Incident Overview

Date: Friday 30 September 2016
Aircraft Type: Cessna 208B Grand Caravan
Owner/operator: Llanera de Aviaci¢n
Registration Number: HK-3804
Location: near San Antonio de Prado – ÿ Colombia
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 4 / Occupants: 11
Component Affected: Aircraft Weight & CargoAircraft Weight & Cargo
Investigating Agency: AerocivilAerocivil
Category: Accident
On October 26, 2023, a Cessna 208B Grand Caravan, HK-3804, crashed in a rural area near San Antonio de Prado, Colombia, resulting in the fatalities of the copilot, two passengers, and a newborn baby. The aircraft departed Medell¡n-Enrique Olaya Herrera Airport at 11:58 hours on a domestic charter flight to Jurad¢, and was cleared to fly on a runway course to Cerro El Volador and then make a turn to the right, in a visual climb until crossing the town of San Antonio de Prado. ATC reported the aircraft was estimated to cross the position of San Antonio de Prado at 12:00, but no notification was received. At 13:00, the aircraft was found crashed. The investigation by Aerocivil revealed that the crew used an empty basic weight of 5254 lbs (2383 kg), significantly below the aircraft’s actual weight of 5411 lbs (2454 kg). Furthermore, the crew did not account for the 650 kg of cargo onboard, which significantly reduced the aircraft’s takeoff weight. The crew’s calculations resulted in a takeoff weight of 8719 lbs (3955 kg), which was below the maximum takeoff weight of 8750 lbs (3970 kg). The actual takeoff weight was 10320 lbs (4681 kg). The incident was likely caused by a take-off with a weight approximately 17% higher than the maximum gross operating weight (MTOW) established for the C208B aircraft. Limited climb rate with signs of lift loss due to the overweight during the initial climb, and a forced landing in mountainous terrain due to loss of lift caused by the overweight during the initial climb, contributed to the incident.On October 26, 2023, a Cessna 208B Grand Caravan, HK-3804, crashed in a rural area near San Antonio de Prado, Colombia, resulting in the fatalities of the copilot, two passengers, and a newborn baby. The aircraft departed Medell¡n-Enrique Olaya Herrera Airport at 11:58 hours on a domestic charter flight to Jurad¢, and was cleared to fly on a runway course to Cerro El Volador and then make a turn to the right, in a visual climb until crossing the town of San Antonio de Prado. ATC reported the aircraft was estimated to cross the position of San Antonio de Prado at 12:00, but no notification was received. At 13:00, the aircraft was found crashed. The investigation by Aerocivil revealed that the crew used an empty basic weight of 5254 lbs (2383 kg), significantly below the aircraft’s actual weight of 5411 lbs (2454 kg). Furthermore, the crew did not account for the 650 kg of cargo onboard, which significantly reduced the aircraft’s takeoff weight. The crew’s calculations resulted in a takeoff weight of 8719 lbs (3955 kg), which was below the maximum takeoff weight of 8750 lbs (3970 kg). The actual takeoff weight was 10320 lbs (4681 kg). The incident was likely caused by a take-off with a weight approximately 17% higher than the maximum gross operating weight (MTOW) established for the C208B aircraft. Limited climb rate with signs of lift loss due to the overweight during the initial climb, and a forced landing in mountainous terrain due to loss of lift caused by the overweight during the initial climb, contributed to the incident.

Description

A Cessna 208B Grand Caravan, HK-3804, was destroyed when it impacted a hillside in a rural area near San Antonio de Prado, Colombia. The aircraft departed Medell¡n-Enrique Olaya Herrera Airport at 11:58 hours on a domestic charter flight to Jurad¢. The flight was cleared to fly on a runway course to Cerro El Volador and then make a turn to the right, in a visual climb until crossing the town of San Antonio de Prado. According to ATC information, the aircraft estimated to cross the position of San Antonio de Prado at 12:00, however, no notification was obtained from the flight. At 13:00 the aircraft was found crashed. The copilot, two passengers and a new-born baby suffered fatal injuries. The investigation by Aerocivil showed that the crew used an empty basic weight of the aircraft of 5254 lbs (2383 kg), that is, 157 lbs. (71 kg) below the actual weight of the aircraft, which was 5411 lbs (2454 kg), according to the last certified weighing of the aircraft. They also did not take into account the 650 kg of cargo on board. According to the crew’s calculations, the takeoff weight of the aircraft was 8719 lbs (3955 kg), which was below the maximum takeoff weight of 8750 lbs (3970 kg). Instead, the actual takeoff weight was 10320 lbs (4681 kg). Probable cause: Execution of a take-off with a weight approximately 17% higher than the maximum gross operating weight (MTOW) established for the C208B aircraft. Limited climb rate with signs of lift loss due to the low performance given by the overweight during the initial climb phase. Forced landing in mountainous terrain due to loss of lift caused by overweight during the initial climb. Absence in the identification of the risks associated to an overweight operation of the aircraft. Contributing Factors: Lack of supervision by the Aircraft Operator in relation to the dispatch of aircraft operating from the outside at the main base of operation.

Source of Information

http://www.elespectador.com/noticias/nacional/antioquia/cuatro-muertos-accidente-de-avioneta-san-antonio-de-pra-video-658000, http://www.minuto30.com/fotos-y-video-a-cuatro-ascienden-las-victimas-mortales-de-avioneta-siniestrada-en-san-antonio-de-prado/531135/http://www.elespectador.com/noticias/nacional/antioquia/cuatro-muertos-accidente-de-avioneta-san-antonio-de-pra-video-658000, http://www.minuto30.com/fotos-y-video-a-cuatro-ascienden-las-victimas-mortales-de-avioneta-siniestrada-en-san-antonio-de-prado/531135/

Primary Cause

The aircraft’s excessive weight, particularly the lack of consideration for cargo, combined with a reduced climb rate, likely contributed to the loss of lift during the initial climb, leading to a forced landing in mountainous terrain.The aircraft’s excessive weight, particularly the lack of consideration for cargo, combined with a reduced climb rate, likely contributed to the loss of lift during the initial climb, leading to a forced landing in mountainous terrain.

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