No fatalities

1995-07-01: Fokker F27 Friendship (VT-EWE) — East West Airlines - India — Baroda (Vadodara), India

Baroda (Vadodara), IndiaLanding (descent or approach)

On July 1, 1995, a Fokker F27 Friendship (registration VT-EWE) operated by East West Airlines - India was involved in an aviation accident near Baroda (Vadodara), India during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: 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. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781207861Data APIEditorial standards

During a training flight at Baroda airport, the left main landing gear failed on touchdown, causing the aircraft to slide on the runway. No fire or injuries occurred. The accident was attributed to a locking arrangement failure and non-compliance with service bulletins.

Incident Summary

A training flight operating at Baroda airport experienced a landing gear failure during a touch-and-go exercise. The aircraft, under the command of an examiner pilot with a trainee pilot in the right seat, had completed the first touch-and-go without incident. During the second touchdown, the left main landing gear failed at the shock strut outer cylinder. The inner cylinder and attached main wheel assembly separated from the aircraft.

Event Details

Following the failure, the aircraft continued moving forward. The remaining portion of the left shock strut contacted the runway, along with the left engine propellers and the fuselage bottom. The aircraft came to rest on the left side strip of the runway. There was no fire and no injuries to the persons on board.

Probable Cause

The official investigation determined that 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.