Category Archives: Aviation

17 September 1952

Bell Model 47D-1 N167B with modified landing gear and multiple fuel tanks. (Bell Helicopter)

17 September 1952: Bell Aircraft Corporation test pilot Elton John (“E.J.”) Smith flew a modified Bell Model 47D-1 helicopter, N167B (s/n 21), from Hurst, Texas, to Niagara Falls, New York, setting a Fédération Aéronautique Internationale (FAI) world record for distance without landing of 1,958.80 kilometers (1,217.14 miles).¹

During Smith’s flight, the flight controls’ hydraulic boost system failed. The helicopter’s radio also caught fire, forcing Smith to pull the wiring loose.

Elton John Smith, 1952. (FAI)

BELL HELICOPTER AT NIAGARA AFTER SETTING DISTANCE MARK

     A new world’s record for a nonstop distance flight by helicopter was established Wednesday when a Bell helicopter flew approximately 1,234 miles from the Bell Aircraft Corporation plant near Hurst to the front lawn of the main plant in Niagara Falls, N.Y.

     The pilot was Elton J. Smith, 31-year-old Bell test pilot, who lives with his wife and three small children at 4121 Vance Rd. in North Richland Hills.

     The helicopter was named Longhorn.

     Smith took off from the heliport at the Hurst plant at 4:41 a.m. and landed in Niagara Falls at 5:38 p.m. Fort Worth time. His elapsed time in the air 12 hours and 57 minutes.

     Lawrence D. Bell, president of the corporation, shouted congratulations to Smith while the helicopter’s rotors were still spinning.

     “Thank you, sir,” Smith replied.

     Later he reported that “I wasn’t very tired, it was a good flight. I ran into a little bad weather over the Ozarks, which forced me to detour somewhat from my proposed straight line flight from Fort Worth to Niagara Falls. After that I had pretty good weather and flew most of the route between 6,000 and 8,000 feet.

     “I started having radio trouble about one hour out of Fort Worth, which accounts for the fact that there was no contact with me during a great deal of the trip.

     “I had enough gas left to go another four hours—about 40 gallons,” he said. “I used only two quarts of oil on the trip.

     “I really got a kick out of doing it because a lot of us in the helicopter industry thought it could be done.

     “All in all, I was pretty fresh at the end of the trip—just a little bit stiff.”

     The flight, via Cleveland and Buffalo, broke the official helicopter distance record of 703.6 miles, established in a Sikorsky R05 helicopter on May 26, 1946, by Major F. T. Caschman, U.S. Air Force.

     That flight was from Cleveland to Logan, Mass, Other long distance flights on record, but not recognized by National Aeronautic Association, include:

     A flight of 920 miles from Iceland to Prestwick, Scotland, on July 31, 1952, by a Sikorsky H-19, flown by an Air Force pilot and co-pilot.

     A flight of 956 miles, 843 cross-country and 113 miles in the vicinity of Dayton, Ohio, on July 6, 1951, by Captain Wayne W. Eggert, U.S. Air Force.

     The helicopter  piloted by Smith was a Model 47D, built by Bell in December 1947. It is equipped with a 200-horsepower, six-cylinder Franklin aircooled engine. The ship previously had logged 387 hours and 50 minutes of flying time.

     Official observer for the NAA was E. J. Reeves of Dallas, who placed sealed barographs aboard the Longhorn before takeoff. The NAA also sealed the gas and oil tanks and an official was on hand to certify that the seals had not been broken when the helicopter.

     The helicopter took off with 187 gallons of gasoline and two gallons of oil. Estimated cost for the fuel on the flight was $59.30, a Bell release issued after the takeoff declared.

     Normal gross weight for a 47D model helicopter is 2,350 pounds, the release said. Gross for the record-breaking flight was 2,750 pounds.

     Smith carried with him several candy bars, a half-gallon of drinking water, and a beef sandwich.

