Forced Landing Following Engine Thrust Loss

Casualties unknown • San Antonio, TX, US

A pilot executed a forced landing into a vacant lot after experiencing a loss of thrust in the right engine during takeoff.

What happened

During the takeoff roll, air traffic control advised the pilot that the aircraft was trailing smoke. The pilot disregarded this report, believing the smoke was a normal condition based on previous experiences, and continued the takeoff sequence.

Shortly after liftoff, the aircraft experienced a loss of thrust from the right engine. Although an attempt was made to return to the airport, the maneuver was unsuccessful. The pilot subsequently executed a forced landing into a vacant lot. There were no reported injuries.

The investigation

The investigation determined that the loss of thrust was caused by the failure of the right unfeathering accumulator hose. This failure was due to chaffing, which occurred because the hose had been misrouted during engine installation.

Additionally, the smoke initially observed by the pilot was traced to cracks in the right exhaust system. These cracks originated from previous weld repairs performed during the engine installation process. Maintenance personnel had failed to identify either the misrouted hose or the cracks in the exhaust system.

Probable cause

The loss of thrust resulted from a chafed unfeathering accumulator hose that was improperly routed during engine installation, compounded by the pilot's failure to raise the landing gear and feather the propeller while operating at 9.4% above gross weight.

Frequently asked questions

What happened in the 1989-10-19 Cessna 414 accident near San Antonio, TX?

A pilot executed a forced landing into a vacant lot after experiencing a loss of thrust in the right engine during takeoff.

What aircraft was involved and where did it happen?

The accident on 1989-10-19 involved a Cessna 414, registration N5820H, operated by Eglin Aero Club, at San Antonio, TX.

What was the probable cause of the accident?

The loss of thrust resulted from a chafed unfeathering accumulator hose that was improperly routed during engine installation, compounded by the pilot's failure to raise the landing gear and feather the propeller while operating at 9.4% above gross weight.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X29598. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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