Beechcraft G36 N89SN

Summary

On 18 December 2013 at about 13:20 local time, a Beechcraft G36 registered N89SN, operated by Grey Aviation Advisors & Solutions Inc, was involved in an accident near Panama City, Florida, United States. One person was on board and one died. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

18 December 2013 at 13:20

Classification

Accident

Location

Panama City, Florida, United States

Nearest airport

Sandy Creek Airpark (75FL)

Coordinates

30.1019, -85.4622

Aircraft

Beechcraft G36

Registration

N89SN

Category

Airplane

Year built

2006

Engines

1

Operator

Grey Aviation Advisors & Solutions Inc

Operating rule

Part 91: General Aviation

Purpose of flight

Business

Phase of flight

Not recorded

Route

West Palm Beach → Destin

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

ERA14FA074

1 person died.

The pilot’s inadequate preflight and inflight fuel planning, which resulted in a total loss of engine power due to fuel exhaustion. Contributing to the pilot’s injuries was his failure to use the available shoulder harness.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The flight was about 60 miles from the destination airport when the pilot reported a total loss of engine power to air traffic control. The controller provided information on nearby airports, and the pilot maneuvered the airplane toward the closest airport. The pilot reported the airport in sight; radio and radar contact were subsequently lost. A search for the airplane was initiated, and the wreckage was located in a heavily wooded swamp about 1 mile east of the airport. There were no known witnesses to the accident. The fuel tank selector handle was found in the "left main" (left wing tank) position. The left wing tank was not breached, and about 1 pint of fuel was recovered from the tank. The right tank was breached, and it contained residual fuel; however, there was no evidence of fuel leakage on the ground beneath the tank. The airplane was fitted with optional wing tip tanks, which were found empty. The total amount of fuel recovered, including the residual fuel in the tanks and fuel recovered from a small pool of water directly under the airplane, was about 2.5 gallons, which was less than the manufacturer-reported unusable fuel quantity of 6 gallons. The airplane was last serviced with fuel about 28 days before to the accident; however, the total fuel onboard at that time could not be determined. The propeller blades exhibited no rotational damage or signatures. After the accident, the engine was removed from the airframe and successfully test run at the manufacturer's facilities; no evidence of pre-accident malfunction or failure was observed. Although a shoulder harness was available, the pilot was found in the left seat with only his lap belt fastened. Damage to the airplane's multi-function display was consistent with impact by the pilot's head during the accident sequence. The pilot's cause of death was blunt force head trauma, and the impact forces that he experienced would likely have been reduced if he had been wearing his shoulder harness.

Quoted verbatim from the NTSB record.