Crash of a Douglas C-124A-DL Globemaster II at McChord AFB: 18 killed

Date & Time: May 24, 1961 at 0222 LT
Operator:
Registration:
51-0174
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
McChord - Lawton
MSN:
43508
Crew on board:
6
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
18
Circumstances:
The four engine aircraft christened 'Old Shakey' was involved in a flight from McChord AFB to Lawton, Oklahoma, carrying a truck, several jeeps, two trailers and soldiers from Fort Sill who had been taking part in Exercise Lava Plains at the Yakima Firing Center. After a night takeoff, while climbing to a height of 500 feet, the airplane went out of control and crashed in flames in a wooded area located two miles south of the airport. 18 people were killed while four others were injured. The aircraft was totally destroyed.
Crew:
Cpt Warren J. Fair, pilot, †
Cpt Alvin W. Hill, copilot, †
Sgt Robert Wayne Cummins, †
M/Sgt Arnold R. Neldens, †
M/Sgt Raymond E. Overby, †
S/Sgt Ernest T. Landrum,
A2c James M. Smallwood. †
Passengers:
Pvt James Aldrich,
M/Sgt Llewellyn Morris Chilson,
P1c Jimmie R. Hunter,
P1c C. L. Buchanan, †
P1c T. E. Pulliam, †
P1c D. F. Radcliff, †
P1c D. J. Smith, †
P1c O. M. Wellings, †
P1c David Hoskins, †
P1c R. R. Kubik, †
S4c W. M. Gordon, †
S4c W. T. Kelly, †
S4c Joseph Lee, †
Sgt A. G. Neria, †
Sgt Lawrence Harrison. †
Probable cause:
It was determined the accident was probably caused by a ruptured fuel line resulting in engine failure during takeoff. It was also confirmed that the total weight of the aircraft was below the MTOW at the time of the accident.

Crash of a De Havilland L-20A Beaver near Stehekin: 2 killed

Date & Time: Jan 12, 1959
Type of aircraft:
Operator:
Registration:
53-2806
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Ellensburg - McChord
MSN:
600
YOM:
1954
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
En route from Ellensburg to the McChord AFB, the aircraft crashed in unknown circumstances in a mountainous area covered by snow. As the aircraft failed to arrive at destination, SAR operations were conducted but eventually suspended few days later as no trace of the aircraft nor the crew was found. The following summer, walkers found the wreckage in an isolated area.
Crew:
Cpt Wade L. Shankle Jr.
Passenger:
John A. Ardussi.
Source & photos:
http://washingtonwreckchasing.blogspot.ch/2009_06_01_archive.html

Crash of a Douglas C-124C Globemaster II near Homer: 9 killed

Date & Time: Jan 11, 1959
Operator:
Registration:
50-0111
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
McChord – Kodiak
MSN:
43249
YOM:
1950
Location:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The crew was performing a flight from McChord AFB, Washington, to Kodiak, with a load of various goods for a total weight of 34,500 pounds. While approaching the Kenai Peninsula, the crew informed ATC about engine problems and elected to divert to Anchorage. Few minutes later, the captain reported he was unable to maintain a safe altitude when, at an altitude between 3,000 and 4,000 feet, the airplane struck the slope of a mountain located in the Petrof Glacier, about 26 miles southeast of Homer. The wreckage was found a day later and all nine occupants were killed.
Probable cause:
It was reported the aircraft suffered a double engine failure in flight for unknown reason.

Crash of a Fairchild C-123B-12-FA Provider near Payette: 19 killed

Date & Time: Oct 9, 1958 at 1825 LT
Type of aircraft:
Operator:
Registration:
55-4521
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Ogden-Hill - McChord
MSN:
20182
YOM:
1954
Location:
Crew on board:
5
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
19
Circumstances:
The crew was returning to his base in McChord after he took part to an airshow at Ogden-Hill AFB, supplying the Thunderbird's team. While flying in cruising altitude, the airplane went out of control, dove into the ground and crashed in a field located seven miles east of Payette. The airplane was totally destroyed upon impact and all 19 occupants were killed, among them two civilians.
Probable cause:
It is believed that the loss of control was the consequence of an in-flight collision with a flock of birds, maybe goose.

Crash of a Douglas SC-47A at McChord AFB: 3 killed

Date & Time: Apr 13, 1958
Operator:
Registration:
42-93183
Flight Type:
Survivors:
No
Schedule:
McChord - McChord
MSN:
13066
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Crashed in unknown circumstances at McChord AFB while completing touch-and-go maneuvers. All three crew members were killed, among them T/Sgt Roy Edwin Craft.

Crash of a Douglas C-124C Globemaster II off Elmendorf AFB

Date & Time: Jan 27, 1957 at 2015 LT
Operator:
Registration:
50-0088
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Elmendorf – McChord
MSN:
43226
YOM:
1950
Crew on board:
11
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Just after liftoff from Elmendorf AFB, while in initial climb, the crew informed ground about an engine failure and elected to return. The captain realized it could not make it so he ditched the aircraft in the icy Cook Inlet. The airplane came to rest and was damaged beyond repair while all 12 occupants were rescued.
Probable cause:
Engine failure after takeoff.

Crash of a Lockheed L-1049 Super Constellation in McChord AFB

Date & Time: Sep 6, 1953 at 0231 LT
Operator:
Registration:
N6214C
Survivors:
Yes
Schedule:
Seattle – Chicago
MSN:
4014
YOM:
1952
Flight number:
NW008
Crew on board:
6
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10863
Captain / Total hours on type:
263.00
Copilot / Total flying hours:
4230
Copilot / Total hours on type:
206
Aircraft flight hours:
4509
Circumstances:
Northwest Airlines' Flight 8 departed Seattle-Tacoma Airport at 0148, September 6, 1953, for a nonstop flight to Chicago, Illinois. Gross weight on takeoff was 105,839 pounds; maximum allowable for takeoff was 116,740; maximum allowable for landing was 98.500 pounds. The location of the center of gravity was within prescribed limits. Weather at Seattle-Tacoma Airport during takeoff was: ceiling 200 feet and one-fourth mile visibility. Just after the aircraft became airborne No. 3 propeller oversped. Attempts by the flight engineer to correct this condition were unsuccessful and feathering was started one and one-half minutes later. However, the propeller continued to rotate at about 400 r.p.m. The flight's takeoff alternate was Yakima, Washington (a distance of 122 miles), but due to high terrain en route the captain elected to request clearance to proceed to Portland, Oregon (a distance of 132 miles), at 5,000 feet. This clearance was granted immediately. Using METO 2 power the aircraft reached 5,000 feet, well above the overcast, about 14 minutes after takeoff. Near the end of this climb the oil temperature of No. 4 engine was exceeding limits and the oil supply was being rapidly reduced. The flight engineer attempted to lower the temperature by fully opening the oil cooler flap. Temperature, however, remained high and the oil quantity continued to dwindle fast. Accordingly, the No. 4 propeller was feathered at about 0205 at the order of the captain who then declared an emergency and elected to land at McChord Air Force Base. Radio communication was established with McChord and arrangements made for a GCA approach after a short delay in establishing a frequency. No. 3 propeller had not feathered fully and was still windmilling at approximately 400 r.p.m. Meanwhile the captain had requested "takeoff" flaps, but the flaps would not extend hydraulically, and the copilot went to the cabin to crank them down. He stated that he turned the crank about 15-20 turns, at which point he found that it would no longer turn freely, whereupon he backed it to its original position. He was then called back to the cockpit to assist the captain in controlling the aircraft. Control difficulty had been continuously experienced with the aircraft yawing sharply and dropping a wing. The captain had placed the trim controls approximately in neutral, believing that he had a better feel and control of the aircraft without them at the recommended minimum speed of 130 knots. The aircraft, which had re-entered the overcast at about 2,000 feet, was then several miles from McChord Field under GCA direction on its first approach when its position and heading became such that the GCA operator directed a box pattern be flown to establish a proper approach. The second approach was executed in accordance with the directed pattern and the final approach was in line with Runway 34. The landing gear control was not actuated for gear extension until the aircraft broke out of the overcast at an altitude estimated at between 500 and 800 feet on a GCA controlled straight-in approach to Runway 34. At this time the captain ordered that No. 3 be unfeathered but it would not unfeather and continued to windmill. Only the right main gear extended fully and locked, as Indicated by its green light, but the landing was then committed. Shortly after touchdown retraction of the unlocked nose and left main gears allowed the aircraft to veer off the runway to the left. It then skidded sideways to its right, folding the right main gear inward, and the No. 2 engine was torn free. The aircraft came to rest on a heading of 212 degrees some 3,000 feet from the point of touch and about 7,000 feet short of the far end of the 10,000-foot runway. At about that time a gasoline fire started and spread rapidly over the ground below the airplane. Previously alerted fire apparatus, already standing by, kept the fire from spreading while all passengers and four of the crew left quickly by the main cabin door, the door sill being five or six feet above the ground. The flight engineer and the captain left by the cockpit crew door after ascertaining the cabin to be empty. All 32 occupants ware clear within an estimated two minutes. There were no fatalities although several persons were treated for burns at the McChord Air Force Base Hospital.
Probable cause:
The Board determines that the probable cause of this accident was a sequence of mechanical failures resulting in an emergency landing under adverse weather conditions with insufficient hydraulic pressure in the secondary system to extend fully the landing gear in the time available. A contributing factor was the design of the hydraulic system which did not permit use of the available pressure in the primary system for that purpose. The following findings were pointed out:
- Shortly after takeoff the aircraft lost the use of No. 3 engine due to an overspeeding propeller, and continued windmilling,
- Weather conditions at Seattle-Tacoma were satisfactory for takeoff but were below landing minimums and the captain elected to proceed to Portland,
- After reaching cruising altitude No. 4 propeller was feathered because of high engine oil temperature and depletion of oil supply,
- After losing the use of No. 4 engine, the captain declared an emergency and set up a GCA approach to McChord Air Force Base,
- A malfunction of the landing gear selector valve prevented normal use of the diminished hydraulic pressure to extend the flaps,
- A GCA instrument approach to McChord was necessary because of weather conditions. The captain decided that he would extend the gear only after breaking out under the low overcast,
- The short time interval between breaking out and touchdown was insufficient for extension and locking of all three landing gears with the existing hydraulic pressure,
- After touchdown the unlocked and partially extended left main and nose gears were forced up into their wheel wells with complete loss of control of the aircraft's ground movement, and fire occurred after rupture of the fuel tanks,
- The functional failure of No. 3 propeller governor was due to foreign metallic particles,
- The reason for the loss of oil supply for No. 4 engine was undetermined,
- The landing gear selector valve was improperly seated, resulting in insufficient hydraulic pressure.
Final Report:

