Aerospatiale AS 355F1
Service difficulty reports · 203
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 aircraft_model_key = 'AS355F1' 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 aircraft_model_key = 'AS355F1' 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 TLLA205070200139Engine · making metal#1 ENGINE CHIP LIGHT ILLUMINATED DURING FLIGHT. PILOT LANDED AT FIRST SAFEST SPOT AT SOUTHWEST WYOMING REGIONAL AIRPORT WITH NO INCIDENT. GROUNDED AC. SENT MECHANIC OUT AND FOUND CHIPS ON UPPER MAG. PLUG ON GEARBOXSDR CA150411001Control Cable · frozen(CAN) AIRCRAFT WAS PARKED OUTSIDE ON COLD MORNING. DURING START, PIC NOTED NOT BEING ABLE TO BRING ENGINES FROM IDLE TO FLIGHT RPM. SUBSEQUENT INSPECTION OF CONTROL SYSTEM FOUND MOISTURE PENETRATED AND FROZE INSIDE THE FLEXIBLE CONTROL CABLE RENDERING IT INOSDR VMIA201506101671Bearing · failedENGINE FAILURE INFLIGHT DUE TO COMPRESSOR BEARING NR 2 FAILURE.SDR CA111125001Line · cracked(CAN) FLARED END OF OIL PRESSURE DELIVERY TUBE CRACKED UNDER FERRULE, CAUSING OIL PRESSURE LOSS AND SUBSEQUENT IN-FLIGHT SHUTDOWN OF RT ENGINE. US REG NR N355AG INCIDENT OCCURED 18 NOV 2011 ENGINE RECEIVED 23 NOV 2011 CRACK DISCOVERED 23 NOV 2011.SDR CA150108008Bearing · failed(CAN) ENGINE CHIP LIGHT ILLUMINATED. FOUND NR 5 BEARING BRINELLED.SDR 2012FA0000808Servo Control · wornDURING THE ACCIDENT INVESTIGATION, ABNORMALITIES IN THE FORE & AFT SERVO ACTUATOR WERE NOTED. THE SERVO ACTUATOR WAS SENT TO THE NTSB LAB FOR EXAMINATION IN WHICH THERE IS A STRONG POSSIBILITY THAT THE UPPER ROD END ON THE FORE & AFT SERVO WAS A PROBLEM. THE SDR MHIA082G001Canopy · crackedCANOPY FOUND DAMAGED AT THE UPPER LT DOOR FRAME.SDR S9H2010F00000Structure · crackedDURING ROUTINE 100 HR INSPECTION OF TAIL ROTOR DRIVE SHAFT BEARINGS, FOUND CRACK IN THE UPPER VERTICAL STABILIZER. REPLACED VERTICAL STABILIZER WITH SERVICEABLE UNIT.SDR S9H2010F00002Cowling · looseLT ENGINE COWLING CAME LOOSE IN FLIGHT DAMAGING THE COWLING AND THE MAIN ROTOR BLADES. DAMAGED BLADES AND COWLING WERE R & R WITH SERVICEABLE UNITS AND IMPACT DAMAGE INSPECTION WAS PERFORMED IAW MM.SDR S9H2010F00001Fuel Filter · unserviceableRT ENGINE FLAMED OUT WHILE IN FLIGHT, AUTO RE-LIGHT, RE-ENGAGED THEN FLAMED OUT AGAIN, PERFORMED EP IAW POH. R & R ENGINE FUEL FILTER, BLED FUEL SYS AT BOOST PUMP AND FUEL NOZZLE.SDR BAQA20070010Oil System · defectiveMAIN GEAR BOX OIL PUMP FAILED AD03-21-09-R1, DARK PURPLE COLORED OIL IN SIGHT GLASS. REMOVED AND REPLACED MAIN GEAR BOX CONTAINING OIL PUMP, COMBINER GEAR BOX, EPICYCLIC, AND ROTOR SHAFT ASSEMBLY IAW EMERGENCY ALERT SB 05.00.40 REV 2 DATED DECEMBER 20,2006SDR BAQA20070006Terminal · brokenDURING CRUISE FLIGHT PILOT OBSERVED THE NR 2 ENGINE FIRE LIGHT ILLUMINATE . PILOT DID A PRECAUTIONARY LANDING AT AIRPORT. MECHANIC DISPATCHED AND FOUND WIRE ON TERMINAL LUG ON FIRE DETECTOR BROKEN. REPLACED TERMINAL LUG AND COMPLIED WITH AN OPERATION CHECK OFSDR MHI2005F00000Skin · cracked(REF NR: 104942) DURING INSPECTION, FOUND THE UPPER STABILIZER FIN, RT LWR DOUBLER AND NOSE SKIN CRACKED FROM THE 2ND FORWARD RIVET OF THE DOUBLER ACCROSS THE NOSE SKIN. REPLACED STABILIZER WITH SERVICEABLE STABILIZER. (K)SDR MHIA104942Skin · crackedDURING INSPECTION FOUND THE UPPER STABILIZER FIN, RIGHT HAND LOWER DOUBLER AND NOSE SKIN CRACKED FROM THE 2ND FORWARD RIVIT OF THE DOUBLER ACCROSS THE NOSE SKIN. REPLACED STABILIZER WITH SERVICEABLE STABILIZER.SDR HE89099847Starter Gen · unserviceableSTARTER WOULDN'T START ENGINESDR CA040909005Pitch Link · broken(CAN) DURING CRUISE FLIGHT PILOT FELT SUDDEN VIBRATION IN THE M/R FLIGHT CONTROLS SYSTEM. A/C LANDED AT FIRST SUITABLE SITE. UPON INSPECTION, AME DISCOVERED THAT THE 'SCREW IN' RETAINING CUPS ON ONE OF THE M/R PITCH LINKS LOWER ROD ENDS DISINTEGRATED THUS ALSDR CA040811008Blower · damaged(CAN) DURING OPERATION A NOISE WAS HEARD FROM THE BACK OF THE AIRCRAFT, AIRCRAFT WAS LANDED AND DURING INSPECTION TO DETERMINE THE ORIGIN OF THE SOUND IT WAS NOTED THAT THE OIL COOLER BLOWER ASSY WAS DAMAGED AND HAD SEVERAL PIECES MISSING. THE AIRCRAFT WAS RETSDR BAQA094102Pump · inoperativeFUEL PRESSURE DROPPED TO ZERO, AND FUSE BLOWN. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004SDR BAQA094005Fuel Control · failedWARRANTY / EXCHANGE - CORE RETURN FOR WARRANTY/EXCHANGE PO 202317205. CORE S/N 333014 WAS RECEIVED UNDER EXCHANGE PO 202267101 AND INSTALLED ON ENGINE S/N 841012 ON 02/26/2004 AND FAILED 04/02/2004 FOR A TOTAL TSO OF 9.4 HOURS. PLEASE ADVISE WARRANTY MANAGER OSDR CA040324004Ring · worn(CAN) ALL 3 DROOP RING YOKES WERE FOUND WITH WEAR DAMAGE ON OUTSIDE DIAMETER. THIS WEAR CORRESPONDS WITH WEAR FOUND ON THE DROOP RING CONTACT FITTINGS P/N 350A31-1852- 20 ON EACH STAR ARM. SUSPECT THAT THE YOKES WERE AT ONE TIME INSTALLED UNDER EACH STAR ARM SDR CA040324003Bellcrank · damaged(CAN) TAIL ROTOR BELLCRANK FOUND WITH WEAR DAMAGE ON INSIDE YOKE AREA AT THE ATTACHMENT BOLT WITH THE TAIL ROTOR PITCH CHANGE SPIDER. THE WEAR CORRESPONDS TO THE BEARING SURFACE OF BALL END P/N 350A33-2150-01. IT IS SUSPECTED THAT THE ATTACHMENT BOLT WAS NOT TSDR BAQA092581Valve · inoperativeVALVE ONLY LASTED 1.5 HOURS. SCRAPED ON SITE REPLACED WITH SERVICABLE UNIT. 02/10/2004SDR BAQA092580Pressure Switch · failedPRESSURE SWITCH ONLY LASTED 1.5 HOURS REPLACED WITH SERVICABLE UNIT. 02/10/2004SDR BAQA092100Altimeter · stickingRADAR ALTIMETER UNIT INOPERATIVE, STICKING. FAILED OUT OF BOX. REPLACED WITH SERVICABLE UNIT. 01/20/2004SDR BAQA091750Pump · failedFUEL BOOST PUMP PRODUCING INSUFFICIENT PRESSURE. UNIT FAILED OUT OF BOX, REPLACED WITH SERVICEABLE UNIT. 01/19/2004SDR BAQA091886Governor · inoperativeGOVERNOR HAS SLUGGISH RESPONSE IN FLIGHT. 