# Service difficulty reports: Air Tractor AT-802

A list on [Air Tractor AT-802](https://openairdocs.org/model/air-tractor-at-802.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 87 reports

- [SDR 2026FA0000484](https://openairdocs.org/sdr/2026FA0000484.md): Door Latch · loose · Jun 5, 2026 · Airtrc AT802 · Passenger/Crew Doors
  > PILOTS R/H FWRD DOOR LATCH DOES NOT CONTACT STRIKER PLATE. SHIMMED R/H FWD COPILOTS DOOR LATCH STRIKER PLATE. CONTACT ACCEPTABLE. NO DEFECTS NOTED.
- [SDR 2026FA0000412](https://openairdocs.org/sdr/2026FA0000412.md): Actuator · separated · Feb 11, 2026 · N80253 · Airtrc AT802 · Trailing Edge Flap Actuator
  > WHEN FRONT COCKPIT PILOT ACTUATED THE FLAP SWITCH, BOTH SIDES DROPPED TO FULL DOWN IMMEDIATELY AND THE FLAP SWITCH WAS UNABLE TO MOVE THE FLAPS ON EITHER SIDE. MAINTENANCE FOUND THAT THE FLAP ACTUATOR HAD SEPARATED FROM THE FLAP MOTOR/GEARBOX. REMOVED AND REP
- [SDR 2026FA0000483](https://openairdocs.org/sdr/2026FA0000483.md): Door Latch · bent · Feb 3, 2026 · Airtrc AT802 · Passenger/Crew Doors
  > RCP LH DOOR HANDLE PUSH ROD IS BENT. REMOVED AND REPLACED RCP L/H DOOR HANDLE PUSH ROD. NO DEFECTS NOTED.
- [SDR 2026FA0000499](https://openairdocs.org/sdr/2026FA0000499.md): Access Door · misaligned · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > PILOTS L/H FWD DOOR LATCH DOES NOT CONTACT STRIKER PLATE. SHIMMED PILOTS L/H FWRD DOOR LATCH STRIKE PLATE. CONTACT ACCEPTABLE. NO DEFECT NOTED.
- [SDR 2026FA0000498](https://openairdocs.org/sdr/2026FA0000498.md): Access Door · misaligned · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > FORWARD COCKPIT R/H DOOR LOWER FORWARD LATCH DOES NOT MAKE FULL ENGAGEMENT WITH STRIKE PLATE. SHIMMED FORWARD COCKPIT R/H LOWER FORWARD LATCH TO INCREASE LATCH ENGAGEMENT.
- [SDR 2026FA0000497](https://openairdocs.org/sdr/2026FA0000497.md): Access Door · misaligned · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > AFT COCKPIT R/H DOOR UPPER LATCH HAS LIMITED ENGAGEMENT WITH STRIKE PLATE. SHIMMED AFT COCKPIT R/H UPPER LATCH TO INCREASE LATCH ENGAGEMENT.
- [SDR 2026FA0000496](https://openairdocs.org/sdr/2026FA0000496.md): Access Door · misaligned · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > PILOTS L/H DOOR UPPER LATCH DOES NOT CONTACT STRIKER PLATE. SHIMMED PILOT L/H DOOR UPPER LATCH STRIKE PLATE TO INCREASE LATCH ENGAGEMENT. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.
- [SDR 2026FA0000495](https://openairdocs.org/sdr/2026FA0000495.md): Access Door · misaligned · Dec 5, 2025 · Airtrc AT802 · Windshield/Door Rain/Ice Removal
  > AFT COCKPIT R/H FORWARD LOWER DOOR LATCH DOES NOT FULLY CONTACT STRIKE PLATE. SHIMMED AFT COCKPIT R/H FORWARD DOOR LATCH STRIKE PLATE. CONTACT ACCEPTABLE. NO DEFECTS NOTED.
- [SDR 2026FA0000494](https://openairdocs.org/sdr/2026FA0000494.md): Access Door · misaligned · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > FORWARD COCKPIT R/H DOOR LOWER LATCH DOES NOT CONTACT STRIKER PLATE. SHIMMED PILOT R/H FWD COCKPIT LATCH STRIKE PLATE. CONTACT ACCEPTABLE. NO DEFECTS NOTED.
