Category Archives: Aviation

28 December 1978

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United Airlines’ McDonnell Douglas DC-8-61, N8082U, photographed at New York–JFK, 3 January 1978. (© Howard Chaloner. Image used with permission.)

28 December 1978: United Airlines Flight 173, A McDonnell Douglas DC-8, N8082U, departed Stapleton International Airport (DEN), Denver, Colorado, enroute to Portland International Airport (PDX), Portland, Oregon. Under the command of Captain Malburn Adair McBroom, the airliner carried 181 passengers and 8 crew members. The planned duration of the flight was 2 hours, 26 minutes. The DC-8 carried 46,700 pounds (21,183 kilograms) of jet fuel, sufficient for the flight plus an additional 1 hour, 5 minutes fuel for the required 45-minute reserve and any contingencies.

On approach to Portland, the crew lowered the DC-8’s landing gear and flaps. They felt a heavy thump followed by a vibration and the airplane yawing. The indicator light showing that the main gear was down and locked did not illuminate.

Concerned that there was a problem with the landing gear, Captain McBroom aborted the landing and put the airliner in a holding pattern south of the airport. For approximately one hour, Captain McBroom, First Officer Roderick Duane Beebe, and Flight Engineer Forrest Ervin Mendenhall attempted to determine the nature of the problem. Finally, though the situation was not resolved, the crew turned toward Portland and prepared for an emergency landing.

At 18:06:46, the flight engineer reported, “We’re going to lose an engine,” and three seconds later, said, “We’re losing an engine.” The captain asked “Why?” The first officer responded, “Fuel.” The captain again asked “Why?”

At 18:07:06, Flight Engineer Mendenhall reported that the engine had “flamed out” (stopped running due to fuel exhaustion). Captain McBroom called Portland Approach Control and requested an immediate clearance to land at PDX, “now.” The airliner was then 18 miles south of the airport. McBroom asked Mendenhall to reset the landing gear circuit breakers. “See if we get gear lights.”

At 18:13:21, Mendenhall said, “We just lost two engines, guys.” Four seconds later, he said, “We just lost two engines—one and two.” [Both engines on the left wing.] McBroom said, “They’re all going,” and told First Officer Beebe to declare an emergency.

At 18:13:50, Beebe called, “Portland Tower, United One-Seventy-Three Heavy, mayday. We’re—The engines are flaming out. We’re going down. We’re not able to make the airport.” There were no further transmissions.

At approximately 18:15, United Flight 173 crashed in a residential area, about 6 nautical miles (11 kilometers) southeast of Portland International Airport. Eight passengers were killed, along with Flight Engineer Mendenhall and Senior Flight Attendant Joan Newton Wheeler. Another 23 persons were seriously injured. Two unoccupied homes were destroyed.

The scene of the crash of Flight 173. The airliner came to rest just north of E. Burnside Street, and east of NE 157th Avenue. (Multnomah County Sheriff’s Office)

The National Transportation Safety Board (NTSB) investigation found:

3.2 Probable Cause

     The National Transportation Safety Board determined that the probable cause of the accident was the failure of the captain to monitor properly the aircraft’s fuel state and to properly respond to the low fuel state and the crew-members’ advisories regarding fuel state. This resulted in fuel exhaustion to all engines. His inattention resulted from preoccupation with a landing gear malfunction and preparations for a landing emergency.

     Contributing to the accident was the failure of the other two flight crewmembers either to fully comprehend the criticality of the fuel state or to successfully communicate their concern to the captain.

—NATIONAL TRANSPORTATION SAFETY BOARD AIRCRAFT ACCIDENT REPORT NTSB-AAR-79-7 , 7 June 1979, at Page 29

United Airlines Flight 173 crashed in a wooded area, southeast of PDX.

When the landing gear was lowered, a gear retraction cylinder failed, allowing the right main gear to fall into place. It locked, but a microswitch which should have activated the landing gear indicator light was damaged.

United Airlines’ operations manual required that the crew have the control tower make a visual check that the gear was down. Though it could not confirm that the gear was locked, if the visual check indicaated that landing gear appeared to be down, a landing was authorized. Captain McBroom deviated from this procedure.

