Incident Overview

Date: Friday 4 March 1988
Aircraft Type: Fairchild FH-227B
Owner/operator: Transport A‚rien Transr‚gional – TAT
Registration Number: F-GCPS
Location: 1,6 km E of Machault – ÿ France
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 23 / Occupants: 23
Component Affected: Aircraft attitude reference system and autopilot system.Aircraft attitude reference system and autopilot system.
Category: Accident
A TAT Flight 230 experienced a sudden and catastrophic descent following a power line strike near Paris-Orly. The aircraft pitched nose down due to an electrical system failure in instrument weather conditions, leading to a loss of attitude reference and autopilot disconnect. The crew lacked usable attitude reference while in a high-speed dive without an independent horizon.A TAT Flight 230 experienced a sudden and catastrophic descent following a power line strike near Paris-Orly. The aircraft pitched nose down due to an electrical system failure in instrument weather conditions, leading to a loss of attitude reference and autopilot disconnect. The crew lacked usable attitude reference while in a high-speed dive without an independent horizon.

Description

TAT Flight 230 departed Nancy, France, at 06:53 hours for Paris-Orly and climbed to a cruising altitude of FL140. At 07:26 the aircraft was cleared to descend to FL90 and later FL70. Approaching the MEL VOR, clearance was given to descend further to FL60. About 07:37 the aircraft entered a steep descent at a rate of 16000 ft/min. Twenty seconds later the aircraft struck power lines and impacted the ground. PROBABLE CAUSE (translated from original French language report): Immediately after an electrical systems failure occurred in instrument weather conditions, the aircraft pitched nose down. The Committee was unable to acquire any certainty as to the cause of this catastrophic descent. After eliminating various assumptions invalidated by the established facts and findings and after reviewing the results of flight tests conducted at its request, the commission assigned higher probability to the hypothesis that the electrical fault caused a loss of attitude reference and autopilot disconnect which would have occurred while the aircraft was configured ‘out of trim’ in a nose down attitude. In the absence of independent standby horizon, the crew had no usable attitude reference immediately available while the aircraft was in a high-speed dive.

Source of Information

http://www.aerosteles.net/fiche.php?code=machault-fokkerhttp://www.aerosteles.net/fiche.php?code=machault-fokker

Primary Cause

Electrical system failure in instrument weather conditions leading to a loss of attitude reference and autopilot disconnect.Electrical system failure in instrument weather conditions leading to a loss of attitude reference and autopilot disconnect.

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