Turbomeca ARRIEL-1B
Service difficulty reports · 807
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 = 'ARRIEL1B' 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 = 'ARRIEL1B' 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 CA980406028Deflector · cracked(CAN) DEFLECTOR CENTRAL ATTACHMENT AREA FOUND TO HAVE A SMALL CIRCUMFERENTIAL CRACK AROUND HOLE APPROXIMATELY .1250 INCH - .1875 INCH OUTBOARD. ON APPLYING LIGHT FINGER PRESSURE, THE WHOLE CENTRAL AREA BROKE AWAY AND POPPED OUT.SDR CA980406029Cover · gouged(CAN) DURING REAR BEARING CLEANING, THE BEARING COVER WAS FOUND TO BE GOUGED IN AREA OF CONTACT WITH BEARING ATTACHMENT NUT. PART TC: 3,848.SDR CA971231004Tach Box · shorted(CAN) TACH BOX CYCLED BLEED VALVE OPEN AND CLOSED A COUPLE OF TIMES BEFORE STAYING OPEN. THIS HAPPENED SPORADICALLY AND AT LOW ALTITUDE, COULD NOT GET FULL POWER.SDR CA980317071Transmitter · inaccurate(CAN) WHEN DEFUELING AIRCRAFT, GAUGE READ 20 PERCENT WHEN EMPTY AND LOW LEVEL FUEL LIGHT WAS NOT ILLUMINATED. FUEL TRANSMITTER REPLACED.SDR CA980602048Switch · leaking(CAN) SMALL FUEL LEAK ON TOP OF MICHIGAN DYNAMICS AIRFRAME FUEL FILTER. FUEL SEEPING AROUND PINS OF THE CANNON PLUG.SDR CA971216040Shaft · sheared(CAN) DRIVESHAFT SHEARED, SUSPECT ON START. PART TC: 65.SDR CA971216038Directional Gyro · failed(CAN) DIRECTIONAL GYRO SPINS CONTINUOUSLY AND VERY RAPIDLY.SDR CA971104013Switch · miswired(CAN) HYDRAULIC CUT-OFF SWITCH WAS MISWIRED TO WARNING HORN, BUT FUNCTIONED PROPERLY IN THE HYDRAULIC CUTOFF MODE. RE: SB 29.01. PART TC: 692.SDR CA971104012Belt · broken(CAN) HYDRAULIC BELT BROKE WITH RESULTANT HYDRAULIC PRESSURE FAILURE.SDR CA971113057Pump · overheated(CAN) BEARINGS VERY TIGHT AND NOISY, AND RUNNING HOT. CAUSED DAMAGE TO THE HYDRAULIC PUMP DRIVE BELT P/N 704-A33-690-004.SDR CA971021012Friction Cup · defective(CAN) PILOT REPORTED CYCLIC CONTROLS WERE BINDING WHEN FRICTION KNOB WAS TURNED TO APPLY FRICTION. OK WITHOUT FRICTION. LOWER CUP NOT PERFECTLY ROUND. SURFACE REWORKED.SDR CA971007003Belt · slipping(CAN) LOSS OF HYDRAULICS ON CLIMB OUT. PILOT CUT OFF HYDRAULIC PRESSURE. AIRCRAFT LANDED. HYD BELT LIKELY SLIPPING AS BELT TENSION COULD NOT BE OBTAINED.SDR CA971113036Fcu · malfunction(CAN) PILOT REPORTED THE MAIN ROTOR RPM TO BE FLUCTUATING WITH POWER CHANGES. RPM TESTER INSTALLED AND CONFIRMED RPM DROP TO APPROX 370 RPM, THEN RETURNED TO 380. SLIGHT POWER REDUCTION RPM WOULD INCREASE TO 395-400 RPM, THEN RETURN TO 380-385 RPM. FCU REPLSDR CA970930001Servo · failed(CAN) SERVO CAUSED FEEDBACK FOR FIRST 20 MINUTES OF FLIGHT THEN IS ALRIGHT. OAT 20C.SDR