Country
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National Capital Territory of Delhi

Crash of a Beechcraft 200 Super King Air in New Delhi: 10 killed

Date & Time: Dec 22, 2015 at 0938 LT
Operator:
Registration:
VT-BSA
Flight Phase:
Survivors:
No
Site:
Schedule:
New Delhi - Ranchi
MSN:
BB-1485
YOM:
1994
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
964
Captain / Total hours on type:
764.00
Copilot / Total flying hours:
891
Copilot / Total hours on type:
691
Aircraft flight hours:
4766
Aircraft flight cycles:
2745
Circumstances:
Beechcraft Super King Air B-200 aircraft, VT-BSA belonging to BSF Air Wing was involved in an accident on 22.12.2015 while operating a flight from IGI Airport, New Delhi to Ranchi. The flight was under the command of a CPL holder with another CPL holder as Second-in-Command. There were ten persons on board including two flight crew members. As per the scheduling procedure of the Operator, the flying programme for 22.12.2015 was approved by the ADG (Logistics) on the recommendation of the DIG (Air) for VT-BSA on 21.12.2015. The programme included names of the flight crew along with the following sectors: from Delhi to Ranchi ETD 0800 ETA 1030 and from Ranchi to Delhi ETD 1300 ETA 1600. The task was as per instructions on the subject dated 23rd July 2015. As per the weight & load data sheet there were 8 passengers with 20 Kgs. of baggage in the aft cabin compartment. The actual take-off weight shown was 5668.85 Kgs as against the maximum take-off weight of 5669.9 Kgs. Fuel uplifted was 1085 Kgs. The aircraft was taken out of hangar of the Operator at 0655 hrs on 22.12.2015 and parked outside the hangar for operating the subject flight. At around 0745 hrs, the passengers reached the aircraft who were mainly technical personnel supposed to carry out scheduled maintenance of Mi-17 helicopter of the Operator at Ranchi. They were carrying their personnel baggage along with tools and equipment required for the maintenance. At around 0915 hrs the flight crew contacted ATC Delhi and requested for clearance to operate the flight to Ranchi. The aircraft was cleared to Ranchi via R460 and FL210. Runway in use was given as 28. At 0918 hrs the doors were closed and the flight crew had started carrying out the check list. After the ATC issued taxi clearance, the aircraft had stopped for some time after commencing taxiing. The pilot informed the ATC that they will take 10 minutes delay for further taxi due to some administrative reasons. The taxi clearance was accordingly cancelled. After a halt of about 6 to 7 minutes, the pilot again requested the ATC for taxi clearance and the same was approved by the ATC. Thereafter, the aircraft was given take-off clearance from runway 28. The weather at the time of take-off was: Visibility 800 meters with Winds at 100°/03 knots. Shortly after take-off and attaining a height of approximately 400 feet AGL, the aircraft progressively turned left with simultaneous loss of height. It had taken a turn of approximately 180o and impacted some trees before hitting the outside perimeter road of the airport in a left bank attitude. Thereafter, it impacted 'head on' with the outside boundary wall of the airport. After breaking the outside boundary wall, the wings impacted two trees and the aircraft hit the holding tank of the water treatment plant. The tail portion and part of the fuselage overturned and went into the water tank. There was post impact fire and the portion of the aircraft outside the water tank was destroyed by fire. All passengers and crew received fatal injuries due impact and fire. The ELT was operated at 0410 hours UTC (0940 hours IST). The fire fighting team reached the site and extinguished the fire. The bodies were then recovered from the accident site. 08 bodies were recovered from the holding tank of the water treatment plant and bodies of both pilots were recovered from the heavily burnt portion of the cockpit lying adjacent (outside) to the wall of the holding tank of the water treatment tank.
Probable cause:
The accident was caused due to engagement of the autopilot without selecting the heading mode by the flight crew just after liftoff (before attaining sufficient height) in poor foggy conditions and not taking corrective action to control the progressive increase in left bank; thereby, allowing the aircraft to traverse 180° turn causing the aircraft to lose height in a steep left bank attitude followed by impact with the terrain.
Final Report:

Crash of a Raytheon 390 Premier IA in New Delhi

Date & Time: Sep 22, 2012 at 1129 LT
Type of aircraft:
Operator:
Registration:
VT-UPN
Flight Type:
Survivors:
Yes
Schedule:
Lucknow - New Delhi
MSN:
RB-236
YOM:
2008
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft departed Lucknow Airport in the morning on a flight to New Delhi-Indira Gandhi Airport with a crew of three (two pilot and a cabin crew) and three passengers, among them Shivpal Yadav, Minister by the Uttar Pradesh Government. Following an uneventful flight, the crew completed the approach to runway 27. After touch down, the left main gear collapsed and the aircraft slid on runway for about one km when the right main gear collapsed as well. Out of control, the aircraft veered off runway to the right and came to rest in a grassy area. All six occupants escaped uninjured while the aircraft was damaged beyond repair.

