Agusta S P A A109K2
Service difficulty reports · 52
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 = 'A109K2' 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 = 'A109K2' 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 I7LA2010F00073Pitch Control · separatedDURING CRUISE FLIGHT, PILOT NOTED A SLIGHT VIBRATION IN THE MAIN ROTOR SYS. THE FLIGHT WAS COMPLETED. UPON POST FLIGHT 1 OF THE 4 UPPER PITCH CHANGE LINK ROD ENDS WERE FOUND TO BE SIGNIFICANTLY WORN. A DETAILED INSP BY MX REVEALED THE PITCH CHANGE LINK RODSDR 109RX042008Longeron · crackedDURING A 3,000-HOUR INSPECTION THE UPPER LT TAILBOOM ATTACH FITTING WAS FOUND TO HAVE A 2-INCH CRACK. THIS EXACT LONGERON/ATTACH FITTING WAS REPLACED JUNE 2004 AT AIRCRAFT TOTAL TIME 5626.7 THE ORIGINAL REPAIR WAS COMPLETED AND APPROVED ON FAA FORM 337 DATED SDR I7LA0002746Trunnion · overheatedSEPT 5, 2004. AIRCRAFT TT: 3518.7 UPON 25 HOUR INSPECTION, TAIL ROTOR TRUNION ENAMEL PAINT DISCOLORED. SIGNS OF EXCESSIVE HEAT.SDR I7AL0002748Trunnion · overheatedUPON DAILY INSPECTION, MECHANIC FOUND ABNORMAL PLAY IN TAIL ROTOR ASSEMBLY. TRUNION- FURTHER INSPECTION FOUND SIGNS OF EXCESSIVE HEAT TO TRUNION ENAMEL PAINT DISCOLORED (BROWN).SDR I7LA0002736Trunnion · looseUPON DAILY INSPECTION, MECHANIC NOTED EXCESSIVE PLAY IN TAIL ROTOR HUB AT TRUNION AREA. TAIL ROTOR HUB WAS REMOVED FOR INSPECTION A SOFT FACE MALLET WAS REQUIRED TO FREE THE TRUNION FROM TAIL ROTOR GEARBOX OUTPUT SHAFT. REMOVAL OF TRUNION NOTED SIGNS OF EXCESDR I7LA0002739Gearbox · damagedREMOVAL OF TAIL ROTOR HUB AND BLADE ASSY. FOUND TAIL ROTOR GEARBOX OUTPUT SHAFT TO HAVE METAL TRANSFER TYPE DAMAGE TO SPLINE AREA. HEAT GENERATED FROM THE TAIL ROTOR TRUNION WAS ALSO EVIDENT.SDR I7LA0002728Trunnion · overheatedUPON 25 HOUR INSPECTION, SIGNS OF HEAT NOTED. ENAMEL PAINT WAS BROWN-DISCOLORED.SDR I7LA0002725Trunnion · overheatedUPON 25 HOUR INSPECTION, TRUNION SHOWS SIGNS OF EXCESSIVE HEAT, DISCOLORED (BROWN) COATING. ENAMEL PAINT.SDR 2002FA0001228Fuel Cell · contaminatedPILOT REPORTS FILLING MAIN TANK THINKING IT IS FULL. AFTER A TIME GAUGES INDICATE LESS THAN FULL. INSPECTION OF INSIDE TANK THROUGH FILLER HOLE REVEALED DATA PLATE FROM FUEL PROBE COVERING THE FLANGE ASSY WHICH ALLOWS FUEL TO CROSSFEED TO OTHER TANK. REMOVESDR R7MA0000801Rod Ends · wornUPPER ROD END WORN BEYOND LIMITS. (X)SDR 99ZZZX4121Trunnion · scoredDURING A PRE-FLGIHT INSPECTION, PILOT NOTED FLAPPING OF TAIL ROTOR BLADES TO BE TIGHTER THAN NORMAL AND FELT TO BE ROUGH. MAINTENANCE NOTIFIED, TAIL ROTOR ASSY REMOVED AND INSPECTED. TAIL ROTOR TRUNNION WAS FOUND SCORED WITH TWO AREAS THAT