Crash of a Douglas C-49K near Vail: 21 killed

Date & Time: Sep 1, 1953 at 1830 LT
Type of aircraft:
Operator:
Registration:
N19941
Flight Phase:
Survivors:
No
Site:
Schedule:
Fort Ord - McChord
MSN:
6333
YOM:
1942
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
21
Captain / Total flying hours:
3935
Captain / Total hours on type:
1000.00
Copilot / Total flying hours:
2085
Copilot / Total hours on type:
500
Aircraft flight hours:
8398
Circumstances:
The aircraft was performing a special flight from Fort Ord AFB (Monterey) to McChord AFB, carrying 19 military passengers and two pilots. En route, the crew cancelled the IFR flight plan and continued under VFR in poor weather conditions. At an altitude of 2,600 feet in foggy conditions, the aircraft hit the slope of a mountain, was totally destroyed by impact forces and a post crash fire and all 21 occupants were killed.
Probable cause:
The Board finds that the probable cause of this accident was the pilot’s attempt to continue flight under the provisions of Visual Flight Rules during instrument conditions. The following findings were pointed out:
- All ground radio facilities were functioning normally,
- An instrument flight plan had been cancelled and the flight was proceeding in accordance with visual flight rules,
- The crash occurred during daylight on a fog-covered hillside at an altitude of about 2,600 feet MSL,
- The crash site was on the airway and the direction of impact was near the on-course heading.
Final Report:

