Crash of a Beechcraft 65 Queen Air in Fort Pierce: 4 killed

Date & Time: Jun 29, 1980 at 2217 LT
Type of aircraft:
Operator:
Registration:
N156F
Flight Type:
Survivors:
No
MSN:
LC-200
YOM:
1966
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
656
Circumstances:
While cruising by night over Florida, the pilot contacted ATC and reported a loss of engine power. He was cleared to divert to Fort Pierce-St Lucie County Airport. On final approach, the airplane stalled, entered a dive and crashed few miles from the airfield. The aircraft was destroyed and all four occupants were killed.
Probable cause:
Engine failure, stall on final approach and subsequent crash caused by an inadequate preflight preparation on part of the pilot. The following contributing factors were reported:
- Mismanagement of fuel on part of the pilot,
- The pilot was inattentive to fuel supply,
- Fuel exhaustion,
- The pilot failed to maintain flying speed,
- Partial loss of power on both engines.
Final Report:

Crash of a Lockheed L-1049H Super Constellation in Columbus: 3 killed

Date & Time: Jun 22, 1980 at 1359 LT
Registration:
N74CA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Columbus - Seattle
MSN:
4850
YOM:
1959
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
17250
Captain / Total hours on type:
2000.00
Copilot / Total flying hours:
8000
Copilot / Total hours on type:
100
Aircraft flight hours:
20000
Circumstances:
The four engine airplane departed Columbus-Municipal (Bakalar) Airport on a cargo flight to Seattle, carrying a load of aircraft spare parts. After takeoff, during initial climb, the airplane encountered difficulties to gain height, struck power cables, stalled and crashed in flames in a soybean field. Both pilots and a passenger were killed while five other occupants were injured. The aircraft was totally destroyed by impact forces and a post crash fire.
Probable cause:
The flight crew's inadequate and uncoordinated response to the No 2 engine fire warning. The flight engineer failed to correct a gradual power decay on the other engines which occurred while he was retarding the No 2 engine throttle, and the power decay went uncorrected by the pilot and co-pilot. The lack of co-ordination and the lack of corrective action may have been caused by the lack of recent flight crew experience in the L-1049 aircraft. Contributing to the accident was the aircraft's over maximum take-off weight, the crew's use of less than full power for take-off, and the use of less than take-off cowl flaps which precluded adequate engine cooling.
Final Report:

Crash of a McDonnell Douglas MD-81 in Yuma

Date & Time: Jun 19, 1980 at 1849 LT
Type of aircraft:
Operator:
Registration:
N1002G
Flight Type:
Survivors:
Yes
Schedule:
Yuma-Yuma
MSN:
48001
YOM:
1979
Location:
Crew on board:
3
Crew fatalities:
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8200
Captain / Total hours on type:
150.00
Copilot / Total flying hours:
3199
Copilot / Total hours on type:
223
Aircraft flight hours:
6
Circumstances:
The airplane skidded off the right side of runway 21R while attempting a simulated hydraulic-systems-inoperative landing at the Yuma International Airport, Yuma, Arizona. The aircraft came to rest about 6,700 feet beyond the landing threshold of the runway. Although the aircraft was damaged substantially the three flightcrew members were not injured. There were no passengers. The weather was clear and the runway was dry. The aircraft was on an FAA certification test flight to demonstrate compliance with a special condition to 14 CFR Part 25. The purpose of the flight was to show that the aircraft could be controlled adequately and landed safely with a complete failure of its hydraulic systems. The aircraft landed about 1,735 feet beyond the threshold of runway 21R, and the pilot deployed the thrust reverses and applied reverse thrust before the nosewheel touched down. The aircraft began to yaw, continued to yaw after the nosewheel touched down, it then ground looped to the right, and slid off the right side of the runway. All three crew members were slightly injured and the aircraft was damaged beyond repair.
Probable cause:
Inadequate procedures established for certification test flight, and the pilot's mismanagement of thrust following the initial loss of directional control.
Final Report:

