1 fatality

Pilot Killed, Two Injured After Engine Failure and Loss of Control During Instrument Approach (N74982)

Bryceville, United States of AmericaFlight

On September 28, 1984, a Piper PA-31-350 Navajo Chieftain (registration N74982) operated by Ronald Kaldor was involved in an aviation accident near Bryceville, United States of America in flight. One person was killed. Investigators recorded the probable cause as: Partial loss of engine power due to mechanical failure (burned piston and disconnected connecting rod); improper in-flight planning/decision-making by the pilot; failure to maintain airspeed (Vmc) leading to a stall/spin; pilot's lack of total experience in… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

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

A pilot was killed and two passengers injured after experiencing a right engine failure and subsequent loss of control during an instrument approach in low visibility conditions.

Flight History

The flight departed in instrument meteorological conditions (IMC). Shortly after takeoff, the pilot failed to maintain assigned headings on multiple occasions and had to be corrected by air traffic control (ATC). Approximately 15 minutes into the flight, the pilot reported problems with the right engine and requested to return to the airport. ATC advised that Craig Airport was available and reporting visual flight rules (VFR) conditions, but the pilot declined, stating the 4,000-foot runway at Craig was not long enough. Instead, the pilot opted to continue to Jacksonville International Airport (Jax Int'l), which was reporting IFR conditions.

Engine Failure

Post-crash inspection of the right engine revealed significant mechanical damage. The #5 cylinder had detonated to the point of burning a hole in the piston. Additionally, the #5 and #6 connecting rods exhibited burn damage, and the #6 rod bolts had failed in overload.

Loss of Control

While being vectored for an instrument landing system (ILS) approach, the pilot continued to have difficulty maintaining assigned headings. While on the downwind leg, the pilot asked ATC, 'how far is 982 from landing?' As the aircraft was turned onto the localizer, the pilot called and stated that control had been lost and the aircraft was in a spin. The aircraft subsequently collided with terrain. The pilot was killed and both passengers were injured.

Probable Cause

The official probable cause includes: a partial loss of engine power due to a mechanical failure involving a burned piston and disconnected connecting rod; improper in-flight planning/decision-making by the pilot; failure to maintain airspeed (Vmc) resulting in a stall/spin; and the pilot's lack of total experience in the type of aircraft. Contributing factors were low ceiling, fog, and the pilot not feathering the propeller.

Frequently asked questions

What happened in the 28 Sept 1984 Piper PA-31-350 Navajo Chieftain accident near Bryceville, United States of America?

A pilot was killed and two passengers injured after experiencing a right engine failure and subsequent loss of control during an instrument approach in low visibility conditions.

Were there any fatalities in the 28 Sept 1984 Piper PA-31-350 Navajo Chieftain accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 28 Sept 1984 involved a Piper PA-31-350 Navajo Chieftain, registration N74982, operated by Ronald Kaldor, at Bryceville, United States of America.

What was the probable cause of the accident?

Partial loss of engine power due to mechanical failure (burned piston and disconnected connecting rod); improper in-flight planning/decision-making by the pilot; failure to maintain airspeed (Vmc) leading to a stall/spin; pilot's lack of total experience in the aircraft type. Contributing factors: low ceiling, fog,…