Aerospatiale AS 355F2
Service difficulty reports · 69
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 = 'AS355F2' 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 = 'AS355F2' 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 CA190528012Gearbox · making metal(CAN) MAIN GEARBOX BEVEL REDUCTION (MGB) CHIP LIGHT ON AIRCRAFT STARTUP, AIRCRAFT GROUNDED. DURING STARTUP PILOT NOTICED, MGB CHIP LIGHT ILLUMINATED. PILOT SHUTDOWN, AND INSPECTED ALL MGB CHIP PLUGS. THE LOWER MGB CHIP PLUG CONTAINED A LARGE CHIP. A PICTURE SDR H0CR2018050101Compressor · delaminatedNR 1 AND 2 ENGINE POWER CHECKS WERE TRENDING DOWN. DURING ROUTINE 300HR/12MONTH INSPECTION, FOUND EXCESSIVE DELAMINATION OF THE LINING OF THE COMPRESSOR CASE HALVES ON THE ENGINES. REPLACED THE WORN CASE HALVES, AND PERFORMED POWER CHECKS, RESULTS WERE IMPROVSDR CA150603011Servo · failed(CAN) RIGHT MAIN SERVO PN 31026-110 TSO 0.0 RETURNED FROM OVERHAULED. SERVO INSTALLED ON AIRCRAFT & FAILED ELECTRICAL SERVO FUNCTION TEST. SERVO PN 31026-110 REMOVED UNENVIABLE TSO 0.0. SERVO RETURNED. DESCRIPTION OF DEFECT, SERVO LIMIT WARNING INDICATION SDR 2015FA0000049Scissors · unserviceableINSTALLED THE O/H SCISSORS LINK AND WAS NOTIFIED BY THE CUSTOMER THAT ON A ROUTINE ALF CHECKS, ON THE ROTATING SCISSORS LINK THAT ABLE ENGINEERING HAD RE-BUSHED AND REFINISHED AT CONSIDERABLE COST AND DELAY, THE UPPER ATTACHMENT TO MAST FITTING EXHIBITED SOME SDR CA140627006Starter Gen · inoperative(CAN) AFTER ATTEMPTING TO START RT ENGINE, A SMALL NOISE OCCURRED BUT THE ENGINE DID NOT ROTATE, MUCH LESS START.SDR CA130603019Shaft · damaged(CAN) IN FLIGHT SURGE ON NR 1 ENGINE DURING MAINTENANCE OPERATIONS, THE FCU WAS REMOVED AND FOUND INPUT SHAFT DAMAGED.SDR 2011FA0000529Skin · crackedDURING INSPECTION, A LARGE CRACK WAS FOUND ON UPPER VERTICAL FIN NEAR THE FWD ATTACHMENT POINT. CRACK IS LOCATION ON L/E EXTENDING FROM RT SIDE TO LT SIDE OF ACFT IN THE AREA ABOVE THE FWD REINFORCEMENT. TOTAL LENGTH OF CRACK IS 8 INCHES. COULD BE IMPROPER SDR CA110321007Bearing · broken(CAN) ENG CHIP LIGHT EXPERIENCED. SERVICEABILITY CHECK CARRIED OUT. ENG CHIP LIGHT EXPERIENCED. GEARBOX REMOVED, DISCOVERED OUTER RACER OF NR 4 BEARING BROKEN. GEARBOX REPLACED.SDR 2011F00023Fire Detector · false indicationWHILE FLYING TO DESTINATION, THE LT ENGINE FIRE LIGHT ILLUMINATED. 1 PASSENGER WAS ABOARD. PILOTS MADE A PRECAUTIONARY DIVERSION TO OTHER AIRPORT WHICH WAS THE CLOSEST AIRPORT. UPON LANDING, UNLOADED THE PASSENGER AND CALLED OUR MX DEPARTMENT AND OPS DEPARTSDR E30A20090704001Engine · making metalNR 1 ENGINE CHIP LIGHT ILLUMINATED ON MASTER WARNING PANEL. CHIPS FOUND ON DETECTORS, ENGINE REMOVED FOR REPAIR.SDR CA080723004Stop · damaged(CAN) ACFT WAS CLIMBING AT APPROX 6000` ASL. (OAT 1°C). COLLECTIVE HIT ITS UPPER STOP DURING A POWER INCREASE. AT THIS POINT TORQUE READING WAS APPROX 65 PERCENT. T4 AND NG WERE WELL WITHIN MAX CONTINUOUS LIMITATIONS. ON 14 MAY 2006, SB 67.00.12 REV. 2 WAS CASDR 550001062008Unknown · odorAS PILOT STARTED DESCENT, CREW NOTICED STRONG SMOKE ODOR IN