The airliner was a McDonnell Douglas DC-8-61, serial number 45972, which had been delivered to United Airlines on 22 May 1968. At the time of the accident, it had flown a total of 33,114:33 hours.

A United Airlines Douglas DC-8-61, the same type as the accident aircraft. (Jon Proctor)

The DC-8-61 is a four-engine turbojet-powered airliner with swept wings. It was a “stretched” variant of the basic DC-8 design, capable of carrying a maximum of 259 passengers. A 240 inch (6.096 meters) “plug” was installed forward of the wings and a 200 inch (5.08 meters) plug aft. This gave the airliner a total length of 187.4 feet (57.12 meters), with a wingspan of 142.4 feet (43.40 meters) and maximum height of 43 feet, 5.2 inches (13.239 meters). N8082 had a zero fuel weight of 201,927 pounds (91,592.6 kilograms), and a maximum certified takeoff weight (MTOW) of 325,000 pounds (147,418 kilograms). The maximum usable fuel was 23,393 U.S. gallons (88,552 liters).

The DC-8-61 was powered by four Pratt & Whitney Turbo Wasp JT3D-3B engines. This engine was a civil variant of the military TF33 series. The JT3D-7 was a two-spool axial-flow turbojet engine with a 2-stage fan, 14-stage compressor (7 intermediate-, 7 high-pressure stages) and 4-stage turbine (1 high- and 3 low-pressure stages). The JT3D-3B had a maximum power rating of 18,000 pounds of thrust. The engine was 145.5 inches (3.696 meters) long, 53 inches (1.346 meters) in diameter, and weighed 4,340 pounds (1,969 kilograms).

The DC-8-61 had a cruise speed of 0.82 Mach, and a maximum range of 3,200 nautical miles (5,926 kilometers). During a test flight at Edwards Air Force Base, 21 August 1961, a Douglas DC-8-43, N9604Z, reached Mach 1.1012.

© 2020, Bryan R. Swopes

2 December–28 December 1955

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De Havilland DH.106 Comet 3 G-ANLO ay the Farnborough air show, September 1954. (RuthAS via Wikipedia)
De Havilland DH.106 Comet 3 G-ANLO at the Farnborough Airshow, September 1954. (RuthAS via Wikipedia)

2 December 1955: The prototype de Havilland DH-106 Comet 3, G-ANLO, departed Hatfield Aerodrome, Hertfordshire, England, with Chief Test Pilot John Cunningham and Per Buggé in the cockpit. R.W. Chandler was the navigator/radio operator. Other crew members included Chief Flight Engineer E. Brackstone Brown, and flight engineers R.V. Ablett and J. Hamilton.

Several de Havilland executives and engineers were among the passengers. Captain A.P.W. Cane of British Overseas Airways Corporation and Captain I.D.V. Ralfe of Qantas were aboard to observe to new airliner in operation.

De Havilland DH.106 Comet 3 G-ANLO was delayed by heavy fog at Hatfield, 2 December 1955. (De Havilland)
De Havilland DH.106 Comet 3 G-ANLO was delayed by heavy fog at Hatfield, 2 December 1955. (De Havilland)

Departure had been scheduled for 5:30 a.m., local time, but heavy fog delayed the flight. 5 hours, 3 minutes later, the Comet 3 landed at Cairo, Egypt, after flying 2,076 nautical miles (2,389 statute miles, 3,845 kilometers). Rather than continuing on as had originally been planned, the crew remained over night at Cairo.

G-ANLO left Cairo the following morning and with refueling stops at Bombay, Maharashtra India; Singapore, Colony of Singapore; and Darwin, Northern Territory, Australia; the airliner arrived at Sydney, New South Wales, Australia, on 4 December, after a total of 19 hours, 5 minutes of flight. The distance traveled was 8,728 nautical miles (10,044 statute miles, 16,164 kilometers). During the Singapore-Darwin leg, the Comet 3 cruised at 44,000 feet (13,411 meters). More than 20,000 people were waiting at Sydney Kingsford Smith Airport to see the new jetliner arrive.

De Havilland DH-106 Comet 3 G-ANLO arrived at Sydney, New South Wales, Australia, 4 December 1955. (Unattributed)
De Havilland DH-106 Comet 3 G-ANLO arrived at Sydney, New South Wales, Australia, 4 December 1955. (Unattributed)

Group Captain Cunningham made demonstration flights from Sydney to Melbourne, Canberra and Perth.

