Casualties unknown

2009-08-27: BA Swallow 2 (G-AFCL) — Niden Manor, near Daventry, Northamptonshire, GB

Niden Manor, near Daventry, Northamptonshire, GB

On August 27, 2009, a BA Swallow 2 (registration G-AFCL) was involved in an aviation accident near Niden Manor, near Daventry, Northamptonshire, GB. This summary draws on records from the UK Air Accidents Investigation Branch (AAIB).

Sourcesthe UK Air Accidents Investigation Branch (AAIB)Primary reportUpdated 1785053200Data APIEditorial standards
Aircraft registered G-AFCL
Aircraft registered G-AFCL. Photo: RuthAS / CC BY 3.0, via Wikimedia Commons

On 27 August 2009, a BA Swallow 2 (G-AFCL) veered right after landing at a private airstrip near Daventry, striking a fence. The pilot, uninjured, found a fractured right main landing gear cross-strut.

History of the Flight

The aircraft, a BA Swallow 2 registered G-AFCL, had already completed two flights that day without incident. At 1845 UTC on 27 August 2009, the pilot, the sole occupant, returned to a private airstrip at Niden Manor, near Daventry, Northamptonshire, after a five-minute flight. The grass runway was oriented east/west, 800 m long and 20 m wide. The pilot, who held an Airline Transport Pilot’s Licence with 9,000 total flying hours (100 hours on type), estimated the surface wind from the south-west at 10 to 15 kt.

The Landing and Subsequent Event

The pilot flew a curving approach to the westerly runway to avoid obstacles under the final approach path and completed a normal landing. Immediately after touchdown, the aircraft began a slow turn to the right, which the pilot was unable to correct. The aircraft departed the right side of the runway, mounted an earth bank, and struck a fence at slow speed. The pilot, who was uninjured, shut down the engine and vacated the aircraft normally.

Damage Inspection

The accident resulted in damage to the propeller, the leading edges of both wings, the forward left fuselage, and the right main landing gear assembly.

Post-Accident Findings

Following the accident, the pilot determined that the cross-strut on the right main landing gear had fractured, probably at the moment of touchdown, causing the right main gear to fold outwards and resulting in a loss of directional control. The pilot did not consider the landing to have been abnormal or firm and could not explain the failure of the cross-strut.