Category Archives: Aviation

13 August 1914

Aviation, , , , , ,
Lieutenant Harvey-Kelly
Lieutenant Hubert Dunsterville Harvey-Kelly, D.S.O., Royal Flying Corps.

13 August 1914: Lieutenant Hubert Dunsterville Harvey-Kelly, No. 2 Squadron, Royal Flying Corps, departed Dover at 6:25 a.m., 13 August 1914, enroute to Amiens, France. He flew a Royal Aircraft Factory B.E.2.a, number 471. Landing near Amiens at 8:20 a.m., this was the first British airplane to arrive in France following the outbreak of World War I.

Hubert Dunsterville Harvey-Kelly was born at Berry Pomeroy, Devon, 9 February 1891. He was one of five children of Colonel Harvey Hamilton Harvey-Kelly, Indian Staff Corps, and Constance J. Dunsterville Harvey-Kelly. (They were married at Hyderabad, Siad, 15 December 1877.) He attended the Modern School, and the Royal Military College at Sandhurst. On graduation, Harvey-Kelly received a commission as a second lieutenant in the Royal Irish Regiment, 5 October 1910. He was promoted to lieutenant, 23 October 1912.

After learning to fly, Lieutenant Harvey-Kelly received the Royal Aero Club aviator’s license number 501, issued 30 May 1913. At his own request, Harvey-Kelly was then attached to the Royal Flying Corps, as a Lieutenant, R.F.C. Reserve, 14 August 1913.

Lieutenant Harvey-Kelly was created a Companion of the Distinguished Service Order, 18 February 1915, and promoted to captain, 23 May 1915. On 30 January 1916, Captain Harvey-Kelly was promoted to the temporary rank of major.

In command of No. 19 Squadron, R.F.C., Major Dunston was flying a SPAD S.VII C.1 when he was shot down 25 April 1917 by Oberleutnant Kurt Robert Wilhelm Wolff, flying an Albatros D.III. Severely injured, he died in a German field hospital, 29 April.

Major Hubert Dunsterville Harvey-Kelly, D.S.O., Royal Irish Regiment (attd. Royal Flying Corps) was buried at Brown’s Copse Cemetery, northwest of Roeux, Pas-de-Calais, France.

This Royal Aircraft Factory B.E.2.a, No. 347, of No. 2 Squadron, Royal Flying Corps, at Lythe, near Whitby, North Yorkshire, June 1914. Its pilot, Lieutenant Hubert Dunsterville Harvey-Kelly, Royal Irish Regiment, is at the lower right of the photograph. (Imperial War Museum Image number Q 54985)
This Royal Aircraft Factory B.E.2.a, No. 347, of No. 2 Squadron, Royal Flying Corps, at Lythe, near Whitby, North Yorkshire, June 1914. This airplane was manufactured by the Coventry Ordnance Works. Its pilot, Lieutenant Hubert Dunsterville Harvey-Kelly, Royal Irish Regiment, is at the lower right of the photograph. (Imperial War Museum Image number Q 54985)

Royal Aircraft Factory B.E.2.a number 471 had been built by the Coventry Ordnance Works and delivered to the Royal Flying Corps at Farnborough, 5 June 1913. It had initially been assigned to the Central Flying School before being transferred to No. 2 Squadron.

The Royal Aircraft Factory B.E. (which stands for Blériot Experimental, meaning that it was a tractor-type airplane, which had been developed by Louis Blériot) was designed by Geoffrey de Havilland. It was a two-place, single-engine, two-bay biplane which was used as a trainer, reconnaissance aircraft, artillery spotter or bomber. An observer occupied the forward cockpit and the pilot was aft.

The B.E.2.b was essentially the same as the B.E.2.a, except the cockpit sides were higher. The elevator control cables were external from the pilot’s cockpit, aft. Probably the most significant change was the use of ailerons for the B.E.2.b, where the previous versions had used wing-warping like the original 1903 Wright Flyer.

The fuselage was constructed of a wooden framework, cross-braced with wires. The wings had wood spars and ribs. The airframe was covered in doped fabric.