Fort Worth Star-Telegram, 18 September 1952, Page 1, Columns 1–3

Bell Model 47D-1, N167B. (FAI)

Bell 47D-1 N167B (s/n 21) was originally built in December 1947 as a Model 47D. It was assigned to Bell’s Research and Development group for many years and went through numerous modifications. It had been used to develop the U.S. Army’s H-13B Sioux. For the record-setting flight, N167B was modified with seven fuel tanks, with two located in the passenger cabin, and five mounted behind the engine. After starting the engine, the electric starter motor was removed to save weight. At takeoff, it had a gross weight of 2,750 pounds (1,247 kilograms), 400 pounds (181 kilograms) over the certified maximum gross weight of the helicopter. It had flown 387 hours, 50 minutes, before the 17 September 1952 flight. Its FAA registration was cancelled 11 June 1970.

The Bell Model 47D-1 was the first three-place variant of the Model 47 series. Its Type Certificate was approved 29 March 1949. The initial price was $39,500.

The Bell Model 47D-1 had an overall length (with rotors turning) of 41 feet, 4¾ inches (12.618 meters). The main rotor diameter was 35 feet, 1½ inches (10.706 meters) in diameter. The length of the fuselage, from the front of the canopy to the trailing edge of the tail rotor disc, was 30 feet, 5 inches (9.271 meters). It was 9 feet, 4-5/16 inches (2.827 meters) high to the top of the main rotor mast.

The Bell 47D-1 main rotor was a two-bladed, under-slung, semi-rigid assembly that would be a characteristic of helicopters built by Bell for decades. The blades were constructed of laminated wood. An 8 foot, 4 inch (2.540 meters) stabilizer bar was placed below the hub and linked to the flight controls through hydraulic dampers. This made for a very stable aircraft. The main rotor turned counter-clockwise, as seen from above. (The advancing blade was on the right.) Its normal operating range was 322–360 r.p.m. (294–360 r.p.m. in autorotation).

The 47D-1 tail rotor was positioned on the right side of the tail boom in a tractor configuration. It had a diameter of 5 feet, 8-1/8 inches (1.730 meters) and rotated counter-clockwise as seen from the helicopter’s left. (The advancing blade was above the axis of rotation.) The tail rotor blades were also made of wood.

Elton J. Smith tests the modified Bell 47D-1. (Bell Helicopter)

Power was supplied by an air-cooled, normally-aspirated, 333.991-cubic-inch-displacement (5.473 liter) Franklin Engine Company 6V4-178-B32 vertically-opposed six cylinder engine with a compression ratio of 8.5:1. This engine was rated at 200 horsepower at 3,100 r.p.m. at Sea Level. Engine torque was sent through a centrifugal clutch to a transmission. The mast (the main rotor drive shaft) was driven through a two-stage planetary gear reduction system with a ratio of 9:1. The transmission also drove the tail rotor drive shaft, and through a vee-belt/pulley system, a large fan to provide cooling air for the engine.

The standard production Model 47D-1 had a maximum gross weight of 2,350 pounds (1,066 kilograms) and a fuel capacity of 29 U.S. gallons (110 liters). Its cruise speed was 78 miles per hour (126 kilometers per hour) and its service ceiling was 12,000 feet (3,658 meters).

Bell built 129 Model 47D-1 helicopters.

The Bell 47 was produced at the plant in New York, and later at Fort Worth, Texas. It was steadily improved and remained in production until 1974. In military service the Model 47 was designated H-13 Sioux, (Army and Air Force), HTL (Navy) and HUG (Coast Guard). The helicopter was also built under license by Agusta, Kawasaki and Westland. More than 7,000 were built worldwide and it is believed that about 10% of those remain in service.

Elton John Smith was born 4 September 1921 at Walton, New York. He was the second of three children of William H. Smith, a farmer, and Florence (“Flossie”) Delilah Knapp. He attended Parker High School in Clarence, New York.

Aviation Cadet Elton John Smith.

Elton Smith enlisted in the U.S. Army Air Forces as an aviation cadet, 11 December 1941. He completed flight training at the Lubbock Army Flying School, 20 March 1943 and commissioned as a second lieutenant. He was assigned to fly North American Aviation B-25 Mitchell medium bombers.

On 24 December 1943, Lieutenant Mitchell married Miss Rita Marie Follett at a private residence in San Angelo, Texas. They would have four children.

