Incident Overview

Date: Sunday 24 February 2008
Aircraft Type: Dornier 328-100
Owner/operator: South East Asian Airlines
Registration Number: RP-C5328
Location: Manila-Ninoy Aquino International Airport (MNL) – ÿ Philippines
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 35
Component Affected: Aircraft control system (specifically rudder and nose wheel steering)Aircraft control system (specifically rudder and nose wheel steering)
Category: Accident
A Dornier 328-100 operated by South East Asian Airlines experienced a runway excursion accident at Manila-Ninoy Aquino International Airport, Philippines. The aircraft landed on runway 13 and subsequently lost directional control after the captain initiated reverse thrust. The aircraft then turned to the left and settled 130 meters on the left side of the runway against the drainage canal, resulting in substantial damage. The incident was likely caused by the Captain?s failure to maintain positive control, specifically by not holding the tiller to steer the nose wheel, resulting in a 60-degree left and right rudder angle.A Dornier 328-100 operated by South East Asian Airlines experienced a runway excursion accident at Manila-Ninoy Aquino International Airport, Philippines. The aircraft landed on runway 13 and subsequently lost directional control after the captain initiated reverse thrust. The aircraft then turned to the left and settled 130 meters on the left side of the runway against the drainage canal, resulting in substantial damage. The incident was likely caused by the Captain?s failure to maintain positive control, specifically by not holding the tiller to steer the nose wheel, resulting in a 60-degree left and right rudder angle.

Description

A Dornier 328-100 operated by South East Asian Airlines sustained substantial damage in a runway excursion accident at Manila-Ninoy Aquino International Airport, Philippines. The flight landed on runway 13. After selecting reverse prop the aircraft was still aligned with the runway but after the condition lever was pulled by the captain, the aircraft made a sudden turn to the left and the first officer who was still Pilot Flying could not regain directional control. The aircraft went off the runway and settled some 130 meters on the left side of the runway against the main drainage canal. The aircraft sustained substantial damage. There were no injuries among the crew and passengers. PROBABLE CAUSE: “This accident was caused by the failure of the Captain to take positive control of the aircraft after the F/O landed the aircraft. He engaged the CL to minimum without holding the tiller to steer the nose wheel which is now with 60§ left and right range. Additionally, if the black boxes of the aircraft which met an accident on December 18, 2006 were read before they were ordered released to the Vice President of SEAIR, it could have help prevent this accident.”

Primary Cause

Captain?s failure to maintain positive control of the aircraft after the F/O landed the aircraft, resulting in loss of directional control.Captain?s failure to maintain positive control of the aircraft after the F/O landed the aircraft, resulting in loss of directional control.

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