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 QMLA2023050920038Hose · unknownAFTER TAKE OFF WITH AIR CONDITIONING FAN ON AND DEMIST 1 TURN OPEN COCKPIT HAD BURNING SMELL AND SMOKE HAZE. AIRCRAFT RETURNED TO DEPARTURE LOCATION WITHOUT INCIDENT. INSPECTED HEAT AND DEMIST DIFFUSERS FOR DEBRIS WITH NONE FOUND. HEAT AND DEMIST VALVES OPERSDR 2A6D20230505001Frame · chafedDAMAGE WAS NOTED TO THE X1790.15 FRAME (PN: 350A21-4099) IN THE FORM OF A CHAFE DAMAGE AREA. THE CHAFE DAMAGE IS LOCATED NEAR THE INBOARD RH CAMLOC AND WAS MEASURED TO BE APPROXIMATELY 0.70” X 0.175SDR QMLA2023040420024Fire Detector · unknownENG FIRE LIGHT ILLUMINATED DURING FLIGHT WHEN NO FIRE WAS PRESENT. SUSPECT MOISTURE IN A CONNECTOR.SDR QMLA2023032920022Wire Harness · unserviceableDURING CRUISE AT AN APPROXIMATE ALTITUDE OF 1700' AND 110 KNOTS AIRSPEED ON A FLIGHT TO THOMAS JEFFERSON UNIVERSITY HOSPITAL(9PA8) PHILADELPHIA, PA THE CREW AND I NOTICED WHAT SEEMED TO BE A SLIGHT BURNING ODOR. I SECURED THE CABIN DEMIST HEAT AND THE ODOR DISSDR 2023FA0000124Unknown · unknownON A FLIGHT FROM SILVER CITY, NM TO MEMORIAL MEDICAL CENTER IN LAS CRUCES. I GOT A YELLOW AND RED GOV LIGHT. I WAS ABOUT 5 MINS FROM KSVC, SO I TURNED AND LANDED AT GRANT COUNTY AIRPORT. AIRCOM WAS ALERTED, AND THEY GOT NATIVE 30 HEADED OVER TO PICK UP OUR PATSDR 2A6D20230309001Frame · chafedDAMAGE WAS NOTED TO THE RH X-FRAME (PN: 350A21-1051.21) IN THE FORM OF A CHAFE LOCATED AT THE AFT VERTICAL FLANGE OF THE X FRAME. THE CHAFE WAS REPORTED TO BE 0.30” X 0.20” AND 0.05” DEEP.SDR 2A6D20230309002Floor Support · corrodedCORROSION WAS NOTED ON THE LH SIDE OF THE CABIN FLOOR EDGE.SDR 2023F00079Unknown · unknownABOUT 30 MINUTES AFTER TAKEOFF FROM GILA REGIONAL WITH A INTERFACILITY TRANSFER THE COCKPIT STARTED TO SMELL STRONGLY LIKE BURNING PLASTIC/RUBBER. NO SMOKE WAS PRESENT AND INSTRUMENTS AND WARNING LIGHT PANEL WAS NORMAL WITH NO INDICATIONS OF A PROBLEM BESIDES SDR 2023FA0000014Altimeter · misoverhauledRECEIVED ENCODING ALTIMETER, AFTER OVERHAUL UNDER WO# 3267658. DURING THE FUNCTIONAL CHECKS, THE ITEM FAILED TO SEND THE CORRECT ALTITUDE INFORMATION TO THE TRANSPONDER. ITEM TO BE RETURNED.SDR QMLA2022122800776Fadec · faultedREADY FOR DEPARTURE ENGINE WILL NOT START. AMBER ARC FOR NG AND TORQUE INDICATIONS WITH AMBER AND RED GOV LIGHT. HMU WILL NOT GO THROUGH START TEST.SDR 2022FA0000759Indicator · faultedRECEIVED FROM VENDOR IN FAULTY/UNAIRWORTHY CONDITION. THIS IS THE SECOND OCCURRENCE FOR THIS PART. WHILE TURNING THE COURSE SELECT KNOB THE COMPASS CARD ALSO ROTATES. THERE IS ALSO A GOLD METAL OBJECT LOOSE INTERNALLY, THIS PART ALSO HAS THE MOD 1424 REV LSDR 2022FA0000740Indicator · misrepairedPICTORIAL NAV. INDICATOR RECEIVED FROM VENDOR FAULTY. COMPASS OUTER RING WAS FOUND TO OPERATE INTERMITTENTLY. REPAIRED UNDER WO 22-3583.SDR QMLA2022112920080Unknown · odor25 MINUTES INTO THE FLIGHT ON A