No fatalities

1982-07-30: Douglas C-47 Skytrain (DC-3) (N102BL) — Pronto Aviation Services — El Paso, United States of America

El Paso, United States of AmericaTakeoff (climb)

On July 30, 1982, a Douglas C-47 Skytrain (DC-3) (registration N102BL) operated by Pronto Aviation Services was involved in an aviation accident near El Paso, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: Loss of engine power due to loss of oil pressure in the left engine, and undetermined landing gear indication system. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781221321Data APIEditorial standards

A multi-engine aircraft crashed in the desert during an emergency landing after the left engine lost oil pressure and the landing gear indication system failed. All three occupants were unharmed.

Accident Details

Shortly after takeoff at approximately 800 feet above ground level, the left engine's oil temperature became high and oil pressure was reported lost. The pilot feathered the left engine and declared an emergency. During the final approach, the landing gear safe indication was not received. The pilot initiated a go-around but became committed to land. While maneuvering, the aircraft collided with terrain in a desert area. The aircraft was carrying 2,700 pounds of cargo. The field elevation was about 3,950 feet and the temperature was 72 degrees Fahrenheit. All three occupants were uninjured.

Official Findings

The investigation identified three occurrences. The first was a loss of engine power during initial climb due to loss of oil pressure in the lubricating system. The second occurrence was a forced landing involving a return to the airport. During this phase, the pilot performed precautionary landing procedures and attempted to extend the landing gear, but the gear indicating system's status was undetermined. The pilot initiated a go-around, but high density altitude prevented achieving the minimum control speed. The third occurrence was an in-flight collision with terrain during the landing flare. Contributing factors included rough/uneven terrain, loose gravel/sandy ground, and high vegetation.

Probable cause

Loss of engine power due to loss of oil pressure in the left engine, and undetermined landing gear indication system.