Crash of a Piper PA-61 Aerostar (Ted Smith 601P) in Burns: 1 killed

Date & Time: Aug 12, 1977 at 1150 LT
Operator:
Registration:
N9578Q
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
La Verne - La Grande
MSN:
61-368-117
YOM:
1977
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
En route from La Verne to La Grande, while in cruising altitude, a wing separated and detached. Out of control, the airplane entered a spin and crashed in flames. The pilot, sole on board, was killed.
Probable cause:
Airframe failure in flight and uncontrolled descent after the pilot exceeded designed stress limits of aircraft. The following findings were reported:
- Wings spars,
- Overload failure,
- Separation in flight,
- Wings separated.
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith 601) in La Grande: 3 killed

Date & Time: Apr 11, 1974 at 1340 LT
Operator:
Registration:
N7474S
Survivors:
No
Site:
Schedule:
Hailey - La Grande - Walla Walla
MSN:
61-0045-86
YOM:
1970
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
8884
Captain / Total hours on type:
244.00
Circumstances:
While descending to La Grande Airport, the crew encountered poor weather conditions. Flying at low altitude above mountainous terrain, the twin engine airplane struck power cables and crashed in flames on a mountain. The aircraft was destroyed and all three occupants were killed.
Probable cause:
The crew continued VFR flight into adverse weather conditions and failed to see and avoid power cables. The following factors were reported:
- Low ceiling and rain,
- High obstructions,
- Flying at low level below clouds in mountainous terrain.
Final Report:

Crash of a Consolidated PB4Y-2 Privateer in Diamond Lake

Date & Time: Jul 27, 1970 at 1415 LT
Registration:
N3191G
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Medford - Medford
MSN:
59754
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12707
Captain / Total hours on type:
14.00
Circumstances:
The crew was engaged in a firefighting mission and departed Medford Airport around noon. En route, three engines stopped and/or lost power and the crew lost control of the airplane that crashed into Diamond Lake. While the aircraft was damaged beyond repair, both crew members were injured.
Probable cause:
Double engine failure in flight caused by a fuel exhaustion. The following contributing factors were reported:
- Inadequate preflight preparation,
- Mismanagement of fuel,
- Fuel exhaustion,
- Jettisoned load,
- Failure of two or more engine,
- Aircraft came to rest in water,
- Complete power loss on three engines,
- No fuel gauges on aircraft.
Final Report:

Crash of a Beechcraft E18S near Baker: 7 killed

Date & Time: May 15, 1970 at 1233 LT
Type of aircraft:
Registration:
N3621B
Flight Type:
Survivors:
No
Schedule:
San Jose - Baker - Oxbow
MSN:
BA-17
YOM:
1954
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
12500
Circumstances:
While approaching Baker on a flight from San jose, both engines stopped simultaneously. The pilot lost control of the airplane that stalled, struck trees and crashed few miles from Baker. The wreckage was found four days later, on May 19. The aircraft was destroyed and all seven occupants have been killed.
Probable cause:
Powerplant failure for undetermined reasons. The following findings were reported:
- High density altitude (8,100 feet),
- Complete failure of both engines,
- Heavy aircraft.
Final Report:

Crash of a Rockwell Aero Commander 500B near Imnaha: 1 killed

Date & Time: Dec 18, 1968 at 0254 LT
Operator:
Registration:
N5080
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
500-1537
YOM:
1965
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5000
Captain / Total hours on type:
120.00
Circumstances:
While on a night mail flight, the pilot encountered poor weather conditions when both engines stopped simultaneously. The pilot attempted an emergency landing when control was lost and the airplane crashed on a 40° slope mountain. SAR operations were conducted but eventually suspended few days later as no trace of the aircraft nor the pilot was found. Mountaineers found the wreckage on March 21, 1969 near Imnaha.
Probable cause:
The probable cause of the accident was the combination of the following factors:
- Inadequate preflight preparation on part of the pilot,
- Fuel system; vents, drains, tank caps improperly secured,
- Fuel exhaustion,
- Complete failure of both engines in flight,
- Fuel siphoned from loose cap.
Final Report:

