Crash of a Beechcraft B200 Super King Air in Chandigarh

Date & Time: Mar 27, 2014 at 1139 LT
Operator:
Registration:
VT-HRA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Chandigarh – New Delhi
MSN:
BB-1906
YOM:
2005
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9888
Captain / Total hours on type:
2165.00
Copilot / Total flying hours:
2147
Copilot / Total hours on type:
1383
Aircraft flight hours:
2010
Circumstances:
On 25.03.2014, the operator received the travel programme for 27.3.2014, of Hon'ble Governor of Haryana from Chandigarh to Delhi. On 26.3.2014, the operations department took the flight clearances and filed the passenger manifest with the ATC and other concerned agencies. The flight plan was filed by a CPL holder, who is working as flight dispatcher with the Government of Haryana. The departure on 27.3.2014 was fixed at 1130 hrs. The cockpit crew reported at 1045 hrs for the flight. Pre flight medical examination including the breath analyzer test was carried out at 1100 hrs. The breath analyzer test for both the cockpit crew members was negative. Pre flight briefing among the crew members was carried out by using the documents prepared by the flight dispatcher. The aircraft was taxied under its own power from Haryana Government Hangar to bay no. D-2 in front of ATC building. No abnormality was observed or reported on the aircraft during this taxiing. The engines were shut down for passenger embarkation. As per the passenger manifest, in addition to the pilot and co-pilot there were 8 passengers. The baggage on board was approx. 50 lbs. There was 2100 lbs. of fuel on board. After boarding of the passengers, the aircraft engines were started at 1130 hrs. The aircraft was cleared for departure abeam „D‟ link. The aircraft was taxied out via taxiway „D‟. After ATC departure clearance the aircraft was lined up for take-off. On clearance from ATC the take off roll was initiated and all the parameters were found normal. As per the pilot just before getting airborne some stiffness was found in rudder control as is felt in yaw damper engagement. The aircraft then pulled slightly to the left which as per the Commander was controllable. As per the pilot, the rotation was initiated at 98 knots. As per the DATCO the aircraft had lifted up to 10-15 feet AGL. The Commander has stated that after lift-off, immediately the left rudder got locked in forward position resulting in the aircraft yawing and rolling to left. The pilots tried to control it with right bank but the aircraft could not be controlled. Within 3-4 seconds of getting airborne the aircraft impacted the ground in left bank attitude. The initial impact was on pucca (tar road) and the wing has taken the first impact loads with lower surface metallic surface rubbing and screeching on ground. After the aircraft came to final halt, the co-pilot opened the door and evacuation was carried out. There was no injury to any of the occupants. The engine conditions lever could not be brought back as these were stuck. The throttle and pitch levers were retarded. The fuel shut off valves were closed. Battery and avionics were put off. Friction lock nuts were found loose. As per the Commander, after ensuring safety of passengers he had gone to cockpit to confirm that all switches were „off‟. At that time he has loosened the friction lock nuts to bring back the condition lever and throttle lever. However even after loosening the nut it was not possible to bring back these levers. Fire fighting vehicles were activated by pressing crash bell and primary alarm. Hand held RT set was used to announce the crash. RCFF vehicles proceeded to the site via runway and reported all the 10 personnel are safe and out of the disabled aircraft. Water and complementary agents (foam and dry chemical powder) were used. After fire was extinguished, the Fire Fighting vehicles reported back at crash bay except one CFT which was held at crash site under instruction of COO. The aircraft was substantially damaged. There was no fire barring burning of small patch of grass due coming in contact with the hot surfaces and oil. There was no injury to any of the occupants. The accident occurred in day light conditions.
Probable cause:
The accident occurred due to stalling of left wing of the aircraft at a very low height.
The contributory factors were:
- Failure on the part of the crew to effectively put off the yaw damp so as to release the rudder stiffness as per the emergency checklist.
- Checklist not being carried out by the crew members.
- Not putting off the Rudder Boost.
- Speeds call outs not made by co-pilot.
- Not abandoning the take-off at lower speed (before V1).
- Failure of CRM in the cockpit in case of emergency.
- Early rotation and haste to take-off.
Final Report:

Crash of a Douglas C-47A-1-DK in New Delhi: 5 killed

Date & Time: Dec 5, 1970 at 0643 LT
Operator:
Registration:
VT-CZC
Flight Phase:
Survivors:
Yes
Schedule:
New Delhi - Jaipur
MSN:
12103
YOM:
1943
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Shortly after takeoff from New Delhi-Safdarjung Airport, while in initial climb, the right engine failed. The pilot declared an emergency, initiated a turn when the airplane went out of control, stalled and crashed. Three crew members and two passengers were killed. The aircraft was destroyed.
Probable cause:
Failure of the right engine during initial climb due to fuel exhaustion. It was determined that the crew failed to follow the preflight checklist and due to poor flight preparation, the aircraft was not refueled prior to departure.

Crash of a Douglas C-47A-25-DK in New Delhi: 5 killed

Date & Time: Mar 13, 1957 at 0915 LT
Operator:
Registration:
VT-CFB
Flight Type:
Survivors:
No
Site:
Schedule:
New Delhi - New Delhi
MSN:
13626
YOM:
1944
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
VT-CFB took off from Safdarjung Airport at approximately 0832LT on a training flight. At 0839 it reported as being 20 miles north of Safdarjung Airport and at 5 000 ft. There was no further radiotelephony contact with the aircraft. At approximately 0915 hours it crashed 10 miles north of Safdarjung Airport and was destroyed by impact and fire. Both occupants were killed as were three inmates of a hut in the labour colony where the crash occurred.
Probable cause:
The accident was attributed to loss of control of the aircraft as a result of a spin, inadvertently entered into at a height too low for recovery.
Final Report:

Crash of a Douglas C-47A-90-DL in New Delhi: 3 killed

Date & Time: Feb 25, 1954 at 1100 LT
Operator:
Registration:
VT-ATU
Flight Type:
Survivors:
No
Site:
Schedule:
New Delhi - New Delhi
MSN:
20358
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was completing a local test flight out from New Delhi-Safdarjung Airport, a mission that was part of the official investigations from the Indian Civil Aviation Authorities following the crash of a C-47 at Nagpur on 12 December 1953. On approach to Safdarjung Airport, the aircraft went out of control and crashed in the district of Jammu Bridge, near the airfield. While nobody on the ground was injured, all three crew members were killed.

Crash of a De Havilland DH.106 Comet 1 in Calcutta

Date & Time: Jul 25, 1953
Type of aircraft:
Operator:
Registration:
G-ALYR
Flight Phase:
Survivors:
Yes
Schedule:
Calcutta – New Delhi
MSN:
6004
YOM:
28
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
36
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Because taxi lights were too dim to use at night, the crew had to use the landing lights while taxiing. Both lights had to be alternated left and right to avoid a meltdown by using a switch behind the captains seat. In a left hand turn the captain took his left hand off the steering wheel to select another landing light. The steering centered, and then the aircraft right wheel bogies ran off the paved surface. Engine power was applied on the two right engines, causing the bogie struts to be forced up and into the wing structure causing much damage.
Source:
https://aviation-safety.net/database/record.php?id=19530725-0

Crash of a Douglas C-47A-25-DK in New Delhi: 9 killed

Date & Time: Apr 30, 1952
Operator:
Registration:
VT-AUN
Survivors:
No
Schedule:
Madras – New Delhi
MSN:
13405
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
While descending to New Delhi-Safdarjung Airport, the pilot-in-command made a last turn to the left to join the approach path when the left engine failed. The airplane stalled and crashed in a field, killing all nine occupants.
Probable cause:
On account of the inclined attitude of the plane at the critical period during a steep turn of some duration, the port engine very likely became starved of fuel, as it was being fed from the port main tank which unlike the starboard which had more than adequate supply, at the time contained only about 18 gallons of petrol, a quantity inadequate to feed the engine in that position.