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 2A6D2020051301401Bulkhead · crackedCRACK DAMAGE WAS NOTED ON THE 22 DEGREE BULKHEAD WEBSDR 2A6D20200429001Skin Panel · dentedTHE TAILBOOM FWD LOWER SKIN PANEL HAS DENT DAMAGE. THE DENT LOCATION IS JUST AFT OF THE AFT FUSELAGE JUNCTION FRAME AND IS APPROX. 1.5” IN DIAMETER.SDR 2A6D20200428001Frame · chafedTHERE IS DAMAGE ON THE TRANSMISSION DECK FRAME JUST INBOARD OF THE SPLICE. DAMAGE MEASURES AT 0.017” IS 13MM WIDE AND 5MM LONG LOCATED AT APPROX. STA 3640, BL 210R, AND WL 1839.SDR 2A6D2020042701301Frame · chafedTHERE IS CHAFFING ON THE R/H UPPER FORWARD SECTION OF THE X FRAME MEASURED AT .012” DEEP APPROX. 4MM WIDE AND 3 MM LONG.SDR 2A6D2020042201101Structure · gougedCHAFING DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE IS APPROXIMATELY 0.028” DEEP AND 0.35” WIDE BY 0.52”SDR 2A6D20200416001Deck Plate · chafedCHAFING ON THE MAIN GEAR BOX - DECK JUST FORWARD OF DRAIN HOLE. X 4240 , Z 1759, YL 80. THE DEPTH OF THE CHAFE IS 0.010” LENGTH OF 10MM AND WIDTH OF 10MM. THE CHAFE IS ONLY 10MM FWD OF DRAIN HOLE.SDR 2A6D20200415001Deck Plate · chafedTHE TRANSMISSION DECK SKIN HAS CHAFING DAMAGE. THE CHAFE LOCATION IS LOCATED ON THE UPPER SIDE OF THE TRANSMISSION DECK SKINSDR 2A6D2020040300903Frame · chafed3 DIFFERENT LOCATIONS ON THE L/H AND R/H X-FRAMES ON THE INBOARD SIDES.
R/H FWD LOWER LEG
STA 2980, BL 400R, AND WL 2410
.22” X .20”/ .009” DEEP
L/H AFT UPPER LEG
STA 3810, BL 400L AND WL 2440
.24” X .3”/ .012” DEEP
L/H AFT LOWER LEG
STA 3640, BLSDR 2A6D202004010013Bulkhead · chafedCHAFING WAS DISCOVERED ON THE LEFT HAND SIDE OF THE FORWARD BULKHEAD (AIRBUS PN 350A21-1032.59).SDR 2A6D20200401002Stiffener · wornWEAR WAS REPORTED TO THE RH STA2700 STIFFENER (PN: 350A21-1071.23) IN THE FORM OF WEAR
CAUSED BY A NEARBY BOLT HEAD. THE WEAR WAS MEASURED TO BE APPROXIMATELY 7MM (0.276”) IN LENGTH,
1MM (0.040”) WIDE, AND WITH A MAXIMUM DEPTH OF 0.0245”SDR 2A6D20200401003Floor Support · chafedCHAFING WAS DISCOVERED ON THE RH CARGO FLOOR FWD FRAME (PN: 355A21-2122-21). THE CHAFE WAS MEASURED TO BE 0.55" IN LENGTH AND WAS TO BE FOUND TO BE CHAFED THROUGH THE ENTIRE PART THICKNESS OF 0.032".SDR 2A6D2020032600901Stiffener · gougedGOUGE ON THE R/H STA2700 STIFFENER PN:350A21-1071-23SDR QMLA2020031920013Web · crackedDURING 150 HOUR AIRFRAME INSPECTION, THE MECHANIC FOUND THE LEFT HAND PICK UP WEB CRACKED. THIS CRACK WAS REPAIRED PER APPROVED DATA RECEIVED FROM THE OEM/MANUFACTURER.SDR 2A6D2020031600000Floor Panel · corrodedON AIRCRAFT 4553 WE FOUND 3 EACH SPOTS OF CORROSION UNDERNEATH THE L/H SIDE CREW DOORS ON THE FLOOR EDGING. STA.970 TO 2700, WL. 2600, BL. LEFT 736.6.SDR 4DSR2020031201Connector · looseDURING 600HR INSPECTION AFTER REMOVAL OF HORIZONTAL