- [SDR 2026FA0000493](https://openairdocs.org/sdr/2026FA0000493.md): Access Door · bent · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > FORWARD COCKPIT LEFT DOOR HANDLE PUSH ROD ASSY IS BENT. DOES NOT AFFECT DOOR OPERATION.
- [SDR 2026FA0000485](https://openairdocs.org/sdr/2026FA0000485.md): Door Latch · misaligned · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > CO PILOTS (AFT COCKPIT) R/H FWRD DOOR LATCH DOES NOT CONTACT STRIKER PLATE. SHIMMED R/H FWD COPILOTS DOOR LATCH STRIKER PLATE. CONTACT ACCEPTABLE. NO DEFECTS NOTED.
- [SDR 2026FA0000482](https://openairdocs.org/sdr/2026FA0000482.md): Door Latch · unlatched · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > FORWARD COCKPIT R/H DOOR LOWER LATCH DOES NOT MAKE CONTACT WITH STRIKE PLATE. COMMENTS: WUC:11AE0 FWD COCKPIT R/H DOOR LOWER LATCH STRIKER PLATE SHIMMED FOR POSITIVE CONTACT. OPS CHECK GOOD REF A/C 43.13 1B SECTION 4 1-36
- [SDR 2026FA0000479](https://openairdocs.org/sdr/2026FA0000479.md): Striker · loose · Dec 5, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > FORWARD COCKPIT R/H DOOR LOWER LATCH DOES NOT MAKE CONTACT WITH THE STRIKER PLATE.
- [SDR 2026FA0000481](https://openairdocs.org/sdr/2026FA0000481.md): Door Latch · unlatched · Jun 24, 2025 · Airtrc AT802 · Passenger/Crew Doors
  > DOOR SEALS/RIGGING IS A LITTLE OFF FROM NORMAL. COCKPIT IS 5 DB LOUDER THAN TAILS 003 & 005. MEASURED IN FRONT COCKPIT, 30 0#, LEVEL FLIGHT, 105DB IN THIS TAIL, 100DB IN THE REST (INCLUDES BLOCK 0 TAILS TOO) COMMENTS: AWAITING FURTHER DOWNTIME. DOES NOT AF
- [SDR 2024FA0000975](https://openairdocs.org/sdr/2024FA0000975.md): Engine · making metal · Nov 15, 2024 · N8035H · Airtrc AT802 · Engine (Turbine/Turboprop)
  > AIRCRAFT 802-4037 HAD AN ENGINE CHIP DETECTOR LIGHT ILLUMINATE IN-FLIGHT. ABOUT 2 MINUTES LATER, A DROP IN OIL PRESSURE WAS OBSERVED BY THE CREW, ACCOMPANIED BY THE SMELL OF BURNING OIL. AIRCREW SHUT THE ENGINE DOWN & PROCEEDED WITH AN EMERGENCY, ENGINE-OUT
- [SDR 2023FA0000163](https://openairdocs.org/sdr/2023FA0000163.md): Mount · interference · Mar 28, 2023 · N870LA · Airtrc AT802 · Rudder Control System
  > DURING ANNUAL INSPECTION ON ONE OF OUR TWO SEAT AIR TRACTORS, WHILE CLEANING INTERIOR OF AIRCRAFT, DAMAGE TO REAR SEAT MASTER CYLINDERS WAS DISCOVERED. UPON ACTUATION OF RUDDER PEDAL, THE MASTER CYLINDER ON EITHER REAR PEDAL CONTACTS THE SAME SIDE RUDDER PEDAL
- [SDR 2022FA0000616](https://openairdocs.org/sdr/2022FA0000616.md): Gasket · leaking · Oct 13, 2022 · N896WP · Airtrc AT802 · Aircraft Fuel Distribution System
  > FUEL WAS LEAKING FROM FIREWALL AREA OF AIRCRAFT UPON TASING IN. COLINGS WERE REMOVED AND FUEL WAS LEAKING FROM THE TOP OF THE FIREWALL FUEL FILTER. AIRCRAFT BOOST PUMP RAN AND LEAK WAS NOTED TO BE COMING ROM UNDERNEATH BOLT HOLDING FIREWALL FUEL FILTER BOWL ON
- [SDR 2019FA0000175](https://openairdocs.org/sdr/2019FA0000175.md): Adapter · broken · May 29, 2019 · N870LA · Airtrc AT802 · Trailing Flap Position Indicating System
  > WHILE COMPLYING WITH AIR TRACTOR SL 375, A FLAP MOTOR MOUNTING ADAPTER WAS FOUND WITH A BROKEN MOUNTING STUD. IF THE SECOND STUD HAD BROKE THE FLAP MOTOR WOULD FALL DOWN ON THE AILERON PUSH PULL TUBE.