Crash of a Sud-Aviation SE-210 Caravelle VI-R in Atlanta

Date & Time: Jun 19, 1980 at 0456 LT
Operator:
Registration:
N905MW
Flight Type:
Survivors:
Yes
Schedule:
San Jose - Wilmington - Atlanta
MSN:
95
YOM:
1961
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9941
Captain / Total hours on type:
1239.00
Circumstances:
The crew was completing a night cargo flight from San Jose, California, to Atlanta with intermediate stop in Wilmington, Ohio. On approach, the airplane became unstable and rolled left and right. Despite the situation, the crew decided to continue the approach to runway 26 when the airplane landed hard. Upon touchdown, the left main gear collapsed. The airplane rolled for about 4,526 feet then veered off runway to the left and came to rest 250 feet further in a grassy area. All four occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
Hard landing and subsequent failure of the left main gear after the crew failed to follow approved procedures. The following contributing factors were reported:
- Poorly planned approach,
- Vortex turbulences,
- Fast from LOM to airport,
- Closed gap behind a Lockheed L-1011 Tristar that just landed on same runway.
Final Report:

Crash of a Swearingen SA226TC Metro II in Valley: 13 killed

Date & Time: Jun 12, 1980 at 1546 LT
Type of aircraft:
Operator:
Registration:
N650S
Flight Phase:
Survivors:
Yes
Schedule:
Appleton - Minneapolis - Lincoln
MSN:
TC-228
YOM:
1977
Flight number:
ZW965
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
13
Captain / Total flying hours:
8391
Captain / Total hours on type:
6000.00
Copilot / Total flying hours:
4063
Copilot / Total hours on type:
143
Aircraft flight hours:
8055
Circumstances:
The airplane departed Appleton, Wisconsin, at 1245LT on a regular schedule service (ZW965) to Lincoln, Nebraska, with an intermediate stop in Minneapolis. En route, while cruising at 12,000 feet, the crew encountered moderate turbulences and precipitation and was cleared to descend to 8,000 feet then later at 6,000 feet. As turbulences were getting worse, the crew was later cleared to descend to 4,000 feet and finally 3,000 feet. While descending to 6,000 feet, massive water ingestion caused both engines to lose power simultaneously. Both engines were restarted but the Metro couldn't recover and struck a muddy field in a slight nose down, right wing-down attitude. The aircraft bounced and hit the ground 288 feet further on. The plane skidded 1,022 feet before coming to rest inverted. There was no fire. Two passengers were seriously injured while 13 other occupants were killed.
Probable cause:
The flight crew's continued flight into an area of severe thunderstorms, and the resultant precipitation-induced flameout or loss of power of both engines at an altitude from which recovery could not be made. Contributing to the cause of the accident was the failure of the flight crew to utilise all available sources of weather information and the failure of the air traffic control system to disseminate critical weather information to the air traffic controllers and to the crew of Flight 965, the failure of air traffic control supervisory personnel to accomplish key job functions, and the failure of Center Weather Service Unit meteorologists to disseminate critical weather information to the Omaha Radar Approach Control Facility supervisors. Also contributing was the precipitation induced X-band radar attenuation which limited tile ability of airborne weather radar to detect the extent and intensity of the weather disturbances.
Final Report:

Crash of a Piper PA-31P Prerssurized Navajo in Ocala

Date & Time: Jun 4, 1980 at 0615 LT
Type of aircraft:
Operator:
Registration:
N7651L
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
31P-7300125
YOM:
1973
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Parked at a local airport, the twin engine airplane was stolen during the night and the 'pilot' attempted a local flight when the left engine caught fire in flight. The airplane crash landed and came to rest in flames. The sole occupant was not recovered.
Probable cause:
Inadequate preflight preparation on part of the pilot. Fire in left engine due to oil filler cap not secured. The crew fled from stolen aircraft after landing allowing fire to spread and destroy the airplane.
Final Report:

