Incident Overview

Date: Thursday 14 November 1946
Aircraft Type: Douglas C-47A-90-DL (DC-3)
Owner/operator: KLM Royal Dutch Airlines
Registration Number: PH-TBW
Location: Amsterdam-Schiphol Airport (AMS) – ÿ Netherlands
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 26 / Occupants: 26
Component Affected: Douglas DC-3 aircraftDouglas DC-3 aircraft
Category: Accident
A KLM Douglas DC-3 crashed following a loss of control while on approach to Amsterdam-Schiphol Airport, resulting in the deaths of all 26 occupants. The aircraft, a Douglas C-47A, experienced a steep left-hand turn due to visibility limitations caused by fog, leading to a ground impact. The pilot’s actions, including circling the airport three times without visual contact and a left-hand bank, contributed to the accident.A KLM Douglas DC-3 crashed following a loss of control while on approach to Amsterdam-Schiphol Airport, resulting in the deaths of all 26 occupants. The aircraft, a Douglas C-47A, experienced a steep left-hand turn due to visibility limitations caused by fog, leading to a ground impact. The pilot’s actions, including circling the airport three times without visual contact and a left-hand bank, contributed to the accident.

Description

A KLM Douglas DC-3 crashed following a loss of control while on approach to Amsterdam-Schiphol Airport, Netherlands , killing all 26 occupants. A Douglas C-47A, operating a passenger service from London-Croydon Airport, crashed while on final approach to Amsterdam-Schiphol Airport, killing all 26 on board. Visibility at Schiphol Airport was limited due to fog. The captain circled the airport three times without acquiring visual contact with the ground. He likely then observed the runway and airport lights. Not being lined up with runway 23, the pilot made a steep left-hand turn. The aircraft then struck the ground in a 65ø pitch and 45ø left hand bank attitude. Flight testing of the DC-3 aircraft had shown it was vulnerable during low speed steep turns, as the aircraft could enter an asymmetrical stall. It was a.o. concluded that the captain was not sufficiently familiar with the specific flight characteristics of the DC-3 during low speed turns. Also, the captain was not sufficiently proficient in carrying out approaches and landings in the given weather circumstances.

Primary Cause

Insufficient familiarity with low-speed steep turn flight characteristics and inadequate proficiency in approach and landing procedures under the specific weather conditions.Insufficient familiarity with low-speed steep turn flight characteristics and inadequate proficiency in approach and landing procedures under the specific weather conditions.

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