COCKPIT; FIRST ODOR WAS "CHEMICAL ODOR" WHICH QUICKLY BECAME "ELECTRICAL" IN NATURE. AS CREW LOOKED OUTSIDE TO CHECK FOR AN OUTSIDE SOURCE, PILOT CHECKED INSTRUMENTS & CAUTION LIGHT PANEL WITH NOTHINSDR 2007FA0001016Skin · wornRT AND LT FUSELAGE SKIN AT TAILBOOM ATTACH BULKHEAD. FOUND WORKING RIVETS ON BOTH SIDES. (40) FOUND SKIN UNDER WORKING RIVETS WORN .018. ASB 05-00-42 AS FACTOR. FUSELAGE SENT TO A REPAIR FACILITY FOR SKIN REPLACEMENT. (K)SDR CA070912008Pump · defective(CAN) ENGINE AUTO-REIGNITION ACTIVATED IN FLIGHT. REPORTS OF SOFT (BANG) PRECEEDING DECEL. INVESTIGATION REVEALED AIR IN FUEL SYSTEM, SUBSEQUENT TROUBLESHOOTING FOUND ENGINE DRIVEN FUEL PUMP DEFECTIVE. (TC NR 20070912008)SDR CA070518001Lever · broken(CAN) PART BROKE IN (2) PIECES JUST ABOVE ATTACHMENT POINT DURING ENGINE PRE-START CHECK PROCEDURES. (TC NR 20070518001)SDR BAQA20070011Wire Harness · fatiguedDURING CRUISE FLIGHT THE RT (NR 2) ENGINE FIRE WARNING LIGHT ILLUMINATED WITH NO SECONDARY INDICATION OBSERVED. AIRCRAFT LANDED SAFELY AT A NEARBY EMS HELIPAD WHERE TECH FOUND A BROKEN WIRE AT ONE OF THE ENGINE DETECTORS. WIRING REPAIRED IAW MFG STANDARD PRASDR BAQA20070007Line · cutDURING POST FLIGHT WALK AROUND INSPECTION FOUND MAJORITY OF TAILBOOM OF AIRCRAFT COVERED IN BLACK OIL. REPAIRED CUT OIL LINE.SDR BAQA200700005Compressor · seizedPILOT WENT TO START NR 1 ENGINE. ENGINE WOULD NOT TURN. FOUND ENGINE SEIZED. REMOVED AND REPLACED ENGINE ASSEMBLY. BROUGHT ENGINE TO ARC, DISASSEMBLED ENGINE AND FOUND 2 (6TH STAGE) COMPRESSOR BLADES BROKEN AND SEIZED THE COMPRESSOR, ALSO REMOVED THE TURBINE SDR BAQA200600010Gearbox · making metalMAIN GEARBOX CHIP LIGHT ILLUMINATED ON GROUND RUN UP DRAINED AND FLUSHED GEARBOX PERFORMED REQUIRED PENALTY RUN. CHIP LIGHT ILLUMINATED AGAIN. REMOVED AND REPLACED MAIN GEARBOX ASSEMBLY.SDR BAQ2005F00004Pump · unknownPUMP REMOVED IN COMPLIANCE WITH AD 03-21-09. (K)SDR IJA2005F00003Starter Gen · vibrationSTARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. (K)SDR BAQA094539Gyro · failedGYRO FAILED. REPLACED WITH SERVICABLE UNIT.SDR CA040806005Bushing · loose(CAN) ALL 3 BUSHINGS FOUND LOOSE ON D.I. STARFLEX WAS REPLACED.SDR CA040723004Bushing · loose(CAN) ALL 3 BUSHINGS FOUND LOOSE ON D.I. STARFLEX WAS REPLACED.SDR BAQA094679Transmitter · failedTORQUE TRANSMITTER UNIT FAILED OUT OF BOX, WILL NOT ADJUST. RETURNED TO TRADEWIND INTERNATIONAL.SDR BAQA094582Indicator · intermittentACTUATION LIGHT ON CAD AMBER RT ON HSI INTERMITTENT. REPLACED WITH SERVICEABLE UNIT.SDR BAQA094252Shaft · severedSHAFT SEVERED ON UNIT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004SDR BAQA094193Pump · failedPUMP FAILS TO PROVIDE SUFFICIANT PRESSURE. REPLACED WITH SERVICABLE UNIT. 04/26/2004SDR BAQA094236Fuel Nozzle · dirtyREQUIRES CLEANING AND FLOW CHECK. FUEL NOZZLE IS ORIGINAL EQUIPMENT OFF OF ENG. REPLACED WITH SERVICABLE UNIT. 04/22/2004SDR BAQA093729Filter · failedUNIT FAILED FILTER BY-PASS CHECK. THIS UNIT WAS ORIGINALLY ON THE ENGINE WHEN INSTALLED ON A/C S/N 5498. REPLACED WITH SERVICABLE UNIT. 03/11/2004SDR