Plate · chafedCHAFING WAS DISCOVERED IN 2 PLACES ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR THE SCUPPER DRAIN HOLE. THE FIRST DAMAGE AREA IS APPROXIMATELY 0.300” LONG, 0.275”WIDE, AND 0.015” DEEP AT THE DEEPEST POINT. THE SECOND DAMAGE AREA IS APPROX
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