Crash of a Cessna 414 Chancellor in Leeds: 2 killed

Date & Time: Mar 23, 1980 at 1101 LT
Type of aircraft:
Operator:
Registration:
G-BAOZ
Flight Type:
Survivors:
No
Schedule:
Leeds - Leeds
MSN:
414-0381
YOM:
1973
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1440
Captain / Total hours on type:
900.00
Aircraft flight hours:
1931
Circumstances:
One pilot and one engineer departed Leeds-Bradford Airport in the mid-morning on a local post maintenance flight, the aircraft being transferred the following day to Pakistan on behalf of UNO. On final approach to runway 15, the aircraft has been observed to be flying more slowly than usual and at a low height. The turn on to final approach developed into a spin to the left, and after two or three rotations, the aircraft crashed into a wood an caught fire. Both occupants were killed.
Probable cause:
It is concluded that the aircraft entered the spin from an accelerated stall, possibly as the result of the pilot attempting to regain the approach centre line by a higher rate or turn than normal. The relatively slow speed of the aircraft, the gusty conditions and the handling characteristics associated with the aircraft's modified flap system are considered to have been contributory factors.
Final Report:

Crash of a Cessna 421B Golden Eagle II in Tucson: 2 killed

Date & Time: Mar 14, 1980 at 1645 LT
Operator:
Registration:
N59RZ
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Tucson - Tucson
MSN:
421B-0249
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
9590
Circumstances:
The twin engine airplane departed Tucson-Ryan Airport on a local post maintenance flight, carrying one pilot and one mechanic. During initial climb, the airplane went out of control and crashed in flames in a field. Both occupants were killed.
Probable cause:
Airframe failure during climb due to inadequate maintenance and inspection. The following contributing factors were reported:
- Airframe - flight control surfaces: elevator assembly, attachments, missing, flutter,
- Overload failure,
- Bolts missing from elevators,
- Elevator push-pull tube rivets failed,
- Overload elevator/stabilizers twisted.
Final Report:

Crash of a Douglas DC-3A in Bogotá: 4 killed

Date & Time: Jan 24, 1980
Type of aircraft:
Operator:
Registration:
HK-2214
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Bogotá - Bogotá
MSN:
11627
YOM:
1943
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The aircraft was engaged in a local test flight at Bogotá-El Dorado Airport, carrying four crew members, two pilots and two engineers. After passing over runway 12 at an altitude of about 200 feet, the pilot was able to send a brief mayday message when the airplane banked left and crashed in flames. The aircraft was destroyed and all four occupants were killed.
Probable cause:
The exact cause of the accident could not be determined. At impact, the left propeller was feathered while no technical anomalies was detected on the left engine. Nevertheless, it was determined that the forward bearing and connecting rod were seized on the right engine. It was also reported that the pilot-in-command was not qualified on such aircraft type.

Crash of an Antonov AN-26 in Komsomolsk-on-Amur: 9 killed

Date & Time: Dec 10, 1979
Type of aircraft:
Flight Phase:
Flight Type:
Survivors:
No
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The airplane was engaged in a flight where the crew was supposed to test various equipments, probably military ones. According to officials, in poor weather conditions, the airplane deviated from the departure climb course, collided with trees and crashed on a hilly terrain. The wreckage was found in snow about a week later. All nine occupants have been killed.
Probable cause:
Due to the extreme secret character of the mission, no information were published about the circumstances and the causes of the accident. All information related to this tragedy were immediately classified by the Soviet Authorities.

Crash of a PAC Cresco 08-600 in Maramarua

Date & Time: Dec 10, 1979
Type of aircraft:
Operator:
Registration:
ZK-LTP
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
001
YOM:
1979
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, sole on board, was completing a test flight on this first PAC Cresco 08-600 prototype. En route, the pilot lost control of the airplane after the tail detached. The single engine airplane entered a dive and while the pilot was able to parachute to safety, the airplane crashed and was destroyed.
Probable cause:
Structural failure of the tail in flight.