G-ANLO then continued to Auckland, New Zealand, flying the 1,166 nautical miles (1,342 miles, 2,159 kilometers) in 2 hours, 43 minutes. From Auckland to Nadi Airport, Fiji, 1,153 nautical miles (1,326 miles, 2,135 kilometers), took 2 hours, 52 minutes.

The next leg of the around the world tour, Fiji to Honolulu, in the Hawaiian Islands, was completed on 13 December. The Comet 3 covered the 2,791 nautical miles (3,212 statute miles, 5,169 kilometers) in 6 hours, 44 minutes. G-ANLO remained at Honolulu for the next two days.

DH.106 Comet 3 G-ANLO is decorated with a flower lei on its arrival at Honolulu International Airport, 13 December 1955. (Zoggavia)
DH.106 Comet 3 G-ANLO is decorated with a flower lei on its arrival at Honolulu International Airport, 13 December 1955. (Zoggavia)

On 15 December, the Comet 3 left Honolulu for Vancouver, British Columbia, Canada, 2,408 nautical miles (2,771 statute miles, 4,460 kilometers). The duration of this flight was 5 hours, 40 minutes. The Comet 3 flew across Canada to Toronto, Ontario, 1,898 nautical miles (2,184 statute miles, 3,515 kilometers) in 3 hours, 56 minutes, then on to Montreal, Quebec, arriving there on 20 December.

The final leg of the flight, Montreal to London Heathrow Airport, 2,907 nautical miles (3,345 statute miles, 5,384 kilometers) was completed in 6 hours, 9 minutes, on 27 December 1955.

This was the first around-the-world flight by a jet-powered aircraft. The total distance flown by the Comet 3 was 24,324 nautical miles (27,991.6 statute miles/45,048.1 kilometers) The total flight time was 56 hours, 17 minutes.

For this flight Group Captain Cunningham was awarded the Harmon Trophy, which was presented by President Dwight D. Eisenhower, 23 October 1956.

The de Havilland DH.106 Comet 3 was a further development of the Comet 2 series. It was 15 feet (4.572 meters) longer with a length of 111 feet, 6 inches (33.985 meters), a wingspan of 115 feet (35.052 meters) and overall height of 29 feet, 6 inches (8.992. The area of the wings and tail surfaces had been increased. It was powered by four Rolls Royce Avon 521 turbojet engines, rated at 10,000 pounds of thrust (44.48 kilonewtons), each.

De Havilland DH.106 Comet 3 G-ANLO, left quarter, at Entebbe Airport, Uganda, 1955. (Dphne Seager)
De Havilland DH.106 Comet 3 G-ANLO, left quarter, at Entebbe Airport, Uganda, 1955. (Daphne Seager)

The airliner was designed to carry 58–76 passengers on flights ranging to 2,600 miles (4,184 kilometers). In addition to the increased length, visual differences from the previous Comets were the circular passenger windows, and wing tanks extending forward from the wings’ leading edges.

Only two Comet 3s were built and one was used as a static test article. Production continued with the Comet 4, which had even greater improvements. G-ANLO remained a development prototype and was modified several times. In 1958 the wings were shortened and the external wing tanks removed. The airplane was redesignated Comet 3B. It was turned over to the Ministry of Supply and re-registered XP915, 20 June 1961. The airplane was used in instrument landing tests and later converted to a mockup of the Hawker Siddeley Nimrod MR1 maritime patrol aircraft. It was taken out of service in 1966 and scrapped.

Group Captain John Cunningham, Royal Air Force. (Daily Mail)
Group Captain John Cunningham, Royal Air Force. (Daily Mail)

Group Captain John Cunningham C.B.E., D.S.O. and Two Bars, D.F.C. and Bar, A.E., was born 1917 and educated at Croydon. In 1935 he became an apprentice at De Havilland’s and also joined the Auxiliary Air Force, where he trained as a pilot. Cunningham was called to active duty in August 1939, just before World War II began.

Promoted to Group Captain in 1944, Cunningham was the highest scoring Royal Air Force night fighter pilot of World War II, credited with shooting down 20 enemy airplanes. He was responsible for the myth that eating carrots would improve night vision.

