Air Tractor AT-802
Service difficulty reports · 87
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 = 'AT802' 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 = 'AT802' 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 CA070316002Line · broken(CAN) DURING ANNUAL INSPECTION, THE BLEED AIR LINE FOR THE CABIN HEATER WAS FOUND UNSECURED UNDER THE COCKPIT FLOOR. FURTHER INVESTIGATION FOUND THE MUFFLER FOR THE LINE BROKEN IN (2) PIECES AT THE FWD END. THE PARTS WERE REPLACED. THE REMAINING AIRCRAFT IN THSDR CA070313008Fitting · chafed(CAN) UPON INSPECTION OF THE P3 AIR LINES, IT WAS DISCOVERED THAT THERE WAS NO CLEARANCE BETWEEN THE P3 FILTER HOUSING NIPPLE FITTING (P/N 3024606) AND THE ENGINE REAR FIRE SEAL PLATES (P/N 3031003 AND 3031004). UPON REPOSITIONING OF THE FIRE SEAL PLATES, IT SDR CA070115014Skin · cracked(CAN) DURING ANNUAL INSPECTION SEVERAL CRACKS WERE DETECTED AT THE RIVET HOLES WHERE THE FLAP BAY SKIN (PN 20438-2) ATTACH TO THE RIB FLANGES. CRACKS WERE STOP DRILLED AND PLATE INSTALLED OVER THE RIB FLANGE AREA IAW AIR TRACTOR INSTRUCTIONS (ATTACHED). THISSDR 2007FA0000239Light · failedPULSELIGHT UNIT FAILED. EVALUATION OF FAILED UNIT REVEALED HIGH HEAT GENERATED WITHIN UNIT AND SIGNIFICANT BURNING.SDR CA060901005Bearing · worn(CAN) A NOISE WAS DETECTED AND THE TACH GENERATOR WAS REMOVED AND FOUND THAT THE LOWER SHAFT BEARING WAS BADLY WORN. (TC NR 20060901005)SDR CA060710006Line · cracked(CAN) DURING THE APPROACH TO THE AIRPORT, THE ENGINE LOST POWER. THE AIRCRAFT WAS DAMAGED ON LANDING. DURING PRELIMINARY INVESTIGATION, IT IS SUSPECTED THAT THE P3 LINE CRACKED CAUSING THE ENGINE TO GO INTO FLIGHT IDLE. THE ENGINE HAS BEEN REMOVED FROM THE AIRSDR CA060731006Line · fractured(CAN) THE ENGINE WAS REPORTED TO FLAME OUT DURING APPROACH RESULTING IN THE AIRCRAFT LANDING SHORT OF THE RUNWAY. SUBSEQUENT INSPECTION REVEALED A FRACTURED P3 PNEUMATIC LINE TO THE FUEL CONTROL. MFG WILL MONITOR INVESTIGATION AND ADVISE OF ROOT CAUSE ONCE ESDR CA060704001Fuel Control · malfunctioned(CAN) DURING FORMATION FLIGHT THE PILOT REDUCED POWER. WHEN POWER WAS RE-APPLIED THE ENGINE WOULD NOT RESPOND INITIALLY TO THROTTLE INPUT. POWER INCREASED AFTER 7 TO 8 SECONDS. THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED. PWC WILL INVESTIGATE THE INCIDSDR CA060407006Pump · leakingDURING DE-INHIBITING INSPECTION, A FUEL LEAK WAS DETECTED AT THE REAR OF THE FUEL PUMP ASSEMBLY.SDR CA050725009Engine · power loss(CAN) DURING FIRE-FIGHTING OPERATIONS, THE AIRCRAFT FLEW THROUGH A COLUMN OF SMOKE AND THE ENGINE REPORTEDLY LOST POWER. THE AIRCRAFT MADE AN EMERGENCY LANDING AND WAS SUBSEQUENTLY CONSUMED BY FIRE. PWC WILL MONITOR THE INVESTIGATION AND ADVISE OF ROOT CAUSESDR CA041210005Attach Fitting · cracked(CAN) DURING ANNUAL INSPECTION THE RT HORIZONTAL STABILIZER AUX FIN WAS LOOSE. UPON INVESTIGATION BY MAINTENANCE STAFF IT WAS NOTED THAT THE FORWARD AUX FIN ATTACH PLATE WAS COMPLTELY CRACKED THROUGH