Crash of a Britten-Norman BN-2A-21 Islander near Beoga

Date & Time: Apr 26, 1979
Type of aircraft:
Operator:
Registration:
PK-KNG
Flight Phase:
Survivors:
Yes
Site:
MSN:
749
YOM:
1975
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances in a wooded and isolated area located in the region of Beoga, Papua. Both pilots survived the accident and were found alive three months later.

Crash of a Vickers 785D Viscount near Shell: 57 killed

Date & Time: Apr 23, 1979 at 0745 LT
Type of aircraft:
Operator:
Registration:
HC-AVP
Flight Phase:
Survivors:
No
Site:
Schedule:
Quito - Cuenca
MSN:
329
YOM:
1957
Flight number:
EH011
Location:
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
52
Pax fatalities:
Other fatalities:
Total fatalities:
57
Circumstances:
The four engine airplane departed Quito-Mariscal Sucre Airport at 0708LT on a schedule service (EH011) to Cuenca. While cruising at an altitude of 18,000 in clouds, the airplane struck the slope of a mountain and disappeared from radar screens. SAR operations were initiated but eventually abandoned few day slater as no trace of the aircraft nor the 57 occupants was found. The wreckage was located about 5 years later in a mountainous area located in the region of Shell-Mera, province of Pastaza.
Probable cause:
Controlled flight into terrain. At the time of the accident, the airplane was off course by 25 nm for undetermined reasons.

Crash of a Fairchild F27A in Iquique

Date & Time: Apr 20, 1979
Type of aircraft:
Operator:
Registration:
CC-CBR
Flight Phase:
Survivors:
Yes
MSN:
55
YOM:
1959
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after liftoff from runway 01, the crew raised the landing gear when the airplane stalled and struck the runway surface. It skidded for about 750 meters before coming to rest. All five occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
It is believed that one of the engine failed shortly after rotation.

Crash of a Grumman G-21A Goose off Avalon: 1 killed

Date & Time: Apr 14, 1979 at 1007 LT
Type of aircraft:
Operator:
Registration:
N11CS
Survivors:
Yes
Schedule:
San Pedro - Avalon
MSN:
1166
YOM:
1942
Crew on board:
1
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
9335
Captain / Total hours on type:
455.00
Circumstances:
On approach to Avalon (Santa Catalina Island) in marginal weather conditions with low clouds and fog, the pilot decided to initiate a go-around after noticing boat wakes. Doing so, the seaplane stalled, lost height and crashed into the sea few hundred yards off Pebbly Beach. The pilot and two passengers were seriously injured while seven other occupants escaped with minor injuries. A passenger drowned.
Probable cause:
Stall during a go-around after the pilot misjudged distance, speed and altitude. The following contributing factors were reported:
- Failed to maintain flying speed,
- Low ceiling,
- Fog,
- Visibility two miles or less,
- Low altitude straight-in approach toward seaplane ramp,
- Go-around after noticing boat wakes.
Final Report:

Crash of an Aérospatiale SN.601 Corvette in Nkayi

Date & Time: Mar 30, 1979
Operator:
Registration:
TN-ADB
MSN:
22
YOM:
1975
Location:
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Destroyed in a crash while attempting to land at Nkayi Airport. Occupant fate unknown.

Crash of a Fairchild F27 in Quebec: 17 killed

Date & Time: Mar 29, 1979 at 1845 LT
Type of aircraft:
Operator:
Registration:
C-FQBL
Flight Phase:
Survivors:
Yes
Schedule:
Quebec - Montreal
MSN:
47
YOM:
1959
Flight number:
QB255
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
21
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
Shortly after liftoff from Quebec-Ancienne Lorette Airport, en route to Montreal-Dorval Airport, the right engine caught fire. The captain contacted ATC, declared an emergency and was cleared to return for an emergency landing. He initiated a turn to the right when the airplane lost height, struck the ground and crashed in flames about 1,300 meters short of runway. Seven passengers were seriously injured while 17 other occupants were killed.
Probable cause:
It was determined that during initial climb, the low pressure impeller from the right (n°2) engine burst, causing the forward part of the engine to separate. The gear couldn't be raised because of engine debris damage to the electronic gear selection circuitry. This, including the exposed engine and lower cowl, increased the drag. In this configuration the aircraft wasn't capable of out-climbing obstacles straight ahead nor capable of maintaining altitude during the right hand turn. Engine separation and passenger movement resulted in the center of gravity shifting beyond its aft limit. The airspeed then decreased until the aircraft struck the ground at or below the minimum control speed (Vmc). Investigations revealed that the low pressure impeller burst due to the presence of fatigue cracks that had not been detected by the technicians in charge of the aircraft's maintenance.

Crash of a Yakovlev Yak-40K in Chardzhou

Date & Time: Mar 20, 1979
Type of aircraft:
Operator:
Registration:
CCCP-87930
Survivors:
Yes
Schedule:
Ashkhabad - Chardzhou
MSN:
9 74 01 56
YOM:
1977
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Chardzhou Airport, at an altitude of 30-40 meters, the airplane banked left then lost height and crashed onto several datchas located in the approach path. The aircraft was damaged beyond repair but all 35 occupants survived. The flight engineer was injured. There were no injuries on the ground.
Probable cause:
It was determined that the loss of control on short final was the consequence of wake turbulences caused by a Mil-Mi 6 helicopter that was preceding the Yak-40. Investigations revealed that the controller in charge of approaches failed to respect the minimum separation between the helicopter and the Yak-40. Poor organization of ATC in Turkmenistan was considered as a contributing factor.

