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 2A6D20200730001Frame · chafedRH X-FRAME HAS THREE CHAFED AREAS LOCATED ON ITS INBD BEADED FACE DUE TO A/C LINES. THE AFT RH INTERNAL TRANSMISSION DECK “DIAMOND PLATE” DOUBLER ALSO HAS A CHAFE DUE TO THE TAIL ROTOR CONTROL CABLE. 2 OF THE CHAFE MARKS ON THE X-FRAME ARE LOCATED ON ITS UPPESDR 2A6D20200730002Tail Boom · chafed4685 LOWER FWD TAILBOOM SKIN HAS TWO CHAFING MARKS ON ITS RH LOWER INTERNAL FACE LOCATED BETWEEN THE TAILBOOM JUNCTION FRAME AND THE X620 CIRCUMFERENTIAL FRAME CAUSED BY A WIRE HARNESS. THE LARGER OF THE TWO WAS MEASURED AT APPROXIMATELY .007” IN DEPTH, 1.2” SDR 4HYA2021072603Compressor · smokeIN CRUISE NOTICED SMOKE IN CABIN WITH PLASTIC SMELL. MAINTENANCE DISCOVERED AIR CONDITIONER COMPRESSOR TO BE SOURCE.SDR 2A6D20210715001Bulkhead Web · chafedDAMAGE TO THE 15° BULKHEAD LH WEB (PN: 350A21-1032.22) AND THE LH POST (PN:350A21-1031.33) IN THE FORM OF MULTIPLE CHAFES (SEE FIGURES 1-2). THERE IS ALSO DAMAGE TO THE RH WEB (PN:350A21-1032.23) IN THE FORM OF CHAFES. INSIDE THE LH LATERAL CARGO HOLD THE 15 SDR 2A6D20210715002Deck Plate · chafedDAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF A CHAFE AND DENT. THE DAMAGE AREAS WERE DISCOVERED TO BE NEAR THE SCUPPER DRAIN HOLE WITH THE CHAFE MEASURING PPROXIMATELY 0.50” LONG, 0.20” WIDE, AND 0.005” DEEP AT THE DEEPEST POINT, AND THE DENTSDR QMLA2021070220035Unknown · odorAT 8 MINUTES IN TO FLIGHT FLI FAILED WITH ELECTRICAL SMELL IN COCKPIT. ON 6/30/2021 I WAS CALLED OUT FOR A VEMD FLI FAILURE. UPON ARRIVAL I INSPECTED PANEL AND ENGINE HARNESS FOR SIGNS OF OVERHEATING AND VISUAL CHECK WITH ELECTRICAL POWER APPLIED TO SEE IF ANYSDR 2A6D20210614001Deck Plate · chafedAC 4559 HAS CHAFE DAMAGE ON THE ENGINE DECK JUST FWD OF THE SCUPPER DRAIN OPENING LOCATED AT APPROXIMATELY STA 4370, WL 1759, AND BL 650L. THE DAMAGE IS IN AN AREA 1.4” WIDE BY .8” LONG AND MEASURES .019” AT ITS DEEPEST POINT.SDR 2A6D2021032506001Bulkhead · gougedL/H BAGGAGE COMPARTMENT ON THE 15 DEGREE BULKHEAD. THE DAMAGE AFFECTS ONE OF THE STIFFENERS RADII AND IS LOCATED AT APPROXIMATELY STA 2780, WL 1889, AND BL 810LSDR 2A6D20210303001Deck Plate · chafedDAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) WAS NOTED IN THE FORM OF A CHAFE. THE DAMAGE AREA WAS DISCOVERED TO BE JUST AFT OF THE SCUPPER DRAIN HOLE AND IS APPROXIMATELY 0.40” LONG, 0.30” WIDE, AND 0.010” DEEP AT THE DEEPEST POINT.SDR QMLA2021022620010Unknown · odorWE DEPARTED TUCSON MEDICAL CENTER ON AN IFT TO HOLY CROSS HOSPITAL IN NOGALES, AZ AT 10:26 TO PICK UP THE PATIENT TO BRING THEM BACK TO TUCSON. WE LIFTED THE HOSPITAL AND PROCEEDED TO CLIMB TO 4000 MSL AND WAS FLYING TOWARDS NOGALES. ABOUT 8 MINUTES AFTER TAKESDR 2A6D2021021905301Floor Panel · corrodedHAS CORROSION ON THE RT CABIN FLOOR EDGING LOCATED AT APPROXIMATELY STA 1545, WL 2640 AND BL 970R. THE DAMAGE IS .75” LONG BY .90” WIDE AND IS .004”.SDR QMLA2021021620006Switch · dirtyACFT MADE A PRECAUTIONARY LANDING IN A FIELD DUE TO MRGB OIL