West Point - West Point

On September 10, 1995 at 06:40 PM, West Point - West Point experienced a crash involving Beechcraft 65 Queen Air, operated by Peninsula Sky Divers, with the event recorded near West Point-Middle Peninsula Virginia.

The flight was categorized as skydiving / paratroopers and the reported phase was takeoff (climb) at a city crash site.

11 people were known to be on board, 12 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 109.1%.

Crew on board: 1, crew fatalities: 1, passengers on board: 10, passenger fatalities: 10, other fatalities: 1.

The listed crash cause is technical failure. The airplane was loaded with 10 sport parachutists and one pilot. Later, investigators calculated that the maximum gross weight was exceeded by 149.6 pounds, and the center of gravity was 2.87 inches aft of the aft limit. The cabin door had been removed for parachuting operations; however, an altered Flight Manual Supplement had been used as authority for the door removal. The airplane was not on the FAA-approved eligible list for such removal. The airplane needed to be refueled before flight, but the quantity of fuel in the airport's underground storage tank was below the electric cutoff level. Fuel was pumped manually from the storage tank into plastic jugs, which were used to refuel the airplane. Before takeoff, samples of fuel were reported to have been drained from the airplane's fuel tanks (sumps). According to witnesses, they heard an engine misfiring during takeoff. They observed the airplane level off during the initial climb and start a shallow right turn. The bank angle gradually increased from shallow to steep as the nose dropped and the airplane descended. Other witnesses observed the airplane in a steep dive just before it crashed in the rear of a residence. One person in the residence was killed. A postaccident fire destroyed the accessory sections of both engines. Examination of the airplane disclosed evidence that the right engine had been shut down and the right propeller had been feathered; however, no preimpact mechanical failure was found. A sample of excess fuel was obtained from the tank that was used to refuel the airplane, but no observable quantity of water or contamination was found.

Aircraft reference details include registration N945PA, MSN LC-217, year of manufacture 1968.