Following the War, John Cunningham returned to de Havilland as a test pilot. Following the death of Geoffrey Raoul de Havilland, Jr., in 1946, Cunningham became the de Havilland’s chief test pilot. He remained with the firm through a series of mergers, finally retiring in 1980.

He set a Fédération Aéronautique Internationale (FAI) world speed and altitude record with the company’s DH.100 Vampire jet fighter, TG278: 799.644 kilometers per hour (496.876 miles per hour) over a 100 kilometer course at Lympne Airport, 31 August 1947.¹ He flew the DH.100 to 18,119 meters (59,446 feet) over Hatfield Aerodrome, 23 March 1948.² On 24 April 1950, Cunningham flew a DH.106 Comet Mk.I from London to Cairo at an average speed of 686.56 kilometers per hour (426.61 miles per hour), setting a world record for speed over a recognized course.³

Group Captain Cunningham died 21 July 2002 at the age of 84 years.

Per Olivarius Buggé (also known as Peter Bugge) was born at Kristiansund, Norway in 1918. He joined the Royal Norwegian Air Force in 1938. After Germany invaded the country, Buggé escaped to Sweden, April 1940, and in February 1941 arrived in Great Britain. He served with the Royal Air Force for the remainder of the War, flying Bristol Beaufighters and de Havilland Mosquitos with No. 604 Squadron and No. 85 Squadron (while it was under the command of Squadron Leader John Cunningham).

After the War Buggé flew for British Overseas Airways Corporation and Swedish Airlines. In 1949, he joined de Havilland as a test pilot, and stayed with the company after it was absorbed by Hawker Siddeley. He died in 1998.

John Cunningham (left) and Per Bugge in the cockpit of a DH.106 Comet. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
John Cunningham (left) and Per Buggé in the cockpit of a DH.106 Comet. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

¹ FAI record file number 8884

² FAI record file number 9844

³ FAI record file number 6378

© 2017, Bryan R. Swopes

John Leonard Swigert, Jr. (30 August 1931–27 December 1982)

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John L. Swigert, Jr., Astronaut
John L. Swigert, Jr., Astronaut, Command Module Pilot, Apollo XIII. (NASA)

John L. “Jack” Swigert, Jr., was born at Denver, Colorado, 30 August 1931, the first of three children of John Leonard Swigert, a physician, and Virginia Seep Swigert. Interested in aviation from an early age, he was a licensed Private Pilot at age 16. He graduated from Denver’s East High School in 1949.

Jack Swigert, 1952.

Jack Swigert attended the University of Colorado in Boulder, Colorado. He was a member of the Air Force Reserve Officers Training Corps (AFROTC), played on the varsity football team, and was a member of the C Club. He graduated in 1953 with a Bachelor’s Degree in Mechanical Engineering. Following his graduation, Swigert was commissioned as a second lieutenant, United States Air Force Reserve.

Lieutenant Swigert flew fighters from bases in Japan and Korea, then after completing his active duty requirement, 2 October 1956, he  transferred to the Air National Guard. He served with the Massachusetts ANG and Connecticut ANG.

Swigert earned a Master of Science degree in Aerospace Engineering from Rensselaer Polytechnic Institute, Troy, New York, in 1965, as well as a Master of Business Administration degree from the University of Hartford at Hartford, Connecticut.

Captain John L. Swigert, Jr., United States Air Force, F-100 Super Sabre pilot, 118th Fighter Squadron, Connecticut Air National Guard. (U.S. Air Force via Jet Pilot Overseas)
Captain John L. Swigert, Jr., United States Air Force, F-100A Super Sabre pilot, 118th Fighter Squadron, Connecticut Air National Guard. (U.S. Air Force via Jet Pilot Overseas)

While flying with the Air Guard, Swigert also worked for North American Aviation, Inc., as an engineering test pilot, and then for Pratt & Whitney.

He became one of 19 men selected as crewmembers of NASA’s Apollo Program 1965. He requested an assignment as pilot of the Apollo Command and Service Module.

