Air Tractor AT-802A
Service difficulty reports · 184
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 = '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.
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
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 SWDG08RD0113Seal · deformedEXCESSIVE OIL LEAKAGE AROUND PROP SHAFT. FOUND FELT SEAL MISALIGNED AND INTERFERING WITH THE SHAFT SEAL.SDR SWDG20085569Governor · leakingGOVERNOR HAS EXCESSIVE BETA VALVE OIL LEAKAGE AND ERRATIC TORQUE FLUCTUATION. PART REMOVED AND SENT TO REPAIR STATION FOR EVALVUATION.SDR CA080414006Static Line · deterioratedDURING RE-ACTIVATION OF THE AIRCRAFT, THE MAINTENANCE CREW NOTICED THAT THE STATIC LINE FOR THE AUTO PILOT ALTITUDE HOLD P/N 0807-1 WAS DETERIORATED AND CRACKED. THE LINE WAS REPLACED WITH A SERVICEABLE PART. ALL OTHER AIRCRAFT IN THE FLEET WILL BE INSPECTEDSDR CA080128004Control Cable · stuck(CAN) DURING INSP, THE LT RUDDER CABLE WAS FOUND SNAGGED ON THE WATER RUDDER CABLE PULLEY GUARD. (TC NR 20080128004)SDR CA071204003Nut · broken(CAN) THE VACUUM SWITCH WAS SUPPLIED BY MFG. PLASTIC ADJUSTING NUT SPLIT, PREVENTING THE VACUUM SWITCH FROM INDICATING A LOW FUEL PRESSURE WARNING. (TC NR 20071204003)SDR CA071204002Circuit Breaker · cracked(CAN) CB CRACKED. (TC NR 20071204002)SDR CA071203004Spring · cracked(CAN) CRACK FOUND ON TAIL SPRING BEGINNING FROM FWD ATTACH HOLE EXTENDING ALONG SIDE OF SPRING. CRACK THEN EXTENDS TO TOP OF SPRING. LENGTH OF CRACK TOTALS APPROX 6 INCHES. (TC NR 20071203004)SDR CA071016015Engine · power loss(CAN) THE ENGINE LOST POWER DURING FIREFIGHTING OPERATIONS RESULTING IN A FORCED LANDING.SDR CA070830001Bolt · broken(CAN) RETARDANT WAS DISCOVERED LEAKING FROM AROUND THE TANK DOORS. UPON INVESTIGATION, IT WAS NOTED THAT THE BOLT SECURING THE ANGLE INSIDE THE RT DISPERSAL GATE ASSY WAS BROKEN. THE BOLT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 2007083000SDR CA070618003Actuator · failed(CAN) DURING APPROACH FOR A SCOOPING OPERATION, THE FLAPS WOULD NOT EXTEND WITH AN AIR LOAD. THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATION BY MAINTENANCE STAFF, FLAPS WOULD EXTEND THE FIRST 10 DEGREES WITH NO AIR LOAD AND THE ACTUATOR MADE A GRINDING NOSDR CA070803005Turbine Blades · fractured(CAN) THE ENGINE LOST POWER ON TAKEOFF ROLL AND THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED FRACTUED POWER TURBINE BLADES AND A DISCONNECTION BETWEEN THE POWER TURBINE AND PROP. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISDR SWDG20080113Gas Generator · erodedENGINE PARAMETERS ABNORMAL AND SUBSIQUENT INSPECTION FOUND T5 HARNESS DAMAGED AT ASSEMBLY. IT WAS FURTHER NOTED THAT SUBSTANTIAL MATERIAL LOSS IN THE CENTER BOLT HOLE @ THE SCAVENGE TUBE COUPLING WAS ALLOWING COMPRESSOR AIR TO ERODE THE 'T' BOLT SHANK. MANUFSDR SWDG20080024Gas Generator · erodedENGINE REMOVED FOR OVERHAUL EVALUATION. DUE TO THE FINDING OF SEVERE EROSION DAMAGE TO THE 'C' FLANGE AND NUMEROUS BROKEN 'T' BOLTS ON 3 OTHER ENGINES, THE DISSASSEMBLED EXHAUST DUCT AND GAS GENERATOR CASE FLANGES HAVE BEEN PHOTOGRAPHED AND FOUND THAT THIS 4THSDR SWDG20080077Gas Generator · erodedAS THE 'T' HEAD BOLTS WERE BEING REMOVED FOR HSI, ONE NUT DETACHED FROM THE BOLT SHANK WITH THE THREAD INSIDE THE NUT. CLOSE INSPECTION OF THE ADJACENT BOLT REVEALED SEVERE EROSION (NOT CORROSION OR STRETCH DAMAGE) TO THE BOLT SHANK. IT WAS FURTHER NOTED ANDSDR SWD2007F00002Gas Generator · erodedAS THE HEAD BOLTS WERE BEING REMOVED FOR HSI. ONE NUT DETACHED FROM THE BOLT SHANK WITH THE THREAD INSIDE THE NUT. CLOSE INSPECTION OF THE ADJACENT BOLT REVEALED SEVERE EROSION (NOT CORROSION OR STRETCH DAMAGE) TO THE BOLT SHANK. IT WAS FURTHER NOTED AND PHSDR SWDG20080016Gas Generator · erodedBROKEN 'T' HEAD BOLT SHANK FOUND IN COWLING. MANUFACTURER REP VISITED AND TOOK PICTURES OF ERODED GAP IN THE 'C' FLANGE AT THE SCAVENGE TUBE COUPLING LOCATION WHERE THE BOLT HAD BEEN SEVERED. THE DAMAGE TO THE BOLT, FLANGE MATING SURFACES AND COUPLING ARE CLSDR CA070313009Frame · cracked(CAN) DURING ANNUAL INSPECTION, THE LOWER LONGITUDINAL FRAME OF THE STAINLESS STEEL FIREGATE P/N 80450-1 WAS NOTED TO BE CRACKED AT THE FWD END AND BULGED AT THE AFT END. (2) OTHER AC HAVE SIMILAR DAMAGE. WATER WAS FOUND IN THE TUBE AND THE DAMAGE APPEARS TO SDR CA060508014Bolt · loose(CAN) DURING THE ACCOMPLISHMENT OF THE ANNUAL INSPECTION OF THE LANDING GEAR, MAINTENANCE STAFF NOTICED THAT THE LT IB AND RT OB TORQUE PLATES THAT SECURE THE BRAKE CALIPERS WERE LOOSE. THE 6 BOLTS TAHT SECURE THE TORQUE PLATES TO THE MAIN WHEEL AXLE ASSEMBLY SDR CA060303010Hose · chafedWHILE PERFORMING A GEAR SWING DURING THE ANNUAL INSPECTION, IT WAS DISCOVERED THAT THE MLG BRAKE HOSES WERE ROUTED SO THAT THEY WERE RUBBING DIRECTLY ON THE TREAD PORTION OF THE TIRES. THE STRAIGHT BULKHEAD FITTINGS P/N AN832-4D (4 OF) WERE REPLACED WITH 45 DSDR CA050909004Attach Bracket · cracked(CAN) DURING ACCOMPLISHMENT OF A 200 HOUR INSPECTION, A CRACK WAS OBSERVED IN THE ATTACH BRACKET WELD THAT SECURED THE RT UPPER AUX FINLET TO THE HORIZONTAL STABILIZER. THE FINLET WAS REMOVED FROM THE AIRCRAFT FOR REPAIR. UPON COMPLETION OF THE REPAIR THE FINLSDR CA050708005Proximity Switch · looseDURING CRUISE, THE PILOT NOTED A GEAR UNSAFE LIGHT FOR THE NLG. THE AIRCRAFT DID A LOW PASS AT THE AIRPORT. IT WAS DETERMINED THAT THE GEAR WAS DOWN AND IT APPEARED TO BE AN INDICATION PROBLEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. DURING INVESTIGATION BY SDR CA050725016Engine · vibrationTHE ENGINE WAS REPORTED TO EMIT FLAMES ACCOMPANIED BY VIBRATION AND LOUD NOISES. AN EMERGENCY LANDING WAS PERFORMED ON A DIRT ROAD. P&WC WILL INVESTIGATE THE EVENT TO ESTABLISH ROOT CAUSE.SDR CA050614008Torque Tube · cracked(CAN) DURING ANNUAL INSPECTION, RUDDER TUBE ASSY WAS FOUND TO BE UNAIRWORTHY DUE TO CRACKS.SDR CA050516010Fitting · mismanufactured(CAN) DURING INSPECTION, A FUEL LEAK WAS DISCOVERED AT THE FWD ENGINE FIREWALL FITTINGDURING A LEAK/PRESSURE CHECK. UPON INVESTIGATION IT WAS DISCOVERED THAT THE FIREWALL FITTING HAD A FACTORY MANUFACTUINGDEFECT (SCORE MARK) THAT EXTENDED FROM THE HEX NUT PORTSDR CA050513005Frame · cracked(CAN) DURING INSPECTION FUSELAGE LOWER LOGITUDINAL TUBE FRAME LT, A CRACK WAS FOUND. CRACK ESTIMATED TO BE APPROXIMATELY 1/4 TO 1/2 INCHES LENGTH. CRACK EMINATED FROM THE LT AFT FLOAT MOUNT PLATES THAT ARE ATTACHED TO THE FRAMES. PLATES ARE WELDED TO TUBES ASDR CA050510016Line · twistedDURING MAINTENANCE IT WAS DISCOVERED THAT THE FUEL LINE WAS TWISTED, THUS RESTRICTING FLOW. IT WAS ALSO NOTED THAT THE WATER RUDDER RETRACT CABLE PULLEY WAS CHAFING ON THE FUEL LINE. THE LINE WAS INSPECTED AND REPOSITIONED.SDR CA041202005Bolt · cracked(CAN) DURING ANNUAL INSPECTION THE HORIZONTAL STABILIZER STRUT ATTACH BOLTS WERE REMOVED FOR INSPECTION. THE LOWER RH BOLT WAS SUSPECTED OF BEING CRACKED. THE BOLT WAS LPI INSPECTED AND THE CRACK WAS VERIFIED. ALL AIRCRAFT IN OUR FLEET WILL HAVE THE BOLTS INSDR CA041129016Bolt · sheared(CAN) DURING ANNUAL INSPECTION THE IB FORWARD AUX FIN ATTACH BOLT WAS FOUND SHEARED AT THE HEAD. IT APPEARS THAT THE FIN WAS INSTALLED WITH A PRE LOAD CAUSING THE BOLT TO FAIL. SUB-CONTRACTOR HAS BEEN NOTIFIED OF THIS OCCURRENCE AND IS CURRENTLY INVESTIGATINSDR CA041126009Cover · mislocated(CAN) DURING ANNUAL INSPECTION IT WAS NOTED THAT ON THE LT AND RT HORIZONTAL STABILIZERS, THE HOLES THAT WERE DRILLED FOR THE GAP COVER SCREW HOLES WERE DRILLED THROUGH 2 RIVETS ON THE LT AND RT STABILIZERS ON THE LOWER SURFACES ONLY. THE RIVETS ATTACH THE SKSDR CA041118004Fairing · mislocated(CAN) DURING ANNUAL INSPECTION THE HORIZONTAL STAB FAIRING SCREW HOLES FOUND TO BE DRILLED THROUGH THE RIVETS ATTCHING THE SKIN TO THE CLOSING RIBS OF BOTH HORIZONTALSTABS. HOLES WERE LOCATED ON THE LOWER SURFACES ONLY. 7 OF 19 RIVETS WERE DRILL ED ON THE PORTSDR CA030909002O-Ring · torn(CAN) DURING FLIGHT 1 HYDRAULIC PUMP LIGHT ILLUMINATED INDICATING LOW HYDRAULIC FLUID LEVEL. THE LANDING GEAR WAS EXTENDED NORMALLY AND THE AIRCRAFT RETURNED TO THE AIRPORT FOR A NORMAL LANDING. DURING INVESTIGATION THE MAINTENANCE CREW FOUND A HYDRAULIC LEAK SDR AUS20020022Pipe · cracked(AUS) P3 PIPE TO FUEL CONTROL UNIT CRACKED.SDR AU010248Structure · damaged(AUS) RUDDER CRACKED AND SKIN DEFORMED IN UPPER AREA WHERE THE BALANCEHORN ATTACHES TO THE RUDDER STRUCTURE.SDR AU010249Mount · failed(AUS) LT SIDE ENGINE MOUNT RUBBER ISOLATION MOUNTS FAILED. ENGINE LOW ON LT SIDE CAUSING CHAFING OF THE FIRE SEALS ON THE BEARER.
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