Crash of a Rockwell Grand Commander 690B in Konawa: 1 killed

Date & Time: Jun 25, 1992 at 0833 LT
Registration:
N690JC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Norman - Fort Lauderdale
MSN:
690-11479
YOM:
1978
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8857
Captain / Total hours on type:
98.00
Aircraft flight hours:
3355
Circumstances:
As the airplane was deviating around low intensity weather returns, and passing through 20,500 feet during climb out, it departed controlled flight and entered a right spiral. Descent rates exceeded 16,600 fpm during the descent from 18,300 feet to 3,900 feet and then slowed. Witnesses stated they saw the airplane descend from the clouds in a right flap spin. The empennage had separated from the airplane in pieces. Pieces of the wreckage were found up to 1.5 mile from the primary impact point. Both wings remained attached. The right engine was flamed out, and the propeller was feathered at impact. No mechanical reason for the flameout could be determined. At no time did the pilot indicate he was having difficulties. The NTSB weather study indicated that moderate turbulence was present in the area. The pilot's toxicology tests found 0.151 ug/ml of chlorpheniramine in the blood; normal therapeutic concentration is 0.01 to 0.04. Effects of overdosage include sedation, diminished mental alertness, and cardiovascular collapse to stimulation. The pilot, sole on board, was killed.
Probable cause:
The pilot's failure to maintain control of the airplane which resulted in an inadvertent spiral and subsequent rapid descent. The design stress limits of the airframe were exceeded resulting in an overload failure of the empennage. Factors related to the accident were: turbulence and the pilot's physical impairment due to drugs.
Final Report:

Crash of a Cessna 401 in New Port Richey: 1 killed

Date & Time: Apr 23, 1992 at 1606 LT
Type of aircraft:
Registration:
N3271Q
Flight Type:
Survivors:
No
Schedule:
New Port Richey - Gainesville
MSN:
401-0071
YOM:
1967
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
12600
Circumstances:
The pic departed on a ferry flight in VFR conditions without a ferry permit. Witnesses stated they observed the airplane returning to the airport at about 150 to 500 feet. The airplane was observed to begin a left turn with the landing gear extended. A fire was observed in the vicinity of the left engine exhaust. The airplane continued in a steep descending left turn before it disappeared below the tree line and collided with the terrain. The airplane was destroyed and the pilot was fatally injured.
Probable cause:
The pilot-in-command's failure to maintain airspeed (vs) while maneuvering for a forced landing following an in flight left engine fire for undetermined reasons. Contributing to the accident was the pilot in command's inadvertent shutdown of the wrong engine.
Final Report:

Crash of an Antonov AN-26 in Calcutta

Date & Time: Mar 30, 1992 at 1520 LT
Type of aircraft:
Operator:
Registration:
CCCP-26154
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Hanoi - Yangon - Calcutta
MSN:
51 01
YOM:
1977
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
An Antonov 26 was ferried from Hanoi to Calcutta with a refueling stop at Rangoon. The aircraft took-off from Hanoi at 9:00 hours with estimated time of arrival Calcutta at 14:50 hours. On initial contact with Calcutta, the aircraft informed about minimum fuel on board and requested radar vectors for straight-in approach. However, Calcutta ATC did not pay much attention to the problems faced by the aircraft and made no serious attempt to assist the aircraft on radar. The pilot deviated from the track and became lost. The aircraft exhausted its fuel and force landed 28nm NE of Calcutta airport. All seven occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The accident caused by forced landing due to flight crew failure by carrying marginal fuel to reach Calcutta and not making use of correct navigational facility (EA NDB at Calcutta) combined with lack of assistance from Calcutta ATC by not providing radar facilities vectoring/VDF guidance and advising the aircraft to use NDB not having adequate range.

Crash of a Lockheed P2V-7 Neptune near Dixon: 2 killed

Date & Time: Feb 8, 1992 at 1530 LT
Type of aircraft:
Operator:
Registration:
N70600
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Tucson - Greybull
MSN:
726-7227
YOM:
1958
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
6000
Captain / Total hours on type:
180.00
Aircraft flight hours:
8401
Circumstances:
The flight had departed Tucson, AZ, on a special VFR ferry flight to Greybull, WY. The airplane was not instrumented for IFR flight. When the flight reported over Winslow, it was advised that VFR flight was not recommended northbound from its present position. Surface weather conditions in southcentral wyoming/northwestern Colorado at the time of the accident were consistent with low ceilings, clouds and snow as reported by witnesses and surface weather observations. The witnesses, located near the Dixon Airport, reported hearing a low flying aircraft travelling west to east, and another witness northeast of the arpt heard an aircraft 'revving' its engines. Radar data shows the aircraft tracking northbound slightly east of the Dixon airport, and executing a clockwise 360° turn northeast of the airport and in the vicinity of one of the witnesses. The last radar target received placed the aircraft approximately one mile north-northeast of the accident site. The aircraft impacted snow covered terrain in a steep nose-down attitude. Both pilots were killed.
Probable cause:
The pilot-in-command's continued VFR flight into instrument meteorological conditions which resulted in a loss of control due to the lack of aircraft attitude indicators and resultant pilot spatial disorientation. A factor which contributed to the accident was the weather condition(s).
Final Report:

Crash of a Curtiss C-46F-1-CU Commando near Bogotá: 8 killed

Date & Time: Dec 11, 1991 at 1520 LT
Type of aircraft:
Operator:
Registration:
HK-2716
Flight Type:
Survivors:
No
Site:
Schedule:
Medellín – Bogotá
MSN:
22478
YOM:
1945
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
The twin engine aircraft was ferried from Medellín to Bogotá after repairs were conducted at Medellín Airport following a gear problems last September 23. On approach to Bogotá-El Dorado Airport, the aircraft struck the slope of a mountain located 20 km north of the airport. All eight occupants were killed.
Probable cause:
For unknown reasons, the crew was approaching the airport at an insufficient altitude. Lack of visibility due to clouds was a contributing factor.