Crash of a Beechcraft 65-90 King Air in Laredo

Date & Time: Sep 3, 1979 at 1712 LT
Type of aircraft:
Registration:
N332K
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Laredo - Laredo
MSN:
LJ-79
YOM:
1966
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6000
Captain / Total hours on type:
400.00
Circumstances:
Shortly after takeoff from Laredo Airport, while in a local test flight, one engine stopped. The crew attempted an emergency landing and completed a belly landing in an open field located near the airport. The airplane came to rest and was damaged beyond repair while both pilots escaped uninjured.
Probable cause:
Engine failure during climb due to fuel exhaustion. The following contributing factors were reported:
- Inadequate preflight preparation,
- Mismanagement of fuel,
- Fuel exhaustion,
- Intentional wheels-up landing,
- Complete engine failure,
- Forced landing off airport on land.
Final Report:

Crash of a Swearingen SA226T Merlin III in San Marcos

Date & Time: May 31, 1979 at 1042 LT
Operator:
Registration:
N5654M
Flight Type:
Survivors:
Yes
Schedule:
San Marcos - San Marcos
MSN:
T-303
YOM:
1979
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5300
Captain / Total hours on type:
6.00
Circumstances:
The twin engine airplane was engaged in a local experimentation flight at San Marcos Airport on behalf of the Federal Aviation Administration (FAA). During the last segment, at level off, the airplane landed hard and struck the runway surface. Upon impact, the undercarriage were torn off and the airplane came on its belly. All four occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Hard landing following improper operation of powerplant and powerplant controls. The following contributing factors were reported:
- Improper level off,
- Overload failure,
- FAA flight test pilot at controls.
Final Report:

Crash of a PZL-Mielec AN-2R in Ufa: 3 killed

Date & Time: May 28, 1979 at 1626 LT
Type of aircraft:
Operator:
Registration:
CCCP-35595
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Ufa - Ufa
MSN:
1G115-46
YOM:
1970
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
6282
Aircraft flight cycles:
17563
Circumstances:
The crew was engaged in a local test flight before completing a crop spraying mission. Following a running distance of 250-280 meters on takeoff, the pilot-in-command started the rotation. Unable to maintain a positive rate of climb, the airplane struck tree tops, stalled and crashed upside down 78 meters further in a field, about 1,037 meters after the start of the take off run. The aircraft was destroyed and all three occupants were killed.
Probable cause:
It was determined that the total weight of the aircraft at takeoff was 779 kilos above the MTOW. Following a too short takeoff roll, the pilot-in-command rotated prematurely. Due to an insufficient speed, the airplane was unable to maintain a positive rate of climb and a correct climb path.

Crash of a Douglas C-54S Skymaster in Mesa

Date & Time: May 15, 1979 at 1455 LT
Type of aircraft:
Operator:
Registration:
N44905
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Mesa - Chandler
MSN:
22159
YOM:
1945
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12127
Captain / Total hours on type:
4399.00
Circumstances:
During the takeoff roll at Mesa-Falcon Field Airport, the crew started the rotation but the aircraft did not liftoff. It overran, struck a 10 feet high dirt bank, crossed a road where it hit a truck and eventually came to rest in flames in an orange grove. Both pilots, en route to Chandler-Stellar Airpark on a test flight, were seriously injured and the aircraft was destroyed by fire.
Probable cause:
Collision with dirt bank on takeoff due to inadequate preflight preparation. The following contributing factors were reported:
- Failed to abort takeoff,
- Failed to use the checklist,
- Gust locks engaged.
Final Report:

Crash of a Cessna 414 Chancellor in Arlington

Date & Time: Feb 7, 1979 at 1330 LT
Type of aircraft:
Operator:
Registration:
N141WB
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Wichita - Wichita
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9201
Captain / Total hours on type:
31.00
Circumstances:
The pilot, sole on board, departed Wichita Airport on a local test flight, accompanied by a second aircraft. Both aircraft were visually checking each others underside when they collided in flight. Out of control, they crashed in a field located in Arlington, Kansas. Both pilots were injured, the one on board the Chancellor critically.
Probable cause:
In-flight collision during normal cruise after the pilot failed to maintain adequate separation. The following contributing factors were reported:
- Pilot of other aircraft,
- Not under radar contact,
- No control area.
Final Report: