Engine failure and crash of aircraft on beach

No fatalities • San Juan-Luis Muñoz Marín (Isla Verde), Puerto Rico • Takeoff (climb)

An aircraft experienced a left engine power loss shortly after takeoff, resulting in a collision with a tree and a beach landing.

What happened

Following a departure from runway 08, the aircraft reached an altitude of approximately 400 feet above ground level when the left engine experienced a loss of power. Upon identifying the failure, the pilot performed the procedure to feather the left propeller and requested maximum dry thrust from the right engine.

Despite the availability of wet power, which could have added 450 horsepower to the remaining engine, the pilot chose not to utilize this additional power. Consequently, the aircraft was unable to sustain its flight altitude. During the descent, the plane struck a palm tree before eventually coming to a stop on the beach near the surf line.

Findings

Investigation into the specific cause of the left engine malfunction was prevented by damage caused by salt water. However, it was noted that the aircraft was operating at a weight that exceeded its maximum allowable limit by 600 pounds.

Probable cause

The aircraft was unable to maintain altitude following a left engine power loss, exacerbated by the aircraft being 600 pounds over its maximum weight limit.

Frequently asked questions

What happened in the 1997-06-30 Convair CV-240 accident near San Juan-Luis Muñoz Marín (Isla Verde), Puerto Rico?

An aircraft experienced a left engine power loss shortly after takeoff, resulting in a collision with a tree and a beach landing.

Were there any fatalities in the 1997-06-30 Convair CV-240 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1997-06-30 involved a Convair CV-240, registration N344MM, operated by Silver Express Company, at San Juan-Luis Muñoz Marín (Isla Verde), Puerto Rico.

What was the probable cause of the accident?

The aircraft was unable to maintain altitude following a left engine power loss, exacerbated by the aircraft being 600 pounds over its maximum weight limit.

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