Incident Overview

Date: Monday 2 April 1956
Aircraft Type: Boeing 377 Stratocruiser 10-30
Owner/operator: Northwest Orient Airlines
Registration Number: N74608
Location: 8,7 km SW off Seattle/Tacoma International Airport, WA (SEA) – ÿ United States of America
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 5 / Occupants: 38
Component Affected: Boeing 377 and Lockheed L-1049 aircraft, specifically the engine cowl flaps.Boeing 377 and Lockheed L-1049 aircraft, specifically the engine cowl flaps.
Investigating Agency: CABCAB
Category: Accident
Northwest Flight 2 experienced a significant loss of altitude and sank in Puget Sound after a series of maneuvers due to a critical error in control system operation. The aircraft’s unusual cowl flap configuration, coupled with the failure to fully close the engine cowl flaps, was identified as the primary cause of the incident.Northwest Flight 2 experienced a significant loss of altitude and sank in Puget Sound after a series of maneuvers due to a critical error in control system operation. The aircraft’s unusual cowl flap configuration, coupled with the failure to fully close the engine cowl flaps, was identified as the primary cause of the incident.

Description

Northwest Flight 2 (Seattle-Portland-Chicago-New York) took off from Seattle at 08:06. As the aircraft reached 2000 feet, at 145 knots airspeed, the flaps were retracted. Severe buffeting started and the aircraft tended to roll to the left. Thinking it was an asymmetric flap condition, the captain reduced power to stop the buffeting, but of no avail. Full power was applied again and plans were made to divert to McChord AFB. The plane continued to lose altitude and was not able to reach McChord. A ditching was carried out in Puget Sound. The aircraft sank 15 minutes after the ditching. It appeared that the aircraft had taken off with the engine cowl flaps fully open. Though not emphasized as a contributory factor, it must be noted that the cowl flap control on the Boeing 377 and Lockheed L-1049 move in opposite directions for the closing of the cowls. Most of the flight engineers flying time had been on L-1049 and DC-6 aircraft. PROBABLE CAUSE: “The incorrect analysis of control difficulty which occurred on retraction of the wing flaps as a result of the flight engineer’s failure to close the engine cowl flaps – the analysis having been made under conditions of great urgency and within an extremely short period of time available for decision.”

Primary Cause

Incorrect analysis of control difficulty resulting from the flight engineer’s failure to close the engine cowl flaps, exacerbated by conditions of great urgency and limited decision time.Incorrect analysis of control difficulty resulting from the flight engineer’s failure to close the engine cowl flaps, exacerbated by conditions of great urgency and limited decision time.

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