Smith was discharged from the U.S. Army Air Forces, 6 December 1945.

In 1947, E. J. Smith joined the Bell Aircraft Corporation at Buffalo, New York, as a test pilot.

E. J. Smith completes documentation for his world record flight.

On 20 October 1954, along with Bell’s Chief Pilot Floyd W. Carlson, Chief Experimental Test Pilot Smith made the first flight of the Bell XH-40, prototype of the legendary “Huey” military helicopter.

In 1973, Smith became the manager of flight and technical training for Bell Helicopter International’s Iranian training program. He was later the company’s head of international sales. He retired in 1984.

Elton John Smith died Thursday, 18 October 1990, in a hospital in Irvine, Texas. His remains ere buried at Greenwood Memorial Park, Fort Worth, Texas.

¹ FAI Record File Number 976

© 2023, Bryan R. Swopes

17 September 1916

Rittmeister Manfred Albrecht Freiher von Richtofen. (Portrait by C. J. von Dühren)
Rittmeister Manfred Albrecht Freiher von Richtofen. (Portrait by C. J. von Dühren, 3 May 1917)

17 September 1916: At approximately 11:00 a.m., near Villers-Pouich, Nord, France, Rittmeister Manfred Albrecht Freiherr von Richthofen, of Jagdstaffel 2, Die Fliegertruppen des deutschen Kaiserreiches (the Luftstreitkräfte), while flying an Albatros D.II, serial number 491/16, spotted a flight of enemy aircraft. Attacking one, he closed to within 10 meters and fired several bursts of machine gun fire.

2nd Lieutenant Lionel B. F. Morris, R.F.C.

The British airplane, a Royal Aircraft Factory F.E. 2B scout bomber, serial number 7018, was flown by Second Lieutenant Lionel Bertram Frank Morris, with Captain Tom Rees as observer and gunner. Both officers were assigned from their original regiments to No. 11 Squadron, Royal Flying Corps.

The F.E.2B’s engine stopped and it started down. Captain Rees continued firing at von Richthofen until he was killed by the Baron’s gunfire.

Lieutenant Morris was wounded but was able to land the crippled airplane near a German airfield. Von Richthofen landed his Albatross alongside. Lieutenant Morris died while being taken to a field hospital by ambulance.

The body of Lieutenant Morris was buried at Porte-de-Paris Cemetery, Cambrai, France. Captain Rees was buried at Villers-Plouich.

Morris and Rees flew this Royal Aircraft Factory F.E. 2B, serial number 7018, shown surrounded by enemy soldiers. (Unattributed)
Morris and Rees flew this Royal Aircraft Factory F.E. 2B, serial number 7018, shown surrounded by enemy soldiers. (Wikipedia)

Von Richthofen had just joined Jasta 2 after becoming a fighter pilot. Originally a cavalry officer, he had become an aerial observer before training as a pilot. This action was his first confirmed aerial victory. 79 more would follow and he would become known as The Red Baron.

Captain Tom Rees
Lieutenant Tom Rees, 1915

The Royal Aircraft Factory F.E. 2 (also designated Fighter Mk.I) was designed by Geoffrey de Havilland. He had made the first flight in the prototype at Farnborough, Hampshire, 18 August 1911. The F.E. 2B was a two-place, single-engine, pusher biplane used as a scout bomber. It was 32 feet, 3 inches (9.830 meters) long with a wingspan of 47 feet, 9 inches (14.554 meters) and height of 12 feet, 7½ inches (3.848 meters). It had an empty weight of 2,105 pounds (955 kilograms) and gross weight of 2,827 pounds (1,282 kilograms). The airplane’s three-bay wings had a chord of 5 feet, 6 inches (1.676 meters) and were spaced 6 feet, 3½ inches (1.918 meters), vertically. The wings had a 3° 30′ angle of incidence and were not staggered. There was 4° dihedral.

The F.E. 2B was powered by a water-cooled 13.937 liter (850.48 cubic inches) William Beardmore and Company inline six-cylinder engine rated at 120 horsepower at 1,200 r.p.m. It could produce a maximum 154 horsepower at 1,400 r.p.m. This engine was a license-built Austro-Daimler 6, which had been designed by Dr.-Ing. Ferdinand Porsche.