APPEARED TO BE PITSDR R7MA0000800Coupling · wornSPLINES WORN BEYOND LIMITS. (X)SDR R7MA0000793Switch · intermittentSWITCH INTERMITTENTLY INOPERATIVE. (X)SDR R7MA0000786Hub Assy · damagedDURING PRE-FLIGHT INSPECTION, PILOT NOTED THE FLAPPING OF THE TAIL ROTOR BLADES TO BE TIGHTER THA NORMAL AND FELT TO BE ROUGH. MAINTENANCE REMOVED AND INSPECTED TAIL ROTOR ASSEMBLY. THE TAIL ROTOR TRUNNION WAS FOUND SCORED WITH TWO AREAS THAT APPEARED TO BE SDR R7MA0000789Starter · malafunctionedSTARTER INTERMITTENTLY WILL NOT TURN OVER. WHEN ENGINE IS HOT, STARTER WILL NOT TURN. WHEN AIRCRAFT COOLS FOR 30 MINUTES, ENGINE WILL START. SUBMITTER SUSPECTED BEARINGS IN STARTER/GENERATOR TO BE THE PROBLEM. (X)SDR R7MA0000828Faceplate · damagedFACEPLATE DAMAGED AND UNREADABLE. P/N 58410A2B2C2D2F4L92. (X)SDR R7MA0000827Faceplate · damagedFACEPLATE DAMAGED AND UNREADABLE. P/N 58410A2B2C2D2F4L9N2. (X)SDR R7MA0000722Sensor · malfunctionedGPS SLOW TO COME ON LINE. (X)SDR R7MA0000721Window · crackedWINDOW CRACKED IN SEVERAL PLACES. (X)SDR R7MA0000642Drive Coupling · wornSPLINES WORN BEYOND TOLERANCE. (X)SDR R7MA0000637Damper · wornBUSHINGS WORN. PAC WOULD NOT SUPPLY BUSHING. (X)SDR R7MA0000635Bushing · wornMRH SWASHPLATE FIXED SCISSORS. REPLACED BEARINGS.SDR R7MA0000628Rod Ends · wornROD ENDS WORN. REPLACED FOUR EACH. (X)SDR R7MA0000629Rod End · wornROD END WORN. (X)SDR R7MA0000622Bushing · wornBUSHING WORN AND GROOVED BEYOND LIMITS. (X)SDR R7MA0000621Bushing · wornBUSHING WORN AND GROOVED BEYOND LIMITS. (X)SDR R7MA0000620Bushing · wornBUSHING WORN AND GROOVED BEYOND LIMITS. (X)SDR R7MA0000619Bushing · wornBUSHING WORN AND GROOVED BEYOND LIMITS. (X)SDR R7MA0000613Fcu · failedNR 2 ENGINE IDLE AND TORQUE CHANGES IRREGULARLY. UPON REMOVAL, FOUND FUEL IN P2 LINE AT FCU.SDR R7MA0000612Transducer · failedPRESSURE TRANSDUCER FAILED; WENT BELOW ZERO PSI DURING FIRST FLIGHT. (X)SDR R7MA0000608Rubber · peelingRUBBER COATING PEELING OFF EXTERIOR FUEL CELL. (X)SDR R7MA0000607Rubber · peelingRUBBER COATING PEELING OFF EXTERIOR FUEL CELL. (X)SDR R7MA0000624Support · wornCOATING FOR SWASHPLATE SUPPORT WORN TO LIMITS. (X)SDR R7MA0000559Bearing · spalledBEARING SPALLING. (X)SDR R7MA0000564Valve · cloggedBOTH VALVES CLOGGED AND LEAKING. (X)SDR R7MA0000565Rubber · flakingRUBBER FLAKING JUST INSIDE FILLER NECK.SDR R7MA0000579Magnetic Seal · leakingSTARTER SEAL LEAKING ON NR 2 ENGINE. (X)SDR R7MA0000562Tip Cap · separatedMAIN ROTOR BLADE TIP CAP TRAILNG EDGE SEPARATING. (X)SDR 99ZZZX687Duct · damagedFOUND EXHAUST DUCT DAMAGED, CRACKED.SDR 98ZZZX4000Light · failedTHE RELAYS THAT CONTROL EXTENTION, RETRACTION, AND