Incident Overview

Date: Monday 17 December 1973
Aircraft Type: McDonnell Douglas DC-10-30
Owner/operator: Iberia
Registration Number: EC-CBN
Location: Boston-Logan International Airport, MA (BOS) – ÿ United States of America
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 0 / Occupants: 168
Component Affected: Right Main GearRight Main Gear
Investigating Agency: NTSBNTSB
Category: Accident
A DC-10 aircraft, approaching Boston runway 33L, struck approach lights due to a combination of factors during a bad weather landing approach. The aircraft sheared off its right main gear, skidded to a rest 3000 feet from the threshold, and collided with a dyke. The incident was likely caused by a critical, unexpected descent rate that the captain failed to recognize and arrest before impact.A DC-10 aircraft, approaching Boston runway 33L, struck approach lights due to a combination of factors during a bad weather landing approach. The aircraft sheared off its right main gear, skidded to a rest 3000 feet from the threshold, and collided with a dyke. The incident was likely caused by a critical, unexpected descent rate that the captain failed to recognize and arrest before impact.

Description

The DC-10 approached Boston runway 33L in bad weather (rain, fog, 1.2 km visibility). The aircraft struck approach lights 500 feet short of the threshold and collided with a dyke. The right main gear was sheared off, the aircraft then skidded and came to a rest 3000 feet from the threshold. PROBABLE CAUSE: “The captain did not recognize, and may have been unable to recognize, an increased rate of descent in time to arrest it before the aircraft struck the approach light piers. The increased rate of descent was induced by an encounter with a low-level wind shear at a critical point in the landing approach where he was transitioning from automatic flight control under instrument flight conditions to manual flight control with visual references. The captain’s ability to detect and arrest the increased rate of descent was adversely affected by a lack of information as to the existence of the wind shear and the marginal visual cues available. The minimal DC-10 wheel clearance above the approach lights and the runway threshold afforded by the ILS glide slope made the response time critical and, under the circumstances, produced a situation wherein a pilot’s ability to make a safe landing was greatly diminished.”

Primary Cause

Unexpected descent rate induced by a low-level wind shear during the transition from automatic to manual flight control.Unexpected descent rate induced by a low-level wind shear during the transition from automatic to manual flight control.

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