Crash of a Piper PA-31-310 Navajo in Ithaca: 2 killed

Date & Time: Jan 5, 1982 at 0749 LT
Type of aircraft:
Operator:
Registration:
N546BA
Survivors:
No
Schedule:
Utica – Ithaca – Washington DC
MSN:
31-709
YOM:
1971
Flight number:
EMP141
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3300
Captain / Total hours on type:
728.00
Copilot / Total flying hours:
2200
Copilot / Total hours on type:
380
Aircraft flight hours:
5906
Circumstances:
The airplane crashed while attempting an approach to Tompkins County Airport, Ithaca, New York, an en route stop from schedule flight 141 from Utica to Washington DC. The flight crew had contacted Elmira approach control and had received instructions for an instrument landing system (ILS) approach to runway 32 at Tompkins County Airport. About 07:40 EST, the copilot declared an emergency stating that the airplane had a landing flap problem; he later stated that only one flap was down. He also stated that they were not able to maintain altitude and that the airplane was descending. Elmira approach lost radar contact with the airplane about 07:41 EST; the last radio transmission from the flight was recorded about 07:45 EST. The airplane crashed in a wooded area near three suburban residences. The pilot and copilot, the only persons aboard, were killed. There were no injuries to personnel on the ground. The airplane was destroyed by impact and post impact fire.
Probable cause:
The probable cause of the accident was excessive wear of the left flap motor/flexible drive spline and certification of the airplane with a flap system that did not meet the requirements of Civil Air Regulation 3.339. The worn spline caused a split flap condition of 34 that resulted in marginal flight control authority. Moderate low altitude turbulence and transient low level wind shear may have contributed to the upset and loss of control.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain in Durango: 4 killed

Date & Time: Dec 31, 1981 at 2000 LT
Operator:
Registration:
N41070
Survivors:
Yes
Schedule:
Albuquerque - Durango
MSN:
31-8253005
YOM:
1982
Flight number:
SNW070
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4900
Captain / Total hours on type:
1381.00
Circumstances:
While on a night approach to Durango-La Plata County Airport, the pilot decided to initiate a go-around. For unknown reasons, the twin engine airplane failed to gain sufficient height, struck trees and crashed in a wooded area located few miles from the airport. Two passengers were seriously injured while four other occupants were killed.
Probable cause:
Controlled collision with ground during a missed approach for undetermined reasons. The following contributing factors were reported:
- Low ceiling,
- Fog,
- Snow,
- Visibility one mile or less,
- The pilot failed to execute successfully a missed approach procedure for undetermined reasons.
Final Report:

Ground accident of an Avro 748-2A-239 in Sydney

Date & Time: Dec 29, 1981
Type of aircraft:
Operator:
Registration:
C-GEPH
Flight Phase:
Survivors:
Yes
MSN:
1635
YOM:
1967
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following a normal landing at Sydney Airport, the crew completed the braking procedure then vacated the runway and was taxiing to the apron when control was lost. The airplane collided with the main terminal building and came to rest. All 18 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Loss of control during taxiing after both braking systems and nosewheel steering system failed simultaneously for unknown reasons.

Crash of a De Havilland DHC-6 Twin Otter 300 in San Antero: 13 killed

Date & Time: Dec 18, 1981 at 1306 LT
Operator:
Registration:
HK-2216
Survivors:
No
Site:
Schedule:
Medellín – Coveñas
MSN:
609
YOM:
1979
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
While approaching Coveñas Airport on a flight from Medellín, the twin engine airplane struck a hill and crashed near San Antero, about 7 km southwest of runway 06 threshold. The aircraft was destroyed and all 13 occupants were killed.

Crash of a Pilatus PC-6/B2-H2 Turbo Porter in Guatemala

Date & Time: Dec 11, 1981
Registration:
TG-BOC
MSN:
794
YOM:
1978
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances somewhere in Guatemala. Occupant fate unknown.