The airplane had a maximum speed of 73 miles per hour (117 kilometers per hour) at 6,500 feet, and 72 miles per hour (116 kilometers per hour) at 10,000 feet (3,048 meters). The airplane could reach 6,500 feet (1,981 meters) in 19.5 minutes, and 10,000 feet in 45.5 minutes. Its service ceiling was 9,000 feet (2,743 meters).

The F.E. 2B had fuel to remain airborne for 3½ hours.

Boulton & Paul Ltd.-built F.E. 2B A5478 (Aviation News)
Boulton & Paul Ltd.-built F.E. 2B A5478 (Aviation News)

The F.E. 2B was armed with one or two .303-caliber Lewis guns. The second gun was mounted on a telescoping post between the cockpits, and in the raised position could fire over the upper wing to defend the airplane from attacks in the rear. This required the gunner to stand in his seat.

A total of 1,939 F.E.s were built.

An Albatros D.II, similar to that flown by Manfred von Richthofen, 17 September 1916.
An Albatros D.II, similar to that flown by Manfred von Richthofen, 17 September 1916.

The Albatros D.II was a single-place, single-engine biplane fighter designed and built by Albatros Flugzeugwerk GmbH, Johannisthal, Berlin. It was also built under license by Luft-Verkhers-Gesellschaft and Oesterreichische Flugzeugfabrik AG. It was 7.40 meters (24 feet, 3-1/3 inches) long with a wingspan of 8.50 meters (27 feet, 10-2/3 inches) and height of 2.59 meters (8 feet, 6 inches). It had an empty weight of 637 kilograms (1,404 pounds) and gross weight of 888 kilograms (1,958 pounds).

The D.II was powered by a water- and air-cooled, normally-aspirated, 14.778 liter (901.68 cubic inches) Mercedes F1466 (D.III) single-overhead cam inline six-cylinder direct-drive engine with a compression ratio of 4.50:1, which produced 162.5 horsepower at 1,400 r.p.m. The engine weighed 618 pounds (280 kilograms).

The Albatros D.II had a maximum speed of 175 kilometers per hour (109 miles per hour) and a service ceiling of 5,180 meters (16,995 feet).

The fighter was armed with two fixed air-cooled 7.92 mm machine guns.

A total of 291 Albatros D.II fighters were built before production shifted to the D.III.

Manfred von Richtofen with an Albatross D.II. (Unattributed)
Manfred von Richtofen with an Albatross D.II. (Unattributed)

© 2018, Bryan R. Swopes

17 September 1908

Lt. Thomas Etholen Selfridge (Robert B. Williams)

17 September 1908: Orville Wright brought his Wright Flyer to Fort Myer, Virginia to demonstrate it to the U.S. Army Signal Corps.  A crowd of approximately 2,500 spectators had gathered to watch the flight.

Lieutenant Thomas Etholen Selfridge, Signal Corps, United States Army, wanted to ride along with Wright and asked to go first. Lieutenant George Sweet, U.S. Navy was scheduled for the first flight, but he and Wright agreed to let Lieutenant Selfridge go. The two men aboard the Wright Flyer made four circuits of the field approximately 150 feet above the ground. The starboard propeller broke and struck the wires supporting the rudder. As the rudder rotated sideways, it caused the airplane to pitch nose down.

Lieutenant Thomas E. Selfridge and Orville Wright aboard the Wright Flyer. (U.S. Air Force)

Orville Wright later described the accident:

“On the fourth round, everything seemingly working much better and smoother than any former flight, I started on a larger circuit with less abrupt turns. It was on the very first slow turn that the trouble began. . . A hurried glance behind revealed nothing wrong, but I decided to shut off the power and descend as soon as the machine could be faced in a direction where a landing could be made. This decision was hardly reached, in fact I suppose it was not over two or three seconds from the time the first taps were heard, until two big thumps, which gave the machine a terrible shaking, showed that something had broken. . . The machine suddenly turned to the right and I immediately shut off the power. Quick as a flash, the machine turned down in front and started straight for the ground. Our course for 50 feet was within a very few degrees of the perpendicular. Lt. Selfridge up to this time had not uttered a word, though he took a hasty glance behind when the propeller broke and turned once or twice to look into my face, evidently to see what I thought of the situation. But when the machine turned head first for the ground, he exclaimed ‘Oh! Oh!’ in an almost inaudible voice.”