CA980317070Transmitter · stuck(CAN) FUEL QUANTITY GAUGE STICKING AT 55-80% WHEN REFUELING AIRCRAFT. FUEL QUANTITY TRANSMITTER REPLACED.SDR CA971113037Drive Shaft · sheared(CAN) STARTER GENERATOR DRIVE SHAFT SHEARED DURING START.SDR CA971113035Servo · leaking(CAN) SERVO LEAKING AN EXCESSIVE AMOUNT OF OIL.SDR CA971015051Casing · broken(CAN) BACK CYLINDRICAL PIECE OF DIRECTIONAL GYRO FOUND HANGING BY INTERNAL WIRING. MOUNTING HARDWARE RATTLING AROUND ON INSIDE.SDR CA971113044Fuel Filter · failed test(CAN) FUEL FILTER ASSEMBLY DID NOT INDICATE BYPASS WHEN PRE-FLIGHT BUTTON PUSHED OR ON DUMMY FILTER INSTALLATION FOR TESTING.SDR CA971015049Valve · leaking(CAN) START DRAIN VALVE FAILED FUNCTIONAL CHEAK. LEAKS SMALL AMOUNT OF FUEL BACK TO TANK WHEN ENGINE AT BOTH IDLE AND FULL THROTTLE. REPLACED.SDR CA971015048Hose · ruptured(CAN) DEFROST HEATER HOSE DETERIORATED AND BLEW APART MELTING THE FIRST AID KIT.SDR CA970910014Lever · jammed(CAN) CARGO HOOK WOULD NOT RELEASE ELECTRICALLY OR MANUALLY. THE LOCKING MECHANISM WOULD NOT ROTATE WITHIN THE ASSEMBLY ALTHOUGH THE SOLENOID, HEARD CLICKING RELEASING THE TORQUE ON THE RELEASE LEVER BUSHING THRU BOLT, ALLOWED THE HOOK TO WORK PROPERLY. MISMSDR CA971015043He Generator · failed(CAN) HIGH ENERGY GENERATOR INSTALLED TO CORRECT INTERMITTENT IGNITION PROBLEM. PROBLEM PERSISTED. NEW GENERATOR WAS FAULTY.SDR CA971015042Transmitter · failed(CAN) NO FUEL QUANTITY INDICATION. RESISTANCE CHECK OUT OF LIMITS.SDR CA970904026Servo · leaking(CAN) MAIN ROTOR FLIGHT CONTROL HYDRAULIC SERVO LEAKING AT THE PISTON BASE BEYOND LIMITS.SDR CA970904030Bearing · rough(CAN) LIFE LUBRICATED BALL BEARINGS ON THE TAIL ROTOR PITCH CHANGE PLATE WERE ROUGH AND RACHETY, AND FELT HOT TO THE TOUCH.SDR CA970722013Bushing · rotating(CAN) BLADE PIN BUSHING ROTATING.SDR CA970722011Bushing · rotating(CAN) BLADE PIN BUSHINGS ROTATING.SDR CA970722012Stop · delaminated(CAN) SPERICAL STOP DELAMINATED TO MAX LIMITS.SDR AU970788Blade · delaminated(AUS) TAIL ROTOR BLADE LEADING EDGE EROSION STRIP DELAMINATED (DEBONDED) - DEBONDING EXTENDS SPANWISE FROM AN AREA 105MM(4.13IN) FROM THE INBOARD END OF THE STRIP TO 98MM (3.85IN) FROM THE OUTBOARD END AND CHORDWISE FROM THE TRAILING EDGE TO 25MM (1IN) TOWARDSSDR CA970630002Hinge · delaminated(CAN) DELAMINATIONS CAUSED EXCESSIVE VIBRATION (HIGH FREQ) IN-FLIGHT AND ON GROUND. SPLITS AND DELAMINATIONS IN EXCESS OF ALLOWABLE LIMITS OCCURRED AT VERY LOW T.S.N.SDR CA970626014Tach Box · failure(CAN) BLEED VALVE ELECTRICAL SYSTEM TROUBLESHOOTING INDICATED TACH BOX WAS CAUSING BLEED VALVE LIGHT TO REMAIN ON. TACH BOX WAS REPLACED AND BLEED