Zone

Crash of a Fokker F27 Friendship 500RF in Baroda

Date & Time: Jul 1, 1995 at 0840 LT
Type of aircraft:
Operator:
Registration:
VT-EWE
Flight Type:
Survivors:
Yes
Schedule:
Baroda - Baroda
MSN:
10605
YOM:
1980
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9360
Circumstances:
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.
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.
Final Report:

Crash of a Douglas DC-3C in Jaisalmer

Date & Time: Apr 13, 1987 at 0850 LT
Type of aircraft:
Operator:
Registration:
VT-DFM
Flight Phase:
Survivors:
Yes
Schedule:
Jaisalmer – Baroda
MSN:
20269
YOM:
1944
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12500
Circumstances:
The aircraft was engaged in a charter flight on behalf of the Oil & Natural Gas Corporation. During the takeoff roll from Jaisalmer Airfield, the commander experienced yaw to the left which could not be corrected by him. When the aircraft was about to leave the paved surface, the commander prematurely attempted liftoff. The aircraft momentarily became airborne and unable to sustain flight due to low flying speed impacted the kutcha side strip on the left side of the runway. The aircraft got destroyed due to impact force and post impact fire. During the process of evacuation 19 passengers and four crew members received minor injuries.
Probable cause:
The cause of the accident has been attributed to commander attempting takeoff after experiencing uncommanded and uncontrollable yaw to the left during takeoff roll and executed premature liftoff to avoid aircraft rolling onto kutcha surface resulting in the aircraft to crash onto the ground. Loss of directional control was probably due to deflection of left wheel which was a contributory factor to the accident.
Final Report:

Crash of a Douglas DC-3C in Jaisalmer

Date & Time: Apr 13, 1987 at 0850 LT
Type of aircraft:
Operator:
Registration:
VT-DFM
Flight Phase:
Survivors:
Yes
Schedule:
Jaisalmer – Baroda
MSN:
20269
YOM:
1944
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12500
Circumstances:
During the takeoff roll from Jaisalmer Airfield, the commander experienced yaw to the left which could not be corrected by him. When the aircraft was about to leave the paved surface, the commander prematurely attempted liftoff. The aircraft momentarily became airborne and unable to sustain flight due to low flying speed impacted the kutcha side strip on the left side of the runway. The aircraft got destroyed due to impact force and post impact fire. During the process of evacuation 19 passengers and four crew members received minor injuries.
Probable cause:
The cause of the accident has been attributed to commander attempting takeoff after experiencing uncommanded and uncontrollable yaw to the left during takeoff roll and executed premature liftoff to avoid aircraft rolling onto kutcha surface resulting in the aircraft to crash onto the ground. Loss of directional control was probably due to deflection of left wheel which was a contributory factor to the accident.
Final Report:

Crash of a Douglas C-47B-35-DK Dakota IV in Vadodara

Date & Time: Jan 24, 1946
Operator:
Registration:
KN659
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
16610/33358
YOM:
1945
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Enroute, an engine failed and the crew was forced to feather its propeller. Few minutes later, the second engine failed due to a fuel exhaustion. The crew decided to make an emergency landing. The aircraft belly landed in a field near Vadodara and was written off. There were no casualties.
Probable cause:
Double engine failure caused by a fuel exhaustion.