5 March 1966: British Overseas Airways Corporation Speedbird 911, an around-the-world flight, departed Tokyo-Haneda Airport (HND) at 1:58 p.m., enroute Hong Kong-Kai Tak (HKG), with 113 passengers and 11 crew members. The airliner was a Boeing 707-436 Intercontinental, serial number 17706, with British registration G-APFE. It was nearly six years old, having been delivered 29 April 1960, and had 19,523 hours on the airframe.
Shortly before takeoff, the flight crew requested a change from an IFR flight plan to VFR, with a course that would take the airliner near Mount Fujiyama. The 707 climbed to an altitude of 16,000 feet (4,875 meters) as it approached the mountain from the southwest. The weather was very clear. A weather station on Mount Fuji recorded wind speeds of 60–70 knots (111–130 kilometers per hour).
Flying upwind toward Fujiyama at 320–370 knots (592–685 kilometers per hour), Speedbird 911 encountered severe Clear Air Turbulence that resulted in a catastrophic structural failure of the airframe. The vertical fin attachment failed and as it fell away, struck the left horizontal stabilizer, breaking it off. Next, the ventral fin and all four engine pylons failed due to extreme side loads. The 707 went in to a flat spin, trailing fuel vapor from ruptured tanks. The entire tail section broke away, the right wing failed, and the nose section came off.
The 707 left a debris field that was 10 miles (16 kilometers) long. Speedbird 911 crashed in a forest on the lower flanks of Mount Fujiyama at about the 3,500 foot (1,066 meter) level. The forward section crashed about 1,000 feet (300 meters) away from the main wreckage. All 124 persons aboard were killed.
PROBABLE CAUSE: “The aircraft suddenly encountered abnormally severe turbulence over Gotemba City which imposed a gust load considerably in excess of the design limit.”
The accident was photographed by the Japanese Self Defense Forces from the East Fuji Maneuver Area, located in the foothills of the volcano. A passenger aboard Speedbird 911 had been filming with an 8 mm movie camera. The camera and film were recovered from the wreckage and the film was developed as part of the investigation. The film showed that the aircraft had experienced severe turbulence immediately before the accident.
A U.S. Navy Douglas A-4 Skyhawk was sent to look for the accident site. When the fighter approached Mount Fujiyama, it also encountered severe turbulence, to the point that the pilot feared the small fighter would break up in flight. After returning to base, the A-4 was grounded for inspection. Its accelerometer indicated that it had experienced acceleration forces ranging from +9 Gs to -4 Gs.
5 March 1962: Operation Heat Rise: Two Convair B-58 Hustler supersonic bombers from the 65th Bombardment Squadron, 43rd Bombardment Wing, Carswell Air Force Base, Texas, took off at sunrise and headed west to Los Angeles, California. Off the Pacific coast they refueled from a Boeing KC-135A Stratotanker, then headed east at maximum speed. They were to enter a radar starting gate at Los Angeles, but the radar did not pick them up so they returned to the tanker, topped off the fuel tanks again, then proceeded east once again. This time their entry was visually confirmed.
Both B-58s had been assigned a block altitude of Flight Level 250 to Flight Level 500 (between 25,000 and 50,000 feet, 7,620 to 15,240 meters) by the Federal Aviation Administration, and all other aircraft were cleared from those altitudes along the course. The flight outbound from Los Angeles was at 50,000 feet (15,240 meters) at speeds above Mach 2.
Under normal conditions, the maximum speed of the B-58 was limited to a skin temperature of 115 °C. (239 °F.) to prevent the aluminum honeycomb skin panels from delaminating. For this speed run, Convair engineers had authorized a temperature of 125 °C. (257 °F.), which would allow the two bombers to exceed 1,400 miles per hour (2,253 kilometers per hour). Sensors were placed in the skin to monitor the temperature rise (which gave the operation its name: “Heat Rise”).
The first B-58, call sign “Tall Man Five-Five,” had a problem with the navigation radar and had some difficulty locating their tanker, but finally were able to. The B-58s descended to 25,000 feet over Kansas for the third refueling and over a 21-minute period, took on 85,000 gallons (321,760 liters) of fuel, climbed back to 45,000 feet (13,716 meters) and then continued on to New York.
The Cowtown Hustler crossed the radar gate at New York with an elapsed time of 2:00:58.71 for the West-to-East flight, averaging 1,214.65 miles per hour (1,954.79 kilometers per hour). The second B-58, Tall Man Five-Six, was one minute behind.
Passing New York, the two B-58 Hustlers proceeded over the Atlantic Ocean and rendezvoused with tankers for a fourth aerial refueling, then headed back west to Los Angeles. Shortly after passing New York, Tall Man Five-Six developed mechanical troubles and had to withdraw from the round-trip record attempt.
Once again over Kansas, Cowtown Hustler refueled for a fifth time then continued back to Los Angeles. The East-to-West leg from New York to Los Angeles was completed in an elapsed time of 2:15:50.08, averaging 1,081.81 miles per hour (1,741.00 kilometers per hour).
The total elapsed time, Los Angeles–New York–Los Angeles, was 4 hours, 41 minutes, 14.98 seconds (4:41:14.98) for an average speed of 1,044.97 miles per hour (1,681.71 kilometers per hour) The crew and the airplane established three National Aeronautic Association speed records for Speed Over A Recognized Course.
At Los Angeles, the flight crew, Captain Robert G. Sowers, Pilot, Captain Robert MacDonald, Navigator, and Captain John T. Walton, were congratulated by General Thomas S. Power, Chief of Staff, Strategic Air Command, and each airman was awarded the Distinguished Flying Cross.
For the eastbound transcontinental flight, the crew won the Bendix Trophy, and for “the most meritorious flight of the year,” they were also awarded the Mackay Trophy. Their records still stand.
Reportedly, the U.S. Air Force received more than 10,000 damage claims for windows that were broken by the sonic booms created by the two B-58 Hustlers as they flew across the country.
Today, the record-setting, trophy-winning airplane, Convair B-58A-10-CF 59-2458, the Cowtown Hustler, is on display at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.
The Convair B-58 Hustler was a high-altitude, Mach 2+ strategic bomber which served with the United States Air Force from 1960 to 1970. It was crewed by a pilot, navigator/bombardier and a defensive systems operator located in individual cockpits. The aircraft has a delta-winged configuration similar to Convair’s F-102A Delta Dagger and F-106 Delta Dart supersonic interceptors.
The Hustler is 96 feet, 10 inches (29.515 meters) long, with a wing span of 56 feet, 10 inches (17.323 meters) and overall height of 31 feet 5 inches (9.576 meters). The wings’ leading edge is swept back at a 60° angle and the fuselage incorporates the “area rule” which resulted in a “wasp waist” or “Coke bottle” shape for a significant reduction in aerodynamic drag. The airplane’s only control surfaces are two “elevons” and a rudder. There are no flaps.
The B-58A was powered by four General Electric J79-GE-5 axial-flow afterburning turbojet engines, suspended under the wings from pylons. This was a single-shaft engine with a 17-stage compressor and 3-stage turbine, rated at 10,300 pounds of thrust (45.82 kilonewtons), and 15,600 pounds (69.39 kilonewtons) with afterburner. The J79-GE-5 was 16 feet, 10.2 inches (5.136 meters) long and 3 feet, 2.0 inches (0.965 meters) in diameter.
The bomber had a cruise speed of 610 miles per hour (981.7 kilometers per hour) and a maximum speed of 1,325 miles per hour (2,132.4 kilometers per hour). The service ceiling is 64,800 feet (19,751 meters). Unrefueled range is 4,400 miles (7,081 kilometers). Maximum weight is 168,000 pounds (76,203.5 kilograms).
The B-58 weapons load was a combination of W-39, B43 or B61 nuclear bombs. The large weapons could be carried in a jettisonable centerline pod, which also carried fuel, and the smaller bombs could be carried on hardpoints. There was a defensive 20 mm M61 rotary cannon mounted in the tail with 1,200 rounds of ammunition. The gun was controlled remotely by the Defensive Systems Officer.
Convair built 116 B-58s between 1956 and 1961. They were retired by 1970.
The 19 minute, 38 second video below is a General Dynamics informational film about Operation Heat Rise. This video clip is longer than the time it took Cowtown Hustler to fly from Los Angeles, California, to the Grand Canyon in Arizona.
5 March 1936: At 4:35 p.m., Thursday afternoon, Vickers Aviation Ltd.’s Chief Test Pilot, Captain Joseph (“Mutt”) Summers, took off on the first flight of the Vickers-Supermarine Type 300, K5054, prototype of the legendary Supermarine Spitfire, at Eastleigh Aerodrome, Southampton, England. Landing after only 8 minutes, Summers is supposed to have said, “Don’t change a thing!”
The Vickers-Supermarine Type 300 was a private venture, built to meet an Air Ministry requirement¹ for a new single-place, single-engine interceptor for the Royal Air Force. The airplane was designed by a team led by Reginald Joseph Mitchell, C.B.E., F.R.Ae.S., and was built at the Supermarine Aviation Works, Southampton, Hampshire, England.
R.J. Mitchell was famous for his line of Schneider Trophy-winning and world record-setting Supermarine racers of the late 1920s and early 1930s, the Supermarine S.4, S.5, S.6 and S.6B.² Mitchell was appointed Commander of the Most Excellent Order of the British Empire (Civil Division) (CBE) in His Majesty’s New Year’s Honours, 2 January 1932, for “services in connection with the Schneider Trophy Contest.”
The Vickers-Supermarine Type 300 was 29 feet, 11 inches (9.119 meters) long, with a wingspan of 36 feet, 10 inches (11.227 meters) and overall height of 12 feet, 8 inches (3.861 meters). The wings had a distinctively ellipsoid shape, area was 242.0 square feet (22.48 square meters). Its empty weight was 4,082 pounds (1,151.6 kilograms) and loaded weight was 5,359 pounds (2,430.8 kilograms).
K5054 was powered by a right-hand tractor, liquid-cooled, supercharged, 1,648.9-cubic-inch-displacement (27.04-liter) Rolls-Royce Merlin C (“ramp head”) single overhead camshaft (SOHC) 60° V-12 engine, serial number C9 (Air Ministry serial number A111,139), which had a Normal Power rating of 1,029 horsepower at 2,600 r.p.m. at an altitude of 11,000 feet (3,353 meters), with +6 pounds per square inch boost (0.41 Bar). The engine turned aan Airscrew Co., Ltd., Watts-type two-bladed, fixed-pitch, compressed wood propeller through a gear reduction drive (possibly 0.420:1). (K5083, the prototype Hawker Hurricane, was also equipped with a Merlin C.) An improved 1,035 horsepower Merlin F engine, serial number F21 (Air Ministry serial number A115,73 ), was later installed.
Interestingly, Rolls-Royce discovered that using exhaust stacks to direct the flow of gases rearward provided an additional 70 pounds of thrust, an increase of 7% over that provided by the propeller alone. Later testing of K5054 with “fish tail” exhaust stacks increased its top speed to about 360 miles per hour (579 kilometers per hour).
The Type 300 had a cruise speed of 311 miles per hour ( kilometers per hour) at 15,000 feet (4,572 meters), and could reach that altitude in 5 minutes, 52 seconds. maximum speed of 349 miles per hour (562 kilometers per hour) at 16,800 feet (5,121 meters). The prototype had a service ceiling of 35,400 feet (10,790 meters).