Ground accident of an Airbus A300B2-101 in New Delhi

Date & Time: Mar 8, 2002 at 0315 LT
Type of aircraft:
Operator:
Registration:
VT-EFW
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
111
YOM:
1980
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
A group of five technicians/engineers of the company was preparing the aircraft to be transferred to a hangar for maintenance. After engine startup, the power was reduced to idle after someone inadvertently pulled out the circuit breaker. The aircraft jumped the chocks and started to roll. Since the engine's power was in idle, the brakes and the nosewheel steering system were inoperative. The crew elected to reduce power on the left engine but mistakenly increased the power on the right engine by 90%. This caused the aircraft to rotate 80° when control was lost. The airplane rolled through a perimeter wall, causing the nose gear to collapse. All five occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of an Antonov AN-32 in New Delhi: 21 killed

Date & Time: Mar 7, 1999 at 0822 LT
Type of aircraft:
Operator:
Registration:
K2673
Flight Type:
Survivors:
No
Site:
Schedule:
Gwalior – New Delhi – Pokhran
MSN:
108
YOM:
1984
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
21
Circumstances:
While descending to New Delhi-Indira Gandhi Airport runway 10, the crew encountered poor visibility due to thick fog and requested ATC assistance. On short final, the crew failed to realize his altitude was insufficient when the aircraft struck successively a concrete water tank and power cables then crashed in the Pappankalan district, about 2,4 km short of runway. The aircraft and a building were destroyed. All 18 occupants were killed as well as three people on the ground.
Probable cause:
The crew was completing the final approach below the minimum safe altitude in reduced visibility due to thick fog.

Crash of a Boeing 737-2A8 in New Delhi

Date & Time: Dec 2, 1995 at 1253 LT
Type of aircraft:
Operator:
Registration:
VT-ECS
Survivors:
Yes
Schedule:
Bombay – Jaipur – New Delhi
MSN:
20963
YOM:
1974
Flight number:
IC492
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
102
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6088
Circumstances:
Following a wrong approach configuration, the aircraft landed too far down the runway, about 600 metres from the runway end. Unable to stop within the remaining distance, the aircraft overran, struck a concrete wall (45 cm high) and came to rest 450 metres further. All 108 occupants were evacuated safely and the aircraft was damaged beyond repair.
Probable cause:
The accident was the consequence of the combination of the following factors:
- The injudicious and imprudent decision of the Pilot-in-Command to hastily complete the flight in the inadequate time available before the notified closure of Delhi airport for a VVIP flight,
- The dangerously unstabilised approach made by the Pilot-in-Command, primarily due to his failure to decelerate the aircraft in time,
- The failure of the First Officer to call out significant deviations from the stipulated approach parameters,
- The failure of the Pilot-in-Command to carry out a missed approach in spite of his approach being grossly unstabilised,
- The inadvertent omission of the Pilot-in-Command to arm the speed brake before landing,
- Touch-down of the aircraft at excessive speed and too far down the runway,
- Failure of the First Officer and Pilot-in-Command to monitor the automatic deployment of the speed brake, and failure of the Pilot-in-Command to deploy it manually,
- Impact of the aircraft with an 18-inch high cement-concrete cable duct in the kutcha ground beyond the over-run area,
- The pilot disregard of procedures, regulations and instructions.
Final Report:

Crash of a Boeing 737-2R4C in New Delhi: 5 killed

Date & Time: Mar 8, 1994 at 1454 LT
Type of aircraft:
Operator:
Registration:
VT-SIA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
New Delhi - New Delhi
MSN:
21763
YOM:
1979
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
7263
Captain / Total hours on type:
2821.00
Copilot / Total flying hours:
556
Copilot / Total hours on type:
166
Aircraft flight hours:
25947
Aircraft flight cycles:
2861
Circumstances:
The aircraft was engaged in a local training flight at New Delhi-Indira Gandhi Airport, carrying one instructor and three trainee pilots. Five circuits and landings were completed uneventfully and during the sixth touch-and-go exercice, after take off from runway 28, the aircraft took a left turn and crashed on the international apron. The aircraft collided with an Aeroflot Ilyushin II-86 registered RA-86119 that was parked on the apron, bay n°45. Both aircraft were destroyed by fire. All four crew members on board the Boeing 737 were killed as well as four people on board the II-86 and one on the ground.
Probable cause:
Loss of control after rotation due to application of wrong rudder by trainee pilot during engine failure exercice. The instructor did not guard/block the rudder control and give clear commands as instructor so as to obviate the application of wrong rudder control by the trainee pilot.
Final Report:

Crash of an Ilyushin II-86 in New Delhi: 4 killed

Date & Time: Mar 8, 1994 at 1200 LT
Type of aircraft:
Operator:
Registration:
RA-86119
Flight Phase:
Survivors:
Yes
Schedule:
New Delhi - Tashkent - Moscow
MSN:
51483209087
YOM:
1985
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
An Air Sahara (Sahara Airlines) boeing 737-2R4C registered VT-SIA was engaged in a local training flight at New Delhi-Indira Gandhi Airport, carrying one instructor and three trainee pilots. Five circuits and landings were completed uneventfully and during the sixth touch-and-go exercice, after take off from runway 28, the aircraft took a left turn and crashed on the international apron. The aircraft collided with an Aeroflot Ilyushin II-86 registered RA-86119 that was parked on the apron, bay n°45. Both aircraft were destroyed by fire. All four crew members on board the Boeing 737 were killed as well as four people on board the II-86 and one on the ground.
Probable cause:
Loss of control after rotation due to application of wrong rudder by trainee pilot during engine failure exercice. The instructor did not guard/block the rudder control and give clear commands as instructor so as to obviate the application of wrong rudder control by the trainee pilot.

Crash of a Tupolev TU-154B-2 in New Delhi

Date & Time: Jan 9, 1993 at 0408 LT
Type of aircraft:
Operator:
Registration:
85533
Survivors:
Yes
Schedule:
Hyderabad - New Delhi
MSN:
82A533
YOM:
1982
Flight number:
IC840
Country:
Region:
Crew on board:
13
Crew fatalities:
Pax on board:
152
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10245
Circumstances:
On 9th January, 1993 TU-154 aircraft No. 85533 wet leased by Indian Airlines from Uzbekistan Airways was operating flight IC-840 from Hyderabad to Delhi. The aircraft was being flown by Uzbeki operating crew and there were 165 persons on board including the crew. The aircraft touched down slightly outside the right edge of the runway, collided with some fixed installations on the ground, got airborne once again and finally touched down on kutcha ground on the right side of the runway. At this stage the right wing and the tail of the aircraft broke away and it came to rest in an inverted position. During the process, the aircraft caught fire and was destroyed. Most occupants of the aircraft escaped unhurt. Six persons suffered either limb fracture or other serious injuries while 45 persons suffered injuries of a minor nature.
Probable cause:
The probable cause of accident has been attributed to :
- The failure of the Pilot-in-Command to divert to Ahmedabad when he was informed that the RVR on runway 28 was below the minima applicable to his flight.
- The switching on of landing lights, on the instruction of the second Captain, at a height of only about ten metres, resulting in the loss of all visual references due to the blinding effect of
light reflections from fog.
- The failure of captain to carry out a missed approach when visual reference to the runway was lost.
Final Report:

Crash of a Beechcraft B200C Super King Air in New Delhi: 1 killed

Date & Time: Aug 27, 1992 at 1159 LT
Registration:
VT-EOA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
New Delhi - New Delhi
MSN:
BL-129
YOM:
1987
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
13519
Captain / Total hours on type:
1099.00
Aircraft flight hours:
1347
Circumstances:
Border Security Force (BSF) Beechcraft B200 Super King Air VT-EOA was engaged in a local flying (circuits and landings) at IGI Airport, Delhi on 27.8.92. There were two persons on board the aircraft including the commander. After two circuits and landings, the commander asked for full stop landing. However, after landing the commander asked the ATC about one more circuit to which the controller gave the consent and asked him to line up on runway 28 for take off. At this stage, the copilot on board was disembarked. The aircraft took-off without ATC clearance and turned left for circuit. Thereafter, it was seen going down in a nose down attitude and impacted the ground. The aircraft impacted the ground, caught fire and was destroyed. The pilot, who was the sole occupant on board, received fatal injuries.
Probable cause:
The exact cause of the accident could be confirmed. However, on the basis of evidence on record, the probability of deliberate attempt to crash the aircraft by late Captain Dhaliwal could not be ruled out. The probability of incapacitation of Captain Dhaliwal during the last circuit has also not been ruled out.
Final Report:

Crash of a Boeing 747-237B in New Delhi

Date & Time: May 7, 1990 at 0917 LT
Type of aircraft:
Operator:
Registration:
VT-EBO
Survivors:
Yes
Schedule:
London - New Delhi - Bombay
MSN:
20558
YOM:
1972
Flight number:
AI132
Country:
Region:
Crew on board:
20
Crew fatalities:
Pax on board:
195
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8026
Circumstances:
After touchdown at New Delhi-Indira Gandhi Airport following an uneventful flight from London-Heathrow Airport, the crew started the braking procedure and activated the thrust reversers when the pylon of the engine n°1 failed. The engine partially detached, causing a fuel line to rupture and the fuel to ignite. The aircraft was stopped after a course of almost 3 km and all 215 occupants were evacuated safely. The fire was extinguished but the aircraft was damaged beyond repair.
Probable cause:
The accident was caused due to the migration of the improperly installed diagonal-brace aft fuse-pin of the No.1 engine from its fitting which substantially reduced the load carrying capability of the engine fittings resulting in failure of the upper-link forward fuse pin due to excessive loads on account of probably improper landing leading to a partial separation of engine and fire.