The wings of the 2.a and 2.b were straight with no dihedral. Both upper and lower wings had the same span and chord, and were not staggered. (The B.E.2.c added both dihedral and stagger.) The lower wing spars were connected through the fuselage with steel tubing. The landing gear had both wheels and tires, but also wood-covered steel tube skids extending forward to protect the propeller from contacting the ground.

The B.E.2.a–2.b was 29 feet, 6½ inches (9.004 meters) long with a wingspan of 38 feet, 7½ inches (11.773 meters). The wings’ chord was 6 feet, 4 inches (1.930 meters). It had an empty weight of 1,274 pounds (578 kilograms) and gross weight of 1,600 pounds (726 kilograms).

The B.E.2, B.E.2.a and B.E.2.b were powered by an air-cooled, normally-aspirated 6.949 liter (424.036 cubic inch) Renault Type WB side-valve 90° V-8 engine with two valves per cylinder and a compression ratio of 4.12:1. The WB was rated at 70 horsepower at 1,750 r.p.m. The engine drove a four-bladed, fixed-pitch wooden propeller at one-half crankshaft speed. The Renault WB was 3 feet, 9.5 inches (1.556 meters) long, 2 feet, 8.8 inches (0.833 meters) high and 2 feet, 5.8 inches (0.757 meters) wide. It weighed 396 pounds (180 kilograms).

The airplane had a maximum speed of 70 miles per hour (113 kilometers per hour) at Sea Level and 65 miles per hour (105 kilometers per hour) at 6,500 feet (1,981 meters). It could climb to 3,000 feet (914 meters) in 9 minutes and to 7,000 feet (2,134 meters) in 35 minutes. The service ceiling was 10,000 feet (3,048 meters). Maximum endurance was 3 hours.

The B.E.2.b was unarmed. The crew could only defend themselves with their personal weapons. The type was easy prey for German fighters. It could carry a small bomb.

Although designed by the Royal Aircraft Factory, Farnbourough, only 6 B.E.2s were built there. The remainder were built by Armstong Whitworth, British and Colonial Airplane Co., Coventry Ordnance Works, Handley Page, Hewlett and Blondeau, and Vickers. Eighty-five of the B.E.2.b variant were produced, with most being used as trainers. Nineteen were sent to the Expeditionary Force in France, and one to the Middle East Brigade. By late 1915, the type had been almost completely replaced by the improved B.E.2.c.

© 2018, Bryan R. Swopes

12 August 1985

Aviation, , , , , , ,
Japan Air Lines’ Boeing 747-146SR, JA8119. (Robin787)

12 August 1985: The worst accident involving a single aircraft occurred when a Boeing 747 operated by Japan Air Lines crashed into a mountain in the Gunma Prefecture, killing 520 persons. There were just 4 survivors.

JAL Flight 123 was a Boeing 747-146SR, registration JA8119. It departed Tokyo International Airport enroute Osaka International Airport. There were 15 crewmembers, led by Captain Masami Takahama, with First Officer Yutaka Sasaki and Second Officer Hiroshi Fukuda. There were 509 passengers aboard.

Flight 123 lifted off at 6:12 p.m., 12 minutes behind schedule. 12 minutes after takeoff, as the 747 was at its cruising altitude, the fuselage rear pressure bulkhead suddenly failed, causing explosive decompression of the cabin. Cabin air then rushed into the unpressurized tail section. The resulting overpressure caused a failure of the APU bulkhead and the support structure for the vertical fin. The airliner’s vertical fin separated from the fuselage. All four of the 747’s hydraulic systems were ruptured. The hydraulic system was quickly depleted, leaving the crew unable to move any flight control surfaces.

JAL 123 following loss of its vertical fin.

Control of the airplane began to quickly deteriorate and the only control left was to vary the thrust on the four turbofan engines. The flight crew began an emergency descent and declared an emergency.

For the next 32 minutes, JA8119 flew in large uncontrolled arcs. The 747 rolled into banks as steep as 60°, and at one point, the nose pitched down into a dive reaching 18,000 feet per minute (91 meters per second). The crew was able to bring the 747 back to a nose-high attitude at about 5,000 feet (1,524 meters), but again lost control. At 6:56 p.m., JAL 123 disappeared from air traffic control radar.

