1 fatality

2009-04-17: Cessna 421B Golden Eagle II (N1935G) — Sebring Air Charter — Fort Lauderdale-Executive, United States of America

Fort Lauderdale-Executive, United States of AmericaTakeoff (climb)

On April 17, 2009, a Cessna 421B Golden Eagle II (registration N1935G) operated by Sebring Air Charter was involved in an aviation accident near Fort Lauderdale-Executive, United States of America during takeoff. One person was killed. Investigators recorded the probable cause as: The pilot's failure to maintain aircraft control and secure the right engine during an emergency return to the airport after takeoff. Contributing to the accident was an in-flight fire of the right engine for undetermined reasons. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781196786Data APIEditorial standards

Witnesses saw the pilot haphazardly pouring oil into the right engine. After takeoff, fire was seen from the right engine. The airplane banked right for return and descended into a residential area.

Synopsis

A pilot was observed pouring oil into the right engine haphazardly prior to a flight. After running the engines at mid-range power for about 20 minutes, the airplane taxied out and departed. Following rotation, fire was seen emanating from the right engine. The airplane climbed shallowly and flew low with the right engine on fire, then banked right to return to the airport and descended into a residential area.

Preflight Observations

Witnesses saw the pilot pouring oil into the right engine in a haphazard manner. The pilot then ran the engines at mid-range power for approximately 20 minutes. The airplane subsequently taxied out of the ramp area and departed.

Accident Flight

Fire was observed emanating from the right engine after rotation. The airplane continued in a shallow climb from the runway, flying low, with the right engine on fire. The airplane then banked right to return to the airport and descended into a residential area.

Post-Accident Examination

Examination of the right engine revealed an exhaust leak at the No. 4 cylinder exhaust riser flange. One of the flange boltholes was elongated, most likely from resulting vibration. The fuel nozzle and B-nut were secure in the No. 4 cylinder, but its respective fuel line was separated about 8 inches from the nozzle. No determination could be made as to when the fuel line separated (preimpact or postimpact) due to impact and postcrash fire damage. Examination of the right engine turbocharger showed the compressor wheel had uniform deposits of an aluminum alloy mixture, consistent with ingestion during operation, most likely from melting of the aluminum fresh air duct. Additionally, the right propeller was found near the low pitch position, contrary to the owner's manual emergency procedure to secure the engine and feather the propeller in the event of an engine fire.

Probable cause

The pilot's failure to maintain aircraft control and secure the right engine during an emergency return to the airport after takeoff. Contributing to the accident was an in-flight fire of the right engine for undetermined reasons.