Incident Overview

Date: Monday 9 July 1962
Aircraft Type: Douglas DC-4-1009
Owner/operator: Trans Mediterranean Airways – TMA
Registration Number: OD-AEC
Location: 2,2 km NE off Brindisi-Papola Casale Airport (BDS) – ÿ Italy
Phase of Flight: Initial climb
Status: Destroyed, written off
Casualties: Fatalities: 6 / Occupants: 6
Component Affected: EnginesEngines
Category: Accident
A DC-4 aircraft, TMA 104, departed London on a return trip to Beirut via Frankfurt and Brindisi. It lost sufficient altitude and began descending after reaching 60 meters, striking the sea approximately 2250 meters from the end of the runway, 4 degrees left of the extended runway centerline. This resulted in a loss of power to both engines, likely due to fatigue, which led to a gradual loss of height and subsequent descent.A DC-4 aircraft, TMA 104, departed London on a return trip to Beirut via Frankfurt and Brindisi. It lost sufficient altitude and began descending after reaching 60 meters, striking the sea approximately 2250 meters from the end of the runway, 4 degrees left of the extended runway centerline. This resulted in a loss of power to both engines, likely due to fatigue, which led to a gradual loss of height and subsequent descent.

Description

Flight 104, a TMA DC-4 departed London at 12:02 GMT on the return trip to Beirut via Frankfurt and Brindisi. The plane arrived at Brindisi at 20:30 GMT and took off from runway 05 at 21:41 GMT for Beirut. The plane, however, didn’t gain enough height and started to descend again after reaching 60 m. The DC-4 banked slightly to the left and struck the sea 2250 m from the end of the runway, 4 degrees left of the extended runway centreline. PROBABLE CAUSE: “The accident was probably caused by a loss of power on No.1 and 2 engines following takeoff, which resulted in a gradual loss of height. The probable slow psycho-physical reaction of the crew, due to fatigue, may have prevented perception of the danger and the timely execution of manoeuvres to prevent the accident, or minimize its consequences.”

Primary Cause

Loss of power to both engines following takeoff, resulting in a gradual loss of height.Loss of power to both engines following takeoff, resulting in a gradual loss of height.

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