Incident Overview

Date: Friday 3 May 1968
Aircraft Type: Lockheed L-188A Electra
Owner/operator: Braniff International Airways
Registration Number: N9707C
Location: 1,6 km E of Dawson, TX – ÿ United States of America
Phase of Flight: Take off
Status: Destroyed, written off
Casualties: Fatalities: 85 / Occupants: 85
Component Affected: Aircraft Structure (specifically wing)Aircraft Structure (specifically wing)
Investigating Agency: NTSBNTSB
Category: Accident
A Braniff Flight 352 experienced a significant incident during a flight to Dallas due to a sudden and severe thunderstorm. The crew requested a descent to FL150 and a westward deviation, but the Electra crew initially believed the situation was acceptable and continued to request a westward deviation. At 16:47, the aircraft experienced a series of events, including a 180-degree turn, a roll to a 90-degree bank angle, and a subsequent loss of control resulting in a crash at 6750 feet. The aircraft’s structural failure caused it to break up.A Braniff Flight 352 experienced a significant incident during a flight to Dallas due to a sudden and severe thunderstorm. The crew requested a descent to FL150 and a westward deviation, but the Electra crew initially believed the situation was acceptable and continued to request a westward deviation. At 16:47, the aircraft experienced a series of events, including a 180-degree turn, a roll to a 90-degree bank angle, and a subsequent loss of control resulting in a crash at 6750 feet. The aircraft’s structural failure caused it to break up.

Description

Braniff Flight 352 departed Houston (HOU) at 16:11 for a flight to Dallas (DAL) and climbed to FL200. Some 25 minutes into the flight, the L-188A Electra was approaching an area of severe thunderstorm activity. The crew requested a descent to FL150 and a deviation to the west. ARTCC then advised the crew that other aircraft were deviating to the east. The Electra crew still thought it looked all right on the west and were cleared to descend to FL140 and deviate to the west. At 16:44 the flight was further cleared to descend to 5000 feet. At 16:47 the aircraft had apparently encountered an area of bad weather, including hail, and requested (and were cleared for) a 180deg turn. Subsequent to the initiation of a right turn, the aircraft was upset. During the upset, N9707C rolled to the right to a bank angle in excess of 90deg and pitched nose down to approximately 40 degrees. A roll recovery maneuver was initiated and the aircraft experienced forces of 4,35 g. Part of the right wing failed and the aircraft broke up at an altitude of 6750 feet and crashed in flames a little later. PROBABLE CAUSE: “The stressing of the aircraft structure beyond its ultimate strength during an attempted recovery from an unusual attitude induced by turbulence associated with a thunderstorm. The operation in the turbulence resulted from a decision to penetrate an area of known severe weather.”

Primary Cause

The stressing of the aircraft structure beyond its ultimate strength during an attempted recovery from an unusual attitude induced by turbulence associated with a thunderstorm.The stressing of the aircraft structure beyond its ultimate strength during an attempted recovery from an unusual attitude induced by turbulence associated with a thunderstorm.

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