STABILIZER FOR DETAILED INSPECTION. OBSERVED WHAT WAS THOUGHT TO BE A SPOT OF CORROSION ON LOWER LH STABILIZER SKIN, WHICH UNDER CLOSE INSPECTION WAS DETERMINED TO BE A 4 MM HOLE IN SKIN. LOCATION IS 4 INCHESSDR 2A6D2020022760602Deck Plate · gougedAIRCRAFT 7267 HAS A GOUGE LOCATED ON THE AFT R/H SIDE OF THE TRANSMISSION DECK AT APPROXIMATELY STA 3730, WL 1847, AND BL 380R. THE GOUGE MEASURES .25” LONG BY .15” WIDE AND IS .008” AT ITS DEEPEST POINT.SDR 2A6D2020021001Bulkhead · chafedFOUND CHAFE DAMAGE AT THE BACK BAGGAGE COMPARTMENT ON THE FORWARD WALL IN THE TAILBOOM. STA.4174, BL. R355, WL. 2672.2. ATTACHED ARE THE PICTURES OF THE DAMAGE. THERE ARE 3 SEPARATE AREAS THAT MEASURE 10 IN. IN TOTAL LENGTH. THE DEEPEST GOUGE RUNS .028 IN.SDR 2A6D2020021002Cable · unknownTHE METAL FUEL CABLE FROM THE NEW CRFT. L/H INBOARD LOWER AFT LEG ON XFRAME, MAX DEPTH OF .009
APPROX LOCATION OF Z-2867 , X-3705, Y(-398)SDR 2A6D2020021003Bulkhead · chafedDURING INSPECTION FOUND A CHAFE IN THE RIGHT HAND LATERAL BULKHEAD (X-FRAME) ON THE EXTERIOR SIDE AND IS .022" DEEPSDR 2A6D2020020700501Longeron · damagedCHAFING WAS DISCOVERED ON THE LOWER FLANGE OF THE TRANSMISSION DECK LONGERON AT APPROXIMATE STA AND RBL . THE DAMAGE MEASURES APPROXIMATELY 0.006” DEEP, 0.80” LONG, AND 0.12” WIDE.
Y398, X3300, Z-1863. THE TAIL ROTOR YAW CABLE HAS .007 DEEP CHAFFING ON THE SDR QMLA2020012720004Unknown · odorFROM THE PILOTS REPORT: ABOUT 2 MINUTES AFTER DEPARTURE TO PICK UP A SCENE FLIGHT, THE CREW REPORTED THAT THEY BELIEVED THAT THEY SMELLED A HOT SMELL OR SMOKE. I DID NOT NOTICE ANYTHING UNUSUAL, HOWEVER, I IMMEDIATELY INITIATED THE PROCEDURE FOR SMOKE IN CABINSDR QMLA2020013022206Web · crackedDURING AAIP A1660 600HR SCHEDULED INSPECTION IT WAS DISCOVERED THAT THE WEB @ STA. 845 RBL 673.5 HAS A CRACK APPROX 2.50 INCHES ON TOP R/H SIDE IN WHICH IS ALMOST IDENTICAL TO EA 17-5310-EA-2632 DATED 01/23/2019 FOR ACFT. 7248. THIS CRACK IS BEYOND LIMITS SDR 2A6D2020011300101Deck Plate · gougedTRANSMISSION DECK HAS A GOUGE ON THE RIGHT SIDE LOCATED AT APPROXIMATELY STA 3732, WL -2750, AND BL 385R. THE DAMAGE IS APPROXIMATELY .6" LONG AND .2" WIDE AND .022" AT ITS DEEPEST POINT.SDR 2A6R202001104282Frame · chafedL/H INBOARD SIDE OF AFT LOWER LEG OF THE X-FRAME HAS CHAFFING MEASURING APPROXIMATELY 0.011" DEEP AND 0.3" WIDE BY 2.4".SDR QMLA2019121751998Warning Bell · false activationPILOTS REPORT: JUST PRIOR TO LANDING, A WARNING SYSTEM AUDIO “GONG” WENT OFF IN THE PILOTS HEADSET WITH NO ASSOCIATED LIGHT ON CAUTION & WARNING PANEL. WITHIN 4 SECONDS, 2 MORE WARNING AUDIO ALARMS WITH NO ASSOCIATED LIGHT FOLLOWED BY A 5TH AUDIO ALARM WITH ASDR QMLA2019121119097Duct · odorPILOT REPORTED: ELECTRICAL/SMELL FROM HEATING/DEMISTER SYSTEM.