Swigert was a member of the support team for the Apollo 7 mission, and was then selected as Command Module Pilot for the Apollo 13 backup crew, along with John Watts Young and Charles M. Duke, Jr.  When the primary crew CMP, Ken Mattingly, was thought to have been exposed to measles, he was withdrawn from Apollo 13 and Jack Swigert took his place in the primary crew.

Apollo 13 was planned as the third lunar landing mission. The circumstances of its flight are well known. When disaster struck, all three astronauts performed an amazing feat as they had to improvise their safe return to Earth.

Swigert left NASA in 1977 and entered politics. He was elected to the U.S. House of Representatives in 1982, representing the the 6th District of Colorado.

On the night of 27 December 1982, before he could be sworn into office, John Leonard Swigert, Jr., aerospace engineer, fighter pilot, test pilot, astronaut and congressman, died from complications of cancer.

John L. Swigert, Jr. Memorial, bronze sculpture by Mark and George Lundeen, in the National Statuary Hall Collection, United States Capitol. Gift of the State of Colorado, 1997. (Architect of the Capitol)
John L. Swigert, Jr. Memorial, bronze sculpture by Mark and George Lundeen, in the National Statuary Hall Collection, United States Capitol. Gift of the State of Colorado, 1997. (Architect of the Capitol)

© 2018, Bryan R. Swopes

27 December 1951

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The first prototype North American Aviation XFJ-2B Fury, Bu. No. 133756, lifts off the runway at Los Angeles International Airport, 27 December 1951. (north American Aviation)
The first prototype North American Aviation XFJ-2B Fury, Bu. No. 133756, lifts off the runway at Los Angeles International Airport, 27 December 1951. (San Diego Air and Space Museum Archive)
North American Aviation XFJ-2B Fury prototype Bu. No. 133756 climbs out after takeoff from Los Angeles International Airport, 27 December 1951. (San Diego Air and Space Museum Archive)
North American Aviation XFJ-2B Fury prototype Bu. No. 133756 climbs out after takeoff from Los Angeles International Airport, 27 December 1951. (San Diego Air and Space Museum Archive)

27 December 1951: The North American Aviation XFJ-2B Fury, Bu. No. 133756, made its first flight at Los Angeles International Airport with test pilot Robert Anderson Hoover at the controls.

The XFJ-2B was a prototype aircraft carrier-based fighter for the United States Navy and Marine Corps. It was modified from a standard production U.S. Air Force F-86E-10-NA Sabre day fighter. The primary difference was the substitution of four 20 mm Colt Mark 12 autocannon for the six .50-caliber Browning M-3 machine guns of the F-86E. 150 rounds per gun were carried. The aircraft was flown to the Naval Ordnance Test Station, Armitage Field, China Lake, California, for armament testing.

The second and third prototypes were unarmed but fitted with an arrestor hook, catapult points, folding wings and a lengthened nose gear strut to increase the fighter’s static angle of attack for takeoff and landings. These two prototypes were used for aircraft carrier trials.

Production FJ-2 Fury fighters were built at North American’s Columbus, Ohio plant, along with F-86F Sabres for the Air Force.

Prototype North American Aviation XFJ-2B Fury, Bu. No. 133756, in flight, eastbound, just southwest of the Palos Verdes Peninsula. Santa Monica Bay and the Santa Monica Mountains are in the background. (North American Aviation, Inc./Boeing)
Prototype North American Aviation XFJ-2B Fury Bu. No. 133756 in flight, eastbound, just southwest of the Palos Verdes Peninsula. Santa Monica Bay and the Santa Monica Mountains are in the background. (North American Aviation, Inc./Boeing)
North American Aviation test pilot Robert A. ("Bob") Hoover with XFJ-2 Fury, Bu. No. 133754, the second prototype. (North American Aviation, Inc.)
North American Aviation test pilot Robert A. (“Bob”) Hoover with XFJ-2 Fury Bu. No. 133754, the second prototype. Note the extended landing gear strut. (North American Aviation, Inc.)

Robert A. Hoover was one of the world’s best known exhibition pilots. He was a fighter pilot in the U.S. Army Air Corps during World War II. While flying a British Supermarine Spitfire with the 52nd Fighter Group based at Sicily, he was shot down, captured, and held as a prisoner of war at Stalag Luft I in Germany.