Mount Takamagahara, 1,978.6 meters above Sea Level. (Σ64, via Wikipedia)

The airliner struck a ridge on 1,978.6 meter (6,491.5 feet) Mount Takamagahara at 340 knots (391 miles per hour, or 630 kilometers per hour), then impacted a second time at an elevation of 5,135 feet (1,565 meters). The aircraft was totally destroyed.

The four survivors had been seated in the last three rows of the airliner, though their exact seat assignments have not been determined. Several others actually survived the impact but died from their injuries and exposure before they could be rescued.

Investigation of the accident determined that the 747 had previously been damaged when its tail struck the runway during a landing, 2 June 1978. The rear pressure bulkhead had cracked as a result of the tail strike, but was repaired by a team of Boeing technicians. After the crash, it was discovered that the repair had not been correctly performed. Boeing engineers calculated that it could be expected to fail after 10,000 cycles. It was on the 12,219th cycle when the bulkhead failed.

Boeing 747-146SR JA8119 had accumulated a total of 25,030 flight hours by the time of the accident, on 18,835 flights.

Computer-generated image depicting the damage to JAL Flight 123. (Anynobody via Wikipedia)

© 2017, Bryan R. Swopes

12 August 1960

Aviation, Space Flight, , , , , , , , , , ,
Major Robert M. White, U.S. Air Force. (NASA)

12 August 1960: At Edwards Air Force Base, California, Major Robert M. White flew the North American Aviation X-15 rocketplane to an altitude of 136,500 feet (41,605 meters), exceeding the previous unofficial record of 126,200 feet (38,466 meters) set by the late Captain Iven C. Kincheloe, Jr., with the Bell X-2, 7 September 1956.

Iven Kincheloe had been assigned as the Air Force’s project pilot for the X-15. When he was killed on a routine flight, Bob White was designated to replace him.

This was White’s fourth flight in an X-15, and the 19th flight of the X-15 Program. The Number 1 rocketplane, serial number 56-6670, was carried aloft under the right wing of the “mothership,” Boeing NB-52A Stratofortress 52-003. At 08:48:43.0 a.m., PDT, 56-6670 was dropped over Silver Lake, near the Nevada-California border. White fired the two Reaction Motors XLR11-RM-13 rocket engines and they burned for 256.2 seconds.

This flight took place in Phase II of the Program and was intended to gradually increase the envelope of X-15 performance with the XLR11 engines while waiting for the much more powerful XLR99. The purpose of Flight 19 was to reach maximum altitude in order to test the rocketplane’s stability and controllability above the atmosphere.

The X-15 accelerated to Mach 2.52, 1,773 miles per hour (2,853 kilometers per hour) while climbing at nearly a 70° angle and reached a peak altitude of 136,500 feet (41,605 meters). After engine shutdown, White glided to a landing on Rogers Dry Lake and touched down. The duration of the flight was 11 minutes, 39.1 seconds.

Neither Kincheloe’s or White’s altitudes are recognized as records by the Fédération Aéronautique Internationale(FAI). Over the next few years, the X-15 would reach to nearly three times higher.

An X-15 is dropped from the NB-52A, 52-003, at an altitude of 45,000 feet at 0.8 Mach. (NASA)

© 2016, Bryan R. Swopes

12 August 1908

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Signal Corps Dirigible No. 1 at Fort Myer, Virginia, 1908 (U.S. Army)

12 August 1908: Test flights begin for Signal Corps Dirigible No. 1 at Fort Myers, Virginia, with Thomas Scott Baldwin as pilot and Glenn Hammond Curtiss as flight engineer.

Brigadier General James Allen, Chief Signal Officer, 1906–1913. (U.S. Army)

On 1 August 1907, Brigadier General James Allen, Chief Signal Officer, United States Army, issued a directive establishing the Aeronautical Division within the Signal Corps. Captain Charles Chandler was the officer in charge. Specifications were published in Signal Corps Bulletin No. 5, soliciting bids for both lighter- and heavier-than air vehicles. There were 41 responses. Plans were submitted and a board of officers selected plans for those that seemed most practical.