Crash of a Fairchild F27A in Klamath Falls: 4 killed

Date & Time: Mar 10, 1967 at 0503 LT
Type of aircraft:
Operator:
Registration:
N2712
Flight Phase:
Survivors:
No
Schedule:
Klamath Falls – Medford – North Bend – Portland – Seattle
MSN:
73
YOM:
1960
Flight number:
WC720
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
9271
Captain / Total hours on type:
4684.00
Copilot / Total flying hours:
1064
Copilot / Total hours on type:
258
Aircraft flight hours:
16202
Circumstances:
Fairchild F-27 N2712 operated on a flight from Klamath Falls to Seattle via Medford, North Bend and Portland. Because snow was falling at Klamath Falls, the aircraft was loaded in the hangar instead of on the ramp. There was some delay in pushing out the aircraft onto the ramp because the tow tractor lost traction in the snow. The aircraft was exposed to the falling snow for about 11 minutes before the plane was able to taxy out to runway 14. A few minutes later, at 05:01 the aircraft took off. During the takeoff roll, after rolling about 1000 feet, the aircraft gradually served to the left. The nose wheel left the ground 600 feet prior to the main gear at a point where the track was half way between the center of the runway and the left row of runway lights. The left main gear was about 12 feet off the left edge of the runway for a distance of 250 feet prior to lift-off. Just after lift-off the aircraft swerved sharply to the right and immediately back to the left. On climb out the aircraft tended to the left, despite several course corrections. After reaching 5250 feet, the altitude dropped again to 4700 feet. The aircraft continued to climb until it crashed on a steep ridge on the northwest slope of Stukel Mountain at an elevation of 5049 feet (1539 m). The F-27 was in a right wing low attitude when this wing contacted the mountain; the aircraft then cartwheeled up the 30° up slope of the mountain. The aircraft was destroyed and all four occupants were killed.
Probable cause:
Loss of control due to ice accretion on airframe surfaces. The Board further determines that the pilot should have required that deicing fluid be applied to the aircraft to remove the accumulation of ice and snow prior to takeoff. This had not been done by the appropriate maintenance personnel.
Final Report:

Crash of a Douglas DC-9-14 near Wemme: 18 killed

Date & Time: Oct 1, 1966 at 2010 LT
Type of aircraft:
Operator:
Registration:
N9101
Survivors:
No
Site:
Schedule:
San Francisco – Eugene – Portland – Seattle
MSN:
45794/52
YOM:
1966
Flight number:
WC956
Location:
Crew on board:
5
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
18
Captain / Total flying hours:
18998
Captain / Total hours on type:
17.00
Copilot / Total flying hours:
9545
Copilot / Total hours on type:
9
Aircraft flight hours:
164
Circumstances:
West Coast Flight 956 departed San Francisco (SFO) at 18:44 for a flight to Eugene (EUG), Portland (PDX) and Seattle (SEA). The brand new DC-9 aircraft, which had been delivered to West Coast Airlines just 2 weeks earlier, arrived at Eugene at 19:34 and took off again 18 minutes later. At 20:04 the crew were cleared to descend from the cruising altitude of FL140 to 9000 feet. While turning to heading 300°, the aircraft descended below the clearance altitude and impacted the wooded eastern slope of Salmon Mountain at the 3830 feet level. The aircraft attitude was 30° right bank, in a 3-4° climbing flight path on a heading of 265°. The aircraft disintegrated on impact and all 18 occupants were killed.
Probable cause:
The descent of the aircraft below its clearance limit and below that of surrounding obstructing terrain, but the Board had been unable to determine the cause of such descent.
Final Report:

Crash of a Consolidated PBY-5A Catalina in Klamath Falls: 2 killed

Date & Time: Oct 4, 1965 at 1353 LT
Type of aircraft:
Registration:
N6455C
Flight Phase:
Flight Type:
Survivors:
No
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
6280
Captain / Total hours on type:
200.00
Aircraft flight hours:
1807
Circumstances:
The crew was engaged in a fire-fighting mission in the region of Klamath Falls. While flying at low height in strong wind conditions, one of the engine failed. The crew was unable to maintain a safe altitude nor the good track when the airplane struck tree tops and crashed in flames in a wooded area. Both pilots were killed.
Probable cause:
Failure of one engine caused by a master rod bearing failure. Improper in-flight decisions on part of the crew and unfavorable wind conditions (up to 60 mph at the time of the accident) were considered as contributing factors.
Final Report:

Crash of a Boeing B-52D-75-DO Stratofortress near Burns: 5 killed

Date & Time: Jun 23, 1959 at 1200 LT
Type of aircraft:
Operator:
Registration:
56-0591
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Seattle - Seattle
MSN:
17274
YOM:
1956
Location:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
At 11:05 a.m. on Tuesday, June 23, 1959, Tommy’s Tigator took off from Boeing Field for an experimental low-level flight test. Five employees of the Boeing Airplane Company were on board the B-52D: Lewis E. Moore, commander/pilot; Joseph Q. Keller, copilot; Gerald G. Green, navigator; Charles K. McDaniel and Neil Johnson, flight-test engineers. The aircraft had been making test runs over Eastern Washington, Oregon, and Idaho since April 10, 1959, and was loaded with special electronic equipment for measuring stresses on the airframe and flight surfaces. The bomber was scheduled to fly at lower than 500 feet above the ground on an elliptical course from The Dalles, Oregon, to Malheur Lake, Burns, and back to Walla Walla, Washington, at near maximum speed of 638 miles-per-hour. At 11:30 a.m., Tommy’s Tigator radioed that it was over The Dalles and preparing to descend for the low-level test flight. No further reports were heard from the pilot after it passed the checkpoint. Leslie Heinz, a lineman for the Harney County Rural Electric Cooperative, was an eyewitness to the accident. He was working with a crew on power lines in a remote area approximately 35 miles west of Burns and three miles from the crash site. At about 12:00 noon, he spotted the B-52 flying southeast approximately 300 feet above the desert floor when it suddenly crashed. The aircraft disintegrated on impact and all five crew members were killed:
Crew:
Lewis E. Moore, pilot,
Joseph Quentin Keller, copilot,
Gerald G. Green, navigator,
Neil Johnson, flight engineer,
Charles Kenneth McDaniel, flight engineer.
Source: http://www.historylink.org/File/10063
Probable cause:
The investigation by Air Force and Boeing experts concluded the accident was caused by the catastrophic failure of the horizontal stabilizer (tail plane), affecting the B-52’s longitudinal stability. The plane was not designed for the excessive turbulence of high-speed, low-level flight and began to disintegrate. Minus the horizontal stabilizer, the nose of the plane pitched sharply upward and it stalled, struck a knoll and exploded. At an altitude of 500 feet, there was virtually no chance for the crew to escape.
Final Report:

Crash of a Boeing 307 Stratoliner near Madras

Date & Time: May 10, 1958
Type of aircraft:
Registration:
N75385
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
2002
YOM:
1940
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Parked since few months on a regional airport, the aircraft was recently purchased by a new owner who wanted to know the exact consumption of oil and fuel. A test flight was scheduled with two test pilots. To be able to perform a longer flight, additional fuel tanks were installed in the cabin. While cruising at a relative low altitude, the crew informed ATC that a fire erupted in the cabin and elected to make an emergency landing. The airplane crash landed in flames in a field located 15 miles from Madras and came to rest. While both pilots were able to evacuate with no injury, the aircraft was destroyed by fire.
Probable cause:
Additional fuel tanks were installed in the cabin to perform the test flight but it was determined that these fuels tanks were not sealed and were leaking. The technicians who installed the fuel tanks on board were aware of the fact that these tanks were leaking, but since they had not been able to find the source of the leaks, they decided to install them despite a major risk of fire. In flight, some fuel leaked from a tank and ignited while in contact with an incandescent element whose nature remains unknown. In such conditions, the crew was unable to continue the test flight and an emergency landing was therefore necessary.