After 16 months in captivity, Hoover escaped, stole a Luftwaffe Focke-Wulf Fw 190 and flew it to The Netherlands.

After the war, Bob Hoover trained as a test pilot at Wright Field, Ohio, and remained in the Air Force until 1948. He worked as a test pilot for the Allison Division of General Motors, and then went on to North American Aviation.

Bob Hoover was famous  for flying aerobatic demonstrations around the world in his yellow P-51D Mustang and a twin-engine Shrike Commander, both built by North American Aviation.

Robert Anderson Hoover died 25 October 2016 at the age of 94 years.

Robert Anderson Hoover, Test Pilot, with North American Aviation F-100D-30-NA Super Sabre 55-3702A. (The Washington Post)

© 2018, Bryan R. Swopes

27 December 1935

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Mauna Loa viewed from Hilo, Hawaii. (Donnie MacGowan, Lovingthebigisland’s Weblog)
Advancing lava flow, December 1935. (USGS)

27 December 1935: When an eruption of Mauna Loa, a volcano on the Island of Hawaii (ongoing since late November) threatened the town of Hilo on the island’s northeastern coast, a decision was made to try to divert the flow of lava by aerial bombing. (The population of Hilo in 1935 was 15,633.)

Until recently, Mauna Loa was thought to be the largest volcano on Earth, but has been downgraded to second-place status by the Tamu Massif in the northwestern Pacific Ocean. It is a shield volcano, meaning that it was built up of fluid lava flows, as opposed to a stratovolcano, such as Vesuvius, which is created by the build up of solids like ash and pumice. The summit of Mauna Loa is 13,679 feet (4,169 meters) above Sea Level, but the volcano actually rises 30,085 feet (9,170 meters) from the floor of the Pacific Ocean.

“Lava flows from Pu’u ‘O’o Crater on Kilauea,” one of five active volcanoes on the Island of Hawaii in the Hawaiian Islands. (USGS)

The mission was planned by Lieutenant Colonel George S. Patton. The U.S. Army Air Corps’ 23d Bombardment Squadron, 5th Composite Group, based at Luke Field on Ford Island, Oahu, Territory of Hawaii, sent three Keystone B-3A and two Keystone B-6A bombers. The five airplanes dropped twenty 600-pound (272.2 kilogram) Mark I demolition bombs, each containing 355 pounds (161 kilograms) of TNT, with 0.1-second delay fuses.

A Keystone bomber flying over the Ko’olau Range on the island of Oahu, Territory of Hawaii. (U.S. Air Force)

Five of the twenty bombs struck molten lava directly; most of the others impacted solidified lava along the flow channel margins. . . Colonel William C. Capp (USAF, ret.), a pilot who bombed the lower target, reported direct hits on the channel, observing a sheet of red, molten rock that was thrown up to about 200′ elevation and that flying debris made small holes in his lower wing. Bombs that impacted on solidified, vesicular pahoehoe along the flow margin produced craters averaging 6.7 m diameters and 2.0 m depth. . .

Pilots observed that several bombs collapsed thin lava tube roofs, although in no case was sufficient roof material imploded into the tube to cause blockage. The extrusion of lava ceased within a week, however, and Jaggar wrote that the bombing caused the fluid pahoehoe to thicken and block the vent by the process of gas release. . . .

—Diversion of Lava Flows by Aerial Bombing — Lessons from Mauna Loa Volcano, Hawaii, by J.P. Lockwood, USGS, and F.A. Torgerson, USAF, abstract.

A flight of three Keystone B-3A bombers of the 23d Bombardment Squadron take off at Luke Field, Territory of Hawaii. Diamond Head is visible in the background. (U.S. Air Force)
A flight of three Keystone B-3A bombers of the 23d Bombardment Squadron take off at Luke Field on the island of Oahu, Territory of Hawaii. Diamond Head is visible in the background. (U.S. Air Force)

Eventually the lava turned to follow the natural drainage toward Hilo, instigating a crisis. On December 26, the flow was moving 1.6 km per day (1 mile per day), and at that rate scientists calculated the flows would reach Kaumana Road by January 9 (disrupting mochi-pounding parties). A suggestion to bomb the eruption was made. The U.S. Army Officer who planned the bombing operation was then Lt. Colonel George S. Patton, who would go on to WWII fame.

