Air Tractor AT-802A

Service difficulty reports · 184

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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 = 'AT802A'
  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.

SDR CA140818018Actuator · failed(CAN) AFT CAP OF SCOOP ACTUATOR FAILED DURING FUNCTION TEST BY PILOT ON GROUND RT SCOOP.Aug 8, 2014 · Airtrc AT802A · Standard Practices/StructuresSDR CA140806013Gearbox · making metal(CAN) CHIP LIGHT IN FLIGHT, FOUND TO BE WITHIN LIMITS, SMALL SLIVER, ON THE AGB CHIP PLUG.Aug 1, 2014 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA140630017Engine · malfunctioned(CAN) THE PILOT PERFORMED WATER DROPPING EXERCISES. UPON COMPLETION OF THE LAST OF 3 WATER DROPS, DURING CLIMB PORTION OF FLIGHT, THE PILOT OBSERVED SEVERE ENGINE VIBRATION, NOISE AND BELCH FLAME AT REGULAR INTERVALS OF SOMEWHAT LESS THAN ONE SECOND WITH "NORJun 16, 2014 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA140425006Crossover Tube · out of adjust(CAN) PILOT REPORTED ACFT ROLLING SLIGHTLY RIGHT. RUDDER/AILERON INTERCONNECT FOUND CROSSED OVER. THIS CONDITION WAS REPLICATED ON GROUND WHEN HARD RT OR LT RUDDER AND AILERON APPLIED. BRACKET ADJUSTED TO ENSURE CABLE RUN STRAIGHT ON FUSELAGE FRAME TO PREVEApr 23, 2014 · Airtrc AT802A · Rudder Control SystemSDR CA140414003Belt · torn(CAN) AIR CONDITIONER DRIVE BELT FOUND TO BE TORN IN HALF. AIR CONDITIONER COMPRESSOR FOUND TO BE SIEZED.Apr 11, 2014 · Airtrc AT802A · Cabin Cooling SystemSDR KTEG2014FA0000051Arm · lack of lubeBETA BLOCK ASSY, PART OF BETA ARM ASSY, WAS NOT LUBRICATED AT INSTALLATION. LACK OF LUBRICATION CAN CAUSE THE ARM ASSY TO FREEZE UP IN THE BETA ARM. IF IT CAN NOT ROTATE, IT WILL WEAR INTO THE BETA RING CAUSING EXCESSIVE WEAR. THIS THE THE 3RD ACFT THIS WASJan 23, 2014 · N802PR · Airtrc AT802A · Propeller Controlling SystemSDR CA131219019Tank · cracked(CAN) CRACK FOUND IN AFT LT CORNER OF THE AFT HOPPER TANK. ABOUT 12" LONG AND CRACKED HALF WAY THROUGH THE FIBERGLASS.Dec 17, 2013 · Airtrc AT802A · Agricultural Spray SystemSDR CA131219018Tank · cracked(CAN) CRACK FOUND IN FORWARD RT CORNER OF FORWARD HOPPER TANK. ABOUT 12" LONG AND CRACKED HALFWAY THROUGH THE FIBERGLASS.Dec 17, 2013 · Airtrc AT802A · Agricultural Spray SystemSDR CA131219021Skin · cracked(CAN) WHERE THE GAP COVER, PN: 30314-1, AT802 IPC, EMPENNAGE GROUP, FIGURE 4, ITEM 17. ATTACHES TO THE RT HORIZONTAL STABILIZER, CRACKS ARE PROPAGATING FROM ATTACH SCREW HOLES IN THE WING SKIN, AT THE 5TH, 6TH, AND 7TH HOLE FROM THE AFT, BOTTOM SIDE.Dec 1, 2013 · Airtrc AT802A · Horizontal Stabilizer, Plate/SkinSDR CA131219020Skin · cracked(CAN) WHERE THE GAP COVER ATTACHES TO THE RT HORIZONTAL STABILIZER, CRACKS ARE PROPAGATING FROM ATTACH SCREW HOLES IN THE LOWER WING SKIN.Dec 1, 2013 · Airtrc AT802A · Horizontal Stabilizer, Plate/SkinSDR CA131121006Tube · cracked(CAN) DURING WHAT WAS THOUGHT TO BE A ROUTINE WELD OVERLAP REPAIR, IT WAS BROUGHT TO OUR ATTENTION THAT IT WAS ACTUALLY A CRACK. .7500 OF THE DIAMETER OF TUBE NUMBER 11029-7, AT802 IPC REF FUSELAGE GRP 1 ITEM 169, WAS FOUND TO BE CRACKED AROUND DIAMETER OF TUBNov 18, 2013 · Airtrc AT802A · Fuselage Main, StructureSDR CA130822010Gearbox · making metal(CAN) CHIP PLUG ILLUMINATED DURING CLIMBOUT, ALT 9000FT, PILOT RECORDED ENGINE PARAMETERS 4200 LBS TORQUE, 1700 PRO RPM, ITT 815, OIL TEMP 55, OIL PRESSURE 135. AGB PLUG WAS DETERMINED TO HAVE CAUSED ILLUMINATION. PLUG REMOVED AND SMALL SLIVER FOUND. OIL FIAug 20, 2013 · Airtrc AT802A · Accessory GearboxesSDR CA130822003Engine · power loss(CAN) ACFT WAS FLYING A FIRE SUPPRESSION FLIGHT WHEN THE PILOT EXPERIENCED A LOSS OF POWER. DROPPED THE LOAD OF RETARDANT AND WAS FORCED TO LAND AT A PRIVATE AIR STRIP. ENGINE WILL BE REMOVED ON-SITE AND A RENTAL INSTALLED.Aug 16, 2013 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA130812002Tire · ruptured(CAN) FRONT RT TIRE BLEW OUT UPON LANDING.Aug 9, 2013 · Airtrc AT802A · TireSDR CA130807004Pump · failed(CAN) AFTER LANDING, FUEL WAS DRAINING FROM THE EPA CAN OVERFLOW TUBE. IT WAS DISCOVERED THAT THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP WAS LEAKING FUEL FROM ITS DRAIN LINE AT A RAPID RATE. THE FUEL PUMP WAS REPLACED AND NO LEAKS WERE FOUND. (TC# 20130807004)Aug 5, 2013 · Airtrc AT802A · Engine Fuel PumpSDR CA130807011Gearbox · making metal(CAN) AGB CHIP LIGHT CAME ON IN FLIGHT, SMALL SLIVER FOUND. ALLOWABLE TYPE & AMOUNT, ACFT GROUNDED. RUN RECHECKED & RETURNED TO SERVICE IAW ENGINE MM PROCEDURES. MFG CURRENTLY INVESTIGATING ENG, TSO 1027.2, CYCLES 7818.Aug 2, 2013 · Airtrc AT802A · Accessory GearboxesSDR CA130726013Gearbox · making metal(CAN) CHIP LIGHT ILLUMINATED IN FLIGHT, PILOT RETURNED AND UPON TROUBLESHOOTING IT WAS FOUND THAT AGB CHIP WAS THE PROBLEM. 1 SMALL METAL SILVER AND BLACK MAGNETIC FUZZ FOUND ON CHIP. RGB AND OIL FILTER ALSO CHECKED FOR CONTAMINENTS. NONE FOUND. ACFT RETURJul 25, 2013 · Airtrc AT802A · Accessory GearboxesSDR CA130729017Tube · cracked(CAN) CRACKS FOUND IN LT FUSELAGE CLUSTER FRAME AT REAR FLOAT SUPPORT ATTACH. ACFT FLOWN TO BASE FOR WELD REPAIRS.Jul 21, 2013 · Airtrc AT802A · Wheel/Ski/FloatSDR CA130718001Shaft · worn(CAN) AIR CONDITIONING DRIVE PAD ASSY, PULLY FOUND LOOSE WITH RADIAL PLAY ON REAR BEARING SHAFT SUPPORT. BEARING NOT SEIZED AND WEAR RESTRICTED TO SHAFT OUTSIDE DIAMETER ONLY.Jul 17, 2013 · Airtrc AT802A · Cabin Cooling SystemSDR CA130709008Gearbox · making metal(CAN) WHILE PERFORMING A 1000 HR INSPECTION OF THE ENGINE ACCESSORY GEARBOX SCAVENGE OIL PUMP, 3 HAIR-LIKE FILAMENTS WERE FOUND ON THE ACCESSORY GEARBOX