Casualties unknown

2005-01-14: Beech 95-B55 (N7912R) — Patterson, LA

Patterson, LA, US

On January 14, 2005, a Beech 95-B55 (registration N7912R) was involved in an aviation accident near Patterson, LA. Investigators recorded the probable cause as: The pilot's failure to follow check-list procedures and the required placard instructions, which resulted in the fuel selectors being selected to the improper fuel tanks for take-off, resulting in a loss of engine power to the left engine. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An airplane experienced a loss of control during initial climb after takeoff, impacting terrain. Investigation revealed fuel selectors set to auxiliary tanks instead of main tanks as required for takeoff, and a related airworthiness directive placard.

Accident Sequence

The pilot, an airline transport pilot with 6,000 hours of flight experience, was observed making a steep climb followed by a shallow left turn during the initial climb after takeoff. The bank angle increased progressively, then the nose of the airplane dropped. Subsequently, the airplane entered a spin and impacted a tree before hitting the ground.

Fuel Selector Examination

Examination of the airplane after the accident found that the fuel selector handles were set to the auxiliary fuel tanks. According to the Normal Procedures section of the airplane's Pilot Operating Handbook (POH), the fuel selectors must be set to the main tanks for takeoff.

Airworthiness Directive

The Federal Aviation Administration (FAA) issued Airworthiness Directive (AD) 68-26-06 in 1974 to prevent a power loss. This AD required that a placard be installed on the pilot's instrument panel with the text: "TAKE OFF AND LAND ON MAIN TANKS ONLY. TURNING TYPE TAKE OFFS OR TAKE OFFS IMMEDIATELY FOLLOWING FAST TAXI TURNS PROHIBITED."

Performance Information

The POH states that the best rate of climb speed with one engine inoperative (Vyse) is 100 knots, and the minimum controllable airspeed (Vmc) is 78 knots. The POH also notes: "Two major factors govern one engine operations; airspeed and directional control. The airplane can be safely maneuvered or trimmed for normal hands-off operation and sustained in this configuration by the operative engine AS LONG AS SUFFICIENT AIRSPEED IS MAINTAINED... The most important aspect of engine failure is the necessity to maintain lateral and directional control. If airspeed is below 78 knots, reduce power on the operative engine as required to maintain control."

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20050119X00074. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.