PRESSURE WARING LIGHT. PULLED AND CLEANED SWITCH. NO DEFECTS NOTED. ACFT WAS RUN UP AND OPS CHECK WAS NORMAL.SDR 2A6D2021021105401Structure · corrodedCORROSION WAS DISCOVERED ON THE LEFT SIDE CABIN FLOOR EDGINGSDR 2A6D2020123104403Access Door · chafedBATTERY ACCESS DOOR IN LT SIDE OF TAIL BOOM. DESCRIPTION NR 1: INTERNAL DOUBLER FOR BATTERY DOOR CUT OUT IS CRACKED AT UPPER FORWARD AND UPPER AFT CORNERS NEAR DOOR HINGE, NR 2: LOWER ANGLE DOUBLER HAS 100 % THICKNESS CHAFE DAMAGE FROM BATTERY DOOR LOWER CAMLSDR QMLA2020122120068Structure · separatedRT LOWER MAIN GEARBOX COWLING DEPARTED AIRCRAFT IN FLIGHT AND STRUCK THE TAIL ROTOR OF THE AIRCRAFT AFTER THE IMPACT THE AIRCRAFT HAD TO MAKE A PRECAUTIONARY LANDING. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THIS TIME WHILE ALL OF THE REQUIRED INSPECTIONS ARE SDR 2A6D2020121504402Deck Plate · chafedDAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF A CHAFE. THE DAMAGE AREA WAS DISCOVERED TO BE JUST AFT OF THE SCUPPER DRAIN HOLE AND IS APPROXIMATELY 0.50 LONG,
0.375 WIDE, AND 0.015 DEEP AT THE DEEPEST POINT. THE REMAINDER OF THE CHAFE EXTENDSDR QMLA2020121420066Chip Detector · fodMGB CHIP LIGHT ILLUMINATED AFTER DEPARTURE FROM BASE WITH PAT ON BOARD. MAINTENANCE FOUND FOUR SMALL METALLIC PARTICALS (.2MM OR LESS IN SIZE), DETERMINED TO BE CATEGORY F (SWARF) MATERIAL, NOTE TSO IS 15 HOURS AT TIME OF EVENT. PARTICALS WERE RECOVERED AND SDR 2A6D2020121004401Structure · corrodedCORROSION WAS DISCOVERED ON THE RIGHT AND LEFT SIDE CABIN FLOOR EDGE SECTION.SDR QMLA2020121120065Belt · failedIN FLIGHT, CREW AND PILOT SMELLED A BURNING SMELL. PILOT THEN NOTICED HYDRAULIC AND SERVO CAUTION LIGHTS ILLUMINATED. IT WAS THEN DETERMINED TO DO A PRECAUTIONARY LANDING IN AN OPEN FIELD. UPON LANDING, PILOT CHECKED THE RIGHT HAND BELT DRIVEN HYDRAULIC PUMSDR 2A6D20201116001Floor Panel · corrodedCORROSION WAS DISCOVERED ON THE RIGHT HAND SIDE CABIN FLOOR EDGE SECTION (AIRBUS PN 350A21-1359) RANGING FROM STA 1120 TO 2437.SDR 2A6D20201112001Skin · dentedAC 4613 HAS A SMOOTH DENT ON THE TAILBOOM’S RT SKIN LOCATED AT APPROXIMATELY STA 8098, WL 1829, AND BL 70R JUST FORWARD OF THE HORIZONTAL STABILIZER OPENING. THE DENT IS .4 BY .4 AND .035 AT ITS DEEPEST.SDR 2A6D20201109001Deck Plate · dentedA/C 4613 HAS SEVERAL DENTS LOCATED ON THE ENGINE DECK LOCATED AT APPROXIMATELY STA 4387, WL 1759, AND BL 650L. THE DAMAGE IS IN AN AREA 2.4 BY 1.8 WITH THE DEEPEST DENT MEASURING .045. THE DENTS ARE LOCATED ABOVE A FRAME WHICH IS UNDAMAGED.SDR 2A6D2020110503703Structure · corrodedCORROSION WAS DISCOVERED ON THE RIGHT HAND SIDE CABIN FLOOR EDGE SECTION (AIRBUS PN 350A21-1359) RANGING FROM STA X1120 TO X2437.SDR 2A6D2020110403702Bulkhead · chafedCHAFING DAMAGE WAS DISCOVERED ON THE LT LATERAL BULKHEAD (X FRAME) P/N: 350A21-1051 ON THE INBOARD FACE. THE DAMAGE IS LOCATED ON THE INTERIOR (INBOARD) SIDE OF THE X FRAME LT AFT LOWER LEG STA 3650, BL 430L AND WL 2305.SDR 2A6D2020110203701Support Frame · chafedTHE TRANSMISSION SUPPORT FRAME (PN 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE.SDR 2A6D20201021001Floor Panel · corrodedCORROSION DAMAGE ON LT AND RT FLOOR EDGING THAT WILL REQUIRE REPAIRS.SDR 2A6D20201510001Stiffener · chafedDAMAGE LT AFT LOWER LEG LOCATED AT STA 3650, WL 2305, AND BL 430L THE DAMAGE IS 0.022 DEEP, 0.5 X 0.3.SDR QMLA2020100920053Unknown · odorPILOT REPORTED THE SMELL OF RAW JET FUEL IN THE CABIN IN FLIGHT AND ELECTED TO ABORT THE FLIGHT AND RETURN TO BASE. MAINTNENANCE ARRIVED AND INSPECTED ALL FUEL LINES AND FITTINGS, HMU, AND FUEL PUMP. PERFORMED GROUND RUN WITH AIR CONDITIONING AND HEATING SYSSDR QMLA2020092520048Gearbox · making metalPILOT REPORTED A TAIL ROTOR CHIP LIGHT DURING CRUISE FLIGHT. IT FLICKERED AT FIRST, AND AFTER ABOUT 30 SECONDS CAME ON SOLID. THE PILOT IMMEDIATELY DIVERTED TO THE CLOSEST AIRPORT. ONCE SAFELY ON THE GROUND, HE CONTACTED MAINTENANCE. THE MECHANIC ARRIVED ASDR QMLA2020092820049Starter Gen · malfunctionedON SEPTEMBER 24TH 2020, AT APPROXIMATELY 15:30, THE GENERATOR ON AIRCRAFT N629AM FAILED IN FLIGHT. THE AIRCRAFT LOST ELECTRICAL POWER AND THE RADIOS AND VEMD WENT OFFLINE. THE PILOT EXECUTED A PRECAUTIONARY LANDING AT AN OFF AIRPORT LOCATION. AFTER LANDING,SDR QMLA2020091820047Drain Valve · leakingPILOT WROTE UP SMOKE AND FUMES IN COCKPIT. UPON TROUBLESHOOTING MAINTENANCE FOUND THAT THE START ELECTRO VALVE HAD FAILED CAUSING FUEL VAPOR AND MIST TO BE FORCED THROUGH THE P2 AIR LINE USED FOR CABIN HEAT. REPLACED START ELECTRO VALVE. OPS CHECK GOOD.SDR 2A6D20200916001Floor Panel · corrodedCORROSION DAMAGE ON OUR LT AND RT FLOOR EDGING THAT WILL REQUIRE REPAIRS.SDR QMLA2020090420043Fire Detector · false activationILLUMINATED ENG. FIRE LIGHT, DETECTED 8 MIN INTO A PATIENT FLIGHT FROM A REFERRING FACILITY TO ANOTHER HOSPITAL. PILOT COMPLETED A PRECAUTIONARY LANDING, THE LANDING WAS UNEVENTFUL AND WITHOUT ISSUE. THERE WAS NO EVIDENCE OF AN ENGINE FIRE AT ANY TIME. MAINTSDR 2A6D2020082702603Frame · chafedCHAFING ON THE LT X-FRAMES AFT UPPER AND LOWER LEGS. THE AFT UPPER LEG DAMAGE IS .24” BY .22” AND IS .024” AT ITS DEEPEST POINT LOCATED AT STA 3650, WL 1979, AND BL 430L. THE AFT LOWER LEG DAMAGE IS .74” BY .19” AND MEASURES .002” LOCATED AT STA 3650, WL 2305,SDR 2A6D2020082872604Support · chafedCHAFING ON THE TRANSMISSION DECK SUPPORT (350A21-1041-143) THAT IS .5” BY .2” AND .013” AT ITS DEEPEST POINTSDR 2A6D2020082402602Floor Panel · corrodedCORROSION WAS DISCOVERED ON THE RT HAND SIDE CABIN FLOOR EDGE SECTION AIRBUS PN 350A21-1359 RANGING FROM STA 1000 TO 1550.SDR 2A6D2020082002601Skin · chafedCHAFING ON THE RT INTERIOR SIDE OF THE TAILBOOM SKIN LOCATED AT APPROXIMATELY STA 7898, WL 2089, AND BL 90R JUST FORWARD OF THE HORIZONTAL STABILIZER OPENING. THE CHAFE IS .95” BY .12” AND IS .007” AT ITS DEEPEST POINT.SDR 2A6D20200813001Stiffener · chafedTHE LOWER AFT SECTION OF THE L/H X FRAME AT STA 3640,BL400L AND WL 2010. THE DAMAGE MEASURES AT 0.2” X 0.2” AND HAS A DEPTH OF 0.010”.SDR 2A6D20200813002Support · chafedTHE TRANSMISSION