Crash of a Douglas C-54G Skymaster in McChord AFB: 37 killed

Date & Time: Nov 28, 1952 at 0048 LT
Type of aircraft:
Operator:
Flight Type:
Survivors:
Yes
Schedule:
Fort Wainwright – McChord
Crew on board:
7
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
37
Circumstances:
The C-54G, assigned to the Military Air Transport Service (MATS), 1701st Air Transport Wing at Malmstrom Air Force Base (AFB), Great Falls, Montana, was inbound from Ladd AFB, Fairbanks, Alaska, carrying 32 American servicemen and their dependents, and a crew of seven. At 0030LT, the pilot, Captain Albert J. Fenton, radioed the McChord air traffic control tower for field conditions and was informed that visibility was approximately three-quarters of a mile. Captain Fenton was directed to execute a wide left-hand turn and descend for a ground-controlled landing from the south. As the aircraft neared the field, a thick fog bank, rising 300 feet high, suddenly developed, reducing visibility to near zero. At 0048LT, Captain Fenton, now on final approach, decided to abort the landing and radioed the control tower that he was proceeding to Malmstrom AFB instead. Minutes later, witnesses telephoned the control tower and the Pierce County Sheriff’s Department to report a downed aircraft. The Skymaster crashed into an open field (now Wards Lake Park) approximately one mile north of McChord AFB and one-half mile east of S Tacoma Way between S 84th and S 88th Streets in the unincorporated community of Lakewood. It barely missed the Edgewood Park apartments, 35 four-family units built to ease the military’s housing shortage during the Korean War (1950-1953), and other nearby homes. Several people who saw the accident said the Skymaster was on fire before it crashed. Upon impact, the aircraft broke in two and exploded into flames. Bodies, personal belongings, packages and luggage were scattered around the crash scene for 200 yards. Most of the fire was in the forward section of the fuselage, the tail and aft section remaining almost intact. Some witnesses said they could hear the cries of people caught in the burning wreckage, but were helpless to render assistance. Meanwhile, fire and rescue teams from McChord AFB, Lakewood, and Tacoma rushed to the crash site and extinguished the fires in the fuselage and scattered debris. Using magnesium flares and flashlights, police and sheriff’s officers, firemen, and military personnel searched the smoldering, twisted wreckage, looking for victims. Of the 39 people aboard the C-54G, they found only three survivors: Airman Bobby R. Wilson, age 20, a member of the plane’s crew, Airman Curtis Redd, age 23, and Joseph M. Iacovitti, age 8, both passengers. Wilson, who had third-degree burns, internal injuries, and multiple skull fractures, died at Pierce County Hospital on Saturday, November 29. Redd was taken to St. Joseph Hospital in Tacoma in critical conditions with third-degree burns, but survived. Iacovitti was taken to Pierce County Hospital in serious condition with burns, broken legs and a fractured neck. He lived through the ordeal, but his parents, two brothers, and a sister died in the mishap, leaving him an orphan and the only surviving member of his family. Three other families were wiped out entirely.
Crew:
Benedict, John H., 20, Airman Second Class
Bentley, Patricia, 24, Airman Third Class
Bokinsky, Joseph H., 24, Staff Sergeant
Childers, Wilber C., 21, Airman Second Class
Fenton, Albert J., 29, Captain, pilot
Harvey, James D., 27, First Lieutenant, copilot
Wilson, Bobby R., 20, Airman Third Class.
Passengers:
U.S. Army:
Coons, Robert F., 22, Corporal
Galloway, Calvin, 18, Private First Class
Hockenberry, Denny L., 22, Sergeant
Hockenberry, Elda M., 21, spouse
Hockenberry, Susan E., 2, daughter
Hockenberry, Denise M., 1, daughter
Lebonitte, Joseph T., 23, Private First Class
Zeravich,Christoph, 24, Corporal
U.S. Air Force
Alsbury, Jack R., 21, Airman Third Class
Cook, Robert H., 20, Airman First Class
Farley, Donna L., 20, (spouse of Farley, Glen D., Staff Sergeant)
Iacovitti, Anthony R., First Lieutenant
Iacovitti, Dorothy E., 31, spouse
Iacovitti, Anthony F., 6, son
Iacovitti, John A., 4, son
Iacovitti, Barbara, 2, daughter
Johnson, Dwight P., 23, Airman Second Class
Morris, George E., 33, Master Sergeant
Morris, Anna D., 28, spouse
Morris, George E., Jr., 3, son
Morris, Geraldine A., 5, daughter
Niemi, Edwin, 35, Staff Sergeant
Parlett, Frederick D., 18, Basic Airman
Pickerel, Robert L., 22, Airman First Class
Smith, Raymond D., 24, Staff Sergeant
Swang, Marion E., 41, Major [incorrectly listed as Swann]
Weikum, Elmer, 23, Airman Second Class
Wells, Samuel R., 35, Master Sergeant
Wells, Margaret A., 33, spouse
Wells, Samuel R. III, 3, son
Survivors
Iacovitti, Joseph M., 8, (son of Dorothy and Anthony Iacovitti)
Redd, Curtis, 23, Airman Second Class.
Source:
http://www.koreanwar-educator.org/topics/airplane_crashes/c54_tacoma_19521128/p_c54_tacoma_11_28_52.htm
Probable cause:
An Air Force crash-probe team, commanded by Brigadier General Richard J. O’Keefe, was immediately dispatched from Norton AFB, San Bernardino, California, to begin sifting through the wreckage for clues to the accident. They wanted to determine why the aircraft was so low as to clip the tops of two fir trees before crashing. One of the aircraft’s four propellers was found 100 yards from the wreckage, sitting upright in the field. The condition of the blades indicated the propeller had stopped turning before it hit the ground. Twelve witnesses, who saw the Skymaster just prior to the crash, said the right wing or an engine was on fire. Captain Fenton had been in constant radio contact with the tower until the final moment, but never reported a mechanical difficulty or fire. Just before announcing his decision to fly to Malstrom AFB, the pilot inquired about weather at the Seattle-Tacoma International Airport and was told conditions were clear. The Air Force Board of Inquiry determined that as Captain Fenton was on final approach to land at McChord AFB, he boosted power to regain altitude, but the Skymaster’s number three engine failed. In the thick fog, the pilot was unable to see, much less avoid, a line of towering fir trees immediately north of the base. The aircraft sheared off the tops of two 100-foot tall Douglas firs, slammed into an open field and exploded into flames.

