Crash of a Douglas DC-6A in Luzamba

Date & Time: Aug 7, 1996
Type of aircraft:
Operator:
Registration:
9Q-CJR
Flight Type:
Survivors:
Yes
MSN:
45373
YOM:
1957
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing, the four engine aircraft veered off runway and came to rest in the bush. There were no casualties.

Crash of a Gulfstream GIII in Vágar: 9 killed

Date & Time: Aug 3, 1996 at 1345 LT
Type of aircraft:
Operator:
Registration:
F-330
Flight Type:
Survivors:
No
Schedule:
Keflavik – Vágar
MSN:
330
YOM:
1981
Location:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
On final approach to Vágar Airport runway 12, the crew encountered extreme atmospheric turbulences. Control was lost and the aircraft crashed on the slope of a mountain located 2 km short of runway. All nine occupants were killed, among them Admiral Hans Jørgen Garde, Chief of the Danish Army, and his wife Anna garde. At the time of the accident, the visibility was good but severe turbulences were present in the approach path.

Crash of a Cessna 404 Titan II in Benton Harbor

Date & Time: Aug 3, 1996 at 0740 LT
Type of aircraft:
Operator:
Registration:
N8919G
Flight Type:
Survivors:
Yes
Schedule:
Kalamazoo - Benton Harbor
MSN:
404-0098
YOM:
1977
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3250
Captain / Total hours on type:
53.00
Aircraft flight hours:
10624
Circumstances:
The pilot said that during the landing approach, the flight visibility was inadequate for landing, and he aborted the landing. Witnesses observed the airplane touchdown long and fast, then it
entered fog that shrouded the runway. Subsequently, the airplane collided with trees, then impacted on marshland about 70 feet below the runway elevation. No mechanical anomalies were found with the airplane or engines that would prevent flight. On the day before the accident, the pilot's duty day began at 0500. He had a 9-hour rest period (during the day) that did not involve any sleep. The pilot said that after work on the day before the accident, he arrived home about 2300. His wife said he awoke about 0230 on the accident date, then he returned to bed and arose between 0430 and 0500, departing for work about 0530. During his regular duty day rest period, the pilot would drive a total of 4 hours to and from his home each day. The pilot said he would generally get to bed about 2300 to 2330, arising about 0430 each work day. Also, he said he needed between 6 and 8 hours of sleep at night.
Probable cause:
The pilot's delay in initiating a go-around after not attaining the proper touchdown point during the landing, and his failure to remain clear of obstructions (trees) during the go-around. Factors relating to the accident were the adverse weather condition (fog and low ceiling), pilot fatigue, and the proximity of trees to the runway.
Final Report:

Crash of a De Havilland DHC-4A Caribou in New Stuyahok

Date & Time: Aug 2, 1996 at 1100 LT
Type of aircraft:
Operator:
Registration:
N800NC
Flight Type:
Survivors:
Yes
Schedule:
Anchorage - New Stuyahok
MSN:
98
YOM:
1963
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15670
Captain / Total hours on type:
850.00
Aircraft flight hours:
14638
Circumstances:
The airplane's nose gear collapsed during a landing roll on a gravel airstrip. Subsequent examination of the nose gear locking mechanism disclosed a failed hydraulic drag strut locking actuator.
Probable cause:
The collapse of the nose gear precipitated by the failure of the hydraulic nose gear drag strut locking actuator.
Final Report:

Crash of a Grumman G-159 Gulfstream I in Lubi

Date & Time: Aug 2, 1996
Type of aircraft:
Operator:
Registration:
N190LE
Flight Type:
Survivors:
Yes
MSN:
190
YOM:
1968
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing an humanitarian flight from Kenya. Upon landing on soft ground at Lubi Airstrip, the nose gear sank then collapsed. The aircraft slid on its nose for few dozen metres and both propellers struck the ground as well. The aircraft came to rest and was damaged beyond repair. Both pilots escaped uninjured. At the time of the accident, the aircraft was still registered HK-4022X while its official new registration was N190LE since last 9 of July.

Crash of a Canadair CL-215-1A10 in Lake Fanaco: 1 killed

Date & Time: Jul 30, 1996
Type of aircraft:
Operator:
Registration:
I-CFSU
Flight Type:
Survivors:
Yes
MSN:
1074
YOM:
1985
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was engaged in a fire fighting mission and was supposed to land on Lake Fanaco to proceed to a scooping manoeuvre. For unknown reasons, the aircraft landed hard, causing the hull to rupture. The aircraft sank and was lost. A pilot was killed and the second was injured.

