Incident Overview

Date: Friday 22 May 1953
Aircraft Type: Curtiss C-46F-1-CU Commando
Owner/operator: Resort Airlines, lsf United States Air Force – USAF
Registration Number: N1669M
Location: 18 km NE of Des Moines, IA – ÿ United States of America
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: Right wing panelRight wing panel
Investigating Agency: CABCAB
Category: Accident
An aircraft, a C-46, experienced a catastrophic failure during a severe thunderstorm over Nebraska. The pilot requested a change in altitude, which was denied due to another aircraft flying at a higher altitude. The aircraft lost control, resulting in the right wing panel failing and subsequent disintegration. A strong downward force caused by the thunderstorm overwhelmed the wing’s design strength, leading to a separation of the aileron tab motor from its support bracket.An aircraft, a C-46, experienced a catastrophic failure during a severe thunderstorm over Nebraska. The pilot requested a change in altitude, which was denied due to another aircraft flying at a higher altitude. The aircraft lost control, resulting in the right wing panel failing and subsequent disintegration. A strong downward force caused by the thunderstorm overwhelmed the wing’s design strength, leading to a separation of the aileron tab motor from its support bracket.

Description

The aircraft arrived at Cheyenne, Wyoming at 00:38 on a Civil Air Movement flight from New York International Airport. The aircraft departed Cheyenne at 01:32, on an instrument flight plan to Chicago at 7,000 feet. The C-46 progressed uneventfully until it reached Omaha. The pilot contacted Omaha INSAC and requested a change of altitude to 3,000 feet. This was denied because another flight proceeded at 2,600 feet between Des Moines and Omaha. The aircraft flew then into a severe thunderstorm in the vicinity of Des Moines. The aircraft lost control and subsequently the right wing panel failed at the attach angles to the center section due to a strong downward force which exceeded the design strength of the wing. The wing panel then struck the tail, causing it to disintegrate. PROBABLE CAUSE: “Separation of the right aileron tab motor from its support bracket due to loss of its outboard trunnion while the aircraft was in the severe turbulence of a thunderstorm. These conditions resulted in a tendency to roll erratically, and in conjunction with the extreme turbulence, caused loss of control and subsequent overloading of the wing to the point of failure.”

Primary Cause

Separation of the right aileron tab motor from its support bracket due to loss of its outboard trunnion while the aircraft was in the severe turbulence of a thunderstorm.Separation of the right aileron tab motor from its support bracket due to loss of its outboard trunnion while the aircraft was in the severe turbulence of a thunderstorm.

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