NTSB Identification: ANC03LA085.
Nonscheduled 14 CFR Part 135: Air Taxi & Commuter
Accident occurred Thursday, July 31, 2003 in Anchorage, AK
Probable Cause Approval Date: 3/30/2004
Aircraft: Cessna 207, registration: N29CF
Injuries: 1 Serious, 1 Minor, 2 Uninjured.
The commercial pilot was conducting an on-demand passenger flight with
three passengers aboard. As the airplane approached the destination
airport, about 800 feet agl over a city, the engine began to run rough and
lose power. In an attempt to restore engine power, the pilot confirmed
that the fuel selector valve was placed to the right fuel tank, and
momentarily placed the auxiliary fuel boost pump in the high boost
position. Engine power was momentarily restored, followed by a complete
loss of power. The pilot selected a forced landing area adjacent to
several baseball fields. During the forced landing approach, the airplane
passed over four occupied baseball fields. During touchdown, the
airplane's left wing collided with a chain link fence, the airplane veered
to the left, collided with a concrete embankment, and cart wheeled to the
left. During an on scene interview the pilot reported that he routinely
flew the accident route using only the right fuel tank. He said that fuel
stored in the left fuel tank was considered a reserve tank. Another pilot
had flown the accident airplane prior to the accident flight, and usually,
when an airplane returned to the operator's base, line service personnel
would routinely fill the right fuel tank, to be ready for the next flight.
Prior to departing on the outbound leg of the flight, the pilot said that
he did not visually check the fuel quantity in the right wing fuel tank,
and that the entire round trip flight was flown with the fuel selector
valve selected to the right fuel tank. When asked if he attempted to
switch the fuel selector valve from the right fuel tank to the left tank,
the accident pilot responded "no." During wreckage recovery efforts, and
in the presence of the NTSB IIC, about 0.8 gallons of fuel was drained
from the right wing-mounted fuel tank, and associated fuel lines. About 30
gallons of fuel were drained from the left wing-mounted fuel tank. The
tanks were not damaged during the accident and did not leak.
The National Transportation Safety Board determines the probable
cause(s) of this accident as follows:
The pilot's incorrect positioning of the fuel tank selector valve to a
nearly empty tank, which resulted in a loss of engine power due to fuel
starvation, and subsequent emergency landing at an off-airport site.
Factors associated with the accident were the pilot's inadequate preflight
inspection, and his inadequate remedial action.