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Accidents · NTSB ERA17FA140 · Final report

Beech A36 accident near Dadeville, Alabama, March 28, 2017

On March 28, 2017 at about 5:00 pm local time, a 1991 Beech A36, registered N8169Y, was destroyed in an accident during enroute (cruise) near Dadeville, Alabama. It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A loss of engine power for reasons that could not be determined due to postcrash thermal damage to the engine accessories and the airframe. Contributing to the accident was the pilot's failure to navigate to any of the available forced landing sites within gliding distance of the airplane following the loss of engine power.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
March 28, 2017 · about 5:00 pm local time
Place
Dadeville, Alabama · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Beech A36 UNDESIGNAT, built 1991 · all A36s on the register
Registration
N8169Y · no longer on the register · serial E-2598
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The private pilot was conducting a cross-country flight at a cruise altitude of 5,000 ft mean sea level (msl) in day visual meteorological conditions when the airplane experienced a total loss of engine power. Over the next minute, the airplane continued a northerly track before it began a turn to the west as the controller identified the closest public airport, private strip, state highway, and open areas for potential forced landing sites, which the pilot acknowledged. About 3 minutes later, the airplane collided with trees and terrain and was consumed by postcrash fire. All engine accessories were destroyed by fire and could not be examined except for the engine-driven fuel pump, which revealed no anomalies. The engine displayed internal and external thermal damage, but internally displayed signatures consistent with normal wear and lubrication. Tree damage at the site was consistent with a rotating propeller at the time of tree contact. An NTSB performance specialist plotted potential glide ranges and trajectories for the airplane from the assumed point of engine power loss. About the time of the loss of engine power, the airplane was about 1 mile abeam an abandoned airport. This airport was not plotted on the visual flight rules sectional chart nor was it visible to the controller, and it may not have been readily visible to the pilot due to its location on the right side of the airplane. However, the airplane's projected glide distance and trajectories indicated that the airplane was within gliding distance of numerous open fields as well as a four-lane divided highway with a large grass median. It could not be determined why the pilot chose to forgo any of the potential suitable forced landing sites.

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

  1. Loss of engine power (total) during enroute (cruise) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during emergency descent
  3. Fire/smoke (post-impact) during post (impact)

The NTSB's findings

  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • factor Personnel issues › Task performance › Use of equip/info › Use of available resources › Pilot

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 11,000 hours in all; 100 in this make and model
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 4,006.7 hours
  • Last inspection: annual inspection, May 5, 2016
  • Maximum gross weight: 3,651 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: Continental IO-550B (piston); 482 hours total
  • Fire on the ground

The flight

  • Departed from: EDN Enterprise AL at 4:18 pm
  • Destination: SRB Sparta TN
  • Flight plan: IFR

Weather at the time

  • Light: daylight
  • Wind: from 270° at 6 knots
  • Visibility: 10 statute miles
  • Sky: scat at 2,500 ft
  • Temperature: 75°F (24°C), dew point 64°F (18°C)
  • Altimeter: 30.03 inHg
  • Observation at 4:55 pm from ALX, 14 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

13 documents, released by the NTSB on June 21, 2018. 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.