No fatalities

10 May 2018: ENSTROM HELICOPTER CORP 280C C (N67RE) — Kerens, TX

Kerens, TX, United States

On 10 May 2018, an ENSTROM HELICOPTER CORP 280C C (registration N67RE) was involved in an aviation accident near Kerens, TX. No fatalities were reported. Investigators recorded the probable cause as: The total loss of engine power due to fuel exhaustion and the pilot’s inadequate in-flight fuel management. This summary draws on records from NTSB; 7 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On May 10, 2018, an Enstrom 280C helicopter experienced a loss of engine power during maneuvering, executed an autorotation, and impacted trees and terrain. The pilot was seriously injured; the helicopter sustained substantial damage.

Accident Overview

On May 10, 2018, at approximately 1745 central daylight time, an Enstrom Helicopter Corporation 280C helicopter, registration N67RE, impacted trees and terrain following an autorotation near Kerens, Texas. The private pilot, who was the sole occupant, sustained serious injuries, and the helicopter sustained substantial damage. The flight was conducted under Title 14 Code of Federal Regulations Part 91 as a personal flight by a private individual. Visual meteorological conditions prevailed, and no flight plan was filed.

Flight History

The helicopter had undergone recent major maintenance, and the pilot was picking it up to return to his residence. Before the accident flight, the pilot completed a flight review with a flight instructor in the accident helicopter. During the review, the pilot experienced issues with the radio and difficulty with trim control. A mechanic later inspected the radio and completed unspecified repairs. After the flight review, the pilot added 25 gallons of fuel, bringing the total to about 35 gallons for the return flight.

The helicopter departed from Wood County Airport (JDD) in Mineola, Texas, about 1615, destined for a private residence. During the return flight, the pilot noticed increasing transmission and cylinder temperatures on his instrument gauges. He performed an off-airport landing in a field, kept the engine running, and waited for the temperatures to return to normal. After they did, the pilot departed.

While maneuvering at 1,000 feet above ground level about 1.5 miles from his residence, the pilot heard a noise or bang. The engine then lost total power, and the pilot entered an autorotation. During the descent, the helicopter impacted trees and terrain, coming to rest upright in wooded terrain.

Post-Accident Examination

A Federal Aviation Administration inspector examined the helicopter at the accident site and at a recovery facility. The mixture control was found in the rich position. Both left and right fuel tanks were empty, and the fuel tanks and fuel lines were not compromised. No mechanical failures or malfunctions were noted that would have precluded normal operations.

Contributing factors

Causes

Fluid levelPilotFluid management

Other contributing factors

Contributed to outcome