REQUEST, PILOT/MED-CREW STARTING SMELLING A FOREIGN ODOR RESEMBLY SOMETHING BURNING; NO VISUAL SMOKE OBSERVED. DIVERTED TO THE NEARESET LOCATION KRVS. CHECKED OUT BY MX AT THE MX HANGAR AND NOTHING WAS FOUND AT THIS TIME.SDR QMLA2022100720067Bushing · failedDURING ASSEMBLY OF THE LOWER SCISSOR THE CLEARANCE “J” COULD NOT BE OBTAINED. REF MM REV 16 AMM 62-33-00,4-1 PARA F.2.C.1.G. THE SCISSORS LINK WAS DISASSEMBLED, AND THE BUSHING LENGTH WAS MEASURED AND FOUND TO BE 3.3046”. A NEW AIR BUS BUSHING P/N 704A33-640-0SDR 2A6D202209260101Bulkhead · chafedCHAFING DAMAGE WAS FOUND ON INBOARD FACE OF THE L/H LATERAL BULKHEAD (X-FRAME) AT APPROXIMATELY STA: 3650, WL: 2305, AND BL: 430L WITH THE DAMAGE MEASURING 0.25” LONG AND 0.18” WIDE WITH A MAX DEPTH OF 0.006.SDR 2A6D20220831002Support Beam · damagedDAMAGE 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 2A6D20220831003Support Beam · chafedTHE MAIN GEARBOX SUPPORT FRAME (P/N: 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM THE TAIL ROTOR CONTROL CABLE. THE DAMAGE IS UNDER THE MAIN GEARBOX DECK AT THE AFT R/H CORNER OF THE MAIN GEARBOX CUTOUTSDR 2A6D20220623001Support 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 2022F00266Pressure Switch · unserviceableFUEL FILTER CAUTION LIGHT ILLUMNATED ON TAKEOFF.SDR QMLA2022062020035Pressure Switch · warning messageFUEL FILTER CAUTION LIGHT ILLUMNATED ON TAKEOFF.SDR 2A6D20220527001Bulkhead · chafedDAMAGE WAS NOTED TO THE 15 DEGREE BULKHEAD LH WEB (P/N: 350A21-1032.86) IN THE FORM OF CHAFES. THE TWO CHAFING DAMAGE AREAS WERE FOUND NEAR THE X-FRAME AND UPPER CHAFING DAMAGE WAS MEASURED TO BE APPROXIMATELY 0.20” IN LENGTH, 0.3” IN WIDTH AND 0.008” DEPTH; TSDR QMLA2022050920027Nozzle · faultyUPON DEPARTURE FROM THE AIRFIELD AT 0133, AT 500' AGL, 70 KIAS, AND 8.5 FLI WITH THE DEMIST ON, SMOKE BEGAN FILLING THE COCKPIT ORIGINATING FROM THE DEMIST NOZZLES. CREW OPENED THE SLIDING WINDOWS TO VENT THE COCKPIT, DEMIST WAS SHUT OFF, AND THE AIRCRAFT WAS SDR 2A6D20220421Deck Plate · chafedTHERE ARE TWO CHAFING MARKS ON THE R/H SIDE OF TRANSMISSION DECK JUST AFT OF THE MAIN ROTOR GEAR BOX. THE DEEPEST DEPTH IS 0.010" WITH A LENGTH OF 0.35" AND WIDTH OF 0.005"SDR QMLA2022042220026None · unserviceableWHILE ON A FLIGHT TO A PR, PILOT NOTICED AN AMBER GOV LIGHT IN FLIGHT FOLLOWED BY A DECREASE IN ENGINE POWER AND ROTOR SPEED. PILOT ABORTED THE LANDING AND LANDED AT A NEARBY AIRPORT BEING THE SAFFORD AIRPORT.SDR 2A6D20220325001Support Beam · chafedTHE TRANSMISSION SUPPORT FRAME (PN 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE. THE DAMAGE IS UNDER THE TRANSMISSION DECK AT THE AFT RH CORNER OF THE TRANSMISSION CUTOUTSDR 2A6D20220325002Support Beam · elongatedDAMAGE WAS DISCOVERED ON THE LH BEAM UNDER THE ENGINE DECK (PN: 355A21-2110.25) IN THE FORM OF AN ELONGATED HOLE IN THE LOWER FLANGE NEAR THE AFT END OF THE PARTSDR 2A6D20220318001Crossbeam · damagedDAMAGE TO THE FWD BULKHEAD CROSSBEAM L/H AND R/H CORNERS. CORNERS SEEM TO HAVE BEEN DAMAGED WHILE LOCATING NUTPLATES ON 15 DEGREE BULKHEAD. DAMAGE DIMENSIONS FOR BOTH LH AND RH CORNERS ARE APPROXIMATELY ( .100” L X .020” W X .015” D)SDR 2A6D20220315001None · usedCUSTOMER HAS REPORTED DAMAGE TO THE AFT BULKHEAD WEB (PN: 350A21-1036.60) IN THE FORM OF NUMEROUS
