Incident Overview

Date: Saturday 15 May 1993
Aircraft Type: Douglas DC-6BF
Owner/operator: Carga del Caribe
Registration Number: XA-SEA
Location: 22 km N off Cozumel Airport (CZM) – ÿ Mexico
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 3 / Occupants: 5
Component Affected: AircraftAircraft
Investigating Agency: SCTSCT
Category: Accident
A Douglas DC-6 aircraft crashed off Canc£n Airport, Mexico, during a test flight. Two crew members and one passenger perished. The aircraft was instructed to descend to 2000 feet altitude, but experienced unfavorable weather conditions leading to a collision with the water. The pilot in command and a passenger suffered serious injuries, while the co-pilot was fatally injured and the other two passengers were reported missing.A Douglas DC-6 aircraft crashed off Canc£n Airport, Mexico, during a test flight. Two crew members and one passenger perished. The aircraft was instructed to descend to 2000 feet altitude, but experienced unfavorable weather conditions leading to a collision with the water. The pilot in command and a passenger suffered serious injuries, while the co-pilot was fatally injured and the other two passengers were reported missing.

Description

A Douglas DC-6 hit the water off Canc£n Airport, Mexico, during a test flight. One pilot and two passengers died in the accident. The aircraft departed Canc£n Airport at 09:22 hours on a test flight to Cozumel, without the intention to land there, and back to Canc£n. The intention was to verify the operation of the engines. In the flight plan the pilot noted that would fly at 2000 feet. At 15 miles from Cozumel, the flight requested authorization from the control tower of Canc£n to descend. This was approved. The aircraft descended in unfavorable weather conditions (rain) until it hit the water. The pilot in command and a passenger suffered serious injuries. The co-pilot was fatally injured and the other two passengers were reported missing. Probable cause: Performing an altitude loss operation, in low visibility conditions, with an exaggerated descent angle considering the flight level (2000 feet) over water, not allowing space for the recovery of the aircraft, until impacting the water surface.

Primary Cause

Performing an altitude loss operation, in low visibility conditions, with an exaggerated descent angle considering the flight level (2000 feet) over water, not allowing space for the recovery of the aircraft.Performing an altitude loss operation, in low visibility conditions, with an exaggerated descent angle considering the flight level (2000 feet) over water, not allowing space for the recovery of the aircraft.

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