Casualties unknown

2001-02-27: Piper PA-28R-200 (N1488T) — Brenham, TX

Brenham, TX, US

On February 27, 2001, a Piper PA-28R-200 (registration N1488T) was involved in an aviation accident near Brenham, TX. Investigators recorded the probable cause as: The disconnection of the throttle linkage from the fuel injector body, which resulted in a loss of engine power. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An aircraft experienced an in-flight engine power loss while climbing after takeoff, forcing the pilot to execute an emergency landing in a nearby field where it struck livestock and fencing.

What happened

The airplane departed from runway 16 and began its climb toward traffic pattern altitude. Shortly after becoming airborne, the engine lost power unexpectedly. The pilot made the decision to land the aircraft in a field located south of the airport. During the landing roll, the airplane collided with two cows and a fence.

The investigation

A mechanical examination of the engine was conducted to determine the cause of the power loss. Investigators found that the throttle linkage had become disconnected from the fuel injector body. This separation prevented proper fuel delivery control, leading to the in-flight failure.

Findings

The primary factor contributing to the accident was the disconnection of the throttle linkage from the fuel injector body. This mechanical failure resulted in a complete loss of engine power during the critical climb phase. The pilot's decision to select a field for an emergency landing was necessitated by this sudden mechanical failure. The impact with the cows and fence occurred during the subsequent landing roll.

Safety message

Regular inspection of engine components, particularly throttle linkages and fuel system connections, is essential to prevent in-flight power loss. Ensuring that all mechanical linkages are secure and properly installed can help avoid catastrophic failures during critical phases of flight.

Probable cause

The disconnection of the throttle linkage from the fuel injector body, which resulted in a loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010302X00532. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.