The wreck of the Wright Flyer, Fort Myer, Virginia, 17 September 1908. (Library of Congress)

The Wright Flyer struck the ground and both men were seriously injured. Thomas Selfridge suffered a fractured skull. He underwent neurosurgery but died without regaining consciousness. Orville Wright had a broken leg, several broken ribs and an injured hip. He spent seven weeks in the Army hospital.

This was the first fatal accident involving an airplane. Lieutenant Thomas Etholen Selfridge was the first person to die in an airplane accident.

Doctors attend to the unconscious Lieutenant Selfridge following the crash of the Wright Flyer at Fort Myer, Virginia, 17 September 1908. He died later that day. (Library of Congress)

© 2015, Bryan R. Swopes

16 September 2011

Unlimited Division racer The Galloping Ghost just before impact. The pilot is not visible in the cockpit. (AP photo/Grass Valley Union/Tim O’Brien via The Press Democrat)

16 September 2011: In the late afternoon, six highly-modified World War II-era fighters were competing in a preliminary heat for the Unlimited Division championship of the National Championship Air Races, being held at the Reno-Stead Airport (RST), about 12 miles (19 kilometers) northwest of the central business district of the city of Reno, Nevada. The field elevation is 5,050 feet above Sea Level (1,539 meters). The races were being flown over an 8.4-mile (13.5 kilometers) ovate course, marked by ten pylons. All turns were made to the left.

The competitors for Heat 2A were three North American Aviation P-51D Mustangs, a Goodyear F2G-1 Corsair, a Grumman F8F-2 Bearcat, and two Hawker Sea Furies.

The Galloping Ghost taking off at Reno-Stead Airport in 2010. (Shawna Malvini Redden, the bluest muse)

The Galloping Ghost, race number 177, was flown by its owner, James Kent Leeward. On lap number three, Leeward was 4.5 seconds behind the second-place P-51, Voodoo, and 8.8 seconds behind the heat leader, Strega, also a radically-modified Mustang. The airplane was at approximately 445 knots (512 miles per hour, or 824 kilometers per hour) as it rounded Pylon 8 in a steep left bank.

At 16:24:28.9 Pacific Daylight Time, The Galloping Ghost‘s angle of bank rapidly increased from 73° to 93° in just 0.83 seconds. (The NTSB referred to this as a “left-roll upset.”) (Wake vortices from the leading air racers may have been a factor in this left-roll upset. Investigators found that they could not exclude the possibility.) The air racer, corrected by its pilot’s aileron input, rolled back to the right, but then violently pitched up. The airplane essentially flew itself into an inside loop, then crashed into the ground directly in front of a seating area.

The left elevator trim tab falls away from The Galloping Ghost. (Julia Kirchenbauer, from NTSB Accident Brief AAB-12/01)
177 rolls inverted. The left elevator trim tab is missing. (AP photo/Grass Valley Union/Tim O’Brien via The Press Democrat)
The Galloping Ghost in its final dive. (Ward Howes/The Los Angeles Times)
Impact 1 (Ward Howes/The Los Angeles Times)

The Galloping Ghost was totally destroyed. Jimmy Leeward and 11 spectators were killed, with at at least 69 others injured.

The Galloping Ghost had been built in 1944 as a P-51D-15-NA Mustang, serial number 44-15651, by North American Aviation, Inc., at its Inglewood, California factory. Following World War II, the very low-time fighter was sold off as surplus equipment.