UPON ARRIVAL AND BRIEFING FROM PILOT OF PROBLEM, HE COULD NOT EXACTLY DETERMINE THE TYPE OF SMELL. JUST ELECTRICAL CAME TO MIND, BUT THE SMELL WASN’T EXACTLY THAT. I HAD REMEMBERED SEEING A DISSDR QMLA2019121019095Floorbeam · gougedGOUGING FOUND ON RIB UNDERNEATH CABIN FLOOR AT THE RIB BEHIND THE CO PILOTS COLLECTIVE. GOUGING WAS THROUGH THE COMPLETE THICKNESS OF THE RIB. THE DAMAGE WAS APPROXIMATELY 13/32" IN LENGTH AND LOCATED AT THE BEND RADIUS OF THE RIB. ** THIS AIRCRAFT REMAINS OOSSDR QMLA2019120619094Frame · chafedCHAFFING DAMAGE TO EXTERNAL L/H X FRAME BULKHEAD FROM THE BAGGAGE COMPARTMENT TRIM PANELS AS WELL AS CHAFFING DAMAGE TO THE INTERNAL X FRAME FROM THE T/R CONTROL CABLE. ** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION. **SDR QMLA2019112531989Brushes · failedPILOTS REPORT: AS THE AIRCRAFT APPROACHED THE SENDING HOSPITAL FOR PATIENT TRANSPORT, THE NURSE IN THE BACK DESCRIBED SMELLING AN ELECTRICAL BURNING TYPE ODOR. THE AIR CONDITIONING WAS IMMEDIATELY TURNED OFF AND THE WINDOWS WERE OPENED TO VENTILATE THE CABIN. SDR QMLA2019120639091Frame · chafedGOUGE DAMAGE WAS NOTED ON THE BAGGAGE DOOR FRAME FWD ANGLE IN THE FORM OF 3 GOUGES AS WELL AS CHAFING TO THE TAIL CONE FRONT FRAME. THE DAMAGE IS LOCATED ON P/N 350A21-1240.22 ANGLE AND THE P/N 350A21-4389.20 FRAME. ** THIS AIRCRAFT REMAINS OUT OF SERVICE AT TSDR QMLA2019120619092Frame · chafedCHAFING DAMAGE WAS DISCOVERED ON THE LH AND RH LATERAL BULKHEAD (X FRAME) (PN: 350A21-1051-20/-21). THE LH CHAFE IS APPROXIMATELY 0.011” DEEP AND 0.2” WIDE BY 0.2” LONG AS SHOWN IN FIGURE 1. THE RH CHAFE IS APPROXIMATELY 0.012” DEEP AND 0.40” WIDE BY 0.75” LONSDR QMLA2019120619093Support Frame · 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. ** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OSDR 2020F00065Belt · destroyedDURING A TOUR FLIGHT, SMOKE WAS SEEN IN THE COCKPIT AND A BURNING SMELL WAS NOTED. THE AIRCRAFT RETURNED TO THE AIRPORT WITHOUT INCIDENT. AFTER SHUTDOWN, IT WAS DISCOVERED THAT THE AIR CONDITIONING COMPRESSOR BELT HAD SHREDDED. THE AIR CONDITIONING BELT AND A/SDR QMLA2019091319075Switch · melted30A PANEL PCB SMOKED IN FLIGHT WHILE RETURNING TO BASE. AIRCRAFT LANDED SAFELY BUT SMOKE WAS SMELLED AND SEEN IN COCKPIT, STROBE