Incident Overview

Date: Monday 6 June 1994
Aircraft Type: Tupolev Tu-154M
Owner/operator: China Northwest Airlines
Registration Number: B-2610
Location: 29 km SE of Xian-Xianyang International Airport (XIY) – ÿ China
Phase of Flight: En route
Status: Destroyed, written off
Casualties: Fatalities: 160 / Occupants: 160
Component Affected: Autopilot yaw-channel and bank control.Autopilot yaw-channel and bank control.
Category: Accident
A Tupolev 154M aircraft operated by China Northwest Airlines crashed in an accident after takeoff from Xian (XIY) to Guangzhou (CAN) on flight 2303. Twenty-four seconds after takeoff, the flight crew reported difficulties with control, exhibiting uncommanded banking to the left and right, increasing to 30 degrees, and an increasing angle of attack. The aircraft then rolled to the left, resulting in a nose drop and a pitch angle of -65 degrees, reaching 747 km/h. The altitude dropped from 4717 meters to 2884 meters within 12 seconds, and the aircraft’s airframe overloaded, leading to a breakup.A Tupolev 154M aircraft operated by China Northwest Airlines crashed in an accident after takeoff from Xian (XIY) to Guangzhou (CAN) on flight 2303. Twenty-four seconds after takeoff, the flight crew reported difficulties with control, exhibiting uncommanded banking to the left and right, increasing to 30 degrees, and an increasing angle of attack. The aircraft then rolled to the left, resulting in a nose drop and a pitch angle of -65 degrees, reaching 747 km/h. The altitude dropped from 4717 meters to 2884 meters within 12 seconds, and the aircraft’s airframe overloaded, leading to a breakup.

Description

A Tupolev 154M operated by China Northwest Airlines as flight 2303 from Xian (XIY) to Guangzhou (CAN) was destroyed in an accident after takeoff from Xian. All 146 passengers and 14 crew members were killed. The aircraft took off from Xianyang Airport at 08:13. Twenty-four seconds after takeoff the flight crew reported that the aircraft was difficult to control with uncommanded banking to the left and right of about 20ø, increasing to 30ø. The angle of attack increased to 20ø, activating the stall warning. After that, the airplane suddenly rolled to the left and the nose dropped to a pitch angle of -65ø. The speed reached 747 km/h and the overspeed warning sounded in the flight deck. In 12 seconds, the altitude dropped from 4717 to 2884 meters. The airframe was overloaded beyond structural limits and the aircraft began to break up. PROBABLE CAUSE: Auto-pilot induced oscillations caused the aircraft to shake violently. It appeared that the autopilot yaw-channel had been connected to the bank control and the bank-channel to the yaw controls. This was done the previous evening ‘in the field’ rather than in a workshop.

Source of Information

http://www.safehoo.com/Case/Case/Air/201204/269782.shtmlhttp://www.safehoo.com/Case/Case/Air/201204/269782.shtml

Primary Cause

Auto-pilot induced oscillations caused the aircraft to shake violently.Auto-pilot induced oscillations caused the aircraft to shake violently.

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