Crash of a Convair CV-240D in Akron

Date & Time: Nov 28, 1991 at 1434 LT
Type of aircraft:
Operator:
Registration:
N450GA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Akron - Columbus
MSN:
52-83
YOM:
1954
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
18528
Circumstances:
Shortly after departure the airplane was seen climbing to an altitude of about 200 feet agl. Witnesses saw smoke coming from one of the engines and heard a 'popping noise.' The pilot executed a forced landing in a field. The airplane struck electrical wires and fence then burst into flames. The airplane had refueled just prior to take off, and the fuel receipt showed that 300 gallons of jet (A) fuel was put into the tanks. The normal fuel used in the airplane was 100LL.
Probable cause:
The use of an improper grade of fuel, which was approved by the captain and resulted in a loss of engine power during climbout and an in flight collision with terrain.
Final Report:

Crash of a Fokker F27 Friendship 100 in Dori: 3 killed

Date & Time: Aug 15, 1991
Type of aircraft:
Operator:
Registration:
J5-GBB
Flight Type:
Survivors:
No
Schedule:
Kano - Bamako - Bissau
MSN:
10119
YOM:
1959
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The aircraft already completed other rotations that day between Bamako and Kano and was returning empty, carrying three Palestinian crew members. En route from Kano to Bamako at dusk, the crew lost his orientation and was unable to report his position. For unknown reasons, he failed to contact Ouagadougou and Niamey ACC. After few dozen minutes, the captain decided to attempt an emergency landing in Dori when the right wing struck a tree and was torn off. Out of control, the aircraft crashed in an open field located few km from Dori Airport. Two occupants were seriously injured while a third crew was killed. The following day, both survivors died from their injuries.
Probable cause:
The crew did not file any flight plan and the accident was the consequence of negligences on part of the crew.

Crash of a Piper PA-31-310 Navajo in Lydd

Date & Time: Jul 17, 1991 at 0930 LT
Type of aircraft:
Operator:
Registration:
G-LYDD
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Lydd - Blackpool
MSN:
31-537
YOM:
1969
Location:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3035
Captain / Total hours on type:
1.00
Circumstances:
The aircraft, which had not flown for over 2 years, had been worked-on during the past days and had to be ferried to Blackpool with two pilots on board. During the takeoff roll on runway 22, at a speed of about 60 knots, a loud report was heard and the outboard section of the right wing disintegrated. The crew abandoned the takeoff procedure and was able to stop the aircraft on the runway. They exited the cabin and were uninjured while the aircraft was damaged beyond repair.
Probable cause:
The exact cause of the double explosion in the right wing could not be determined with certainty. A possibility was that the non-wetted areas of the tanks had become slightly porous during the time that the aircraft had not been in use and consequently may have allowed small leakages of fuel through the porous areas when the tanks had been filled to capacity. The resultant vapour could then have migrated outboard around the edges of the ribs at the end of the tank bay.
Final Report:

Crash of a Mitsubishi MU-2B-36A Marquise in Uchiza

Date & Time: Jul 10, 1991
Type of aircraft:
Registration:
OB-1219
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Uchiza - Lima
MSN:
730
YOM:
1978
Location:
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Uchiza Airport, while climbing, the pilot reported engine problems to ATC and elected to return. On approach, he realized that a landing was not possible as weather conditions deteriorated rapidly. He then decided to attempt an emergency landing along the Huallaga River. Upon landing, the aircraft slid for few dozen meters and eventually came to rest upside down. Both occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Fire on the left engine after takeoff for unknown reasons.

Crash of a Grumman G-64 Albatross in the Pacific Ocean

Date & Time: Jun 18, 1991 at 1910 LT
Type of aircraft:
Registration:
N7029C
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Santa Barbara – Kahului
MSN:
G-288
YOM:
1953
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During cruise flight the accident aircraft lost oil pressure in the n°2 engine. Flight could not be sustained using the remaining engine. According to the pilot, the remaining engine would overheat when power was applied. The crew descended to just above the water and tried to fly the aircraft in ground effect, but to no avail. They elected to ditch the aircraft. During the landing, the aircraft received substantial damage and was almost immediately flooded, causing the aircraft to sink. The crew escaped, but did not have time to retrieve emergency gear. They were rescued after about 20 hours in the water. Evidence revealed that the pilot did not have a pilot's certificate. No evidence could be found to indicate that the pilot had any experience in the accident aircraft or with any sea plane. Since the aircraft sank, a cause for the engine problems could not be determined.
Probable cause:
Improper touchdown in the water causing substantial damage. Loss of power on the n°2 engine and the pilot's lack of qualifications were factors in the accident.
Final Report: