Incident Overview

Date: Monday 14 April 2003
Aircraft Type: Grumman HU-16C Albatross
Owner/operator: private
Registration Number: N7026Y
Location: 6,5 km W of Chetumal Airport (CTM) – ÿ Mexico
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 3 / Occupants: 3
Component Affected: Aircraft AirframeAircraft Airframe
Category: Accident
A Grumman HU-16 amphibian airplane, N7026Y, crashed near Chetumal, Quintana Roo, Mexico, resulting in the fatal injuries of the pilot and two passengers. The aircraft was operating under VFR conditions and was instructed to land on runway 10 at the airport. A loss of control during a turn resulted in the aircraft rolling and nosed over, leading to a crash approximately 4 miles from the threshold.A Grumman HU-16 amphibian airplane, N7026Y, crashed near Chetumal, Quintana Roo, Mexico, resulting in the fatal injuries of the pilot and two passengers. The aircraft was operating under VFR conditions and was instructed to land on runway 10 at the airport. A loss of control during a turn resulted in the aircraft rolling and nosed over, leading to a crash approximately 4 miles from the threshold.

Description

A Grumman HU-16 amphibian airplane, N7026Y, was destroyed following a loss of control during the turn from base to final approach near Chetumal, State of Quintana Roo, in the Republic of Mexico. The instrument rated private pilot and his 2 passengers were fatally injured. The airplane was owned and operated by the pilot. Visual meteorological conditions prevailed for the personal flight for which a visual flight rules (VFR) flight plan was filed. The flight originated from Tulum at 17:30 with Chetumal (CTM) as its intended destination. Local authorities reported the airplane had been cleared to land on runway 10 at the Chetumal International Airport. Witnesses reported that the airplane rolled and nosed over during the turn from left base to final approach. The airplane came to rest about 4 miles from the threshold of runway 10. A post-impact fire consumed the airframe.

Primary Cause

Loss of control during a turn.Loss of control during a turn.

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