CHAFES. THE CHAFES WERE MEASURED TO BE ON AVERAGE 0.50” IN LENGTH WITH THE DEEPEST CHAFE
BEING 0.008” DEEP.SDR 2A6D20220315002None · usedCUSTOMER HAS REPORTED DAMAGE TO THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.22). THE CREASE AND GOUGE
DAMAGES WERE DISCOVERED TO BE JUST FORWARD OF THE TAIL ROTOR GEAR BOX. THE CREASE DAMAGE IS APPROXIMATELY 0.40”
WIDE AND THE GOUGE DAMAGE IS APPROXIMATELYSDR 2A6D620220309001Bulkhead · usedDAMAGE TO THE 15° BULKHEAD LH POST (PN: 350A21-1031.33) WAS NOTED IN THE FORM OF CHAFING. THE CHAFING DAMAGE IS APPROXIMATELY 0.40” IN LENGTH, 0.07” IN WIDTH AND 0.017” IN DEPTH.SDR 2A6D20220127001Floor Support · corrodedCORROSION WAS NOTED ON THE LH AND RH SIDE OF THE CABIN FLOOR EDGE. THE DAMAGE WAS REPAIRED VIA BLENDING AND TRIMMING OUT THE DAMAGED PORTION(S) OF THE EDGE FRAME, ALONG WITH FABRICATING AND INSTALLING SPLICE DOUBLER(S) AT LH STA 75.19 AND RH STA 73.19 TO REINFSDR 2A6D20220120001Bulkhead · chafedAIRCRAFT HAS CHAFE DAMAGE ON THE AFT SIDE OF THE 15 DEGREE BULKHEAD LOCATED IN THE L/H LATERAL BAGGAGE COMPARTMENT IN TWO DIFFERENT LOCATIONS. THE DAMAGE IS LOCATED AT APPROXIMATELY STA 2700, WL 2300, AND BL 500L. THE OB DAMAGE MEASURES.2” LONG AND .11” WIDE WSDR 2A6D20220120002Bulkhead · chafedDAMAGE TO THE 15 DEGREE BULKHEAD LH WEB (PN: 350A21-1032.60 IN THE FORM OF CHAFES. THE FIRST CHAFE DAMAGE AREA WAS FOUND NEAR THE X-FRAME AND WAS MEASURED TO BE APPROXIMATELY 0.40” X 0.39” AND 0.015” DEEP; THE SECOND CHAFE DAMAGE AREA WAS FOUND ON THE STIFFENISDR 2A6D20220120003Bulkhead · gougedTHE L/H LATERAL BAGGAGE COMPARTMENT WE IDENTIFIED THE LANDING GEAR’S L/H VIBRATION DAMPENER FITTING WAS GOUGED. DAMAGE LOCATED AT APROX. STA 2700, WL 2550, BL 600L. THE DAMAGE MEASURES L=0.600”, W=0.300”, D=0.025”.SDR 2A6D20220120004None · chafedTHE TRANSMISSION SUPPORT FRAME (PN 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE. THE DAMAGE IS UNDER THE TRANSMISSION DECK AT THE AFT RH CORNER OF THE TRANSMISSION CUTOUT. THE CHAFING ON THE TRANSMISSION DECK FRAME WITH A LENSDR 2A6D20220120005None · chafedAC 7015 HAS CHAFE DAMAGE TO THE L/H X-FRAME’S AFT LOWER LEG LOCATED AT APPROXIMATELY STA 3650, WL 2305, AND BL 430L. THE DAMAGE MEASURES .21” LONG AND .2” WIDE WITH A MAX DEPTH OF .019”.SDR 2A6D2022010710401Deck Plate · dentedSHARP DENTS ON THE R/H SIDE IN AN AREA .35” LONG BY 1.1” WIDE WITH A MAX DEPTH OF .033” DEEP. THE DAMAGE IS LOCATED AT APPROXIMATELY STA 4370, WL 1759, AND BL 350R.SDR 2A6D20211216001Door Frame · chafedC130 S/N 7174 WAS FOUND TO HAVE LUGGAGE COMPARTMENT DOOR FRAME DAMAGE AT APPROXIMATELY STA 1863, WL 1990, AND BL 280L/R WITH A MAXIMUM DEPTH OF 0.021SDR 2A6D2021112409703Latch · crackedLH CREW DOOR LOWER LATCH SUPPORT SHELL CRACKEDSDR 2A6D2021110509702Tail Boom · chafedCHAFING WAS DISCOVERED ON THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.AL) MEASURING APPROXIMATELY 0.10” X 0.10” AND 0.011” DEEP.SDR 2A6D2021110109701Frame · gougedDAMAGE WAS NOTED TO THE RH X1790.15 FRAME (PN: 350A21-1368.23) IN THE FORM OF CHAFES NEAR THE TOP FLANGE. THE CHAFES WERE MEASURED TO BE APPROXIMATELY 0.10” X 0.20” AND 0.007” DEEP, AS WELL AS 0.10” X 0.10” AND 0.003” DEEP.SDR QMLA2021111020060Frame · noneFOUND DAMAGE ON RIB STRUCTURE WHERE THE HEAT/ DEMIST LINE IS SECURED TO THE RIB.SDR 2A6D20211018Floor Support · gougedA/C 7267 HAS A GOUGE LOCATED RBL 17.75 MEASURING APPROXIMATELY .017” IN DEPTH, .125” IN LENGTH, AND .100” IN WIDTH ON THE BOTTOM OF THE X1790.15 FRAME WHERE IT MATES WITH THE BELLY PANEL.SDR QMLA2021102920055Skin · dentedDAMAGE WAS NOTED TO THE TAIL BOOM LOWER FWD SKIN (PN: 350A23-0020.20) IN THE FORM OF MULTIPLE DENTS, AS WELL AS A DENT IN THE TAIL BOOM UPPER FWD SKIN (PN: 350A23-0020.21). THE LARGEST DENT IMPACTS BOTH THE LOWER FWD SKIN AND THE UPPER FWD SKIN AND WAS MEASURESDR 2A6D2021101409003None · chafedRING FRAME CHAFING DAMAGE AT APPROXIMATELY STA 4918, WL 1759, AND BL 320L MEASURING 0.92” LONG X 0.08” WIDE AND IS 0.008” AT ITS DEEPESTSDR 2A6D2021092409002Deck Plate · chafedDENT AND CHAFING WAS DISCOVERED ON THE ENGINE DECK (AIRBUS PN 350A21-1239.21) JUST NEAR THE SCUPPER DRAIN HOLE. THE DENT WAS MEASURED TO BE 0.20” X 0.10” AND 0.040” DEEP, AND THE CHAFE WAS MEASURED TO BE 1.0” X 0.40” AND 0.005” DEEPSDR 2A6D2021092309001Structure · corrodedCORROSION ON FLOOR EDGING HAS MULTIPLE SPOTS THAT RANGE FROM (.010 TO .003) IN DEPTH. THE DEEPEST IN DEPTH IS .010 (TWO INCHES LONG AND .60 WIDE), THE SECOND HAS A DEPTH OF( .008 AND IS 1.6 IN LENGTH AND .60 WIDE).SDR QMLA2021091020045Bleed Valve · malfunctionedDURING CRUISE FLIGHT EXPERIENCED A YAW KICK, BURNING RUBBER SMELL AND FLI FAILURE. NO LOSS OF FLIGHT CONTROLS OR OTHER INDICATIONS. PRECAUTIONARY LANDED AT AIRPORT MINUTES LATER. SUBSEQUENT FLIGHT CHECKS SHOWED LOSS OF ENGINE POWER AT A HOVER. INSUFFICIENT POSDR QMLA2021102920056Seal · unsecureCHECKS SHOWED LOSS OF ENGINE POWER AT A HOVER. INSUFFICIENT POWER AVAILABLE TO EVEN EXECUTE A NORMAL TAKEOFF. BLEED AIR VALVE WASN'T CLOSING UNTIL 98% NG AND BURNING SMELL STILL NOTICEABLE. **SUPPLEMENTAL INFORMATION**10-29-2021, FOUND THAT THE REAR INLET BARRSDR 2A6D2021081208401Deck Plate · chafedDAMAGE WAS NOTED TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF CHAFES. THE DAMAGE AREAS WERE DISCOVERED TO BE OUTBOARD FROM THE SCUPPER DRAIN HOLE WITH THE LARGEST CHAFE MEASURING 0.40” X 0.30” AND REPORTED TO BE 0.108MM (0.004”) DEEP.
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