Crash of a Fokker F28 Fellowship 3000 in Bandar Lampung: 3 killed

Date & Time: Jun 2, 1983 at 0850 LT
Type of aircraft:
Operator:
Registration:
PK-GFV
Flight Phase:
Survivors:
Yes
Schedule:
Bandar Lampung - Jakarta
MSN:
11132
YOM:
1978
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
57
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
9334
Aircraft flight cycles:
9227
Circumstances:
At liftoff from Bandar Lampung-Branti Airport runway 14, the captain realized that one of the engine failed. He abandoned the takeoff procedure and landed back onto runway. Unable to stop within the remaining distance, the airplane overran, struck a concrete wall and crashed on a small hill located 138 meters past the runway end. Both pilot and a passenger were killed while 12 occupants were injured and 46 others escaped uninjured. The aircraft was destroyed.
Probable cause:
It was determined that none of the engine failed at takeoff. Following a poor flight preparation, the crew failed to follow the pre-takeoff checklist and adopted a wrong takeoff configuration.

Crash of a Britten-Norman BN-2A Islander at Schleswig AFB

Date & Time: May 18, 1983
Type of aircraft:
Operator:
Registration:
D-IOLT
Survivors:
Yes
MSN:
21
YOM:
1968
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Suffered an accident at Schleswig AFB. There were no casualties.

Crash of a PZL-Mielec AN-2R in Blagodarnoye

Date & Time: May 11, 1983
Type of aircraft:
Operator:
Registration:
CCCP-70057
Flight Phase:
Survivors:
Yes
MSN:
1G135-24
YOM:
1972
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
En route, the single engine airplane suffered a bird strike. The bird got stuck in the engine air intake, forcing the crew to attempt an emergency landing. The aircraft crash landed in a field and was damaged beyond repair. There were no casualties.
Probable cause:
In-flight collision with bird.

Crash of a PZL-Mielec AN-2TP in Tavildara

Date & Time: May 9, 1983
Type of aircraft:
Operator:
Registration:
CCCP-02515
Flight Phase:
Survivors:
Yes
MSN:
1G119-58
YOM:
1970
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was forced to make an emergency landing after the engine failed in flight. There were no casualties.
Probable cause:
Engine failure for unknown reasons.

Crash of a PZL-Mielec AN-2R near Kaunas

Date & Time: May 4, 1983
Type of aircraft:
Operator:
Registration:
CCCP-35637
Flight Phase:
Schedule:
MSN:
1G116-28
YOM:
1970
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crash landed in a field near Kaunas following an in-flight fire in the cockpit for unknown reasons.

Crash of a PZL-Mielec AN-2P near Bidzhan: 8 killed

Date & Time: May 2, 1983 at 1443 LT
Type of aircraft:
Operator:
Registration:
CCCP-07741
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Amurzet – Birobidzhan – Khabarovsk
MSN:
1G159-16
YOM:
1974
Flight number:
SU274
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
8
Aircraft flight hours:
8866
Circumstances:
The aircraft departed Amurzet at 1414LT on a flight to Khabarovsk with an intermediate stop in Birobidzhan, carrying 11 passengers and a crew of two. Weather conditions were considered as marginal with a visibility reduced to 5 km due to rain showers. The crew decided to take off despite the VHF radio communication system was unserviceable. About half an hour into the flight, while cruising at an altitude of 400 meters, weather conditions deteriorated with limited visibility due to mixed rain and snow. The aircraft struck trees and crashed in a wooded area located 15 km north of Bidzhan, bursting into flames. The copilot and four passengers were critically injured while eight other occupants were killed.
Probable cause:
The accident was the consequence of the followings:
- The crew decided to take off while the visibility was below minimums,
- The crew decided to take off while the VHF radio communication was unserviceable,
- The crew failed to inform ATC about the deterioration of the weather conditions,
- When weather conditions deteriorated, the crew failed to return and continued the flight into such conditions,
- The crew modified its route without ATC clearance.

Crash of an Antonov AN-2 in Tsaghkahovit

Date & Time: Apr 29, 1983
Type of aircraft:
Operator:
Registration:
CCCP-33093
MSN:
1140 473 11
YOM:
1960
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach, the single engine airplane lost height and crashed in a field, bursting into flames. Occupant fate unknown.

Crash of a Britten-Norman BN-2A-21 Islander in Landikma

Date & Time: Apr 29, 1983
Type of aircraft:
Operator:
Registration:
PK-OBE
Flight Phase:
Survivors:
Yes
MSN:
429
YOM:
1975
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, one of the engine failed. The pilot abandoned the takeoff procedure and initiated an emergency braking maneuver. Unable to stop within the remaining distance, the aircraft overran and came to rest. The pilot, sole on board, was uninjured while the aircraft was damaged beyond repair.
Probable cause:
Engine failure during takeoff for unknown reasons.

Crash of a Sud-Aviation SE-210 Caravelle VI-R in Guayaquil: 8 killed

Date & Time: Apr 29, 1983
Operator:
Registration:
HC-BAT
Survivors:
Yes
Schedule:
Guayaquil - Quito
MSN:
125
YOM:
1962
Flight number:
WB832
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
94
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
After takeoff from Guayaquil-Simon Bolivar Airport runway 21, while in initial climb, the left engine failed. The pilot informed ATC about the situation and was cleared to return for an emergency landing. On final approach, the right engine lost power and the airplane lost height and crashed in a swampy area short of runway threshold. A crew member and seven passengers were killed while 20 other occupants were injured. 72 other occupants escaped uninjured. The aircraft was destroyed.
Probable cause:
The exact cause of the engine failure could not be determined. However, the day prior to the accident, the captain proceeded to a test flight following an engine overhaul and noted that the power was insufficient and that the engine failed to respond properly. Engines were rechecked by ground personnel and it was noted in the log book there was no anomalies.

Crash of a De Havilland DHC-6 Twin Otter 310 in Flotta

Date & Time: Apr 20, 1983 at 1300 LT
Operator:
Registration:
G-STUD
Survivors:
Yes
Schedule:
Aberdeen - Flotta
MSN:
545
YOM:
1977
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9010
Captain / Total hours on type:
1503.00
Copilot / Total flying hours:
184
Copilot / Total hours on type:
100
Aircraft flight hours:
7000
Circumstances:
Strong winds were reported at Flotta as the Twin Otter approached Orkney Island. The aircraft first contacted the airport at 11:56, and was informed that the surface wind was indicating 260°/26 knots. The pilot accordingly elected to make a straight in approach to runway 35. The pilot preferred the cross-wind to come from his left-hand side, so that he could 'see' the left main wheel onto the runway. The aircraft touched down left main wheel first, then on the right main wheel and, as the nosewheel touched, the commander selected reverse thrust from the propellers. As the aircraft touched down, the audible stall warning sounded momentarily. Shortly after reverse thrust from the propellers had been selected and achieved, the aircraft’s left wing started to rise. The captain applied full left wing down aileron and full left rudder, then cancelling reverse thrust from the right-hand propeller and increasing forward power on that engine. However, he was still unable to prevent the left wing from rising further. The right-hand wing-tip contacted the ground, the aircraft yawed to the right and then fell back momentarily onto the main wheels before ‘cartwheeling’ through an aerodrome boundary fence and coming to rest on its left side, with both wings detached. All 12 occupants escaped uninjured while the airplane was damaged beyond repair.
Probable cause:
The accident was caused by a loss of control, shortly after touchdown, following a strong lateral gust which was in excess of the maximum cross-wind capability of the aircraft. The lack of accurate surface wind information at the runway threshold was a contributory factor.
Final Report: