Aircraft stall and crash following takeoff

3 fatalities • Farmington, United States of America • Takeoff (climb)

An aircraft experienced a loss of altitude during its initial climb, resulting in a crash near the runway end that caused three fatalities.

What happened

During the takeoff phase of flight, the aircraft struggled to maintain sufficient altitude after leaving the ground. In an attempt to compensate for the lack of climb, the pilot applied additional engine power. However, this maneuver led to an aerodynamic stall, causing the plane to descend and impact the ground near the end of the runway.

The accident resulted in three fatalities among the passengers, while five other occupants sustained injuries during the impact.

Findings

Investigations into the crash revealed that the aircraft was operating at a weight exceeding its maximum takeoff weight by 220 lbs. Furthermore, the pilot did not adequately account for the challenges posed by a high density altitude of 7,100 feet during flight preparations.

Probable cause

The accident was caused by an overweight aircraft operating in high density altitude conditions without proper flight preparation.

Frequently asked questions

What happened in the 1967-09-08 Beechcraft C-45 Expeditor accident near Farmington, United States of America?

An aircraft experienced a loss of altitude during its initial climb, resulting in a crash near the runway end that caused three fatalities.

Were there any fatalities in the 1967-09-08 Beechcraft C-45 Expeditor accident?

The accident was fatal, resulting in 3 fatalities.

What aircraft was involved and where did it happen?

The accident on 1967-09-08 involved a Beechcraft C-45 Expeditor, registration N9507Z, operated by Private United States of America, at Farmington, United States of America.

What was the probable cause of the accident?

The accident was caused by an overweight aircraft operating in high density altitude conditions without proper flight preparation.

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