2 fatalities

2020-11-08: Quest Kodiak 100 (TG-SMT) — Cachapoyas Investment — Guatemala City-La Aurora, Guatemala

Guatemala City-La Aurora, GuatemalaTakeoff (climb)

On November 8, 2020, a Quest Kodiak 100 (registration TG-SMT) operated by Cachapoyas Investment was involved in an aviation accident near Guatemala City-La Aurora, Guatemala during takeoff. 2 people were killed. Investigators recorded the probable cause as: The following contributing factors were identified: - The demand for food and the population's urgent need for aid likely led the crew to make the erroneous decision to increase the load and materials for transport. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781190260Data APIEditorial standards

A humanitarian flight from Guatemala City to Cobán crashed after takeoff, killing both occupants. The aircraft was destroyed by impact and post-crash fire. Investigators cited excess weight and a probable rearward cargo shift as contributing factors.

Accident Overview

A humanitarian flight departed from Guatemala City-La Aurora airport on a mission to transport one pilot, one passenger, and a load consisting of food and essential products to Cobán. After taking off from runway 02, the aircraft entered an uncontrolled descent during the initial climb. It struck trees and high tension wires before crashing in the 4th Avenue located in the Zone 9 district, approximately 980 meters from the end of runway 02.

Aftermath

The aircraft was destroyed by the impact forces and a post-crash fire. Both occupants were killed.

Probable Cause

The investigation identified the following contributing factors: the demand for food and the population's urgent need for aid likely led the crew to make the erroneous decision to increase the load and materials for transport; the aircraft exceeded the permissible flight load capacity, carrying 8,055 lbs instead of the allowable 7,255 lbs; and a probable shift of the cargo toward the rear of the aircraft negatively affected the center of gravity, disrupting the minimum weight and balance requirements, which prevented the aircraft from climbing and maintaining proper flight.