BAQA092464Shaft · wornBLEED VALVE SHAFT WORN. BLEED VAVLE IS ORIGINAL EQUIPMENT OFF OF ENGINE. REPLACED WITH SERVICABLE UNIT. 02/25/2004SDR BAQA092608Case Half · crackedPLASTIC MISSING/CRACKED BEYOND LIMITS. UNIT ORIGINAL EQUIPMENT OFF OF ENG.. REPLACED WITH SERVICABLE UNIT. 02/26/2004SDR BAQA091613Case · damagedCASE HALVES OF COMPRESSOR, COATING LIFTING. PART REPLACED WITH SERVICABLE UNIT.SDR BAQA091155Receiver · failedRECEIVER DISPLAY DOES NOT WORK. REPLACED WITH SERVICEABLE UNIT.SDR BAQA089603Fuel Control · malfunctionedFUEL CONTROL PRODUCING HUNG STARTS, OCCURING BETWEEN 50 PERCENT AND 60 PERCENT. REPLACED WITH SERVICEABLE UNIT. 11/10/03SDR BAQA088838Transmitter · inoperativeTORQUE TRANSMITTER IS INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.SDR BAQA088677Servo · leakingTAIL ROTOR SERVO LEAKING AT SHAFT. REPLACED WITH SERVICEABLE UNIT.SDR BAQA088189Servo · leakingMAIN ROTOR SERVO LEAKING. REPLACED WITH SERVICEABLE UNIT.SDR BAQA087566Transceiver · malfunctionedTRANSCEIVER DOES NOT POWER UP. REPLACED WITH SERVICEABLE UNIT.SDR CA030407010Frame · cracked(CAN) DURING A 6000 HR. 2T AIRFRAME INSPECTION, TAILBOOM TAILCONE AREA WAS INSPECTED AS AN REQUIREMENT OF EUROCOPTER S/B 55.00.09 'CHECK OF FIN ATTACHMENT FRAME. A CRACK WAS FOUND EMANATING FROM AN ANCHOR NUT ATTACHMENT RIVET IN TWO DIRECTIONS. THIS CRACK HAD SDR BAQA084698Controller · brokenBACK OF CONNECTOR ON HSI IS BROKEN. BROKEN AT TIME OF RECEIVING.SDR BAQA081640Engine · malfunctionedENGINE FAILING POWER CHECK. REPLACED WITH SERVICEABLE UNIT.SDR BAQA081639Engine · malfunctionedENGINE FAILING POWER CHECK. REPLACED WITH SERVICEABLE UNIT.SDR CA020815001Drive Shaft · sheared(CAN) IN CRUISE FLT, NR 2 ENGINE TORQUE DROPPED BELOW ENGINE TRIM ADJUSTMENT WITH POWER FLUXS. NR 2 ENGINE THROTTLED BACK FROM FLT TO IDLE. RETURNED TO GATE AS A PRECAUTION. ENGINE DECELED FROM POINT TO ACTIVATE REIGNITION SYS, & CONTINUED TO SPOOL DOWN TO ASDR 2002FA0000789Seal · leakingMECHANIC NOTICED DRIPPING OF FLUID WHILE AIRCRAFT TOOK OFF, RADIOED PILOT AND REQUESTED AIRCRAFT TO RETURN TO BASE. INSPECTION FOUND FUEL COMING FROM (SEAL DRAIN). REMOVAL OF PUMP, INSPECTION FOUND SHAFT SEAL DETERIORATED.SDR 2001FA0000234Blade · crackedFOUND CRACK ON PREFLIGHT. NO SURE CAUSE FOR CRACK. CRACK BEYOND LIMITS.SDR 20000515SH033Cowling · departedRIGHT HAND MAIN GEARBOX COWLING CAME OFF OF AIRCRAFT DURING FLIGHT. NO DAMAGE TO AIRCRAFT OTHER THAN MGB COWL ITSELF. NO PERSONAL OR PROPERY DAMAGE OCCURRED. (X)SDR 98ZZZX2596Blade · defectivePILOT REPORTED T/R GEARBOX CHIP LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. PILOT DIVERTED TO NEAREST AIRPORT AND SECURED HELICOPTER. EXAMINATION OF CHIP DETECTOR BY MAINTENANCE DETERMINED GEARBOX FAILURE. DUE TO PREVIOUS DIFFICULTY IN BALANCING TAIL ROTOR, MASDR 98ZZZX1683Control Cable · frayedCABLE FRAYED AND BEARING WORN OUT CAUSING BINDING OF N2 LINKAGE. SUBMITTER SUGGESTED INSTALLING A BETTER, MORE RELIABLE SYSTEM.SDR HEEA0012199Indicator · defectiveHIGH RESISTANCE ACROSS RED AND BLUE WIRES.
Back to Aerospatiale AS 355F2