Crash of a Cessna 402 in Deer Lake: 6 killed

Date & Time: Mar 24, 1980
Type of aircraft:
Registration:
C-FEIA
Flight Phase:
Survivors:
Yes
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Crashed in unknown circumstances. Three passengers were seriously injured while six other occupants were killed.

Crash of a Piper PA-31-350 Navajo Chieftain in Houston: 7 killed

Date & Time: Mar 21, 1980 at 1949 LT
Registration:
N59932
Flight Phase:
Survivors:
Yes
Schedule:
Houston - Brownwood
MSN:
31-7552046
YOM:
1975
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
4313
Captain / Total hours on type:
813.00
Copilot / Total flying hours:
3250
Aircraft flight hours:
5545
Circumstances:
The flight from William P. Hobby Airport, Houston, Texas, to Brownwood, Texas, was scheduled to depart Hobby Airport at 1915. Two intermediate stops were scheduled. It was operating behind schedule because of delays in the first three flights of the day which were flown by the same captain who was readying Flight 108. The aircraft had been on the ground for 31 minutes between the time it landed and the time it taxied for takeoff. Two crewmembers and eight passengers were on board Flight 108. At 1941, the ground controller cleared Flight 108 to taxi to runway 22. At 1943:40 the captain reported that Flight 108 was ''ready to go on 22," and at 1945:10 transmitted "Eagle Air 108 is No. 1 for 22." At 1945:55, Flight 108 was cleared to taxi into position and to hold on runway 22. A pilot of an aircraft in the runup area adjacent to runway 22 stated that Flight 108 did not use the runup area, nor did he see the crew conduct an engine runup while awaiting takeoff clearance. At 1947:50, Flight 108 was cleared for takeoff, and at 1948:35, the tower air traffic controller inquired if Flight 108 would be making a right turn away from the airport. Flight 108 responded, "Eagle 108 just lost the right engine." The controller stated that when this transmission was made the aircraft was about 4,300 ft from the start of its takeoff roll and about 100 ft above the runway. A pilot witness on the ground stated that the aircraft was between 100 and 200 ft above the runway when the crew reported the loss of the right engine. An Eagle Airlines employee identified the person who made the transmission as a company employee--a pilot-in-command trainee who was in the copilot seat. The aircraft maintained runway heading for about 10 sec more before it began a right turn and a shallow descent. The rate of turn, the angle of bank to the right, and the rate of descent continued to increase as the aircraft turned 90° away from the runway heading. The angle of bank also increased as the aircraft descended, but the crew managed to level the wings just before impact. A passenger who was seated two seats behind the captain stated that when the aircraft was about 50 ft in the air he heard an engine "sputter" which continued until impact. The aircraft dropped, veered left, then right, and down." He recalled that a crewmember said, "What's next or what do we do now." A passenger on the right side, four seats back, heard a "popping or thudding" noise after the aircraft left the runway and veered to the right. He recalled that someone said, 'What do I do?". The third survivor was seated in the left rear seat. He heard an engine go "pop-pop like a backfire." He saw the captain pull back the "left red controls and the right pilot reach and turn things." None of the survivors could tell who was flying the aircraft. The aircraft crashed on a concrete airport parking ramp in a nearly level pitch attitude, with the right wing slightly lowered, about 1,000 ft from the runway. It then slid 200 ft on the ramp and hit two aircraft, four cars, and finally a hangar. A fire broke out when the aircraft hit the cars and the hangar. The accident occurred during hours of darkness.
Probable cause:
The probable cause of the accident was a power loss in the right engine for undetermined reasons at a critical point in the takeoff phase, the aircraft's marginal single-engine performance capability, and the captain's immediate landing on the remaining runway, or to configure the aircraft properly for the engine-out incorrect emergency response to the engine power loss when he failed either to land condition.
Final Report:

Crash of an Antonov AN-24RV in Changsha: 26 killed

Date & Time: Mar 20, 1980
Type of aircraft:
Operator:
Registration:
B-484
Survivors:
No
Schedule:
Kunming – Guiyang – Changsha
MSN:
47309402
YOM:
1974
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
26
Circumstances:
On final approach to Changsha-Datuopu Airport, the airplane crashed in flames in a field. The aircraft was totally destroyed and all 26 occupants were killed. It was reported that the aircraft was not properly aligned at the time of the accident.

Crash of a Douglas DC-9-14 in Baton Rouge

Date & Time: Mar 17, 1980 at 1645 LT
Type of aircraft:
Operator:
Registration:
N9103
Survivors:
Yes
Schedule:
Houston - Baton Rouge
MSN:
45796/74
YOM:
1966
Crew on board:
4
Crew fatalities:
Pax on board:
46
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15732
Captain / Total hours on type:
8720.00
Circumstances:
The airplane landed in rain falls with a 18 knots tailwind about 2,000 feet down runway 13 which is 5,800 feet long. Unable to stop within the remaining distance, the airplane overran and came to rest in a ditch about 350 feet further and 200 feet to the right of the extended centreline. All 50 occupants escaped without injuries while the aircraft was damaged beyond repair. At the time of the accident, the total weight of the airplane was 71,000 lbs.
Probable cause:
Overshoot on landing and subsequent overrun and collision with ditch because ATC cleared the aircraft to wrong runway for existing conditions. The following contributing factors were reported:
- Improper in-flight decisions on part of the pilot-in-command,
- Improper operation of brakes and flight controls on part of the pilot-in-command,
- Rain,
- Wet runway,
- Downwind,
- Haze,
- Aircraft over 25,000 lbs upon landing on runway 13, restricted to zero tailwind/10 knots crosswind when wet,
- Runway 22 available,
- Spoilers not used after touchdown.
Final Report:

Crash of an Ilyushin II-62 in Warsaw: 87 killed

Date & Time: Mar 14, 1980 at 1114 LT
Type of aircraft:
Operator:
Registration:
SP-LAA
Survivors:
No
Schedule:
Montreal - New York - Warsaw
MSN:
11004
YOM:
1971
Flight number:
LO007
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
77
Pax fatalities:
Other fatalities:
Total fatalities:
87
Circumstances:
The four engine airplane was completing flight LO007 from Montreal to Warsaw via New York-JFK. On final approach to Warsaw-Okecie Airport runway 15, the crew reported problems with the landing gears that seemed to be down but not locked. At a height of about 250 meters, the captain was cleared to initiate a go-around and increased engine power when the engine n°2 exploded, damaging the engine n°1. Debris damaged the rudder and elevator control cables, causing the aircraft to enter an uncontrolled descent. In a 20° nose-down attitude, the aircraft speed increased to 380 km/h when it crashed in an embankment located by the Okecie Fort, about 900 meters short of runway 15 threshold. The aircraft disintegrated on impact and all 87 occupants were killed. On board were 14 members of the US boxing team and 10 coaches as well as Anna Jantar, a Polish singer.
Probable cause:
Explosion of the engine n°2 caused by the disintegration of a compressor stage due to fatigue cracks.

Crash of a Douglas C-47B-20-DK in San Borja

Date & Time: Mar 13, 1980
Operator:
Registration:
CP-1243
Flight Phase:
Survivors:
Yes
MSN:
15861/32609
YOM:
1945
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff, one of the engine failed. The airplane stalled and crashed by the runway. There were no casualties.
Probable cause:
Engine failure on takeoff for unknown reasons.

Crash of a De Havilland DHC-2 Beaver in Buffalo Narrows: 1 killed

Date & Time: Mar 11, 1980
Type of aircraft:
Operator:
Registration:
C-GZBE
Flight Phase:
Survivors:
Yes
MSN:
1082
YOM:
1957
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
After takeoff, while climbing, the single engine airplane struck power cables and crashed. A passenger was killed while five other occupants were injured.

Crash of a PZL-Mielec AN-2 in Boguchar

Date & Time: Mar 8, 1980
Type of aircraft:
Operator:
Registration:
CCCP-70545
Flight Phase:
Survivors:
Yes
MSN:
1G145-21
YOM:
1973
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed on takeoff for unknown reasons. There were no casualties.

Crash of a Tupolev TU-154A in Orenburg

Date & Time: Mar 1, 1980
Type of aircraft:
Operator:
Registration:
CCCP-85103
Survivors:
Yes
Schedule:
Simferopol - Sochi - Orenburg - Novosibirsk
MSN:
75A-103
YOM:
1975
Flight number:
SU3324
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
152
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
6922
Aircraft flight cycles:
3075
Circumstances:
On final approach to Orenburg, the aircraft dropped below the glide path and the crew did not take the decision to attempt a go around. The three engine aircraft hit the ground 68 meters short of runway threshold with a positive aerodynamic force of 3 g, bounced and touched down again 635 meters further. On the second touchdown, the positive aerodynamic force was 3,9 g, causing the aircraft to brake in two. The airplane went out of control and eventually came to rest. Two crew members and one passenger were injured.
Probable cause:
Wrong approach configuration on part of the crew who failed to follow the approach checklist and published procedures. A series of errors and omissions on part of the flying crew led the aircraft descending below the glideslope and despite several alarms sounded, the captain failed to attempt a go-around manoeuvre. An inappropriate usage of approach charts, stabilizers at -5,5°, flaps at 45° and procedures violation caused the airplane to follow a wrong approach path. Also, the controller in charge of the approaches cleared the crew to land in lieu of giving the instruction to initiate a go-around.

Crash of a Boeing 707-309C in Manila: 2 killed

Date & Time: Feb 27, 1980 at 1345 LT
Type of aircraft:
Operator:
Registration:
B-1826
Survivors:
Yes
Schedule:
Taipei - Manila
MSN:
20262/830
YOM:
1969
Flight number:
CI811
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
124
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
On final approach to Manila Intl Airport, the airplane was too low and struck the ground about 50 meters short of runway threshold. Upon impact, two engines were torn off and out of control, the aircraft crash landed and came to rest in flames. 82 occupants escaped uninjured while 51 others were injured. Two passengers were killed. The aircraft was partially destroyed by fire.
Probable cause:
Wrong approach configuration on part of the crew who failed to follow the approach checklist. A lack of crew coordination led the aircraft descending below the glide.