Casualties unknown

Cessna A188B Crashes After Hitting Palm Tree During Initial Climb in Maní (HK1648)

Maní, CO

On July 17, 2008, an A188B (registration HK1648) was involved in an aviation accident near Maní, CO. This summary draws on records from the Aircraft Accident Investigation Group of the Colombian Civil Aviation Authority (GRIAA).

Sourcesthe Aircraft Accident Investigation Group of the Colombian Civil Aviation Authority (GRIAA)Primary reportUpdated 2026-09-13Data APIEditorial standards

A Cessna A188B (HK1648) impacted a palm tree and other obstacles during initial climb after takeoff from Pista Los Milagros, resulting in the death of the sole occupant pilot.

Accident Overview

On July 17, 2008, at approximately 14:00 local time, a Cessna A188B agricultural aircraft, registration HK1648, operated by ASAM (Agrícola de Servicios Aéreos del Meta Ltda.), crashed during the initial climb phase after departing from Pista Los Milagros in the municipality of Maní, Casanare department (Meta region). The aircraft was performing its fourth takeoff of the day, carrying 160 gallons of liquid spray for aerial application.

Sequence of Events

During the initial climb, the aircraft struck a palm tree located to the right of the departure path. Subsequently, it collided with another tree, a light post, and came to rest in a field approximately 200 meters from the runway threshold. No fire occurred following the impact.

Aircraft and Pilot Information

The single-engine aircraft was a Cessna A188B, model 188B, and was registered in Colombia with airworthiness certificate number 2128. The owner was Agrícola de Servicios Aéreos del Meta "ASAM Ltda.". The sole occupant was the pilot, Gustavo Antonio Restrepo Acevedo, who held a PCA (Piloto Comercial de Aviación) license number 2280, with a valid medical certificate expiring on August 8, 2008.

Injuries and Damage

The pilot sustained fatal injuries. The aircraft sustained substantial damage: the left wing detached, the empennage fractured, the left landing gear separated, the right wing fractured, the cabin fractured, propeller blades bent, and the engine experienced a sudden stop. Repair feasibility was pending evaluation by the UAEAC technical group.

Investigation Status

The accident is under investigation by the Grupo de Investigación de Accidentes (GIA) of the UAEAC. No probable cause has been determined at this preliminary stage. Recommendations include sending the engine and propeller to an UAEAC-authorized workshop for post-accident inspection and urgently appointing an investigator in charge per internal circular 0002-GIA-2005.