The lighter-than-air craft was required to be a self-propelled dirigible (a “directable” balloon) able carry two persons and to be able to travel at 20 miles per hour (32.2 kilometers per hour). Thomas Scott Baldwin’s proposal was selected. (The Wright brothers’ Military Flyer was selected as the heavier-than-air winner on 2 August 1909, and designated Signal Corps Airplane No. 1.)

Signal Corps Dirigible No. 1 (SC-1) emerges from its shed at Fort Myer, Virginia, 3 August 1908. (Carl Harry Claudy/NASM-Claudy-205)

On 3 August 1908, Baldwin No. 8 was presented to the Army for trials. Although the the Baldwin No. 8 reached an average speed of just 19.61 miles per hour (31.56 kilometers per hour). It demonstrated the required endurance of two hours, averaging 14 miles per hour (22.5 kilometers per hour). Although the airship’s speed was short of the requirement, on 5 August, the Army purchased it from Baldwin for $5,737.59. The airship was designated Signal Corps Dirigible No. 1.

Contemporary sources give the airship’s dimensions as being 96 feet (29.26 meters) long with a maximum diameter of 19 feet, 6 inches (5.94 meters). The envelope was made of two layers of silk fabric separated by a layer of vulcanized rubber, and supported by 30 wooden frames. Buoyancy was provided by hydrogen gas. The envelope’s volume was approximately 20,000 cubic feet (566 cubic meters).

An open girder beam gondola (or “car”) built of spruce was suspended beneath the balloon. The gondola was 66 feet (20.12 meters) long with a  2½ feet × 2½ feet (0.76 × 0.76 meters) cross section. A water-cooled Curtiss-built inline four-cylinder gasoline engine was mounted at the front end of the gondola. The engine produced 20 horsepower and drove the tractor propeller through a steel drive shaft at 450 r.p.m. The two-bladed spruce propeller had a diameter of 10 feet, 8 inches (3.25 meters) and pitch of 11 feet (3.35 meters).

A two-plane “box-kite” canard elevator unit behind the engine provided control for pitch. The pilot was located behind the control surfaces. Another crew member was at the rear of the gondola, followed by a fixed cruciform stabilizer unit.

The dirigible had a lifting capacity of  1,350 pounds (612.4 kilograms). The payload was 500 pounds (226.8 kilograms).

The U.S. Army’s first aviators, Lieutenants Benjamin D. Fulois, Thomas Etholen Selfridge and Frank P. Lahm were taught to fly the airship. Lahm and Fulois made the first flight of an all-Army crew on 26 August.

Signal Corps Dirigible No. 1 was assigned to the Signal Corps Post at Fort Omaha, Nebraska, where the Army had a balloon factory. It was operated there until 1912. The airships envelope needed to be replaced, and unwilling to spend money for that, the airship was sold.

Second Lieutenants Lahm and Fulois flying Signal Corps Dirigible No. 1 (SC-1) at Fort Myer, Virginia, 28 August 1908. (U.S. Air Force)

© 2017, Bryan R. Swopes

11 August 1986: The World’s Fastest Helicopter

Aviation, , , , , , , , , , , , , ,
Westland Lynx AH.1 G-LYNX.

11 August 1986: A modified factory demonstration Westland Lynx AH.1 helicopter, civil registration G-LYNX, piloted by Chief Test Pilot John Trevor Egginton and Flight Test Engineer Derek J. Clews, set a Fédération Aéronautique Internationale (FAI) Absolute Record for Speed for helicopters over a straight 15/25 km course with an average speed of 400.87 kilometers per hour (249.09 miles per hour) over a measured 15 kilometer (9.32 miles) course near Glastonbury on the Somerset Levels and Moors, Southwest England.¹ ² ³

Westland WG.13 Lynx G-LYNX, c/n 102. (Vertipedia)

The helicopter was equipped with experimental BERP main rotor blades and two Rolls Royce Gem 60 turboshaft engines with digital electronic fuel control and water-methanol injection, producing 1,345 shaft horsepower, each. The engines’ exhausts were modified to provide 600 pounds of thrust (2,669 Newtons). The horizontal tail plane and vertical fins from a Westland WG.30 were used to increase longitudinal stability and to unload the tail rotor in forward flight. In an effort to reduce aerodynamic drag, items such as steps, antennas and windshield wipers were removed.

