Air Tractor INC AT 402A accident near Shaw, Mississippi, August 21, 2017
On August 21, 2017 at about 11:30 pm local time, a 2012 Air Tractor INC AT 402A, registered N247LA, was substantially damaged in an accident during takeoff near Shaw, Mississippi (Tapley Airport). It was an aerial application (crop spraying) flight under agricultural flying rules (Part 137). 1 person had minor injuries. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s decision to attempt takeoff at high gross weight, in high density altitude conditions, and with insufficient runway length. Contributing to the accident was the pilot’s inadequate preflight planning.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 21, 2017 · about 11:30 pm local time
- Place
- Shaw, Mississippi · Tapley Airport · map
- Type
- Accident
- Injuries
- 1 person had minor injuries.
- Weather
- visual conditions (good weather)
- Aircraft
- Air Tractor INC AT 402A, built 2012 · all AT 402As on the register
- Registration
- N247LA · no longer on the register · serial 402A-1247
- Damage
- Substantial damage
- Flight
- Aerial application (crop spraying) flight · agricultural flying rules (Part 137)
The NTSB's narrative final · quoted from the NTSB record
The pilot was departing on an agricultural application flight from a 2,300-ft-long runway. When the airplane reached the end of the runway, the pilot could "feel that the airplane did not want to fly." The pilot extended the flaps, then dumped the spray load that was in the airplane’s hopper tank in an attempt to become airborne; however, the airplane continued off the end of the runway, crossed a drainage ditch, and came to rest in a bean field, resulting in substantial damage. The airplane’s hopper was loaded with about 3,400 lbs of a mixture of herbicide and other chemicals, which exceeded the hopper’s placarded limitation of 3,250 lbs. The airplane’s estimated weight at the time of the accident was 1,864 lbs higher than the manufacturer’s published gross weight and about 264 lbs more than field experience showed could be carried safely with adequate margins of performance and structural strength. Calculations by the airplane manufacturer using takeoff data of a similar airplane from a previous company test program indicated a takeoff ground roll distance of about 2,322 ft. Given the density altitude about the time of the accident, the airplane’s takeoff distance would have been increased by 24%, and there would have been an 18% decrease in its rate of climb. No preimpact failures or malfunctions were discovered that would have precluded normal operation. Despite the numerous indicators that the takeoff conditions were marginal, such as the high air temperature, high gross weight, and a short runway, the pilot failed to evaluate the conditions that existed in relation to the performance capability of the airplane.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Runway excursion during takeoff defining event
- Collision with terrain or object (not controlled flight into terrain) during takeoff (rejected takeoff)
- Preflight or dispatch event during prior to flight
The NTSB's findings
- Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
- Personnel issues › Task performance › Planning/preparation › Performance calculations › Pilot
- Personnel issues › Task performance › Planning/preparation › Weight/balance calculations › Pilot
- Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High density altitude › Awareness of condition
- Environmental issues › Physical environment › Runway/land/takeoff/taxi surface › (general) › Effect on operation
Pilot
- Certificate: commercial pilot
- Ratings: single-engine land
- Flight time: 5,400 hours in all; 3,850 in this make and model; 325 in the last 90 days; 155 in the last 30 days; 5,300 as pilot in command
- Last flight review: February 21, 2017
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: sngl
- Injury: minor injuries
The aircraft
- Airframe total time: 2,679 hours
- Last inspection: annual inspection, March 1, 2017; 249 hours since
- Maximum gross weight: 7,000 lb
- Seats: 1
- Landing gear: fixed
- Engine: Pratt & Whitney Canada PT6A-31 (turboprop); 9,528 hours total
- Operator: Boair INC
The flight
- Departed from: 1MS0 Shaw MS at 11:30 pm
- Destination: 1MS0 Shaw MS
- Flight plan: none
- Runway 27, 2,300 ft by 50 ft
Weather at the time
- Light: daylight
- Wind: from 280° at 4 knots
- Visibility: 10 statute miles
- Sky: scat at 4,800 ft
- Temperature: 91°F (33°C), dew point 75°F (24°C)
- Altimeter: 30.04 inHg
- Observation at 11:35 pm from RNV, 10 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
17 documents, released by the NTSB on December 31, 2021. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