AND THE REAR ATTACH PLATE WAS CRACKED ON BOTH SIDES OF THE RSDR CA031210005Attach Fitting · cracked(CAN) DURING ANNUAL INSPECTION THE RT HORIZONTAL STABILIZER AUX FIN WAS FOUND TO BE LOOSE. UPON INVESTIGATION BY MAINTENANCE PERSONNEL THE FORWARD STABILZER BRACE AND AUX FIN ATTACH PLATE P/N 30653-2 WAS FOUND CRACKED COMPLETELY THROUGH AND AFT STABILIZER BRACSDR CA031107016Eyebolt · cracked(CAN) DURING MPI INSPECTION OF THE HORIZONTAL STABILIZER STRUT ATTACH EYEBOLTS, A CRACK APPROXIMATELY .1875 INCH IN LENGTH WAS NOTED. ALL EYEBOLTS WILL BE REPLACED PRIOR TO THE AIRCRAFT BEING RETURNED TO SERVICE.SDR CA031107015Eyebolt · cracked(CAN) DURING ANNUAL INSPECTION THE HORIZONTAL STAB STRUT ATTACH EYEBOLTS WERE REMOVED FOR INSPECTION. DURING MPI THERE WAS A CRACK OF APPROXIMATELY .3125 INCH IN LENGTH NOTED AT THE RADIUS. ALL OTHER AIRCRAFT IN OUR FLEET WILL BE INSPECTED. THE EYEBOLTS WILL SDR CA030331005Tank · cracked(CAN) DURING INSPECTION A CRACK WAS DISCOVERED ON THE FUEL HEADER TANK END PLATE. THE HEADER TANK WAS REMOVED AND REPLACED WITH A NEW PART. AIRCRAFT WAS RETURNED TO SERVICE.SDR CA030108006Pump · leaking(CAN) A FUEL LEAK WAS DETECTED DURING ANNUAL INSPECTION IN THE PLENUM CHAMBER AREA. IT WAS TRACED TO THE ENGINE DRIVEN FUEL PUMP.SDR CA020606020Brace · cracked(CAN) DURING INSPECTION IT WAS NOTED THAT THE RH AUX VERTICAL STAB WAS VERY LOOSE. UPON FURTHER INVESTIGATION IT WAS NOTED THAT BOTH THE FORWARD AND AFT AUX VERTICAL STAB BRACE PLATES WERE CRACKED COMPLETELY THROUGH. THE AUX VERTIACL STAB WAS REMOVED FROM THE SDR CA020430001Fuel Filter · leaking(CAN) WHILE DE-INHIBITING ENGINE FCU, FUEL FOUND LEAKING FROM FIREWALL MOUNTED FUEL FILTER AT BASE OF CANISTER O-RING. FILTER CANISTER REMOVED, NEW FILTER ELEMENT AND O-RING WERE INSTALLED, FILTER ASSY TORQUED IAW AT-802 MM AND PRESSURE TESTED SERVICEABLE. SDR CA020311003Wire · chafed(CAN) DURING ANNUAL INSPECTION THE MAIN BUSS FEEDER WIRE BETWEEN THE MAIN 120 AMP CIRCUIT BREAKER AND THE COCKPIT BUSS BAR WAS TIE STRAPPED TO THE RT UPPER ENGINE MOUNT TUBE AND WAS CHAFING ON THE 2 BOLT HEADS THAT SECURE THE RT FORWARD FOAM TANK SUPPORT CLAMPSDR CA020201025Bearing · corroded(CAN) DURING THE ANNUAL INSPECTION MAINTENANCE DISCOVERED SERIOUS CORROSION AT THE TOP AND BOTTOM OF OUTER BEARING RACE.SDR CA020128001Wheel · corroded(CAN) DURING ANNUAL INSPECTION THE MAIN WHEELS WERE REMOVED FOR BEARING LUBRICATION AND INSPECTION. THE BEARING RACES REQUIRED REPLACEMENT. UPON REMOVAL OF THE RACES THE WHEEL WAS FOUND CORRODED BEYOND LIMITS. BOTH WHEEL ASSEMBLIES HAVE BEEN REMOVED FROM SERSDR CA020116005Bolt · worn(CAN) DURING THE ANNUAL INSPECTION MAINTENANCE REMOVED BOLT AN5C-32A, AS PER INSPECTION SCHEDULE. THEY FOUND THAT THE BOLT WAS BADLY WORN AND THAT THREADS WERE DAMAGED.SDR CA011210018Line · chafed(CAN) DURING INSPECTION THE AIR CONDITIONER DRIVE ASSY WAS BEING REMOVED FOR LUBRICATION. IT WAS NOTED THAT THE FIRE SLEEVING OF THE FLEX FUEL PRESSURE LINE, HAD BEEN WORN THROUGH. FURTHER INVESTIGATION REVEALED THAT THE STEEL FITTING ATTACHING THE FUEL LINE SDR CA011127005Coupling · split(CAN) DURING ANNUAL INSPECTION THE FLAP DRIVE RUBBER COUPLING WAS FOUND TO BE SPLIT, EARLIER IN THE OPERATING SEASON A LOOSE WIRE ON THE FLAPS DOWN SWITCH CAUSED THE FLAPS TO OVERTRAVEL AND BOTTOM OUT THE ACTUATOR. EXPERIENCE HAS SHOWN THAT WHEN THIS SITUATIONSDR AUS20011170Control Rod · bent(AUS) LT AILERON CONTROL ROD BENT. SUSPECT CAUSED BY WIND GUST.SDR CA010625014Wheel · corroded(CAN) UPON DISASSEMBLY OF WHEEL MAINTENANCE DISCOVERED SERIOUS CORROSION AT THE TOP AND BOTTOM OF THE OUTER BEARING RACE.SDR CA010622018Potentiometer · sparks(CAN) IN FLT, A/C EXPERIENCED "SHOWER OF SPARKS" EMINATING FROM L OWER INSTRUMENT LIGHTING DIMMER POTENTIMETER. DURING APPROACH PILOT TRIED TO ADJUST THELOWER INSTRUMENT DIMMER THESPAR KS FLEW UPON LDG.THE INST WAS INSP/IT WAS NOTED THAT SOLDERED CONNECTION OFSDR CA010625011Frame · worn(CAN) ON INSPECTION THE RUDDER CABLE AND RUDER TRIM CABLE WERE FOUND TO BE RUBBING ON THE CUT-OUT IN THE BULKHEAD AT THE FS 180.SDR AU001244Gear · worn(AUS) FLAP ACTUATOR FAULTY. INVESTIGATION FOUND THE WORM GEAR AND DRIVE GEAR WORN.SDR CA001201021Control Cable · damaged(CAN) WHILE REMOVING PANELS FOR ANNUAL INSP, CABLE FOR ELEV - FLAP INTERCONNECT HAD POPPED OFF FWD LOWER PULLEY ASSY AND WAS TRAPPED BETWEEN PULLEY AND PULLEY GUARD. CABLE P/N 70810-1 HAD BEEN BENT SHARPLY AND WAS SPIKED. INTERCONNECT PUSH ROD WAS BENT AT BOSDR CA001122005Battery Box · corroded(CAN) DURING WINTER MAINTENANCE, THE BATTERIES WERE REMOVED FROM THE AIRCRAFT, THE CENTE AND LEFT HAND BATTERY BOXES WERE FOUND TO BE BADLY CORRODED. THE FOAM LINE FOR THE RETARDANT SYSTEM WAS FOUND TO BE LEAKING AT THE FITTING ABOVE THE BATTERY BOXES. IT APSDR AU981393Bolt · failed(AUS) BRAKE MASTER CYLINDER EYEBOLT FAILED AT THE LOWER END OF THE LOCKNUT CAUSING THE AIRCRAFT TO SWERVE OFF THE RUNWAY. PART TC: 800.SDR AU980647Cables · frayed(AUS) LT AND RT RUDDER CONTROL CABLES BADLY FRAYED AND CLOSE TO FAILURE IN THE AREA WHERE THEY PASS THROUGH THE FAIRLEADS IN THE AFT SEAL BULKHEAD. PART TC: 382.SDR CA980415001Bracket · cracked(CAN) DURING INSPECTION, A CRACK WAS NOTED ON THE WELD AT THE RIGHT AFT HORIZONTAL STABILIZER LOCATION. REPLACED.SDR AU980276Clevis · failed(AUS) LT BRAKE MASTER CYLINDER CLEVIS BOLT FAILED.SDR 97ZZZX2864Pitch Change Rod · failedAIRCRAFT PARKED IN FIELD. DURING RUN-UP, LOUD BANG WHEN PROPELLER WAS REVERSED. ENGINE WAS SHUT DOWN AND PROPELLER WAS REMOVED FOR INSPECTION. ALL DAMAGE WAS CONTAINED TO THE FEATHER SPRING ASSEMBLY.SDR CA961002005Control Cable · damaged(CAN) DURING INSPECTION IT WAS NOTED THAT THE RUDDER CONTROL CABLES WERE BLENDED AT THE FAIRLEADS WHERE THE CABLES EXIT THE FUSELAGE IN THE TAIL SECTION. SUBMITTER STATES THAT AIR TRACTOR SERVICE LETTER #77 ADDRESSES THIS ISSUE AND ADDS THE BLENDING IS WITHIN
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