No fatalities

In-Flight Fire and Engine Separation During Training Flight at Washington-National (N91068)

Washington-Ronald Reagan-National, United States of AmericaLanding (descent or approach)

On September 12, 1946, a Douglas C-54 Skymaster (registration N91068) operated by Pennsylvania Central Air Lines was involved in an aviation accident near Washington-Ronald Reagan-National, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The accident was caused by exhaust valve and connection failures in the number four engine that ignited a fire, which spread uncontrollably due to inadequate firewall and cowl panel sealing. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Source recordUpdated 2026-08-05Data APIEditorial standards

A crew conducting a local training flight experienced an uncontrollable engine fire that led to the separation of the number four engine from the wing. The aircraft landed safely with no injuries, but was written off due to severe structural damage.

What happened

The incident occurred during a local training flight departing from Washington-National Airport. While en route, a fire started in the number four engine. The crew attempted to extinguish the blaze but was unsuccessful. The captain contacted air traffic control to report the emergency and received authorization to return to the departure airport for an immediate landing.

During the final approach to runway 33, the structural integrity of the wing failed, causing the number four engine to separate from the airframe. Despite this catastrophic loss of part of the aircraft, the crew maintained control and completed a safe landing. All four members of the crew survived without injury. However, the severity of the fire damage sustained by the right wing resulted in the aircraft being declared damaged beyond repair.

Findings

Investigations identified specific mechanical failures as the root cause. The primary issue was a failure in the exhaust valve of the number two cylinder and the exhaust connection of the number one cylinder within the number four engine, which initiated the fire. A significant contributing factor was the inadequate sealing between the firewall and the nacelle skin, as well as between individual cowl panels. These gaps allowed the fire to spread into Zone 3, where it became uncontrollable.

Probable cause

The accident was caused by exhaust valve and connection failures in the number four engine that ignited a fire, which spread uncontrollably due to inadequate firewall and cowl panel sealing.