Double engine failure leads to fatal ditching of Shorts SD3-60

Casualties unknown • Firth of Forth, GB

A scheduled mail flight involving a Shorts SD3-60 Variant 100 ended in a fatal ditching in the Firth of Forth following a simultaneous loss of power in both engines.

What happened

On 27 February 2001, a Shorts SD3-60 Variant 100, registration G-BMNT, was performing a scheduled mail flight from Edinburgh Airport. The aircraft, operated with a crew of two, had been parked at the airport following a period of overnight weather characterized by strong winds and light snow. After a brief technical delay involving a generator issue that was subsequently resolved through ground engine runs, the aircraft departed from Runway 0 06.

During the climb, once the aircraft reached approximately 2,200 feet, the crew activated the engine anti-icing systems. Almost immediately following this action, the torque on both engines dropped rapidly to zero. The crew issued a MAYDAY call to air traffic control, reporting a double engine failure, and subsequently declared an intention to ditch. The aircraft impacted the water in the Firth of Forth near Birnie Rocks. The impact in the shallow water caused severe damage to the airframe, resulting in two fatalities among the crew.

Probable cause

The simultaneous loss of power in both engines was likely caused by the activation of the inertial separator vanes, which altered the airflow conditions within the engine intakes and potentially disturbed accumulated snow or ice that had remained in the intake trunking or plenum chambers.

Frequently asked questions

What happened in the 2001-02-27 SD3-60 Variant 100 accident near Firth of Forth, GB?

A scheduled mail flight involving a Shorts SD3-60 Variant 100 ended in a fatal ditching in the Firth of Forth following a simultaneous loss of power in both engines.

What aircraft was involved and where did it happen?

The accident on 2001-02-27 involved a SD3-60 Variant 100, registration G-BNMT, at Firth of Forth, GB.

What was the probable cause of the accident?

The simultaneous loss of power in both engines was likely caused by the activation of the inertial separator vanes, which altered the airflow conditions within the engine intakes and potentially disturbed accumulated snow or ice that had remained in the intake trunking or plenum chambers.

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