Incident Overview

Date: Tuesday 19 February 1985
Aircraft Type: Boeing 747SP-09
Owner/operator: China Airlines
Registration Number: N4522V
Location: 550 km NW off San Fransisco, CA, USA – ÿ Pacific Ocean
Phase of Flight: En route
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 274
Component Affected: No. 4 engineNo. 4 engine
Investigating Agency: NTSBNTSB
Category: Accident
A flight from Taipei to about 300 nautical miles northwest of San Francisco experienced a significant loss of power on the No. 4 engine, leading to a rapid descent and control issues. The pilot lost control of the aircraft, resulting in a roll, nose-over, and uncontrolled descent. The pilot eventually stabilized the aircraft and diverted to San Francisco International Airport, where a safe landing was achieved. Significant structural damage occurred during the event.A flight from Taipei to about 300 nautical miles northwest of San Francisco experienced a significant loss of power on the No. 4 engine, leading to a rapid descent and control issues. The pilot lost control of the aircraft, resulting in a roll, nose-over, and uncontrolled descent. The pilot eventually stabilized the aircraft and diverted to San Francisco International Airport, where a safe landing was achieved. Significant structural damage occurred during the event.

Description

The flight from Taipei to about 300 nmi northwest of San Francisco was uneventful and the airplane was flying at about 41,000 feet mean sea level when the No. 4 engine lost power. During the attempt to recover and restore normal power on the No. 4 engine, the airplane rolled to the right, nosed over, and entered an uncontrollable descent. The captain was unable to restore the airplane to stable flight until it had descended to 9,500 feet. After the captain stabilized the airplane, he elected to divert to San Francisco International Airport, where a safe landing was made. Although the airplane suffered major structural damage during the upset, descent, and subsequent recovery, only two persons among the 274 passengers and crew on board were injured seriously. The maximum vertical acceleration forces recorded during the descent were 4.8Gs and 5.1Gs as the airplane descended through 30,552 feet and 19,083 feet, respectively. PROBABLE CAUSE: “The captain’s preoccupation with an inflight malfunction and his failure to monitor properly the airplane’s flight instruments which resulted in his losing control of the airplane. Contributing to the accident was the captain’s over-reliance on the autopilot after the loss of thrust on the no. 4 engine.”

Primary Cause

Captain’s preoccupation with an inflight malfunction and failure to properly monitor flight instruments, leading to loss of control.Captain’s preoccupation with an inflight malfunction and failure to properly monitor flight instruments, leading to loss of control.

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