Incident Overview

Date: Saturday 1 July 1995
Aircraft Type: Fokker F-27 Friendship 500RF
Owner/operator: East West Airlines
Registration Number: VT-EWE
Location: Baroda (Vadodara) Airport (BDQ) – ÿ India
Phase of Flight: Landing
Status: Destroyed, written off
Casualties: Fatalities: 0 / Occupants: 3
Component Affected: Left Main Landing Gear and the Left Engine PropellersLeft Main Landing Gear and the Left Engine Propellers
Category: Accident
An East West F-27 VT-EWE aircraft was involved in a training flight at Baroda airport when the left main landing gear failed during touchdown. The aircraft subsequently landed on the runway, resulting in damage to the fuselage and engine propellers.An East West F-27 VT-EWE aircraft was involved in a training flight at Baroda airport when the left main landing gear failed during touchdown. The aircraft subsequently landed on the runway, resulting in damage to the fuselage and engine propellers.

Description

East West F-27 VT-EWE was engaged in a training flight at Baroda airport. The aircraft was under the command of an examiner pilot with the trainee pilot on right hand seat. The first touch and go exercise was uneventful. During the second exercise, immediately on touchdown the left main landing gear failed at its shock strut outer cylinder and the inner cylinder with the main wheel assembly attached to it got liberated. The aircraft continued moving forward with the remaining portion of left shock strut contacting the runway followed by the left engine propellers and fuselage bottom and finally came to rest on the runway left side strip. There was no fire and no injury to persons on board the aircraft. PROBABLE CAUSE: “The accident occurred during aircraft touchdown due to liberation of the sliding piston along with the wheels of the left main landing gear as a result of failure of the locking arrangement on the piston top end. Non-compliance by the operator of the Service Bulletin issued by the Manufacturer and Mandatory Modifications issued by the DGCA regarding piston-adapter and dowel pin lock fitment, is the Contributory Factor in the accident”.

Primary Cause

Failure of the locking arrangement on the piston top end, resulting in liberation of the sliding piston and subsequent damage to the landing gear and aircraft structure.Failure of the locking arrangement on the piston top end, resulting in liberation of the sliding piston and subsequent damage to the landing gear and aircraft structure.

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