Three Keystone B-6As of 20th Bombardment Squadron, 2d Bomb Group, release their bombs on a practice mission. (U.S. Air Force)

On December 27, U.S. Army planes dropped bombs, targeting the lava channels and tubes just below the vents at 2,600 m (8,600 ft). The object was to divert the flow near its source. The results of the bombing was declared a success by Thomas A. Jaggar, Director of the Hawaiian Volcano Observatory.

Jagger wrote that ‘the violent release of lava, of gas and of hydrostatic pressures at the source robbed the lower flow of its substance, and of its heat.’ The lava stopped flowing on January 2, 1936.

— Hawaiian Volcano Observatory, Volcano Watch Archive, November 27, 1997: http://hvo.wr.usgs.gov/volcanowatch/archive/1997/97_11_28.html

“Aerial view of a bomb detonating on Mauna Loa near the 8,500-foot elevation source of the 1935 lava flow on the morning of Dec. 27, 1935. This was one of twenty 600-pound bombs dropped on the lava flow that morning by the Army Bombing Squadron from Luke Field, O’ahu. Photo by Army Air Corps, 11th Photo Section.” (Big Island Now)

The Keystone B-3A was a twin-engine two-bay biplane bomber, among the last biplanes used by the United States Army. It was operated by a crew of five. The B-3A was 48 feet, 10 inches (14.884 meters) long with a wingspan of 74 feet, 8 inches (22.758 meters). The maximum gross weight was 12,952 pounds (5,875 kilograms).

The B-3A was powered by two air-cooled, supercharged, 1,690.537-cubic-inch-displacement (27.703 liters) Pratt & Whitney Hornet A1 (R-1690-3) single-row 9-cylinder radial engines  with a compression ratio of 5:1. The engine was rated at 525 horsepower at 1,900 r.p.m., and turned two-bladed propellers through direct drive. The R-1690-3 was 3 feet, 8.88 Inches (1.140 meters) long, 4 feet, 7.44 inches (1.408 meters) in diameter and weighed 800 pounds (363 kilograms).

The B-3A had a maximum speed of 114 miles per hour (184 kilometers per hour) at Sea Level. Cruising speed was 98 miles per hour (158 kilometers per hour) and the service ceiling was 12,700 feet (3,871 meters) —nearly 1,000 feet (305 meters) lower than Mauna Loa’s summit.

Armament consisted of three .30-caliber machine guns and 2,500 pounds (1,133.9 kilograms) of bombs. With a full bomb load, the Keystone B-3A had a range of 860 miles (1,384 kilometers).

63 Keystone B-3As were built for the Air Corps and they were in service until 1940. The 2nd Observation Squadron at Nichols Field, Philippines, was the last unit equipped with the B-3A.

Keystone B-3A, Air Corps serial number 30-281, the first B-3A built. (U.S. Air Force)
Keystone B-3A, Air Corps serial number 30-281, the first B-3A built. (U.S. Air Force)

The Keystone B-6A was a re-engined B-3A. There was a change to two 1,823.129-cubic-inch-displacement (29.875 liter) air-cooled, supercharged Wright Aeronautical Division Cyclone 9 R-1820E single row 9-cylinder radial engines turning three-bladed propellers. The R-1820E was rated at 575 horsepower at 1,900 r.p.m. The engine weighed 850 pounds (386 kilograms).

Maximum speed increased to 120 miles per hour (193 kilometers per hour) at Sea Level with a cruising speed of 103 miles per hour (166 kilometers per hour). Armament and bomb load remained the same but the service ceiling increased to 14,100 feet (4,298 meters). The range decreased to 350 miles (563 kilometers) with a full bomb load.

39 Keystone B-6As were built and they remained in service until the early 1940s.

A U.S. Army Air Corps Keystone B-6A bomber. (U.S. Air Force)
A U.S. Army Air Corps Keystone B-6A bomber. (U.S. Air Force)

Newsreel footage of the bombing is available at Critical Past:

http://www.criticalpast.com/video/65675069574_bomb-Mauna-Loa_divert-lava_Keystone-B-3A_Keystone-LB-6A_United-States-fliers

© 2018, Bryan R. Swopes