Crash of a Fokker F27 Friendship 400 near Kufra

Date & Time: Nov 28, 1981
Type of aircraft:
Operator:
Registration:
5A-DBE
Flight Phase:
Survivors:
Yes
Site:
MSN:
10275
YOM:
1965
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
20196
Aircraft flight cycles:
13716
Circumstances:
While descending to Kufra, both engines failed. The crew completed an emergency belly landing in a sandy area located 56 km from Kufra. There were no casualties while the aircraft was damaged beyond repair. It was reported that the aircraft ran out of fuel.

Crash of a PZL-Mielec AN-2P in Ust-Kulom: 15 killed

Date & Time: Nov 26, 1981 at 1013 LT
Type of aircraft:
Operator:
Registration:
CCCP-01808
Flight Phase:
Survivors:
No
Schedule:
Ust-Kulom-Syktyvkar
MSN:
1G107-55
YOM:
1969
Flight number:
SU210I
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
15
Aircraft flight hours:
11704
Aircraft flight cycles:
16670
Circumstances:
Few minutes after takeoff from Ust-Kulom Airport, en route to Syktyvkar, the single engine airplane collided with an Aeroflot PZL-Mielec AN-2TP registered CCCP-40564 that was inbound to Ust-Kulom on a flight from Syktyvkar. While the second airplane was able to land without further incident, the first airplane entered a dive and crashed in a field located 12 km from the airport. All 15 occupants were killed. At the time of the accident, the visibility was limited due to low clouds.
Probable cause:
It was determined that the collision was the consequence of the following:
- The crew of AN-2 CCCP-01808 failed to follow the departure route and altitude, departure procedures,
- Limited visibility due to low clouds,
- Lack of ATC assistance who failed to transmit suitable information to both crews,
- Late detection of the climbing aircraft by the inbound crew.

Crash of a Pilatus PC-6 Turbo Porter in Biratnagar: 10 killed

Date & Time: Nov 19, 1981 at 1200 LT
Operator:
Registration:
9N-ABJ
Flight Phase:
Survivors:
No
Schedule:
Biratnagar - Kathmandu
MSN:
746
YOM:
1975
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
After takeoff from Biratnagar Airport, while in initial climb, the single engine airplane lost height and crashed. All 10 occupants were killed.

Crash of a Tupolev TU-154B-2 in Norilsk: 99 killed

Date & Time: Nov 16, 1981 at 1737 LT
Type of aircraft:
Operator:
Registration:
CCCP-85480
Survivors:
Yes
Schedule:
Krasnoyarsk - Norilsk
MSN:
81A480
YOM:
1981
Flight number:
SU3603
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
160
Pax fatalities:
Other fatalities:
Total fatalities:
99
Aircraft flight hours:
1889
Aircraft flight cycles:
697
Circumstances:
Following an uneventful flight from Krasnoyarsk, the crew started the descent to Norilsk-Alykel Airport. At an altitude of about 600 meters and a speed of 370 km/h, the undercarriage were lowered. At a distance of 19 km from the airport, at an altitude of 500 meters and a speed of 300 km/h, flaps were deployed to an angle of 28°. At this time, the crew calculated the landing speed at 265 km/h according to flight conditions and the total weight of the aircraft. Unfortunately, this calculation was wrong and the correct speed should be 270 km/h. On short final, the airplane descended below the glide and struck the ground at a speed of 261 km/h about 470 meters short of runway threshold. It slid for about 300 meters on an icy ground before coming to rest, bursting into flames. 68 occupants were injured while 99 others were killed, among them four crew members. The aircraft was destroyed.
Probable cause:
The accident resulted from a loss of longitudinal controllability on short final due to the combination of the following factors:
- A significant reduction in the efficiency of the stabilizers after they were positioned beyond an angle of -20 °,
- An automatic reduction of power on all three engine close to idle,
- An aircraft with a forward center of gravity,
- An insufficient approach speed,
- An excessive rate of descent,
- The late recognition by the crew of an emergency situation,
- The failure of the crew to initiate a go-around procedure.