- [SDR CA190307013](https://openairdocs.org/sdr/CA190307013.md): Axle · cracked · Mar 7, 2019 · Airtrc AT802 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) AME UP ON INSPECTION DISCOVER ONE CRACK AT THE END OF TAIL WHEEL AXLE.
- [SDR 2017FA0000535](https://openairdocs.org/sdr/2017FA0000535.md): Pressure Sensor · inaccurate · Nov 1, 2017 · N896WP · Airtrc AT802 · Engine Oil Pressure
  > ON FINAL APPROACH, PILOT NOTICED OIL PRESSURE DROPPING AND JUST AT TOUCHDOWN, OIL PRESSURE DROPPED TO ZERO AND RED WARNING LIGHT ON GLASS DISPLAY CAME ON. PILOT SHUT ENGINE DOWN AND ROLLED TO STOP ON TAXIWAY. AFTER TROUBLESHOOTING, FAILURE OF THE ENGINE OIL PR
- [SDR 2016FA0000333](https://openairdocs.org/sdr/2016FA0000333.md): Fuel Sys · malfunctioned · Jun 6, 2016 · N802CE · Airtrc AT802 · Fuel Storage
  > DURING FLIGHT, PILOT REPORTED LOW LEVEL FUEL LIGHT CAME ON AND TURNED ON FUEL BOOST PUMP, LOW LEVEL FUEL LIGHT EXTINGUISHED. FLIGHT CONTINUED AND THEN LOW LEVEL FUEL LIGHT CAME BACK ON AND PILOT NOTICED FUEL FLOW METER NEEDLE STARTED TO FLUCTUATED AND THEN EN
- [SDR CA160224008](https://openairdocs.org/sdr/CA160224008.md): Windshield · cracked · Feb 24, 2016 · Airtrc AT802 · Flight Compartment Windows
  > (CAN) UPON INSPECTION A 4" CRACK WAS DISCOVER ON LT SIDE WINDSHIELD.
- [SDR CA151201013](https://openairdocs.org/sdr/CA151201013.md): Engine · making metal · Nov 27, 2015 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) ENGINE WAS SENT FOR REPAIR WITH THE OPERATOR REPORTING METAL IN OIL. THE OPERATOR ALSO REPORTED THAT BOTH CHIP DETECTOR LIGHTS WERE ILLUMINATED. THE CUSTOMER PROVIDED A LABORATORY ANALYSIS REPORT OF THE METAL FOUND IN THE MAIN OIL FILTER AND FROM AN OIL
- [SDR CA151015009](https://openairdocs.org/sdr/CA151015009.md): Engine · making metal · Oct 6, 2015 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) DURING A SPRAYING MISSION, THE PILOT RECEIVED A CHIP DETECTOR WARNING AND HE ELECTED TO RETURN TO BASE. APPROXIMATELY 7 MIN LATER, TORQUE FLUCTUATIONS STARTED FOLLOWED BY A LOUD NOISE AND LOSS OF POWER. ALL PARAMETERS HAD DROPPED TO ZERO, THE PILOT DUMP
- [SDR CA150506007](https://openairdocs.org/sdr/CA150506007.md): Engine · failed · Apr 11, 2015 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) WHILE TRAINING ON A DUAL SEAT AT802 FIREBOSS, INSTRUCTOR SIMULATED ENGINE OUT BY REDUCING THE PL TO IDLE SPEED, TRAINEE PILOT RE-APPLIED POWER, AND FLAMES WERE NOTICED FROM EXHAUST STACKS. ENGINE WAS NOT ACCELERATING AND EPL DEPLOYED. ENGINE NOT ACCELER
- [SDR CA150224004](https://openairdocs.org/sdr/CA150224004.md): Engine · failed · Feb 3, 2015 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) THE CUSTOMER CONTACTED THE FSR TO REPORT ENGINE IFSD, LOUD BANG FOLLOWED BY POWER LOSS. THE PILOT PERFORMED AN EMERGENCY LANDING ON A BEACH. POST-EVENT INSPECTION REVEALED THE COMPRESSOR FREE TO ROTATE, UNABLE TO TURN PROPELLER BY HAND, EXHAUST DUCT DI
- [SDR CA141202016](https://openairdocs.org/sdr/CA141202016.md): Engine · power loss · Nov 17, 2014 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) ON TAKE-OFF ROLL FOR A WATER BOMBING MISSION, THE AIRCRAFT WAS ONLY ABLE TO ACHIEVE 2800 FT LBS OF TORQUE BEFORE BEING ON MAX ITT LIMIT (TARGET TORQUE FOR THE DAY WAS 3500LBS). ALL OTHER ENGINE PARAMETERS WERE NORMAL. THE AIRCRAFT DUMPED IT`S LOAD OF WAT
- [SDR CA140807010](https://openairdocs.org/sdr/CA140807010.md): Oil System · contaminated · Aug 1, 2014 · Airtrc AT802 · Turbine Engine Oil System
  > (CAN) CHIP LIGHT. METAL CHIPS FOUND ON AGB PLUG.
- [SDR CA130726012](https://openairdocs.org/sdr/CA130726012.md): Control Cable · broken · Jul 25, 2013 · Airtrc AT802 · Rudder Control System
  > (CAN) LEFT RUDDER CONTROL CABLE, FOUND 1 BROKEN STRAND AT SWAGED FITTING ON RUDDER CONTROL HORN.
- [SDR CA130702003](https://openairdocs.org/sdr/CA130702003.md): Gearbox · making metal · Jun 24, 2013 · Airtrc AT802 · Accessory Gearboxes
  > (CAN) ENGINE CHIP LIGHT AFTER TAKEOFF. LOAD ABORTED RETURNED TO DEPARTURE. ACFT REQUIRED ENGINE CHANGE. AGB CHIP.
- [SDR CA130607013](https://openairdocs.org/sdr/CA130607013.md): Governor · malfunctioned · Jun 6, 2013 · Airtrc AT802 · Propeller Governor
  > (CAN) PROP RPM FLUCTUATING AND 30-50 RPM LOWER THEN RECOMMENDED AT HIGH TORQUE VALUES. SUSPECT HIGH OAT CONTRIBUTTED TO PROBLEM. PROPELLER GOVENER REPLACED.
- [SDR CA130214001](https://openairdocs.org/sdr/CA130214001.md): Bearing · separated · Feb 13, 2013 · Airtrc AT802 · Rudder Structure
  > (CAN) RUDDER ASSEMBLY IS ATTACHED TO VERTICAL FIN BY 3 POINTS TOP, MIDDLE AND BOTTOM. UPON INSPECTION, IT WAS DISCOVERED THAT THE MIDDLE BEARING HAD PARTED FROM THE RUDDER AND THAT THE BOTTOM BEARING SHOWED SIGNS OF WEAR.
- [SDR CA121130012](https://openairdocs.org/sdr/CA121130012.md): Pedal · damaged · Nov 30, 2012 · Airtrc AT802 · Rudder Control System
  > (CAN) RUDDER PEDALS HIT STRUCTURE WHEN ADJUSTED TO FULL AFT POSITION WELL BEFORE FULL TRAVEL LIMITS REACHED. THIS SEEMS TO BE A DESIGN FLAW IN THE RUDDER PEDAL, NOT EASILY FIXED WITHOUT RE-ENGINEERING.
