No fatalities

29 Sep 2014: PREISS VANS RV-9A (N259H) — Robert T. Hudson II — Hobart, OK

Hobart, OK, United States

On 29 Sep 2014, a PREISS VANS RV-9A (registration N259H) operated by Robert T. Hudson II was involved in an aviation accident near Hobart, OK. No fatalities were reported. Investigators recorded the probable cause as: A loss of engine power due to fuel exhaustion, which resulted from the pilot's erroneous preflight fuel calculations and inadequate in-flight fuel management. This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

An experimental Preiss Vans RV-9A sustained substantial damage during a forced landing near Hobart Regional Airport after the engine lost power due to fuel exhaustion. The pilot was uninjured; the passenger was seriously injured.

Overview

On September 29, 2014, at 1510 central daylight time, an experimental-homebuilt Preiss Vans RV-9A, registration N259H, was substantially damaged during a forced landing after the engine lost power approximately 2 miles east of Hobart Regional Airport (HBR), Hobart, Oklahoma. The pilot reported no injuries, while the passenger sustained serious injuries.

Flight Details

The aircraft was registered to and operated by Mexico Medical Missions, Glenwood Springs, Colorado, under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from Grove Municipal Airport (GMJ), Grove, Oklahoma, around 1315, with an intended destination of Hobart Regional Airport.

Pilot's Actions and Fuel Management

According to the pilot's accident report and statements to a Federal Aviation Administration (FAA) inspector, preflight calculations indicated sufficient fuel for the flight with a 30-minute reserve. The pilot reported switching fuel tanks every 30 minutes. As the aircraft neared Hobart, the Global Positioning System (GPS) showed an estimated time of arrival (ETA) of 10 minutes, and the fuel monitor indicated 39 minutes of fuel remaining—consistent with preflight estimates.

After depleting the left tank, the pilot switched to the right tank, which displayed 5 gallons remaining. With a fuel consumption rate of 6 gallons per hour, the pilot believed there was adequate fuel to complete the flight. At an ETA of 5 minutes, the fuel monitor indicated 3 gallons remaining in the right tank. Shortly thereafter, while still 2 miles east of HBR, the engine lost power.

Forced Landing and Damage

The pilot executed a forced landing in a field, intentionally allowing the airplane to land hard to avoid an incipient stall. Post-accident inspection revealed crushed nose landing gear, bent main landing gear, and a buckled fuselage.

Post-Accident Findings

A subsequent examination by an FAA inspector found no fuel in the aircraft's tanks. The pilot later stated that the engine lost power due to fuel exhaustion.

Contributing factors

PilotFluid managementFluid level