Incident Overview

Date: Thursday 29 December 1955
Aircraft Type: Lockheed 18-56-23 Lodestar
Owner/operator: Gulf Oil Corporation
Registration Number: N33366
Location: 7,5 km NW of Londonderry, OH – ÿ United States of America
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: The tail group of the aircraft.The tail group of the aircraft.
Investigating Agency: CABCAB
Category: Accident
A flight from Tulsa, Oklahoma, experienced icing conditions and loss of control due to excessive ice accumulation. The pilot requested descent to lower altitudes multiple times, but these requests were denied. The aircraft descended to 8,000 feet msl before striking the ground in a steep angle, with components separating from the aircraft.A flight from Tulsa, Oklahoma, experienced icing conditions and loss of control due to excessive ice accumulation. The pilot requested descent to lower altitudes multiple times, but these requests were denied. The aircraft descended to 8,000 feet msl before striking the ground in a steep angle, with components separating from the aircraft.

Description

The flight departed Tulsa at 18:10 CST and routine position reports were made until over Dayton, Ohio, at 12:00. Over Dayton the aircraft entered icing conditions at the cruise altitude of 9000 feet. The crew requested permission twice to descend to a lower altitude to evade the icing conditions, but these requests were turned down. Around 12:35 the pilot reported “Difficulty maintaining altitude and airspeed request lower altitude.” At 12:37 Columbus CAA cleared the flight to descend to 8,000 feet msl. At approximately 12:40 witnesses observed the aircraft below the overcast; it was on a westerly heading and was descending although it appeared to be in a normal attitude. Several components were seen to separate from the aircraft before it struck the ground in a steep angle. PROBABLE CAUSE: “The Board determines that the probable cause of this accident was the accumulation of enough ice to result in loss of control and the subsequent shedding of vertical surfaces from the tail group of the aircraft.”

Primary Cause

Accumulation of sufficient ice resulting in loss of control and subsequent shedding of vertical surfaces from the tail group.Accumulation of sufficient ice resulting in loss of control and subsequent shedding of vertical surfaces from the tail group.

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