During the speed runs, the main rotor blade tips reached a speed of 0.97 Mach.

Four passes over the course were made at an altitude of 500 feet (150 meters). The results of the two best successive passes were averaged. This set records for helicopters; helicopters in the 3,000–4,500 kilogram weight class; and an Absolute World Record for Rotorcraft. Thirty-two years later, these official speed records still stand.

Westland Lynx AH.1, G-LYNX. This is the World's Fastest Helicopter. (Westland)
Westland Lynx AH.1, G-LYNX. This is the World’s Fastest Helicopter. (Westland)

Another Westland AH.1 Lynx, flown by then Westland Chief Pilot Leonard Roy Moxham and Michael Ball, had set two FAI World Records for Speed, 20 and 22 June 1972. Flying over a straight 15/25 kilometer course, the Lynx averaged 321.74 kilometers per hour (199.92 miles per hour).⁴ Two days later, the Lynx flew a closed 100 kilometer circuit at an average speed of 318.50 kilometers per hour (197.91 miles per hour).⁵ Both of these records were for helicopters in the 3,000–4,500 kilogram weight class.

Westland WG.13 c/n 102 made its first flight in May 1979. After setting the speed record, G-LYNX was used as a demonstrator and as a test platform, before finally being retired in 1992. Beginning in 2007, AgustaWestland restored the Lynx to its speed record configuration, withe more than 25,000 man hours expended on the project.

G-LYNX was unveiled on 11 August 2011, the 25th anniversary of the world record flight. Today, it is on display at The Helicopter Museum, Weston-super-Mare, Somerset, South West England.

On 25 September 2014, the Institution of Mechanical Engineers bestowed its Engineering Heritage Award on G-LYNX. John Wood, chairman of the Institution said,

“The G-Lynx helicopter is a remarkable example of British engineering and vision. It is a testament to the cutting-edge modifications made to the helicopter, that the world speed record still stands 28 years later.

“This award is in recognition of all the people in making the 1986 record possible, but also to the AgustaWestland apprentices who restored the helicopter in 2011 and the Helicopter Museum who continue to maintain the craft in such excellent condition.”

The Engineering Heritage Award was accepted by Elfan Ap Rees, founder of the Helicopter Museum, and John Trevor Egginton, pilot of the world record helicopter.

John Trevor Egginton, O.B.E., A.F.C., FRAeS. Chief Test Pilot, Westland Helicopters. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight test Engineers)

John Trevor Egginton was born in Birmingham, England, 14 March 1933. He was the second child of Alfred T. Egginton and Emma Hammond Egginton. John attended the George Dixon Grammar School at Edgbaston, a suburb of Birmingham.

In 1951, Egginton joined the Royal Air Force. On 7 May 1952, he was appointed a cadet pilot, with date of service from 2 January 1952. He was sent to the United States for flight training, and returned to England aboard RMS Queen Elizabeth, arriving at Southampton, 17 November 1953. He flew the Canadair CL-13 Sabre Mk.4 with No. 67 Squadron and the Hawker Hunter with Nos. 222 and 63 Squadrons.

In December 1956, Pilot Officer Egginton married Miss Joan Mary Wheeler at Bromsgrove, near Birmingham. They would have three children, Jane, Michael and Frazer.

Pilot Officer Egginton was promoted to the rank of Flight Lieutenant, 2 October 1957. His commission was made permanent, 31 August 1961.

Following an overseas tour of duty in the Colony of Aden, Flight Lieutenant Egginton transitioned to helicopters, training in the Bristol Sycamore. He was then assigned to No. 22 Squadron at RAF Chivenor, on the north coast of Devon, as a search and rescue pilot. The squadron was equipped with the Westland Whirlwind HAR.2, a licensed variant of the Sikorsky S-55. In August 1962, the unit upgraded to the turboshaft-powered Whirlwind HAR.10.