SUPPORT FRAME (PN 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE.SDR QMLA2020080320039Fuel Filter · faultedDURING PATIENT TRANSPORT THE "FUEL FILTER" CAUTION LIGHT ILLUMINATED INSIDE CLASS D. THE PILOT ANNOUNCED TO THE MED CREW THAT HE HAD A POTENTIALLY CRITICAL SITUATION AND WAS IMMEDIATELY EXECUTING A PRECAUTIONARY LANDING. DECLARED AN EMERGENCY WITH TOWER. FLEWSDR 2A6D202007244001Floor Panel · corrodedTHERE IS CORROSION DAMAGE TO THE CABIN FLOOR PANEL EDGINGSDR 2A6D202007230001Bulkhead · chafedCHAFING DAMAGE WAS DISCOVERED ON THE LH LATERAL BULKHEAD (X FRAME) (PN: 350A21-1051) ON THE INBOARD FACE. THE CHAFE DAMAGE IS OUTLINED BELOW AND SHOW IN IN FIGURE 1. THE DAMAGE IS LOCATED ON THE INTERIOR (INBOARD) SIDE OF THE X FRAME. L/H AFT LOWER LEG STA 364SDR 2020FA0000327Blade · defectiveTAIL ROTOR BLADE PN 355A12005014, SN 24326 WAS RECEIVED NEW AND INSTALLED ON AC. THE BLADE FAILED TO TRACK & BALANCE AND WAS DETERMINED TO BE THE CAUSE AND WAS REMOVED AND SENT IN FOR REPAIR AFTER ACCUMULATING .2HRS TIS DURING TRACK & BALANCE OPERATION. THE SDR 2A6D20200702001Door Track · damagedOVERSIZED HOLE DAMAGE WAS NOTED UNDER THE LT CARGO SLIDING DOOR UPPER GUIDE THAT WAS PREVIOUSLY PLUGGED WITH A CHERRY MAX RIVET. THE DAMAGE IS LOCATED AT APPROXIMATELY FS 2700, WL 1759, LBL 398.SDR 2A6D2020062201502Frame · crackedDAMAGE TO THE X2258 RH CROSSBEAM (PN: 350A21-4065.22) IN THE FORM OF A CRACK. THE CRACK WAS MEASURED TO BE APPROXIMATELY 1.20” IN LENGTH.SDR 2A6D202006176001Skin · chafedAC 4539 HAS CHAFFING ON THE RT BATTERY TRAY SUPPORT AND ON THE INTERNAL SIDE OF THE TAIL BOOM SKIN. DAMAGE BEING OVER 12 INCHES LONG WITH A MAX DEPTH OF .020 . DAMAGE BEING LOCATED AT APPROXIMATELY BS 7948, BL 190R, AND WL 2039. IT HAS A MAX DEPTH OF .010 IN ASDR 2A6D202006110001Floor Support · crackedDAMAGE TO THE AFT FUSELAGE FLOOR SUPPORT IN THE FORM OF CRACKS. THE FLOOR SUPPORT HAD A 0.50 INCH CRACK AND A 6.70 INCH CRACK. THE FLOOR SUPPORT HAD A 0.50” CRACK AND TWO CRACKS MEASURING 0.70 AND 0.80 IN LENGTH AT RIVET HOLES ALONG THE LENGTH OF THE BASE OF SDR 2A6D20200603001Deck Plate · elongatedHAS AN ELONGATED HOLE ON THE RT SIDE OF THE TRANSMISSION DECK THAT IS UTILIZED IN THE AFT AC EVAPORATOR PN EC130-6204-2 INSTALLATION DWG EC130-622 AS THE MOST INBOARD AFT HOLE UTILIZING AN AN3-4A BOLT. AT THE HOLES WIDEST POINT IT MEASURES AT .35 BY .26. THESDR 2A6D2020052001402Frame · chafedCHAFES TO THE AFT FUSELAGE AFT FRAME (PN: 350A21-1242.20). THE CHAFES ARE FOUND ON
THE FREE EDGES OF THE INBOARD STIFFENING FLANGES ON THE LH AND RH SIDES OF THE FRAME. THE LH SIDE CHAFES
WERE MEASURED TO BE 7MM X 12MM (0.276” X 0.472”) AND 0.014” DEEP; AND SDR 4HYA202005211802Unknown · vaporDURING TRANSITION TO CRUISE, PILOT NOTICED AN ODORLESS VAPOR/MIST EMANATING FROM THE HEAT/DEMIST SYSTEM. RETURNED TO BASE TO HAVE MAINTENANCE CHECK IT OUT. NO DEFECTS NOTED IN SYSTEM AND COULD NOT REPRODUCE CONDITION AFTER GROUND RUN AND MAINTENANCE FLIGHT. S
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