Crash of a Britten-Norman BN-2A-8 Islander in Ajaccio

Date & Time: Jun 23, 1984
Type of aircraft:
Registration:
F-BVTD
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ajaccio - Ajaccio
MSN:
710
YOM:
1974
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Ajaccio-Campo dell’Oro Airport, simulating engine failure. In unclear circumstances, the pilot lost control of the aircraft that crashed near the airport. Both occupants were injured and the aircraft was destroyed.

Crash of a BAe Nimrod MR2 in Newquay-Saint Mawgan

Date & Time: Jun 3, 1984 at 1107 LT
Type of aircraft:
Operator:
Registration:
XV257
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Newquay-Saint Mawgan - Newquay-Saint Mawgan
MSN:
8032
YOM:
1970
Flight number:
Sarex 51
Region:
Crew on board:
13
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The Nimrod aircraft took off on an exercise Search and Rescue (SAR) sortie from its base at RAF St Mawgan. It was carrying in the bomb bay, as part of the SAR equipment, a normal load of 5 inch reconnaissance flares. In accordance with normal practice, the first navigator switched the flare's release units to live shortly after takeoff. Some 30 seconds later a cockpit indicator warned the crew of a fire in the bomb bay. The captain immediately instructed the co-pilot to fly the aircraft back to base while he transmitted a MAYDAY call and informed the rest of the crew. During the return flight ground witnesses saw the Nimrod trailing smoke, with several burning flares, a parachute and other objects falling from the aircraft. The aircraft landed safely. Although the fire services quickly extinguished the intense fire, the aircraft was extensively damaged.
Probable cause:
The accident was caused by a reconnaissance flare becoming detached from its carrier and subsequently igniting in the bomb bay . How it came to be released could not be positively determined.

Crash of a Cessna 414A Chancellor II in Bournemouth

Date & Time: May 15, 1984 at 1427 LT
Type of aircraft:
Operator:
Registration:
G-OFRL
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Bournemouth - Bournemouth
MSN:
414A-0220
YOM:
1979
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14800
Captain / Total hours on type:
1600.00
Circumstances:
After the second overshoot, the aircraft entered the circuit, and was cleared for a touch-and-go landing on Runway 17. The final approach was described as 'steep' and was flown with full (45°) flap. After a short ground run, the pilot under training opened the throttles, and. at about 80 knots, rotated the aircraft with the flaps still at the full (45 degree) setting. Shortly after becoming airborne, there was a loss of power, accompanied by vibration or buffeting; the aircraft yawed and rolled to the right, and the airspeed started to decay. The pilot under training then retracted the flaps to 30°, and, at this point, the instructor took control, closed the throttles, and landed the aircraft on the grass on a heading of about 200° magnetic. The aircraft than ran across the south western taxiway, through the airfield perimeter fence, across a public road, at which point the undercarriage collapsed, before finally coming to rest in an adjacent field. Both fuel tanks were ruptured by the impact with the fence posts, but there was no fire. The crew, who were uninjured, shut off the fuel cocks, switched off the electrics, and vacated the aircraft through the main entry door. The emergency services responded to this incident very quickly, and had arrived at the crash scene by the time the crew vacated the aircraft.
Probable cause:
A safe climb out could not be achieved following the complete loss of power from one engine just when the aircraft became airborne at a speed of about 80 knots with full flap extended. The commander was therefore left with no alternative but to land whilst it was still possible to control the aircraft.
Final Report:

Crash of a Canadair CL-215-1A10 at Elefsis AFB: 3 killed

Date & Time: Mar 10, 1984
Type of aircraft:
Operator:
Registration:
1015
Flight Type:
Survivors:
No
Schedule:
Elefsis - Elefsis
MSN:
1015
YOM:
1969
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew departed Elefsis AFB on a local training flight. While in a circuit, one of the engine failed and the crew feathered its propeller and decided to return when the aircraft lost height and crashed near the airfield. All three occupants were killed.