North American Aviation P-51D Mustang NX79111, “The Galloping Ghost,” circa 1947. (San Diego Air & Space Museum)

Registered NX79111 and carrying the race number 77, it was flown by Bruce Raymond in the 1946 Thompson Trophy Race, finishing in fourth place. In 1947, Steve Beville flew The Galloping Ghost in the Kendall Trophy Race, finishing in first place with an average speed  of 384.602 miles per hour (618.957 kilometers per hour). He then finished in fourth place in the Thompson race. For the 1948 National Air Races, Bruce Raymond was back in the cockpit of number 77. He finished in fourth place in the SOHIO Trophy Race, first in the Tinnerman Trophy Race, and second in the Thompson. In 1949, Beville again flew 77 in the SOHIO and Thompson Trophy Races, finishing fourth in both.

North American Aviation P-51D-15-NA Mustang NX79111, The Galloping Ghost, photographed in 1948. (Classic War Birds)

The airplane was later raced as Miss Candace and Jeannie.

On 18 September 1970, N79111 crash landed near the Reno-Stead Airport following an engine failure during a race. The P-51 was substantially damaged.

Jimmy Leeward purchased the fighter in July 1983. After racing it for years, the airplane was placed in storage. Then, beginning in 2007, the airplane underwent a series of radical modifications. Some of these were similar to those made to other Unlimited Division racing planes, however, there was no evidence of engineering before, or flight testing, following these mods.

The most obvious modifications were made to the profile of the P-51D’s fuselage. The standard windshield and bubble canopy were removed and replaced by a much smaller unit. This was smoothly faired into a raised dorsal “razorback” which carried aft from the cockpit to the vertical fin. The lower fuselage, with its Meredith Effect radiator scoop and cooling ducts, was completely removed and a new fuselage belly constructed.

The standard Mustang cooling system was replaced by a “boil off” system in the aft fuselage. Rather than radiators which remove heat from the engine coolant by the passage of air, heat exchangers were immersed in a solution of water and methanol. A 150 gallon supply was in a tank in the left wing.

The Mustang’s wings had been shortened from the standard span of 37 feet, 0 inches (11.278 meters) to 28 feet, 10 inches (8.788 meters). The ailerons were each shortened from about 7 feet (2.1 meters) to 3 feet (0.9 meters). The horizontal stabilizer span was shortened from 14 feet, 10-5/32 inches (4.525 meters) to 12 feet, 1 inch (3.683 meters), and its angle of incidence increased from +0.5° to +0.91°. The vertical fin was offset to the right of the airplane’s longitudinal axis, instead of to the left, as built by the factory. The ailerons were not properly adjusted, which required the pilot to use constant pressure to the right on the control stick to keep the wings level.

On the standard Mustang, both elevators are equipped with adjustable trim tabs on their trailing edges, which the pilot uses to adjust the flight controls’ neutral positions. On The Galloping Ghost, the right elevator trim tab had been deactivated, placing increased load on the left trim tab. The elevators and rudder used weighted counterbalances. These, too, had been modified. The total weight for both elevator counterweights had been raised to 53.5 pounds (24.3 kilograms), nearly four times the maximum allowable weight of 13.75 pounds (6.24 kilograms). Similarly, the rudder counterbalance weight was increased to 25 pounds (11.3 kilograms). The maximum allowable weight was 16.6 pounds (7.5 kilograms).

According to its maintenance records, at the time of the accident, N79111 had flown a total of 1,453.6 hours. Its Packard V-1650-9A Merlin V-12 engine had been overhauled to military specifications at 1,428.9 airframe hours. The four-bladed Hamilton Standard 24D50 propeller had just 24.7 hours since new. The modified airplane had an empty weight of 6,474 pounds (2,936.6 kilograms). Accident investigators estimated its weight at the time of the upset as 7,760 pounds (3,202.4 kilograms).

Wrinkles in fuselage of The Galloping Ghost during the first lap of Heat 2A, 16 September 2011. (Florian Schmehl, from NTSB Accident Brief AAB-12/01)

Photographs taken during the first lap showed significant diagonal wrinkles in the fuselage of The Galloping Ghost, just behind the right wing, which were not present before the race started. A photograph taken during the third lap showed similar wrinkles on the left side of the fuselage. It is apparent that the modifications to the Mustang’s fuselage had significantly weakened its structure.