Crash of a Cessna 340A in Richland: 2 killed

Date & Time: Jul 27, 1996 at 0855 LT
Type of aircraft:
Operator:
Registration:
N341TL
Flight Type:
Survivors:
No
Schedule:
Richland - Richland
MSN:
340A-1268
YOM:
1981
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4239
Captain / Total hours on type:
1240.00
Circumstances:
The pilot-under-instruction (PUI) who possessed an expired medical, and the pilot-in-command (PIC), an ATP pilot with 1240 hours in the Cessna 340, departed on the third training flight for the PUI in the aircraft. The second training flight, flown the previous Saturday, had included single-engine work. The aircraft was observed in the vicinity of the Richland airport by witnesses, several of whom reported the left propeller turning slowly. All witnesses reported seeing the aircraft descending rapidly to the ground in a nose down attitude and several witnesses described the descent as a spin. The aircraft impacted the ground in a near vertical, nose low attitude and was destroyed by fire. Postcrash examination of the aircraft revealed the left propeller in the feathered position and power signatures on the blades of the right propeller. Disassembly of both engines revealed no pre-impact mechanical malfunction. The gear and flaps were up and the rudder trim tab showed about 5 degrees of left tab trim. The information manual for the Cessna 340 indicates that the air minimum control speed (single engine), Vmca is 82 KIAS. The manual also indicates that a more suitable airspeed for one engine inoperative training events is 91 KIAS.
Probable cause:
The pilot-in-command's allowing the aircraft's airspeed to decrease below the single-engine minimum control speed (Vmc) resulting in a stall/spin condition. Factors contributing to the accident were the pilot-in-command's allowing the left engine to be shut down as well as his allowing the aircraft's airspeed to decelerate below the manufacturer's recommended intentional one-engine inoperative airspeed. A third factor was the aircraft's low altitude at the stall/spin entry which precluded a successful recovery.
Final Report:

Crash of a Dornier DO.128-6 Skyservant in Atar

Date & Time: Jul 27, 1996
Type of aircraft:
Operator:
Registration:
5Y-BLB
Flight Type:
Survivors:
Yes
Schedule:
Lokichogio - Atar
MSN:
6001
YOM:
1981
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft was engaged in an humanitarian flight from Lokichogio to Atar on behalf of UNICEF. On approach, the pilot decided to make a low pass to analyze the runway state and to locate potential animals. During the second approach, on short final, he spotted an animal on the runway and decided to land a little further down. After touchdown, the aircraft was unable to stop within the remaining distance, overran and came to rest in a ditch. All four occupants escaped uninjured and the aircraft was damaged beyond repair.

Crash of a Yakovlev Yak-40 in Monrovia

Date & Time: Jul 25, 1996 at 1037 LT
Type of aircraft:
Operator:
Registration:
RA-87573
Survivors:
Yes
Schedule:
Freetown - Monrovia
MSN:
9 22 05 22
YOM:
1972
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Freetown, the three engine aircraft encountered windshear on final approach to Monrovia, lost height and struck the ground 5 metres before the runway threshold (0.8-1 meter below the runway elevation). The left main gear was torn off and the aircraft slid/rolled for about 300 metres before coming to rest. All 11 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Loss of control on short final after the aircraft encountered windshear.

Crash of a Fokker F27 Friendship 600 in Mergui: 8 killed

Date & Time: Jul 24, 1996
Type of aircraft:
Operator:
Registration:
XY-AET
Survivors:
Yes
Schedule:
Yangon - Mergui
MSN:
10433
YOM:
1970
Flight number:
UB309
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
45
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
While descending to Mergui Airport, the crew encountered poor weather conditions with heavy rain falls. On short final, the aircraft lost height and struck the ground about 250 metres short of runway 18. On impact, the undercarriage were torn off and the aircraft slid for few dozen metres before coming to rest in a 1,2 metre deep excavation located short of runway threshold. Eight passengers were killed while 16 others were seriously injured.
Probable cause:
It was reported that the crew initiated the approach while maintaining a visual contact with the runway. At an altitude of 1,500 feet, visual contact with the runway was lost due to heavy rain falls and the aircraft lost height and struck the ground in a relative flat attitude. The horizontal visibility at the time of the accident was estimated to be 1,500 metres and it is possible that the aircraft encountered windshear.