Crash of a Tupolev TU-104B in Moscow: 59 killed

Date & Time: Mar 17, 1979 at 1948 LT
Type of aircraft:
Operator:
Registration:
CCCP-42444
Survivors:
Yes
Schedule:
Moscow - Odessa
MSN:
9 2 10 01
YOM:
1959
Flight number:
SU1691
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
114
Pax fatalities:
Other fatalities:
Total fatalities:
59
Captain / Total hours on type:
32.00
Aircraft flight hours:
24356
Aircraft flight cycles:
14118
Circumstances:
Five seconds after takeoff from runway 01 at Moscow-Vnukovo Airport, while in initial climb, a fire alarm activated in the cockpit panel, informing the crew about a fire in the left engine. The crew declared an emergency, continued to climb and was cleared to return. Following several turns, the crew started an approach to runway 01 by night and marginal weather conditions. On final, the airplane descended below the MDA until it struck the ground at a speed of 350 km/h and crashed in flames in a snow covered field located along a wooded area, 1,548 meters short of runway 01. 58 passengers and a stewardess were killed while 61 other occupants were injured. The aircraft was destroyed.
Probable cause:
It was determined that the fire alarm that activated in the cockpit was false and not related to an engine fire. Analysis revealed that the temperature of the left engine compartment increased to 253° C due to the disconnection of a pipe coupled to the anti-icing system. The accident was the consequence of the combination of several wrong decisions on part of the flying crew and the following factors:
- The approach was completed by night and icing conditions in a single engine configuration,
- The total weight of the aircraft was 10,201 kg above the maximum weight allowed for landing,
- The approach was completed with a tailwind component,
- Excessive approach speed,
- Premature descent resulting in a collision with ground after passing MDA,
- Lack of crew interaction and coordination,
- The navigator failed to inform the captain about the decision height fixed at 120 meters,
- The approach was completed with the GPWS deactivated,
- The copilot failed to monitor the instruments properly, which contributed to the deviation of the airplane to the right during the last sequence until it lost altitude and impacted the ground.

Crash of a Boeing 727-2D3 in Doha: 45 killed

Date & Time: Mar 14, 1979 at 2340 LT
Type of aircraft:
Operator:
Registration:
JY-ADU
Survivors:
Yes
Schedule:
Amman - Doha - Muscat
MSN:
20886/1061
YOM:
1974
Flight number:
RJ600
Country:
Region:
Crew on board:
15
Crew fatalities:
Pax on board:
49
Pax fatalities:
Other fatalities:
Total fatalities:
45
Circumstances:
Flight Royal Jordanian 600 departed Amman for a flight to Doha and Muscat. With the first officer as the handling pilot the aircraft, called "The City of Petra", left Amman at 21:55. Contact was established with Doha at 23:08 at a range of 45 miles when weather information was received, which included: wind 090° at 17 knots, visibility 10 km in thunderstorms, 1/8 CS at 2500 feet, 3/8 at 3000 feet, and QNH 1008. The controller added that the thunderstorm appeared to be building up over and to the north west of the airfield. The pilot requested runway 16 and was cleared for a visual approach to that runway or for a NDB/VOR approach if visual contact with the airfield was not established. The aircraft reported approaching the overhead position for a NDB/VOR procedure at 23:17. On the airfield rain was falling quite heavily and the controller informed the aircraft of this. The NDB then tripped, presumably as a result of a lightning strike but was back in the air again at 23:22. At 23:25 the aircraft reported procedure turn complete and was cleared to land. At 23:29 the aircraft reported that it had not seen the runway, and initiated a missed approach, requesting and receiving clearance to make an ILS approach to runway 34. At 23:30 a wind was reported 290°/14 knots in heavy rain. At 23:35 the aircraft reported procedure turn complete and field in sight. Landing clearance was given with a wind of 180°/06 kt. During the next 2 minutes of the final approach the controller reported winds of 150° at 13 kt, 150° at 15 kt, and 140° at 17 knots. Because of the increasing tail wind component and difficulties in maintaining the glide slope the crew decided before reaching decision height, that a missed approach was necessary and this was initiated at 23:37:19 at a height of about 300 feet agl. The pilot then requested clearance to Dhahran and the controller cleared the aircraft to climb straight ahead to FL 80. Go around power was applied and 25° flaps was selected, the undercarriage was raised. The aircraft climbed to 750 feet with the indicated airspeed falling to approximately 140 knots. The aircraft then began to descend at an increasing rate until it struck the ground with a vertical speed of 4200 ft/min., with the IAS increasing rapidly to approximately 170 kt in the last 5 seconds. The aircraft struck the left hand edge of the runway, 2050 m from the threshold with the nose approximately 10° above the horizon and with the left wing 5° down. The aircraft bounced off the first impact and turning left, rolled to the right to an inverted position and then slid, tail first, into the Fire Station garage some 800 m from the first impact point and 270 m from the runway edge. The fuselage broke into three main sections during the process. Four crew members and 41 passengers were killed while 19 other occupants were injured.
Probable cause:
The aircraft's encounter with a downburst associated with a thunderstorm, the effects of which exceeded the performance capability of the aircraft. The encounter resulted from the flight crew's decision to conduct an approach to land without due regard to the prevailing weather conditions.

Crash of a Fairchild F27A in Nouakchott

Date & Time: Mar 14, 1979
Type of aircraft:
Operator:
Registration:
5T-CJY
Survivors:
Yes
MSN:
28
YOM:
1958
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed upon landing for unknown reasons. There were no casualties.