SWITCH WAS FOUND MELTED TO BOARD. PANEL HAS BEEN REPLACED AND STROBE SYSTEM IS MEL'D, PLACARD IS INSTALLED AND BREAKER IS PULLED. SDR QMLA2019081659069Frame · corrodedDURING A HEAVY MAINTENANCE INSPECTION, DAMAGE WAS FOUND IN THE FORM OF CORROSION .005" DEEP PITTING TO THE OB FLANGE OF THE RH X FRAME. THIS AIRCRAFT REMAINS OOS WHILE THIS DAMAGE IS EVALUATED, AND REPAIRED.SDR QMLA2019081471968Gearbox · making metalDURING AAIP INSPECTION 50HR/30 DAY CHIP PLUG INSPECTION, FOUND METAL PARTICLES ON BEVEL REDUCTION GEARBOX CHIP DETECTOR PLUG. DUE TO SIZE AND COMPOSITION OF THE PARTICLES, AIRBUS RECOMMENDED REMOVAL AND REPLACEMENT OF BEVEL REDUCTION GEARBOX AND EPICYCLIC REDUSDR CA190814008Bolt · damaged(CAN) DURING ROUTINE REPLACEMENT OF SWASHPLATE BEARING IT WAS NOTICED THAT THE BOLTS THAT RETAIN THE EPICYCLIC HAD FAINT SPIRAL MARKS ON THE RECESSED SHANK OF THE BOLTS. (TC# 20190814008)SDR HCMA2019072900001Wire · looseDURING A TOUR FLIGHT FIRE LIGHT ILLUMINATED AND PILOT PERFORMED A PRECAUTIONARY LANDING. UPON INSPECTION OF FIRE DETECTION SYSTEM, FOUND LOOSE WIRE TO LOWER FIRE DETECTOR. WIRE WAS ADJUSTED AND RE-SECURED TO FIRE DETECTOR AND NO FURTHER PROBLEMS WERE FOUND.SDR QMLA2019072519061Unknown · smokeAFTER TAKE OFF , SMOKE IN CABIN OCCURRED, SUSPECT DEMISTER. MECHANIC INSPECTED HEATING AND DEMISTING SYSTEM. NO DEFECTS OR DISCREPANCIES NOTED. PERFORMED NUMEROUS GROUND RUNS. NOTE: NEW DEMISTER DUCT WAS INSTALLED DURING 600 HR INSP. MAY BE BREAKING IN, CSDR CA190726032Switch · failed(CAN) DURING A ROUTINE INSPECTION OF THE PRE BLOCKAGE SWITCH IN ACCORDANCE WITH THE MANUFACTURERS INSTRUCTIONS IT WAS FOUND THAT THE SWITCH FAILED TO CLOSE AT THE CORRECT PRESSURE. (TC# 20190726032)SDR CA190814004Bearing · cracked(CAN) DURING 600 HOUR INSPECTION IT WAS DISCOVERED THAT ONE OF THE (SET OF FOUR) INWARD FACING LAMINATE BEARING WAS WORN BEYOND LIMITS. (TC# 20190814004)SDR CA190710003Bolt · damaged(CAN) UPPER BOLT ON CLOSURE PLATE WAS FOUND LOOSE DURING A DAILY INSPECTION. UPON REMOVAL OF CLOSURE PLATE IT WAS FOUND THAT THE BOLT HAD BEGUN TO ABRADE THROUGH THE CLOSURE PLATE, ELONGATING ITS BOT HOLE AND THE BOLT HEAD ITSELF WAS ABRADED DOWN PAST NOMINAL SDR CA190705005Servo · abnormal(CAN) DURING THE DAILY INSPECTION