- [SDR CA121213008](https://openairdocs.org/sdr/CA121213008.md): Coupling · twisted · Nov 19, 2012 · Airtrc AT802 · Trailing Edge Flap Actuator
  > (CAN) RUBBER FLAP ACTUATOR COUPLING FOUND EXCESSIVELY TWISTED DURING FLAP ACTUATOR INSPECTION. RUBBER COUPLING REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA120816003](https://openairdocs.org/sdr/CA120816003.md): Adapter · broken · Aug 13, 2012 · Airtrc AT802 · Trailing Edge Flap Actuator
  > (CAN) FLAP MOTOR ACTUATOR ADAPTER PLATE STUD FOUND TO HAVE BROKEN OFF.
- [SDR CA120723008](https://openairdocs.org/sdr/CA120723008.md): Engine · malfunctioned · Jul 16, 2012 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) WHILE THE ACFT WAS ON CRUISE FLIGHT AT 1000 FT. WITHOUT ANY WARNING OR ABNORMAL BEHAVIOUR THE ENGINE SHUTDOWN. A RE-START WAS ATTEMPTED WITHOUT SUCCESS AND THE PILOT PERFORMED A DEAD STICK LANDING ON A FLAT FIELD. PILOT UNINJURED BUT THE ACFT SUSTAI
- [SDR CA120703005](https://openairdocs.org/sdr/CA120703005.md): Control Cable · worn · Jun 30, 2012 · Airtrc AT802 · Rudder Control System
  > (CAN) RUDDER CABLES FOUND WORN AT FS 123.
- [SDR CA120404004](https://openairdocs.org/sdr/CA120404004.md): Rub Strip · damaged · Apr 3, 2012 · Airtrc AT802 · Aileron Control System
  > (CAN) LT AILERON/RUDDER INTERCONNECT ARM, LOCATED AT FUSELAGE BS 159.50, RUB STRIP FOR LT WATER RUDDER STEERING CABLE, HARDWARE BINDING UP ON SECONDARY AILERON/RUDDER INTERCONNECT STOP, CAUSING A LT ROLL INPUT INTO THE AILERON/RUDDER INTERCONNECT SYSTEM WITHIN
- [SDR CA120113007](https://openairdocs.org/sdr/CA120113007.md): Skin · damaged · Jan 13, 2012 · Airtrc AT802 · Leading Edge Devices
  > (CAN) DAMAGE FOUND ON LEADING EDGE OF RT FLAP, AND CORRESPONDING FLAP WELL AT WS 174 AND 187.
- [SDR CA120104004](https://openairdocs.org/sdr/CA120104004.md): Rib · cracked · Jan 4, 2012 · Airtrc AT802 · Trailing Edge Flaps
  > (CAN) CRACK IN RT FLAP L/E AND RIB AT FLAP BS 132.
- [SDR CA111103003](https://openairdocs.org/sdr/CA111103003.md): Bearing · failed · Oct 27, 2011 · Airtrc AT802 · Turbine Engine Reduction Gear
  > (CAN) CHIP DETECTOR LIGHT FOR POWER SECTION CAME ON, PILOT RETURNED TO BASE, FOUND 2 BALL BEARINGS ON CHIP DETECTOR, FOUND 8 MORE IN OIL SCREEN POWER SECTION, SENT PROPELLER GOVERNOR TO MFG, AWATING RESULTS FROM THEM TO SEE IF WE ARE GOING TO PULL THE ENGINE O
- [SDR CA110727011](https://openairdocs.org/sdr/CA110727011.md): Antenna · cracked · Jul 24, 2011 · Airtrc AT802 · Emergency Locator Beacon
  > ACFT SKIN AT BASE OF ELT ANTENNA CRACKED. POSSIBLE LOSS OF ELT ANTENNA AND FURTHER DAMAGE IN NEXT FEW FLIGHT HOURS.