Crash of a Hindustan Aeronautics HAL-748-224-2 in Hyderabad

Date & Time: Mar 5, 1984 at 2046 LT
Operator:
Registration:
VT-DUO
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Hyderabad - Hyderabad
MSN:
506
YOM:
1966
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5585
Circumstances:
The aircraft swung to the right when the instructor simulated a no. 2 engine failure after touchdown during a training flight. The trainee and instructor were not able to regain directional control. The trainee then tried to rotate the aircraft although no VR speed call had been made. The airplane did not become airborne and the instructor took over control. He tried to add power on the no. 2 engine, but the propeller auto-feathered. The aircraft ran off the runway and crashed into an airport boundary wall.
Probable cause:
The instructor adopted wrong procedure for simulating starboard engine failure during reject take-off exercise. The trainee-pilot could not recognise the emergency. He handled the situation incorrectly and rotated the aircraft prematurely disregarding decision speed. The instructor took over the controls without proper call out and he also continued for take-off with one engine inoperative on undulated soft ground disregarding decision speed and the circumstances.

Crash of a Swearingen SA226TC Metro II in Terre Haute: 3 killed

Date & Time: Jan 30, 1984 at 0630 LT
Type of aircraft:
Operator:
Registration:
N63Z
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Terre Haute - Evansville
MSN:
TC-240
YOM:
1977
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
19189
Captain / Total hours on type:
1501.00
Aircraft flight hours:
10607
Circumstances:
After taking off from runway 23, the aircraft crashed ssw of the airport about 6,300 feet from the departure end of the runway and about 1,800 feet to the left of the runway centerline. Impact occurred while the aircraft was in a steep descent. The wreckage path was scattered along a heading of 035° from the initial impact point. The aircraft was demolished by impact and fire and no preimpact part failure or malfunction was found that would have caused the accident. All three occupants were killed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: takeoff
Findings
1. (c) reason for occurrence undetermined
2. Light condition - dawn
3. Weather condition - rain
4. Weather condition - fog
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: takeoff
Final Report:

Crash of a De Havilland C-7A Caribou in Kwajalein

Date & Time: Jan 18, 1984
Type of aircraft:
Operator:
Registration:
66-255
Flight Type:
Survivors:
Yes
Schedule:
Kwajalein - Kwajalein
MSN:
255
YOM:
1967
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training mission at Kwajalein Island Airport. Upon touchdown, one of the undercarriage collapsed. The aircraft came to rest on the runway and was damaged beyond repair. There were no casualties.

Crash of an Antonov AN-12 in Senkovo: 9 killed

Date & Time: Nov 21, 1983
Type of aircraft:
Operator:
Registration:
39
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Smolensk - Smolensk
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The crew was completing a local training flight at Smolensk-Severny Airbase. En route, the four engine airplane went out of control and crashed in a silage pit located 500 meters south of the village of Senkovo, about 53 km north of Smolensk AFB. The aircraft was destroyed and all nine crew members were killed.
Probable cause:
It was determined that the loss of control occurred in severe icing conditions.

Crash of a Morane-Saulnier M.S.760A Paris IA in Alto Pencoso: 2 killed

Date & Time: Nov 4, 1983
Operator:
Registration:
E-237
Flight Phase:
Flight Type:
Survivors:
No
MSN:
25
YOM:
1959
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Crashed in unknown circumstances, killing both pilots.

Crash of a Beechcraft U-8F Seminole in Hiram: 3 killed

Date & Time: Oct 19, 1983 at 1300 LT
Type of aircraft:
Operator:
Registration:
62-3839
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Dobbins - Dobbins
MSN:
LF-37
YOM:
1962
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
6000
Copilot / Total flying hours:
5200
Circumstances:
The twin engine airplane departed Dobbins AFB on a local training flight, carrying two pilots and one instructor. While flying at an altitude between 1,900 and 2,100 feet, the crew reduced the speed, lower the gears and the flaps then initiated a 180 turn when control was lost. The aircraft entered a dive and crashed in a wooded area located in Hiram, bursting into flames. All three occupants were killed.
Crew:
Cw2 James Q. Tyner Jr.,
Civ John R. Bailey,
Maj David M. Bishop.