AFTER THE LAST FLIGHT OF THE DAY , THE FORWARD MAIN ROTOR SERVO INPUT ROD WAS FOUND WITH ABNORMAL MOVEMENT. THE SERVO WAS OVERHAULED 637.6 HOURS PRIOR TO THIS EVENT. THE AIRCRAFT IS GROUNDED AND THE SERVO REMOVED FROM THE AISDR 2019FA0000196Connector · contaminatedDURING A TOUR FLIGHT, THE FIRE LIGHT ILLUMINATED IN FLIGHT AND THE PILOT PERFORMED A PRECAUTIONARY LANDING IN A FIELD. UPON INSPECTION OF THE FIRE DETECTION SYSTEM, WATER WAS FOUND IN THE CONNECTOR PLUG ON THE ENGINE DECK. WATER WAS REMOVED AND NO FURTHER PROBSDR 2019FA0000188Reinforcement · debondedAIRCRAFT WAS IN THE PROCESS OF UNDERGOING A CUSTOMER CONFORMITY INSPECTION WHEN A PIECE OF FOD WAS NOTICED IN THE ENGINE BYPASS VALVE OVERBOARD DUCTING. THE DUCT WAS REMOVED AND THE FOREIGN OBJECT WAS IDENTIFIED AS A PART OF THE DUCT REINFORCEMENT THAT HAD BECSDR QMLA2019061019053Cover · crackedDISCOVERED CRACK ON MAIN ROTOR HUB ANTI VIBRATOR. CRACK WAS ON SIDE BRACKET COVERING SPRING. FOUND DURING AIRWORTHINESS CHECK.SDR 2019FA0000181Shutoff Valve · failedTHE EMERGENCY FUEL SHUT OFF VALVE HAD FAILED THE INTERNAL LEAK RATE OF 1 LITER PER HOUR. A NEW VALVE WAS ORDERED UNDER WO# 267A-2019-I-0049-0093 AND IT TOO FAILED THE INTERNAL LEAK RATE CHECK. ANOTHER NEW VALVE WAS ORDERED UNDER THE SAME WO# AND IT FAILED THE SDR QMLA2019052619051Evaporator · faultyAT APPROX. 0019, DEPARTED FOR A SCENE RENDEZVOUS AT AIRPORT. ABOUT 5 MINUTES INTO FLIGHT, PILOT AND CREW DETECTED AN ACRID ODOR FOLLOWED BY HAZE IN THE CABIN. PILOT TURNED OFF A/C AND OPENED WINDOW AND VENT. THE HAZE CLEARED AND THE ODOR DISSIPATED. AT FIRST ISDR QMLA2019052019048Frame · crackedWHILE WORKING AAIP A 1660.25.1 A CRACK AROUND 68MM LONG WAS FOUND I THE RT PICKUP WEB OF CANOPY FRAME UNDER THE FLOOR. REMOVED PAINT AND PRIMER TO CONFIRM THE CRACK. FOUND THAT IT WAS INDEED CRACKED. DOCUMENTED THE CRACK AND REPORTED IT TO AMC SERVICE ENGINEERSDR QMLA2019043019044Evaporator · malfunctionedCREW SMELLED BURNING ELECTRICAL SMELL IN COCKPIT. TURNED OFF AC AND OTHER UNNECESSARY CONSUMERS. SMELL SOMEWHAT DISSIPATED AND WE MADE A PRECAUTIONARY LANDING AT OUR COMPANY OTHER BASE AS WAS CLOSEST AND BEST OPTION. LANDED SAFELY. UPON POST FLIGHT, FOUND THAT
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