8130 ENCLOSED PART REPLACED WITH SERVICABLE UNIT 01/09/2004.SDR BAQA090117Shaft · shearedSTARTER SHAFT SHEARED. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.SDR CA031114007Connector · burned(CAN) WHILE THE AIRCRAFT WAS IN CRUISE FLIGHT, A BURNING ODOR WAS NOTICED IN THE CABIN. THE PILOT LANDED THE AIRCRAFT UNEVENTFULLY. THE BURNING ODOR WAS TRACED TO THE OVERHEAD LT FUEL PUMP SWITCH. WHEN THE OVERHEAD PANELS WERE REMOVED A BURNED PUMP SWITCH CONSDR BAQA089870Starter Gen · malfunctionedSTARTER GEN HAS INTERMITTENT ROTATION. REPLACED WITH SERVICEABLE UNIT.SDR AUS20030944Skin · cracked(AUS) TAILBOOM SKIN CRACKED IN AREA LOCATED AFT OF THE TAIL ROTOR GEARBOX. CRACK ORIGINATED FROM RIVET HOLE IN TAIL ROTOR GEARBOX COWL BRACKET. CRACKED HAD EXTENDED AFT FOR APPROX 50.8MM TO 76. 2MM (2IN TO 3IN) IN AN AREA NOT NORMALLY VISIBLE WITH VERTICAL STASDR BAQA089028Pump · noisyBOOST PUMP MAKING EXTREMELY LOUD NOISES. REPLACED WITH SERVICEABLE UNIT.SDR CA040806008Planetary Gear · spalled(CAN) EPI CYCLIC WAS MAKING METAL. SOURCE WAS THE PLANET GEAR INNER RACE WAS SPALLING AND MAKING METAL.SDR BAQA088910Indicator · fluctuatesRIGHT FUEL GUAGE FLUCTUATES IN FLIGHT. REPLACED WITH SERVICEABLE UNIT.SDR EJYA566DFire Detector · dirtyENG FIRE WARNING LIGHT ILLUMINATED IN FLT. PILOT PERFORMED REQUIRED EMER PROCEDURES AND PERFORMED EMER LANDING. WHEN MAINT ARRIVED, FIRE WARNING LIGHT HAD EXTINGUISHED. FIRE WARNING SYSTEM WAS INSPECTED AND NO DEFECTS FOUND. MECH CLEANED ALL FIRE DETECTORS SDR BAQA088261Transmitter · failedINSTALLED UNIT AND FAILED ON FIRST FLIGHT OF .2 HOURS. GAGE FELL TO BELOW ZERO. REPLACED WITH SERVICEABLE UNIT.SDR BAQA088263Transmitter · reads lowFUEL QUANTITY FLUCTUATES BETWEEN FULL AND LESS THAN 20 PERCENT. REPLACED WITH SERVICEABLE UNIT.SDR CA030617002Rib · cracked(CAN) DURING ROUTINE INSPECTION OF THE UPPER VERTICAL FIN ATTACHMENT FRAME, AME DISCOVERED RIB TO BE CRACKED. RIB REPLACED AS PER REPAIR MANUAL AND A/C RETURNED TO SERVICE.SDR BAQA086321Adjuster · looseENGINE N1 IDLE ADJUSTMENT SCREW HAS FREE MOVEMENT EITHER RIGHT HAND OR LEFT HAND. REPLACED WITH SERVICEABLE UNIT.SDR BAQA085970Indicator · precessesUNIT PRECESSES BADLY AT TIMES. REPLACED WITH SERVICEABLE UNIT.SDR BAQA085913Circuit Card · failedNR 2 GENERATOR DROPS