- [SDR CA110221006](https://openairdocs.org/sdr/CA110221006.md): Skin · cut · Feb 18, 2011 · Airtrc AT802 · Rotorcraft Tail Boom
  > (CAN) DURING ANNUAL INSPECTION, THE AFT DECK SKIN, PN 11115-1,WAS FOUND TO BE CHAFED THROUGH BY BEING IN CONTACT WITH THE VERICAL STABILIZER ASSY, PN 30501-1. THE CHAFED THROUGH CUT WAS APPROXIMATLY 15" IN LENGTH. THE VERTICAL FIN ASSY WAS TRIMMED TO ALLOW C
- [SDR CA110120007](https://openairdocs.org/sdr/CA110120007.md): Control Cable · chafed · Jan 20, 2011 · Airtrc AT802 · Rudder Control System
  > DURING THE ANNUAL INSP, THE RUDDER CABLE ASSY PN 70524-10-500 WAS FOUND TO BE CHAFED WHERE THE CABLE PASSES THROUGH THE COCKPIT LOWER SKIN ASSY PN 11124-1. THE CABLE REQUIRED REPLACEMENT.
- [SDR CA101217009](https://openairdocs.org/sdr/CA101217009.md): Seal · chafed · Dec 16, 2010 · Airtrc AT802 · Fuselage Main, Structure
  > (CAN) DURING THE ANNUAL INSPECTION THE P3 LINE FITTING THAT PASSES THROUGH THE AFT FIRE SEAL WAS FOUND TO BE CHAFED. THE HOLE WHICH THE FITTING PASSES THROUGH WAS MISALIGNED CAUSING THE FITTING TO CHAFE ON THE FIRE SEAL PLATE. (TC# 20101217009)
- [SDR CA090806004](https://openairdocs.org/sdr/CA090806004.md): Bearing · destroyed · Aug 3, 2009 · Airtrc AT802 · Wheel/Ski/Float
  > UPON LANDING THE PILOT HEARD A BANG AND NOTICED THE TAIL WHEEL TO BE VERY ROUGH AND LOOSE. LT WHEEL BRG AND RACES FOUND DESTROYED, ALL ROLLERS WERE MISSING. WHEEL ASSY AND AXLE WERE REPLACED.
- [SDR CA090501006](https://openairdocs.org/sdr/CA090501006.md): Wire · burned · Apr 28, 2009 · Airtrc AT802 · Flight Control System Wiring
  > (CAN) THE AILERON TRIM TAB POWER WIRE THAT RUNS BEHIND THE CIRCUIT BREAKER PANEL BURNED AND WENT UP IN SMOKE WHILE PERFORMING UNRELATED MX IN THE HANGAR. WIRE WAS REPLACED AND TRIM TAB SYS CHECKS SERVICEABLE.
- [SDR CA080723003](https://openairdocs.org/sdr/CA080723003.md): Sealant · failed · Jul 18, 2008 · Airtrc AT802 · Propeller Blade Section
  > (CAN) DURING CLIMB OUT PILOT EXPERIENCED A BUILD UP OF GREASE ON WINDSHIELD. PILOT ABORTED LOAD IN DESIGNATED AREA AND RETURNED TO BASE. UPON INSP GREASE APPEARED TO BE COMING FROM 1 OR 2 BLADE CLAMPS. BLADE CLAMP SEALS WERE REPLACED IN BOTH UNITS. NO OBVIOUS
- [SDR PJ6G20080147](https://openairdocs.org/sdr/PJ6G20080147.md): Gas Generator · eroded · Apr 14, 2008 · N627JP · Airtrc AT802 · Engine (Turbine/Turboprop)
  > 'C' FLANGE EROSION AT SCAVENGE TUBE OIL COUPLING WITH ASSOCIATED PARTIALLY SEVERED 'T' BOLT.
- [SDR CA070514051](https://openairdocs.org/sdr/CA070514051.md): Engine · flamed out · Apr 18, 2007 · Airtrc AT802 · Engine (Turbine/Turboprop)
  > (CAN) THE ENGINE FLAMED OUT IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070514051)

Next page: https://openairdocs.org/model/air-tractor-at-802/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/air-tractor-at-802/reports

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