Incident Overview

Date: Friday 30 July 1948
Aircraft Type: Douglas C-47A-1-DK Dakota C.3
Owner/operator: British European Airways – BEA
Registration Number: G-AGIX
Location: near Sywell – ÿ United Kingdom
Phase of Flight: Unknown
Status: Destroyed, written off
Casualties: Fatalities: 0 / Occupants: 19
Component Affected: Starboard engine constant speed unitStarboard engine constant speed unit
Category: Accident
On September 12, 1986, a Douglas C-47A G-AGIX aircraft experienced a catastrophic accident during a flight to Northolt. The aircraft overshot the runway and struck high tension cables, resulting in a forced belly landing in a wheat field. The accident was caused by a pilot error during a single-engined landing in dusk conditions, exacerbated by a malfunctioning starboard engine constant speed unit due to filter gauze failure, leading to restricted control valve movement and surging.On September 12, 1986, a Douglas C-47A G-AGIX aircraft experienced a catastrophic accident during a flight to Northolt. The aircraft overshot the runway and struck high tension cables, resulting in a forced belly landing in a wheat field. The accident was caused by a pilot error during a single-engined landing in dusk conditions, exacerbated by a malfunctioning starboard engine constant speed unit due to filter gauze failure, leading to restricted control valve movement and surging.

Description

Douglas C-47A G-AGIX departed Edinburgh at 19:03 GMT for a flight to Northolt. At about 20:37 GMT no. 2 engine problems (a.o. fluctuating rpm) forced the crew to feather the propeller. The remaining no. 1 engine was then set at 2450rpm and 36″ Hg boost. When the oil temperature rose and oil pressure started to fall, a decision was made to divert to Sywell. The aircraft overshot the runway and struck high tension cables in an almost completely stalled condition. A forced belly landing was made in a wheat field. PROBABLE CAUSE: “1) The accident was caused by an error of judgement on the part of the pilot whilst attempting a single-engined landing in dusk conditions. 2) The malfunctioning of the starboard engine constant speed unit was due to the failure if the filter gauze in fatigue. The subsequent surging and overspeeding was due to restriction to free movement of the control valve, occasioned by the passage of pieces of filter wire through the unit.”

Primary Cause

Pilot error during single-engined landing in dusk conditions, exacerbated by a malfunctioning starboard engine constant speed unit due to filter gauze failure.Pilot error during single-engined landing in dusk conditions, exacerbated by a malfunctioning starboard engine constant speed unit due to filter gauze failure.

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