Baroda - Baroda

The aircraft was engaged in a training flight at Baroda airport. It 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.

Flight / Schedule

Baroda - Baroda

Registration

VT-EWE

MSN

10605

Year of Manufacture

1980

Date

July 1, 1995 at 08:40 AM

Type

CRASH

Flight Type

Training

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Baroda (Vadodara) Gujarat

Region

Asia • India

Coordinates

22.3108°, 73.1657°

Crash Cause

Technical failure

Narrative Report

On July 1, 1995 at 08:40 AM, Baroda - Baroda experienced a crash involving Fokker F27 Friendship, operated by East West Airlines - India, with the event recorded near Baroda (Vadodara) Gujarat.

The flight was categorized as training and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

3 people were known to be on board, 0 fatalities were recorded, 3 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 3, crew fatalities: 0, passengers on board: 0, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is technical failure. The aircraft was engaged in a training flight at Baroda airport. It 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.

Aircraft reference details include registration VT-EWE, MSN 10605, year of manufacture 1980.

Geospatial coordinates for this crash are approximately 22.3108°, 73.1657°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

The aircraft was engaged in a training flight at Baroda airport. It 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.

Cause: Technical failure

Occupants & Outcome

Crew On Board

3

Passengers On Board

0

Estimated Survivors

3

Fatality Rate

0.0%

Known people on board: 3

Operational Details

Schedule / Flight

Baroda - Baroda

Flight Type

Training

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

Asia • India

Aircraft Details

Registration

VT-EWE

MSN

10605

Year of Manufacture

1980