No fatalities

8 Sep 2013: SWEET WAYNE A BUSHBY MUSTANG II (N54WS) — Woodstock, IL

Woodstock, IL, United States

On 8 Sep 2013, a SWEET WAYNE A BUSHBY MUSTANG II (registration N54WS) was involved in an aviation accident near Woodstock, IL. No fatalities were reported. Investigators recorded the probable cause as: The pilot's improper fuel management, which resulted in a loss of engine power due to fuel starvation. This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Sweet Bushby Mustang II (N54WS) made a forced landing in a field near Woodstock, Illinois, after a total loss of engine power. The pilot and passenger sustained minor injuries; the aircraft sustained substantial damage.

Accident Overview

On September 8, 2013, at approximately 1750 central daylight time, a Sweet Bushby Mustang II airplane, registration N54WS, impacted terrain during a forced landing near Woodstock, Illinois. The commercial pilot and one passenger sustained minor injuries. The airplane, registered to and operated by the pilot under 14 Code of Federal Regulations Part 91 as a personal flight, sustained substantial damage to the fuselage and right wing.

Flight Details

The flight departed Council Bluffs, Iowa, at about 1630, destined for Grayslake, Illinois. Visual meteorological conditions prevailed, and no flight plan was filed.

Sequence of Events

According to local authorities who spoke with the pilot, while at an altitude of 2,200 feet above ground level, the engine began to lose partial power. The pilot attempted to regain engine power by switching the fuel selector to the auxiliary or header tank; however, the engine subsequently lost total power. The pilot executed a forced landing to a field, during which the airplane impacted vegetation and came to rest upright.

Postaccident Examination

Postaccident examination by a Federal Aviation Administration (FAA) inspector revealed that the right wing fuel tank was empty, the left wing fuel tank contained some fuel, and the auxiliary or header fuel tank was full. The inspector removed the fuel line from the fuel manifold and activated the fuel pump, which resulted in fuel flow from the fuel line. The airplane was recovered for further examination.

Engine Functional Test

Under the supervision of an FAA inspector, the engine was functionally tested on the airframe using the auxiliary fuel tank. During the test, the engine started and operated without any anomalies noted.

Contributing factors

Fluid managementPilot