CHIP DETECTOR. THE HAIR-LIKE FILAMENTS THAT WERE ATTACHED TO THE CHIP DETECTOR WERE NOT TOUCHING, AND THERJul 5, 2013 · Airtrc AT802A · Accessory GearboxesSDR CA130702009Attach Bracket · cracked(CAN) DURING THE POST FLIGHT INSPECTION, IT WAS NOTED THAT THE RT LOWER AUXILAIRY VERTICAL FIN FWD OTBD ATTACH BRACKET WAS CRACKED.Jun 28, 2013 · Airtrc AT802A · Vertical Stabilizer Miscellaneous StructureSDR CA130530007Actuator · damaged(CAN) FLAPS MADE EXCESSIVE NOISE WHEN LOWERING FOUND ACTUATOR END CAP WORN AND BALL BEARINGS ENTERING GEARS.May 28, 2013 · Airtrc AT802A · Trailing Edge Flap ActuatorSDR CA130614002Blade · failed(CAN) DURING T/O ROLL, THE ENGINE LOST POWER. THE T/O WAS ABORTED. POST EVENT ENGINE EXAMINATION FOUND FRACTURED 2ND STAGE POWER TURBINE BLADES. THE ENGINE WAS REMOVED AND FORWARDED, WHERE IT WAS LAST REPAIRED LESS THAN 1000 HRS AGO, FOR INVESTIGATION AND REPAMay 18, 2013 · Airtrc AT802A · Turbine SectionSDR CA130522009Warning Light · false activation(CAN) FUEL FILTER LIGHT CAME ON IN FLIGHT.May 13, 2013 · Airtrc AT802A · Central WarningSDR CA130206009Probe · cracked(CAN) WELDS AT FRONT END OF SCOOPS AT DEFLECTORS CRACKING,BREAKING, 2 FINDINGS.Feb 6, 2013 · Airtrc AT802A · Fuselage Structure (General)SDR CA130214006Muffler · cracked(CAN) PILOTS COMPLAIN OF LACK OF HEAT. BLEED AIR SYS INSPECTED AND FOUND THIS UNIT CRACKED. ALONG WITH WORN SCEET TUBING .7500". NEW MUFFLER INSTALLED WITH NEW SCEET ATTACHING TUBING. SYSTEM CHECKED SERVICABLE. FLEET INSPECTION COMPLETED AND FOUND 2 OTHER Feb 5, 2013 · Airtrc AT802A · Engine Noise SuppressorSDR CA130214010Valve · failed(CAN) SEVERAL MINUTES AFTER START, FUEL WOULD EMIT FROM EPA CAN OVERFLOW LINE. SYSTEM CHECKED AND FOUND THAT PURGE VALVE WAS LEAKED INTO DUMP SYS AFTER ENGINE START. NEW VALVE INSTALLED AND SYSTEM CHECKED SERVICEABLE.Jan 22, 2013 · Airtrc AT802A · Engine Fuel DistributionSDR CA130123007Washer · loose(CAN) AFT FLOAT ATTACH PLYON, AFT PYLON TO FLOAT ATTACH BOLT HAS BEEN FOUND LOOSE ON SEVERAL ACFT. WASHERS UNDER NUT AND BOLT HEAD SHOW WEAR THRU 1/3 THICKNESS OF WASHER. BOLT AND NUT ARE RUSTY AND WORKING IS EVIDENT ON ATTACH FITTING. FLEET CAMPAIGN TO ADDRJan 16, 2013 · Airtrc AT802A · Wheel/Ski/FloatSDR CA121213005Pitot Head · leaking(CAN) RECERTIFICATION OF PITOT AND STATIC SYS, AN ABNORMAL LEAK WAS FOUND, ON CLOSE INSPECTION THE ALUMINUM LINE BETWEEN PITOT TUBE AND DRAIN COCK FOR THE PITOT SYSTEM WAS FOUND TO HAVE A PIN HOLE DUE TO BUILD UP OF FIRE RETARDANT THAT CAUSED CORROSION TO SETDec 13, 2012 · Airtrc AT802A · Pitot/Static SystemSDR CA121213007Fuel Cell · contaminated(CAN) EXCESSIVE AMOUNTS OF WATER FOUND IN LT FUEL CELL. PILOT REPORTED TO MAINTENANCE FUEL CAP WAS LEFT OFF AFTER REFUELING WHEN HEAVY RAINS WERE REPORTED. FUEL CELL AND SYSTEM FLUSHED/CLEANED AND ACFT RETURNED TO SERVICE.Nov 19, 2012 · Airtrc AT802A · Fuel StorageSDR CA121023005Longeron · cracked(CAN) LONGITUDINAL CRACK FOUND ON UPPER RT AFT TAIL TOP TUBE LONGERON, PN 11029-8.Sep 21, 2012 · Airtrc AT802A · Fuselage Main, Longeron/StringerSDR CA120917026Float · cracked(CAN) CRACKS FOUND ON LT AND RT FLOAT HOSE GEAR ACTUATOR ATTACH BULKHEAD EMINATING FROM ACTUATOR ATTACH BOLT HOLES.Sep 17, 2012 · Airtrc AT802A · Wheel/Ski/FloatSDR CA120917025Float · cracked(CAN) CRACKS FOUND ON LT AND RT FLOAT NOSE GEAR ACTUATOR ATTACH BULKHEAD EMINATING FROM ACTUATOR ATTACH BOLT HOLES.Sep 17, 2012 · Airtrc AT802A · Wheel/Ski/FloatSDR CA120917021Float · damaged(CAN) RT NOSE GEAR COLLAPSED ON LANDING ROLL OUT. NOSE GEAR ACTUATOR MOUNTING FLANGE FROM FLOAT NOSE BOX END CAP. THE END CAP THAT THE NOSE GEAR ACTUATOR HARD MOUNTS TO EXPERIENCED STRUCTURAL FAILURE.Sep 16, 2012 · Airtrc AT802A · Wheel/Ski/FloatSDR CA120924004Engine · failed(CAN) THE ENGINE EXPERIENCED A FAILURE DURING TAKEOFF. INVESTIGATION FOUND THAT 3 OF THE P/T BLADES ON THE 2ND STAGE DISK WERE BROKEN IN THE FIR TREE AREA AND THE REST BROKEN OFF ABOVE THE PLATFORM AREA. THE DAMAGE WAS CONFINED TO THE POWER SECTION AND IS UNSep 15, 2012 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA120917004Engine · power loss(CAN) THE PILOT HAD TO ABORT A TAKEOFF DUE TO ENGINE NOT MAKING TORQUE. ENGINE PARAMETERS SHOWED NG 91 PERCENT, TORQUE 2500 FT-LB, FUEL FLOW: 96 GALS/HOUR. THE P3 AND PY AND FUEL FILTER WERE CHECKED, TROUBLESHOOTING IS POINTING TOWARDS A FAULTY FUEL CONTROL.Sep 3, 2012 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA120724004Exciter · failed(CAN) WHEN IGNITION SELECTED ON DURING START OR IN CONTINUOUS MODE, THE 5 AMP START CONTROL C/B WOULD TRIP. IT WAS DETERMINED THAT THE IGNITION EXCITER BOX IS UNSERVICEABLE. IGNITOR EXCITER BOX REPLACED FUNTION CHECKED SERVICEABLE.Jul 23, 2012 · Airtrc AT802A · ExciterSDR CA120718008Pressure Switch · faulted(CAN) FUEL FILTER LIGHT ILLUMINATED, FUEL FILTER REMOVED, CLEANED, INSPECTED AND REPLACED. NO MAJOR CONTAMINATION FOUND. FAULTY SWITCH FOUND TO BE SOURCE OF ILLUMINATION, SWITCH REPLACED.Jul 14, 2012 · Airtrc AT802A · Aircraft Fuel Distribution SystemSDR CA120723004Indication Sys · malfunctioned(CAN) PILOT IS REPORTING TORQUE IS DROPPING FROM 3600 TO 3200 WHILE MAKING TURNS WHEN SPRAYING WITH THE ACFT. TORQUE IS HAVING TO BE MONITORED AND INCREASED TO CARRY THE ACFT THROUGH A TURN. WORK PERFORMED ON ACFT TO DATE: CLOSING CHECK, FCU REPLACED, TRIM STJul 11, 2012 · Airtrc AT802A · Engine BMEP/Torque IndicatingSDR CA120702012Engine · power loss(CAN) PILOT WAS TURNING ACFT WHEN THE TORQUE DROPPED BY 400 TO 500 POUNDS ALMOST CAUSING A STALL. TROUBLESHOOTING IS POINTING TOWARDS A PROP GOVERNOR.Jun 28, 2012 · Airtrc AT802A · Engine (Turbine/Turboprop)SDR CA120606009Pressure Switch · failed(CAN) LOW FUEL PRESSURE SWITCH WARNING LIGHT CAME ON DURING FLIGHT. LOW FUEL PRESSURE SWITCH CHECKED IAW MMS 3086 AND SWITCH FOUND STUCK IN CLOSED POSITITION, LIGHT ON.Jun 3, 2012 · Airtrc AT802A · Engine Fuel DistributionSDR CA120604008Pump · leaking(CAN) LOW PRESSURE ENGINE DRIVEN FUEL PUMP FOUND LEAKING FROM TELL TALE DRAIN. FUEL RESIDUE FOUND ON LOWER FIREWALL AND LT BATTERY BOX.Jun 2, 2012 · Airtrc AT802A · Engine Fuel PumpSDR CA120601007Crosstube · cracked(CAN) CRACKED TUBE FOUND IN AFT FUSELAGE, UPPER LT TUBE. TUBE IS IN AREA OF AIR TRACTOR SL 266 EXCEPT FOR IT IS NOT THE DIAGONAL TUBE BUT THE 1 TO THE LT OF IT.Jun 1, 2012 · Airtrc AT802A · Fuselage Main, StructureSDR CA120620003Indicator · fluctuates(CAN) TORQUE GAUGE FLUCTUATED. GAUGE REPLACED & CHECKED SERVICEABLE.May 5, 2012 · Airtrc AT802A · Engine BMEP/Torque IndicatingSDR CA120502009Shaft · cracked(CAN) STARTER GENERATOR WAS REMOVED FOR OVERHAUL, AT 1786 HRS TTAF ON 21 FEB 2012. DURING OVERHAUL, FOUND A CRACK RADIALLY AND LONGITUDINALLY IN THE DRIVE SPLINE THAT ENGAGES WITH THE ENGINE. THE STARTER GENERATOR WAS MFG IN MARCH 2006. THE CRACKED SHAFT WASApr 9, 2012 · Airtrc AT802A · Starter-GeneratorSDR CA120403005Wire Harness · chafed(CAN) DURING POWER SECTION MODULE REMOVAL FOR CT WHEEL BLADE TIP RUB, THE T5 WIRE HARNESS WAS FOUND CHAFED THROUGH STAINLESS STEEL BRAIDING AND INSULATION TO CONDUCTOR. T5 WIRE HARNESS WAS CONTACTING INNER COMBUSTION CHAMBER LINE AT 11:00 O`CLOCK AND 1:00 OApr 2, 2012 · Airtrc AT802A · Turbine Engine System WiringSDR CA120329011Gusset · cracked(CAN) CRACK FOUND IN RT AREA OF SL 71 REV D AREA C, HOWEVER THIS IS THE UPDATED FRAME CLUSTER. CRACK WAS ON THE WELD WHERE THE FINGER GUSSET ATTACHED TO THE LOWER FUSELAGE TUBE IS WELDED TO THE AFT FLOAT FITTING ATTACH PLATE.Mar 27, 2012 · Airtrc AT802A · Fuselage, Landing Gear Attach FittingsSDR CA120329013Longeron · cracked(CAN) LT LOWER LONGERON TUBE AT REAR KICKER STRUT GUSSETS AND LOWER LONGERON TUBE CRACKED IN AREA "C", SL71 FIGURE 1, APPROXIMATELY 1.25" LONG RISING UP DIAGONALLY.Mar 23, 2012 · Airtrc AT802A · Fuselage Main, Longeron/StringerSDR CA120329012Crosstube · cracked(CAN) TOP CROSS TUBE CRACKED AT WELD ON RT FWD VERTICAL STABILIZER ATTACH FITTING, AFT FITTING FWD SIDE.Mar 23, 2012 · Airtrc AT802A · Fuselage, Stabilizer Attach FittingsSDR CA120227016Control Box · failed(CAN) DURING ACTIVATION AFTER WINTER MX, A TEST OF THE FIRE FOAM INJECTION CONTROLLER WAS CARRIED OUT, AT THAT TIME SMOKE WAS NOTICED IN THE COCKPIT ORIGINATING FROM THE SIMPLEX FOAM SYS CONTROL MODULE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT DURING THEFeb 27, 2012 · Airtrc AT802A · Extinguishing System
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