Incident Overview

Date: Monday 28 June 1965
Aircraft Type: Boeing 707-321B
Owner/operator: Pan American World Airways (Pan Am)
Registration Number: N761PA
Location: near San Francisco, CA – ÿ United States of America
Phase of Flight: Take off
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 153
Component Affected: The third stage turbine diskThe third stage turbine disk
Investigating Agency: CABCAB
Category: Accident
A Pan Am flight 843 experienced a catastrophic event following takeoff, resulting in the disintegration of the third stage turbine disk of the No. 4 engine. This led to a fire and an explosion in the engine area, with the No. 4 engine and a significant portion of the right outer wing separating from the aircraft. The incident occurred at an altitude of approximately 800 feet above the ground, and the flight concluded with a successful emergency landing at Travis Air Force Base, California.A Pan Am flight 843 experienced a catastrophic event following takeoff, resulting in the disintegration of the third stage turbine disk of the No. 4 engine. This led to a fire and an explosion in the engine area, with the No. 4 engine and a significant portion of the right outer wing separating from the aircraft. The incident occurred at an altitude of approximately 800 feet above the ground, and the flight concluded with a successful emergency landing at Travis Air Force Base, California.

Description

Pan Am flight 843 experienced an explosive disintegration of the third stage turbine disk of the No. 4 engine. The accident occurred shortly after takeoff from San Francisco, at an altitude of about 800 feet above the ground. Disintegration of the turbine disk was followed by a fire in the No. 4 engine area and an explosion in the outboard reserve fuel tank. The No. 4 engine and approximately 25 feet of the right outer wing separated from the aircraft. The fire was extinguished and a successful emergency landing was accomplished at Travis Air Force Base, California, with no injuries to the 143 passengers or 10 crewmembers aboard the flight. PROBABLE CAUSE: “The failure of the third stage turbine disk. This failure was caused by a transient loss of operating clearance between the third stage turbine disk and the third stage inner sealing ring. This loss of clearance resulted from a combination of improper turbine rotor positioning during engine assembly, the use of serviceable worn parts, and an operating clearance which was less than predicted in design analysis.”

Primary Cause

Transient loss of operating clearance between the third stage turbine disk and the third stage inner sealing ring, resulting from improper turbine rotor positioning, use of serviceable worn parts, and insufficient operating clearance.Transient loss of operating clearance between the third stage turbine disk and the third stage inner sealing ring, resulting from improper turbine rotor positioning, use of serviceable worn parts, and insufficient operating clearance.

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