ROTATION (AIM) ARC, AND THE POINTS EITHER MELT (FUSE) TOGETHER OR IN SOME CASES, HAVE TOTALLY VAPORIZED. THE LIGHT CANNOT BE AIMED ONCE THIS OCCURS. THE EMS NIGHT SCENE FLIGHTS. WHEN THE LIGHT FAILS THE DANSDR R7MA0000231Altimeter · inoperableMODE 'C' IS INOPERABLE. TRANSPONDER READS ONLY DASH MARKS INSTEAD OF THE ALTITUDE. (X)SDR R7MA0000232Altimeter · inoperableMODE 'C' IS INOPERABLE. TRANSPONDER READS DASH MARKS INSTEAD OF THE ALTITUDE. (X)SDR 96ZZZX4869Bearing · failedDURING THE PRE-FLIGHT INSPECTION, THE SEAL OF THE DUPLEX BEARING WAS OBSERVED TO BE DETACHED FROM THE BEARING. DISASSEMBLY SHOWED A TOTAL LOSS OF LUBRICANT AND SEVERAL BALLS MISSING FROM THE OUTER DUPLEX BEARING.SDR 96ZZZX2276Shaft Assy · damagedDURING THE ENGINE 100-HOUR INSPECTION, DAMAGE TO THE ENGINE TO TRANSMISSION DRIVE SHAFT WAS OBSERVED. THE DAMAGE WAS FULL CIRCUMFERENCE AND WAS CAUSED BY CONTACT WITH THE FIREWALL. THE SHAFT PASSES THROUGH TWO HALF FLANGE ASSEMBLIES. THE CLEARANCE BETWEEN TSDR 95ZZZX5919Gyro · loose partsAFTER REMOVING GYRO FROM THE AIRCRAFT, A RATTLING NOISE WAS HEARD INSIDE THE GYRO HOUSING. THE UNIT WAS DISASSEMBLED AND INSPECTED. A SMALL BRASS KNURLED NUT (TOOL?) WAS FOUND INSIDE. THERE WAS IMPACT DAMAGE IN THE SPINNING PORTION OF THE GYRO.SDR 95ZZZX2531Transducer · defectiveUPON LANDING, PILOT REPORTS TRANSMISSION OIL PRESSURE WAS PEGGED TO THE HIGH SIDE ON APPROACH TO HOSPITAL HELIPAD. REPLACED TRANSDUCER, OPS CHECKED OKAY.SDR 95ZZZX2530Lens · failedUPON POST-FLIGHT INSPECTION, ALL 4 'LOGO LIGHTS' HAD BROKEN LENS, APPROXIMATELY ONE-HALF OF THE LENS DEPARTED THE AIRCRAFT IN-FLIGHT. REPLACED LENS AND INSPECTED MAIN AND TAIL ROTOR BLADES. NO DAMAGE FOUND. LENS RETURNED TO DEVORE AVIATION FOR INSPECTION.SDR 95ZZZX2529Lens · failedUPON POST-FLIGHT INSPECTION, ALL 4 'LOGO LIGHTS' HAD BROKEN LENS, APPROXIMATELY ONE-HALF OF THE LENS DEPARTED THE AIRCRAFT IN-FLIGHT. REPLACED LENS AND INSPECTED MAIN AND TAIL ROTOR BLADES. NO DAMAGE FOUND. LENS RETURNED TO DEVORE AVIATION FOR INSPECTION.SDR 95ZZZX2528Trunnion · sleeve looseUPON 100-HOUR INSPECTION OF AIRCRAFT, TAIL ROTOR HUB ASSY WAS DISASSEMBLED FOR INSPECTION. UPON REMOVAL OF TRUNNION, THE PRESSED-ON SLEEVE HAD MOVED .1250 INCH TO .25 INCH OUTBOARD. TRUNNION AND BUSHINGS WERE REPLACED. AIRCRAFT TT, 396.5.SDR 95ZZZX2144Trunnion · damagedPOST-FLIGHT INSPECTION FOUND PLAY IN T/R HUB ASSY. END CAPS OF TRUNNION WERE REMOVED TO SHOW BURNED TEFLON DEBRIS, SOLDER, AND PRO-SEAL, AND ONE SLEEVE PULLED OFF TRUNNION OUTBOARD .0625 INCH. SUBMITTER STATES REDESIGN IS UNDER WAY.
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