2 fatalities

Single-Engine Flight Test Ends in Collision with Guy Wire (N62957)

Lakeland, United States of AmericaLanding (descent or approach)

On September 2, 1982, a Piper PA-31-350 Navajo Chieftain (registration N62957) operated by Piper Aircraft Corporation was involved in an aviation accident near Lakeland, United States of America during landing or approach. 2 people were killed. Investigators recorded the probable cause as: Loss of engine power due to undetermined propeller system/feathering system issue; in-flight collision with guy wire due to poor planned approach and improper decision-making by the pilot, combined with a landing gear malfunction and deteriorated engine-out… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 4 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary report: the U.S. National Transportation Safety Board (NTSB) historical archiveUpdated 2026-07-04Data APIEditorial standards

During single-engine flight tests with inboard gear doors removed, a pilot unable to restart the left engine attempted a single-engine landing, overshot, and executed a go-around. The aircraft then experienced gear problems, descended slowly, and collided with a guy wire on a powerline pole.

Accident Overview

The accident occurred during a single-engine flight test conducted with the inboard gear doors removed. A chase aircraft was photographing the test. After the tests concluded, the pilot was unable to restart the left engine and returned to the airport for a single-engine landing. The pilot overshot the landing attempt and performed a single-engine go-around, subsequently reporting a gear problem.

Flight Details

An occupant of the chase aircraft observed that the main landing gear were hanging 75 to 80 degrees from the horizontal. A company employee at the airport reported that the nose gear was about 10 degrees aft of the normal down-and-locked position. The aircraft continued on a west-southwest heading away from the airport, passing over several suitable emergency landing sites while in a slow descent, until it collided with the guy or grounding wire atop a powerline pole located 4 miles west-southwest of the airport. The aircraft was destroyed, and both occupants were killed.

Official Findings

The probable cause includes two occurrences. Occurrence #1: loss of engine power during maneuvering, with an undetermined cause related to the propeller system or feathering system. Occurrence #2: in-flight collision with an object during the go-around phase. Contributing factors included the pilot's poor planned approach, initiated go-around, performed aborted landing, issues with the landing gear doors and normal retraction/extension assembly making gear retraction not possible, deteriorated aircraft performance due to engine-out capability, and improper in-flight planning and decision-making. The object was the guy wire.

Frequently asked questions

What happened in the 2 Sept 1982 Piper PA-31-350 Navajo Chieftain accident near Lakeland, United States of America?

During single-engine flight tests with inboard gear doors removed, a pilot unable to restart the left engine attempted a single-engine landing, overshot, and executed a go-around. The aircraft then experienced gear problems, descended slowly, and collided with a guy wire on a powerline pole.

Were there any fatalities in the 2 Sept 1982 Piper PA-31-350 Navajo Chieftain accident?

The accident was fatal, resulting in 2 fatalities.

What aircraft was involved and where did it happen?

The accident on 2 Sept 1982 involved a Piper PA-31-350 Navajo Chieftain, registration N62957, operated by Piper Aircraft Corporation, at Lakeland, United States of America.

What was the probable cause of the accident?

Loss of engine power due to undetermined propeller system/feathering system issue; in-flight collision with guy wire due to poor planned approach and improper decision-making by the pilot, combined with a landing gear malfunction and deteriorated engine-out capability.