Crash of a Douglas C-124A-DL Globemaster II on Mt Gannett: 52 killed

Date & Time: Nov 22, 1952 at 2015 LT
Operator:
Registration:
51-0107
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
McChord – Elmendorf
MSN:
43441
YOM:
1951
Crew on board:
11
Crew fatalities:
Pax on board:
41
Pax fatalities:
Other fatalities:
Total fatalities:
52
Circumstances:
The four engine aircraft was completing a flight from McChord AFB to Elmendorf AFB, carrying 41 passengers and a crew of 11. En route, the crew was informed about strong winds gusting up to 40 knots from the west. While cruising by night and marginal weather conditions, the aircraft hit the slope of Mt Gannett (9'650 feet high) located about 53 miles east of Elmendorf. As the airplane failed to arrive, SAR operations were conducted but due to poor weather conditions, first rescuers arrived on scene six days later only, on November 28. The wreckage was found on the Surprise Glacier, about 1,000 feet below the summit. The aircraft disintegrated on impact and all 52 occupants were killed. On June 9, 2012, some debris were found and on June 28, 2012, the wreckage was spotted again. Two years later, on June 18, 2014, the remains of 17 of the victims were identified and returned to their respectives families for burial.
Probable cause:
It was determined that the information transmitted to the crew regarding the wind component was erroneous as the wind was gusting up to 80 knots at the time of the accident, causing the aircraft to drift off from the prescribed flight path. The crew was unable to establish his real position due to the low visibility caused by night and fog and the absence of ground reference points. It is believed the accident was the result of a controlled flight into terrain.