The left and right elevator trim tabs are attached to their hinges by three screws, each. These are secured by locknuts. NTSB investigators found that two of these screws had broken due to overload during the flight. (One screw was found to have had a pre-existing fatigue fracture.) All of the screws were loose in their locknuts and could easily be turned by hand. All six locknuts were worn beyond limits and were incapable of maintaining torque.

The loose trim tab attachment allowed the trim tabs to flutter because of the aerodynamic loads of very high speed flight. This flutter produced loads beyond the strength of the trim system. These loads caused the linkage to the left tab to break. Without the linkage, flutter increased the movement of the tab beyond its limit and the hinge broke. The left tab moved beyond its normal limit, and caused the the linkage to bend and then fracture. With the left tab uncontrolled, the flutter was transmitted to the right elevator tab which had been fixed in place with a steel rod. The vibrations caused its fixed link assembly to fracture.

The loss of the downward force which the left trim tab applied to its elevator caused the elevator to move upward. This caused the airplane to violently pitch up. Investigators calculated that Leeward would have been subjected to an acceleration of 17.3 Gs, far beyond human tolerance. He was immediately incapacitated.

With its pilot unconscious and the airplane traveling at such high speed, it went completely out of control. It flew inverted into a “helical” pattern and then, with the Merlin engine still at wide-open throttle, crashed into the ground at a very steep angle.

The National Transportation Safety Board reported:

3. PROBABLE CAUSE

          The National Transportation Safety Board determines that the probable cause of this accident was the reduced stiffness of the elevator trim tab system that allowed aerodynamic flutter to occur at racing speeds. The reduced stiffness was a result of deteriorated locknut inserts that allowed the trim tab attachment screws to become loose and to initiate fatigue cracking in one screw sometime before the accident flight. Aerodynamic flutter of the trim tabs resulted in a failure of the left trim tab link assembly, elevator movement, high flight loads, and a loss of control. Contributing to the accident were the undocumented and untested major modifications to the airplane and the pilot’s operation of the airplane in the unique air racing environment without adequate flight testing.

—National Transportation Safety Board. 2012. Pilot/Race 177, The Galloping Ghost, North American P-51D, N79111, Reno, Nevada, September 16, 2011. NTSB/AAB-12-01. Washington, DC.

James Kent (“Jimmy”) Leeward with his Unlimited Division racer, The Galloping Ghost. (Marilyn Newton, The Reno-Gazette Journal)

James Kent Leeward was born at Brackenridge, Pennsylvania, 21 October 1936, He was the son of Albert James Leeward and Mary Virginia Leeward. He was educated at the Culver Military Academy, a college-preparatory boarding school at Culver, Indiana. He graduated in 1952.

In July 1959, Leeward married Miss Bette L. Hofacker in Dade County, Florida. They had four children.

At the time of his death, James Kent Leeward was 74 years old.

© 2018, Bryan R. Swopes

16 September 1999

NASA 008, known as “Balls 8,” a modified Boeing RB-52B-10-BO Stratofortress, serial number 52-008, with NASA 824, a Lockheed TF-104G Starfighter, N824NA. The DAST 1 drone is under the bomber’s right wing. (NASA)

16 September 1999: 44 years, 3 months and 6 days after its very first flight, NASA’s airborne launch aircraft, or “mothership,” Balls 8, completed its 1,000th flight.

Balls 8, so-called because of the double zeros in it U.S. Air Force serial number, 52-008, is a Boeing NB-52, modified as a drop ship from its original configuration as an RB-52B-10-BO Stratofortress reconnaissance bomber assigned to the Strategic Air Command. It made its first flight 11 June 1955 and was reassigned from SAC to Edwards Air Force Base to support NASA flight testing operations, 8 June 1959. Balls 8 served NASA until 17 December 2004, when it was replaced by a newer NB-52H Stratofortress.

52-008 was altered at the North American Aviation facility at Air Force Plant 42, Palmdale, California. A pylon was mounted under the bomber’s right wing. A large notch was cut into the trailing edge of the inboard flap for the X-15’s vertical fin. A 1,500 gallon (5,678 liter) liquid oxygen tank was installed in the bomb bay. A station for a launch operator was installed on the upper deck of the B-52 at the former electronic countermeasures position. A series of control panels allowed the panel operator to monitor the X-15’s systems, provide electrical power, and to keep the rocketplane’s liquid oxygen tank full as the LOX boiled off during the climb to launch altitude. The operator could see the X-15 through a plexiglas dome, and there were two television monitors.

The NB-52B was used during the X-15 Program and carried the three hypersonic research aircraft aloft on 159 of their 199 flights. (NB-52A 52-003, The High and Mighty One, made the other 40 launches.) It has also been used to carry the X-24 and HiMat lifting body research aircraft and to launch Pegasus research rockets.

At the time of its retirement, Balls 8 was the oldest B-52 in service, and also the lowest time B-52. It is on display near the north gate at Edwards Air Force Base.

Balls 8, Boeing NB-52B Stratofortress 52-008, as seen from a KC-135A Stratotanker. (NASA)
Balls 8, NASA’s Boeing NB-52B Stratofortress 52-008 “mothership”, as seen from a KC-135A Stratotanker. (NASA)

Of the 744 B-52 Stratofortresses built by Boeing, 50 were B-52Bs and 27 of these were RB-52B reconnaissance bombers.

The airplane was 156 feet, 6.9 inches (47.724 meters) long with a wingspan of 185 feet, 0 inches (56.388 meters) and overall height of 48 feet, 3.6 inches (14.722 meters). The wings were mounted high on the fuselage (“shoulder-mounted”) to provide clearance for the engines which were suspended on pylons. The wings’ leading edges were swept 35°. The bomber’s empty weight was 164,081 pounds (74,226 kilograms), with a combat weight of 272,000 pounds (123,377 kilograms) and a maximum takeoff weight of 420,000 pounds (190,509 kilograms).

Early production B-52Bs were powered by eight Pratt & Whitney J57-P-1W turbojet engines, while later aircraft were equipped with J57-P-19W and J57-P-29W or WA turbojets. The engines were grouped in two-engine pods on four under-wing pylons. The J57 was a two-spool, axial-flow engine with a 16-stage compressor section (9 low- and 7-high-pressure stages) and a 3-stage turbine section (1 high- and 2 low-pressure stages). These engines were rated at 10,500 pounds of thrust (46.71 kilonewtons), each, or 12,100 pounds (53.82 kilonewtons) with water injection.

The B-52B/RB-52B had a cruise speed of 523 miles per hour (842 kilometers per hour). The maximum speed varied with altitude: 630 miles per hour (1,014 kilometers per hour) at 19,800 feet (6,035 meters), 598 miles per hour (962 kilometers per hour) at 35,000 feet (10,668 meters) and 571 miles per hour (919 kilometers per hour) at 45,750 feet (13,945 meters). The service ceiling at combat weight was 47,300 feet (14,417 meters).

Maximum ferry range was 7,343 miles (11,817 kilometers). With a 10,000 pound (4,536 kilogram) bomb load, the B-52B had a combat radius of 3,590 miles (5,778 kilometers). With inflight refueling, the range was essentially world-wide.

This "score board" painted on the side of Balls 8 shows many of the missions that it flew as a "mothership" for NASA. (NASA)
This “score board” painted on the side of Balls 8 shows many of the missions that it flew as a “mothership” for NASA. (NASA)

Defensive armament consisted of four Browning Aircraft Machine Guns, Caliber .50, AN-M3, mounted in a tail turret with 600 rounds of ammunition per gun. These guns had a combined rate of fire in excess of 4,000 rounds per minute. (Eighteen RB-52Bs were equipped with two M24A1 20 mm autocannon in the tail turret in place of the standard four .50-caliber machine guns.)

The B-52B’s maximum bomb load was 43,000 pounds (19,505 kilograms). It could carry a 15-megaton Mark 17 thermonuclear bomb, or two Mark 15s, each with a maximum yield of 3.8 megatons.

Balls 8 lands on a runway marked on Rogers Dry Lake at Edwards Air Force Base, California. The drogue parachute helps to slow the airplane. (NASA)
Balls 8 lands on a runway marked on Rogers Dry Lake at Edwards Air Force Base, California. The drogue parachute helps to slow the airplane. (NASA)

© 2017, Bryan R. Swopes