VALVE FUNCTIONED NORMALLY.SDR CA970731018Blade · cracked(CAN) THREE INCH CRACK FOUND IN THE LOWER SKIN OF A MAIN BLADE. CRACK LOCATED 53 INCHES IN FROM THE BLADE ROOT. CRACK RUNS 90 DEGREES FROM LEADING EDGE.SDR CA970626011Bleed Valve · intermittent(CAN) BLEED VALVE CLOSING INTERMITTENTLY.SDR CA970620004Bleed Valve · failed(CAN) BLEED VALVE DID NOT OPERATE FOLLOWING INSTALLATION. BENCH TEST CONFIRMED INTERNAL FAILURE. WHEN POWER APPLIED, VALVE BECAME VERY HOT.SDR CA970618014Starflex · cracked(CAN) TWO CRACKS IN CENTER SECTION OF STAR, AREA G1 PER MWC 62..20.00.601, FIG. 3. CRACKS EXTENDED DOWNWARD 21 AND 25 MM RESPECTIVELY AND AROUND BOTTOM EDGE AND CONTINUED INBOARD 2 AND 3 MM RESPECTIVELY.SDR AU970624Shear Head · failed(AUS) EMERGENCY FLOTATION DEVICE INFLATED DURING FILLING OF BOTTLE -DAMAGE CAUSED TO SIDE DOOR AND LOWER STRUCTURE - SAFETY LOCK PINON SHEAR HEAD FITTED AT THE TIME - INVESTIGATION FOUND THAT THE PISTON ASSEMBLY THAT PREVENTS BOTTLE DISCHARGE WAS NOT FULLYENGASDR CA970609011Accumulator · leaking(CAN) HYDRAULIC ACCUMULATOR LEAKING HYDRAULIC FLUID AND WILL NOT HOLD PRESSURE.SDR CA970528024Mount · broke(CAN) MIRROR MOUNT BROKE OFF WHERE UPPER ARM TRANSITIONS FROM TUBE TO FLATTENED AREA FOR BOLTING TO UPPER BRACKET. THIS IS COMPANY BUILT FIXTURE.SDR CA970528026Hose · leaking(CAN) HOSE FROM T-VALVE TO LOWER OIL COOLER FOUND LEAKING, 12 INCHES FROM OIL COOLER, BEHIND FRONT STRUT.SDR CA970609009Frame · cracked(CAN) WINDOW ON PILOT''S DOOR WAS FOUND CRACKED. THE CRACK WAS LOCATED ON THE FRAME OF THE SLIDING PORTION OF THE DOOR.SDR CA970528019Tube · chaffed(CAN) P3 AIR LINE CHAFED IN 5 PLACES. REPLACED.SDR CA970609007Belt · broken(CAN) HYDRAULIC BELT FOUND CRACKED NEAR THE BONDED JOINT.SDR CA970528023Diaphragm · burst(CAN) ACCUMULATOR DIAPHRAGM BURST.SDR CA980407015Spline · sheared(CAN) HYDRAULIC PRESSURE LOST DURING FLIGHT. LOSS OF PRESSURE DUE TO SHEARED INTERNAL SPLINES ON THE HYDRAULIC PUMP DRIVE COUPLING SLEEVE P/N S40.SDR CA970421021Hinge · delaminated(CAN) TAIL ROTOR LAMINATED HINGE FOUND WITH EXCESSIVE CRACKS AND DELAMINATIONS.SDR CA970528011Chip Detector · inoperative(CAN) CHIP DETECTOR INOPERATIVE, OPEN CIRCUIT BETWEEN TIP AND PIN B. REPLACED.SDR CA970409001Hinge · delaminated(CAN) OVER A PERIOD OF 5 HOURS, PILOT NOTED AN INCREASED VIBRATION. INSPECTION REVEALED DELAMINATED ELASTOMERS ON LAMINATED HINGE OF TAIL ROTOR. PART TC: 1,208.SDR CA970409002Starflex · cracked(CAN) STARFLEX ASSEMBLY FOUND CRACKED ON TRAILING EDGE OF ARM. PART TC: 2,102.SDR HAIHEEA9281Engine · making metalIRON IN OIL - SAMPLE INCREASED.
Back to Turbomeca ARRIEL-1B