A report summarizing the flight testing of K5054 stated, “The aeroplane is simple and easy to fly and has no vices.” Visibility was good, the cockpit was comfortable, and it was a stable gun platform.
On 22 March 1937, K5054’s engine lost oil pressure and the pilot made a belly landing on Marlesham Heath. The Spitfire was damaged, but was repaired and returned to service.
The prototype Spitfire stalled on landing at RAE Farnborough, 4 September 1939. After several bounces on the runway, it nosed over. The pilot, Flight Lieutenant Gilbert Stanbridge (“Spinner”) White, was severely injured. He died 9 September.
K5054 was disassembled and scrapped.
The Air Ministry ordered the Spitfire Mk.I into production before K5054’s first flight, with an initial order for 310 airplanes. The first production fighter was delivered to the Royal Air Force 4 August 1938. Between 1938 and 1948, 20,351 Spitfires were built in 24 variants.
Captain Joseph Summers, C.B.E., was born 10 March 1904. He was the older brother of Group Captain Maurice Summers, who was also a test pilot for Vickers. In 1922, he married Miss Dulcie Jeanette Belcher at Sculcoates, Yorkshire. They would have several children.
In 1924, Summers received a short-service commission as an officer in the Royal Air Force. He trained as a pilot with No. 2 Flight Training Squadron, at RAF Duxford. He was hospitalized for six months, which delayed his training, but he graduated in 1924 and was assigned to No. 29 Fighter Squadron. Summers was considered to be an exceptional pilot, and with just six months’ operational experience, he was assigned as a test pilot at the Aircraft and Armaments Engineering Establishment (A&AEE) at RAF Martlesham Heath. He remained there for the reminder of his military service. In June 1929 he became a test pilot for Vickers Ltd. (Aviation Department). He became the company’s chief test pilot in 1932.
During his career as a test pilot, “Mutt” Summers made the first flights of 54 prototype aircraft, including the Spitfire, the Vickers Type 618 Nene-Viking, the Vickers Type 630 Viscount four-engine turboprop airliner, and the Vickers Type 667 Valiant, a four-engine jet bomber. He flew more than 5,600 hours in 366 different aircraft types.
“Mutt’s approach to test flying was much more in sympathy with the knee-pad than with the complicated automatic observers which nowadays are an indispensable part of test flying. He vigorously defended the feel of an aeroplane as measured by his hand or by the seat of his pants, and I believe was always suspicious of the scientific approach. . . One learned never to regard his criticism or advice lightly. In a world of science and instrumentation his judgement and horsesense often threw an unscientific but accurate light on some dark problem.” —Sir George R. F. Edwards, OM, CBE, FRS, DL, Executive Director of the British Aircraft Corporation, quoted in Flight and Aircraft Engineer, No. 2357, Vol. 65, Friday, 26 March 1954, at Page 355, Column 2.
Joseph Summers, Esq., was appointed an Officer of the Most Excellent Order of the British Empire, Civil Division (O.B.E.), in His Majesty’s New Year’s Honours, Wednesday, 9 January 1946. He was promoted to Commander of the Most Excellent Order of the British Empire (Civil Division) (C.B.E.) in Her Majesty’s Coronation Honours, Monday, 1 June 1953.
Summers died 16 March 1954 at the age of 50 years.
¹ Air Ministry Specification F.37/34 High Speed Monoplane Single Seater Fighter
² FAI Record File Number 11833, World Record for Speed Over a 3-Kilometer Course: 364.92 kilometers per hour (226.75 miles per hour). Supermarine S.4, Henri Biard, 13 September 1925.
FAI Record File Number 14999, World Record for Speed Over 100 Kilometers: 531.20 kilometers per hour (330.07 miles per hour), Supermarine S.6, Henry Richard Danvers Waghorn, 7 September 1929.
FAI Record File Number 11831, World Record for Speed Over a 3-Kilometer Course: 655 kilometers per hour (407 miles per hour), Supermarine S.6B, George Hedley Stainforth, 29 September 1931.