OFF LINE. REPLACED WITH SERVICEABLE UNIT.SDR CA030305003Nut · loose(CAN) FLT CREW REPORTED THAT THE ROTOR BRAKE HAD NO EFFECT WHEN APPLIED. THE ROTOR BRAKE PACK WAS BEING INSPECTED AND TO HAVE SHIMS ADJUSTED WHEN THE OUT PUT FLANGE LOCK NUT WAS FOUND ON THE DECK BELOW THE FLANGE. THE OUTPUT FLANGE WAS REMOVED AND INSPECTED WISDR BAQA082689Governor · malfunctionedNR 2 ENGINE SN 841010 WOULD NOT TRIM. REPLACED WITH SERVICEABLE UNIT.SDR CA021119003Hub · cracked(CAN) IT WAS NOTED THAT ON THE LAST SHUTDOWN A NOISE WAS BEING GENERATED FROM THE T/R BLADE ASSY REGION. IT WAS MENTIONED TO AN ENGINEER AND THEY CARRIED OUT A EQUIVALENT TO A 30 HOUR INSPECTION AS PER AD 84-064-037(B)R3. (NO DISASSEMBLY) A VERY SLIGHT NOISE SDR CA021031003Bearing · worn(CAN) AIRCRAFT IN CRUISE FLIGHT. PILOT NOTICED NG FLUCTUATION BETWEEN ENGINES, FOLLOWED BY ENGINE AT NR 2 CHIP LIGHT AND AN UNUSUAL NOISE & HOWL. PILOT SHUTDOWN NR 2 ENGINE AND MADE UNSCHEDULED LANDING AT NEARBY AIRPORT. NR 2 ENGINE COMPRESSOR SAGS FOUND WORN SDR CA020911002Bushing · debonded(CAN) ON A DAILY INSPECTION ONE BUSHING WAS FOUND TO BE DEBONDED. THE RETAINING BOLT WAS COMPLETELY PULED OUT OF THE STARFLEX. PILOT REPORTED NO ABNORMAL VIBRATION. STARFLEX ASSEMBLY REPLACED BEFORE NEXT FLIGHT.SDR CA020828005Bearing · elongated(CAN) NOISE WAS HEARD FROM OIL COOLER FAN AREA ON SHUTDOWN. INSPECTION REVEALED NR 6 T/R DRIVESHAFT SUPPORT BEARING BOLT HOLES HAD ELONGATED AND ALLOWED THE T/R DRIVESHAFT AND FAN SHAFT TO MOVE OUT OF ALIGNMENT. NR 6 BEARING SUPPORT, BEARING AND BEARING TRANSDR CA020521008Ball Joint · worn(CAN) AFTER LAST FLIGHT INSPECTION THE LOWER ROD END WAS FOUND TO BE LOOSE. THE STAKED AREA AROUND THE BALL WAS WORN ENOUGH TO ALLOW IT TO COME OUT OF THE ROD END. NEW ROD END INSTALLED.SDR AUS20020106Hook · faulty(AUS) SAFETY HARNESS USED BY CAMERAMAN FAULTY. SNAP HOOK ON HARNESS MAY UNDER SOME CIRCUMSTANCES HAVE THE SPRING LOADED SAFETY CATCH FORCED OPEN ALLOWING THE SNAP HOOK TO SEPARATE FROM THE AIRCRAFT ATTACHMENT POINT.SDR CA020213008Pump · making metal(CAN) NR 1 ENGINE FUEL BOOST PUMP WAS MAKING TOO MUCH NOISE AND VIBRATING AS COMPARED TO NR 2 FUEL BOOST PUMP. INSPECTED THE NR 1 ENGINE DRIVEN FUEL PUMP FILTER AND FOUND NON-FERROUS METAL IN THE FILTER. INSPECTED THE FUEL CONTROL FILTER FOR CONTAMINATION ANSDR AUS20020060Gasket · faulty(AUS) MAIN ROTOR TRANSMISSION EPICYCLIC RING GEAR GASKET FAULTY. GASKET WAS EXTRUDING FROM BETWEEN THE UPPER AND LOWER CASES AND BREAKING INTO PIECES AND CAUSING AN OIL LEAK WHICH WAS PROGRESSIVELY WORSENING. ON DISASSEMBLY THE MATING CASE FLANGES SHOWEDSIGNS
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