On the night of 2–3 November 1962, the French fishing trawler Jeanne Gougy, with a crew of 18 men, went aground at Land’s End, Cornwall. A Royal Air Force helicopter from RAF Chivenor and a lifeboat from the Sennen Cove life boat station went to the scene. The lifeboat was unable to approach the wreck because of the heavy weather, but recovered two dead fishermen offshore. The helicopter also recovered a body. No other sailors were seen, the the two rescue craft returned to there bases with the remains.

Later that morning, observers from the shore saw several men inside the Jeanne Gougy‘s pilot house. A helicopter and the Penlee lifeboat, Soloman Brown, hurried to the scene, but conditions were still too extreme for the lifeboat to approach the trawler.

The Westland Whirlwind, flown by Flight Lieutenants John Lorimer Neville Canham, D.F.C., and John Trevor Egginton, hovered over the capsized fishing trawler while the winch operator, Sergeant Eric Charles Smith, was lowered to the ship’s pilot house. A rescue line was also rigged to the nearby rocks. Sergeant Smith rigged two men for hoisting to the hovering helicopter and continued searching for additional survivors. Four sailors were rescued by the line to the shore. 12 of the fishermen did not survive.

Westland Whirlwind HAR.10, No. 22 Squadron, hoists a man from the fishing trawler Jeanne Gougy at Armoured Knight Rock, Land’s End, Cornwall, England, 3 November 1962. (RNLI Penlee Lifeboat Station)
Sergeant Eric Smith, RAF, is lowered to the wreck of Jeanne Gougy, 3 November 1962. (BFI)

For his bravery during the rescue, Sergeant Smith was awarded the George Medal by Queen Elizabeth II. He was also awarded the Silver Medal of the Société des Hospitalers Sauveteurts Bretons.

The President of the French Republic, Charles de Gaulle, conferred the honor of Chevalier du Mérite Maritime on Flight Lieutenant Canham, Flight Lieutenant Egginton, and Sergeant Smith. On 13 June 1964, Egginton was awarded the Air Force Cross.

In 1965, Flight Lieutenant Egginton attended the Empire Test Pilots’ School at RAF Boscombe Down. On graduation, he was assigned as a helicopter test pilot with D Squadron (now the Rotary Wing Test and Evaluation Squadron, or RWTES). In 1969, Egginton returned to the Test Pilots’ School as a helicopter flight instructor.

Squadron Leader Egginton retired from the Royal Air Force in 1973. He was awarded the Queen’s Commendation for Valuable Service in the Air, 2 June 1973. (London Gazette No. 45984 at Page 6463)

Egginton joined Westland Helicopters at Yeovil as deputy chief test pilot, and later became the company’s chief test pilot. He from Westland retired after 15 years.

In the 1989 New Year’s Honours List, Squadron Leader Egginton was appointed an Officer of the Most Excellent Order of the British Empire (O.B.E.):

Squadron Leader John Trevor Egginton, O.B.E., A.F.C., F.R.Ae.S., Q.C.V.S.A., Chevalier du Mérite Maritime, died at his home in Yeovil, 23 November 2014. He was 81 years of age.

In April 2013, Trevor Egginton spoke to members of the Empire Test Pilots’ School at The Helicopter Museum, Weston-super-Mare. In this photograph, Mr. Egginton is seated in the World Record Helicopter’s pilot seat. (The Helicopter Museum)

¹ FAI Record File Number 11659: Rotorcraft, Absolute Record for Speed Over a 15–25 Kilometer Straight Course

² FAI Record File Number 1842: Rotorcraft, Helicopters, Subclass E-1e, 3,000–4,500 kilograms (6,613.9–9,920.8 pounds), takeoff weight

³ FAI Record File Number 1843: Rotorcraft, Helicopters, Subclass E-1

⁴ FAI Record File Number 1826: Rotorcraft, Helicopters, Subclass E-1e

⁵ FAI Record File Number 1853: Rotorcraft, Helicopters, Subclass E-1e

Westland Lynx G-LYNX.

© 2018, Bryan R. Swopes