Crash of a Cessna T207 Skywagon near Furnace Creek: 6 killed

Date & Time: Jun 1, 1980 at 1530 LT
Registration:
N1535U
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Beatty - Death Valley
MSN:
207-0135
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
While flying at a relative low altitude into a blind canyon, the single engine airplane stalled and crashed between ridges on rising terrain. The wreckage was recovered in an isolated area two days later. All six occupants were killed.
Probable cause:
Stall and subsequent crash due to improper in-flight decisions on part of the pilot. The following contributing factors were reported:
- The pilot misjudged distance, speed and altitude,
- Flew into blind canyon,
- Unqualified person operated aircraft,
- Density altitude approximately 7,000 feet.
Final Report:

Crash of a Piper PA-31-310 Navajo in Mobile: 6 killed

Date & Time: May 28, 1980 at 1005 LT
Type of aircraft:
Operator:
Registration:
N6492L
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Mobile - Ocala
MSN:
31-456
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
1500
Captain / Total hours on type:
30.00
Circumstances:
The twin engine airplane was engaged in a demonstration flight from Mobile to Ocala, Florida, carrying five passengers and one pilot. After takeoff, the airplane encountered serious difficulties to gain height, stalled and crashed. All six occupants were killed.
Probable cause:
Stall during initial climb due to inadequate preflight preparation on part of the pilot. The following contributing factors were reported:
- Lack of familiarity with aircraft on part of the pilot,
- The pilot failed to use or misused flaps,
- The pilot failed to obtain/maintain flying speed,
- High temperature,
- Improperly loaded aircraft,
- The aircraft was 449 lbs over max gross weight, out of forward cg limit,
- Flaps were full down at takeoff.
Final Report:

Crash of a Convair CV-240-0 in Port Orange: 3 killed

Date & Time: May 24, 1980 at 1600 LT
Type of aircraft:
Operator:
Registration:
N300GR
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Port Orange - Santo Domingo
MSN:
115
YOM:
1948
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
7300
Captain / Total hours on type:
25.00
Circumstances:
During the takeoff roll at Port Orange-Spruce Creek Airport, the right engine caught fire and exploded. The crew failed to abort the takeoff and continued. During initial climb, the captain decided to attempt an emergency landing. The aircraft descended, crashed in a field and burst into flames. The aircraft was destroyed by fire and all three occupants were killed.
Probable cause:
Controlled collision with ground during initial climb after the crew attempted operation with known deficiencies in equipment. The following contributing factors were reported:
- The pilot-in-command failed to abort takeoff,
- Inadequate preflight preparation,
- Improperly loaded aircraft,
- Fire in engine,
- Forced landing off airport on land,
- The crew was aware that oil lines were 15 years old,
- The aircraft was approximately 7,353 lbs over gross weight for takeoff conditions.
Final Report:

Crash of a Cessna 401B in Gainesville

Date & Time: May 12, 1980 at 1936 LT
Type of aircraft:
Registration:
N7931Q
Survivors:
Yes
Schedule:
Jacksonville - Gainesville
MSN:
401B-0031
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5000
Captain / Total hours on type:
3.00
Circumstances:
On final approach to Gainesville Airport, both engines failed simultaneously. The airplane lost height, struck trees and crashed in high vegetation. Both occupants were seriously injured.
Probable cause:
Double engine failure on final approach due to inadequate preflight preparation. The following contributing factors were reported:
- Lack of familiarity with aircraft,
- Mismanagement of fuel,
- Inattentive to fuel supply,
- Fuel starvation,
- Fuel selector positioned between tanks,
- High vegetation,
_ Complete failure of both engines,
- Forced landing off airport on land,
- Auxiliary fuel tanks and left main empty,
- Right main fuel tank 10-15 gallons,
- Left engine fuel selector on left main tank,
- Right engine fuel selector between left main and right auxiliary tank.
Final Report: