Category Archives: Aviation

4–5 March 1944

Flight Officer Charles E. Yeager with his North American Aviation P-51B Mustang. (littlefriends.co.uk)
Flight Officer Charles E. Yeager, Air Corps, Army of the United States, with his North American Aviation P-51B-5-NA Mustang, 43-6763, “Glamourus Glen.” (littlefriends.co.uk)

4 March 1944: Flight Officer Charles E. Yeager, Air Corps, Army of the United States, was leading an element of White Flight, 363d Fighter Squadron, 357th Fighter Group, southeast of Kassel, Germany. Yeager was flying a North American Aviation P-51B Mustang, 43-6763, named Glamourus Glen and marked B6 Y. It was his seventh combat mission. At 13:05 British Standard Time, he observed a Messerschmitt Bf 109G fighter. He wrote (errors in original):

Leading the second element of Chambers White Flight, I was flying at 26,000 feet [7,925 meters] when I spotted a Me. 109 to the right and behind us about 2,000 feet [610 meters] below. I broke right and down. The E/A [Enemy Aircraft] turned right and down and went onto a 50° dive. I closed up fast and opened fire at 200 yards [183 meters]. I observed strikes on fuselage and wing roots, with pieces flying off. I was overrunning so I pulled up and did an aleron roll and fell in behind again and started shooting at 150 yards [137 meters]. The e/A engine was smoking and wind-milling. I overran again, observing strikes on fuselage and canopy. I pulled up again and did a wingover on his tail. His canopy flew off and the pilot bailed out and went into the overcast at 9,000 feet [2,743 meters]. The E/A had a large Red and Black “Devil’s Head’ on the left side of the ship. The E/A took no evasive action after the first burst.

A flight of three Luftwaffe Messerschmitt Me 109 fighters, 20 July 1944. (Bundsarchive Bild 101l-676-7975-36)
A flight of three Luftwaffe Messerschmitt Bf 109 fighters, 20 July 1944. (Bundsarchive Bild 101l-676-7975-36)

Flight Officer Yeager’s combat report indicates that he fired 461 rounds of .50 caliber ammunition. He was credited with one enemy aircraft destroyed. (He previously had claimed another enemy plane shot down over the English Channel, but that was not credited.)

The following day, 5 March, Yeager was again in the cockpit of Glamourus Glen. A Focke-Wulf Fw 190A 4 flown by Unteroffizier Irmfried Klotz, shot him down east of Bourdeaux, France.

In his autobiography, Chuck Yeager wrote:

. . . The world exploded and I ducked to protect my face with my hands, and when I looked a second later, my engine was on fire, and there was a gaping hole in my wingtip. The airplane began to spin. It happened so fast, there was no time to panic. I knew I was going down; I was barely able to unfasten my safety belt and crawl over the seat before my burning P-51 began to snap and roll, heading for the ground. I just fell out of the cockpit when the plane turned upside down—my canopy was shot away.

Yeager: an Autobiography, by Charles E. Yeager and Leo Janos, Bantam Books, New York, 1985, Chapter 4 at Page 26.

Focke-Wulf Fw 190A-3, June 1942. (Imperial War Museum)

Yeager was slightly wounded. His Mustang was destroyed. Over the next few months he evaded enemy soldiers and escaped through France and Spain, returning to England in May 1944. He returned to combat with a new P-51D Mustang, and by the end of World War II was officially credited with 11.5 enemy aircraft destroyed.

Colonel Yeager became Commandant of the U.S. Air Force Aerospace Research Pilot School at Edwards Air Force Base, 23 July 1962. (U.S. Air Force)

Yeager remained in the Air Force until retiring in 1975 with the rank of brigadier general, and having served 12,222 days. He was a world famous test pilot, breaking the sound barrier with a Bell XS-1 rocketplane, 14 October 1947. He commanded F-86H Sabre and F-100D fighter bomber squadrons, flew the B-57 Canberra over Southeast Asia during the Vietnam War, and commanded the Air Force Flight Test Center at Edwards Air Force Base in the high desert of southern California.  General Yeager celebrated his 94th birthday 13 February 2017.

Identical to the Inglewood, California-built North American Aviation P-51B Mustang, this is a Dallas, Texas-built P-51C-1-NT, 42-103023. (North American Aviation, Inc.)
Identical to the Inglewood, California-built North American Aviation P-51B Mustang, this is a Dallas, Texas-built P-51C-1-NT, 42-103023. (North American Aviation, Inc.)

The North American Aviation P-51 Mustang is a single-place, single-engine long range fighter. It is a low-wing monoplane with retractable landing gear and is of all-metal construction. The fighter is powered by a liquid-cooled V-12 engine. It was originally produced for the United Kingdom’s Royal Air Force as the Mustang Mk.I. Two examples were provided to the U.S. Army Air Corps, designated XP-51. This resulted in orders for the P-51A and A-36 Apache dive bomber variant. These early Mustangs were powered by the Allison V-1750 engine driving a three-bladed propeller, which also powered the Lockheed P-38 Lightning and Curtiss P-40 Warhawk.

In 1942, soon after the first  production Mustang Mk.I arrived in England, Rolls-Royce began experimenting with a borrowed airplane, AM121, in which they installed the Supermarine Spitfire’s Merlin 61 engine. This resulted in an airplane of superior performance.

In the United States, the Packard Motor Car Company of Detroit, Michigan, had begun building Merlin engines under license from Rolls-Royce. These American engines were designated V-1650. North American modified two P-51s from the production line to install the Packard V-1650-3. These were designated XP-51B. Testing revealed that the new variant was so good that the Army Air Corps limited its order for P-51As to 310 airplanes and production was changed to the P-51B.

Cutaway illustration shows the internal arrangement of the P-51B/C Mustang. (Eugene Clay, North American Aviation, Inc.)

The P-51B and P-51C are virtually Identical. The P-51Bs were built by North American Aviation, Inc., at Inglewood, California. P-51Cs were built at North American’s Dallas, Texas plant. They were 32 feet, 2.97 inches (9.829 meters) long, with a wingspan of 37 feet, 0.31-inch (11.282 meters) and overall height of 13 feet, 8 inches (4.167 meters) high. The fighter had an empty weight of 6,985 pounds (3,168 kilograms) and a maximum gross weight of 11,800 pounds (5,352 kilograms).

P-51Bs and Cs were powered by a right-hand tractor, liquid-cooled, supercharged, 1,649-cubic-inch-displacement (27.04-liter) Packard V-1650-3 or -7 Merlin single overhead cam (SOHC) 60° V-12 engine which produced 1,380 horsepower at Sea Level, turning 3,000 r.p.m at 60 inches of manifold pressure (V-1650-3) or 1,490 horsepower at Sea Level, turning 3,000 r.p.m. at 61 inches of manifold pressure (V-1650-7). (Military Power rating, 15 minute limit.) These were license-built versions of the Rolls-Royce Merlin 63 and 66. The engine drove a four-bladed Hamilton Standard Hydromatic constant-speed propeller with a diameter of 11 feet, 2 inches (3.404 meters) through a 0.479:1 gear reduction.

A Packard Motor Car Company V-1650-7 Merlin liquid-cooled, supercharged SOHC 60° V-12 aircraft engine at the Smithsonian Institution National Air and Space Museum. This engine weighs 905 pounds (411 kilograms) and produces 1,490 horsepower at 3,000 r.p.m. (NASM)
A Packard Motor Car Company V-1650-7 Merlin liquid-cooled, supercharged SOHC 60° V-12 aircraft engine at the Smithsonian Institution National Air and Space Museum. This engine weighs 905 pounds (411 kilograms) and produces 1,490 horsepower at 3,000 r.p.m. (NASM)

The P-51B/C had a cruise speed of 362 miles per hour (583 kilometers per hour) and the maximum speed was 439 miles per hour (707 kilometers per hour) at 25,000 feet (7,620 meters). The service ceiling was 41,900 feet (12,771 meters). With internal fuel, the combat range was 755 miles (1,215 kilometers).

Armament consisted of four Browning AN-M2 .50-caliber machine guns, mounted two in each wing, with 350 rounds per gun for the inboard guns and 280 rounds per gun for the outboard.

1,988 P-51B Mustangs were built at North American’s Inglewood, California plant and another 1,750 P-51Cs were produced at Dallas, Texas. This was nearly 23% of the total P-51 production.

North American Aviation P-51B-1-NA Mustang in flight. (Air Force Historical Research Agency)
North American Aviation P-51B-1-NA Mustang in flight. (Air Force Historical Research Agency)

© 2021, Bryan R. Swopes

4 March 1936

Airship Hindenburg, D-LZ129, at Friedrichsafen, Germany
Airship Hindenburg, D–LZ 129, over Friedrichshafen, Germany, March 1936. (Unattributed)
Dr. Hugo Eckener

4 March 1936: The airship Hindenburg (D–LZ 129) made its first flight at Friedrichshafen, on the north shore of Lake Constance in southern Germany. In command was Hugo Eckener,¹ chairman of Luftschiffbau Zeppelin GmbH. There were 87 passengers and crew aboard.

The airship was operated by a flight crew of 40, with 12 stewards and cooks. There were 50 passenger sleeping berths in private cabins, with large public areas on the upper, “A” deck, with crew quarters, galley, a public bar and smoking lounge on the lower “B” deck. The ship’s control station was located in a gondola below the forward part of the hull.

The airship was designed by Ludwig Dürr. Its rigid structure was built of triangular-section duralumin girders (a specially heat-treated alloy of aluminum and copper, and anodized blue for corrosion protection). There were 15 ring frames and 36 longitudinals.

The airship’s control surfaces were operated by electric servo motors.

The Zeppelin’s covering was cotton fabric painted with a cellulose varnish which had been impregnated with aluminum powder, both to give it the silver color, but also to act as a reflector to protect the sixteen hydrogen-filled bouyancy gas bags contained inside from heat and ultraviolet light.

Hindenburg's dining room (Speisesaal).
Hindenburg‘s dining room (Speisesaal). (O. v. Stetten)

Hindenburg was 803 feet, 10 inches (245.008 meters) long, with a diameter of 135 feet, 1 inch (41.173 meters). Hindenburg had a gross weight of approximately 215,000 pounds (97,522 kilograms).

The huge airship was powered by four liquid-cooled, fuel-injected, 88.514 liter (5,401.478-cubic-inch-displacement) Daimler-Benz DB 602 50° V-16 diesel engines with 4 valves per cylinder and a compression ratio of 16:1. Mounted in a pusher configuration, the engines turned 19 foot, 8.4 inch (6.005 meter) diameter, four-bladed fixed-pitch wooden propellers through a 0.50:1 gear reduction. The DB 602 had a cruise power rating of 850 horsepower at 1,350 r.p.m. It could produce 900 horsepower at 1,480 r.p.m., and a maximum 1,320 horsepower at 1,650 r.p.m. (5 minute limit). The engines could be run in reverse. The DB 602 was 2.69 meters (8 feet, 10 inches) long, 1.02 meters (3 feet, 4 inches) wide and 1.35 meters (4 feet, 5 inches) high. Each engine weighed 1,976 kilograms (4,356 pounds).

A Daimler-Benz DB 602 V-16 diesel airship engine at the Zeppelin Museum Friedrichshafen. (Wikipedia)
This photograph shows Hindeburg's duralumin structure and a latex/cotton hydrogen cell. A walkway goes through the center of the cell.
This photograph shows Hindenburg‘s duralumin structure and a latex/cotton hydrogen cell. A walkway goes through the center of the cell. (Luftschiffbau Zeppelin GmbH)

Lift was provided by 16 hydrogen gas cells which were made of multiple layers of cotton fabric which was brushed with latex gelatin. These contained 7,062,000 cubic feet (199,974 cubic meters) of hydrogen with a lift capacity of 511,500 pounds (232,013 kilograms), nearly double the airship’s weight when fully loaded.

LZ 129 had a cruising speed of 76 miles per hour (122 kilometers per hour) and a maximum speed of 84 miles per hour (135 kilometers per hour).

Airship Hindenburg, D-LZ129, moored.
Airship Hindenburg, D–LZ 129, moored at Lakehurst, New Jersey, 1936. (U.S. Navy).

¹ Eckner is universally referred to as “Dr. Eckener.” He earned a doctorate from the Institute for Experimental Psychology, University of Leipzig, 1892.

© 2019, Bryan R. Swopes

3 March 1942

KNILM Douglas DC-3 PK-AFV derelict on a beach north of Broome, Western Australia.
KNILM Douglas DC-3 PK-AFV derelict on a beach north of Broome, Western Australia. (Geoff Goodall’s Aviation History Site)
Captain Ivan Vasilyevich Smirnov
Captain Ivan Vasilyevich Smirnov

3 March 1942: A Koninklijke Nederlandsch-Indische Luchtvaart Maatschappij (KNILM) Douglas DC-3 airliner, registration PK-AFV, named Pelikaan, was flying from Bandoeng, Java, Dutch East Indies, to Broome, Western Australia. The flight was under the command of Captain Ivan Vasilyevich Smirnov, a World War I fighter ace of the Imperial Russian Air Service. There were three other crew members and eight passengers on board.

And A£300,000 in diamonds.¹

At about 10:30 a.m., as the DC-3 approached the shore of Western Australia, it was attacked by three Mitsubishi A6M2 Navy Type 0 Model 21 (“Zero”) fighters of the Third Kokutai, Imperial Japanese Navy, then based at Timor. The flight was lead by Lieutenant Zenjiro Miyano, IJN.

Lieutenant Zenjiro Miyano, Imperial Japanese Navy. (Ciel de Gloire)

Captain Smirnov and several others were wounded and the airliner’s left engine caught fire. Smirnov made a crash landing on a beach at Carnot Bay, approximately 50 miles (80 kilometers) north of Broome. The fighters continued to strafe the DC-3 on the beach.

The following day, 4 March, the airliner was bombed by a Kawanishi H6K “Mavis” four-engine flying boat, but there was no further injury or damage.

Over the next several days, four of the passengers died of wounds. The survivors were rescued on 9 March.

The diamonds disappeared.

A beach comber, John (“Diamond Jack”) Palmer, later turned in a parcel of diamonds which he said he had found on the beach. These were valued at A£20,447, but were only about 10% of the original amount. Palmer was charged with stealing the diamonds, and he and two others, John Arthur Mulgrue and Frank Archibald Robinson, were charged with unlawfully receiving the diamonds. They were prosecuted in 1943, but all were acquitted.

Wreck of KNILM Douglas DC-3 PH-AFV, north of Broome, Western Australia, 1942.

PK-AFV was a Douglas DC-3-194B, serial number 1965, built in 1937. It was one of twenty-three DC-3s operated by Koninklijke Luchtvaart Maatschappij N.V. (KLM, or Royal Dutch Airlines) and was originally registered PH-ALP. It was transferred to KNILM in the Dutch East Indies in June 1940.

KLM Douglas DC-3-194B PH-ALP (Gavin2806)

The Douglas DC-3 was an all-metal, twin-engine civil transport with retractable landing gear. The airplane was operated by a pilot and co-pilot and could carry up to 21 passengers.

The DC-3-194B was 64 feet, 5 inches (19.634 meters) long with a wingspan of 95 feet (28.956 meters). It was 16 feet, 11 inches (5.156 meters) high. The airplane weighed approximately 18,000 pounds (8,165 kilograms) empty and had a gross weight of 25,200 pounds (11,431 kilograms). The -194Bs were built with the passenger door on the right side of the fuselage.

The DC-3-194B was powered by two air-cooled, supercharged, 1,829.39-cubic-inch-displacement (29.978 liter) Pratt & Whitney Twin Wasp two-row, 14-cylinder radial engines. The specific engine variant is not known. The engines drove three-bladed Curtiss Electric propellers.

[Douglas C-47 Skytrains were equipped with the R-1830-92 (Pratt & Whitney Twin Wasp S1C3-G). These had a maximum continuous rating for normal operation was 1,060 horsepower at 2,550 r.pm., up to 7,500 feet (2,286 meters), and 1,200 horsepower at 2,700 r.p.m., at Sea Level, for takeoff. Each engine drives a three-bladed Hamilton Standard Hydromatic constant-speed full-feathering propeller with a diameter of 11 feet, 6 inches (3.505 meters) through a 16:9 gear reduction. The R-1830-92 is 48.19 inches (1.224 meters) long, 61.67 inches (1.566 meters) in diameter, and weighs 1,465 pounds (665 kilograms).]

The DC-3 had a cruise speed of 150 miles per hour (241 kilometers per hour) and maximum speed of 237 miles per hour (381 kilometers per hour) at 8,500 feet (2,591 meters). The airplane had a service ceiling 24,000 feet (7,315 meters), and its range was 1,025 miles (1,650 kilometers).

The Douglas DC-3 was in production for 11 years with 10,655 civil and C-47 military airplanes built, and another 5,000 license-built copies. Over 400 are still in commercial service.

¹ Equivalent to approximately A$26,922,580.65 in 2025.

© 2025, Bryan R. Swopes

2 March 1978

Republic F-105F-1-RE Thunderchief (converted to F-105G Wild Weasel III) 63-8321, 561st TFS, 35th TFW, at George AFB, Victorville, California. (Image from Michael Klaver Collection at www.thexhunters.com)
Republic F-105F-1-RE Thunderchief (converted to F-105G Wild Weasel III) 63-8321, 561st TFS, 35th TFW, at George AFB, Victorville, California. (Image from Michael Klaver Collection at www.thexhunters.com)

2 March 1978: Major Charles Thomas Fulop and First Lieutenant William A. Stone departed George Air Force Base, Victorville, California, in a Republic F-105G Thunderchief, 63-8321, call sign “Thud 71.” Their mission was a routine instrument training flight, making instrument approaches and departures at NAS Point Mugu on the southern California coast, then return to George AFB.

The weather surrounding Point Mugu was poor, with heavy clouds, rain and fog. Thud 71 made an instrument approach to the airfield and then initiated a missed approach, a normal procedure for a training flight. However, while climbing out, the pilot, Major Fulop, radioed Mugu Approach Control that he had a problem and requested an immediate return to George AFB. His request was approved.

Approach Control then lost the fighter bomber’s radar transponder signal. Fulop declared an emergency, and requested an immediate return to Point Mugu for landing. He stated that the altimeter had failed and that he was trying to climb above the clouds.

Moments later, witnesses in Thousand Oaks and Newbury Park saw the F-105 diving out of the overcast. Major Fulop initiated the ejection sequence for the Electronics Warfare Officer, Lieutenant Stone, in the back seat. Stone was ejected and parachuted to safety. He suffered a broken arm.

The witnesses said that the pilot was obviously steering the Thunderchief away from homes surrounding the open space of Wildwood Regional Park. Thud 71 crashed on the west side of Hill Canyon. The airplane exploded on impact and Major Fulop was killed.

The crash site is less than two miles (three kilometers) from where I am now sitting.

Major Charles T. Fulop, United States Air Force, with his Republic F-105G Thunderchief at George Air Force Base, california.
Major Charles Thomas Fulop, United States Air Force, 561st Tactical Fighter Squadron, 35th Tactical Fighter Wing, with a Republic F-105G Wild Weasel III at George Air Force Base, California. (www.thexhunters.com)

Charles Thomas Fulop was born 6 October 1946 at Barberton, Ohio. He was the second son of Louis James Fulop and Elizabeth Theresa Ittes Fulop. He graduated from Copley High School in Akron, Ohio. He then attended Miami University, Oxford,  where he was a member of the Delta Chi fraternity, graduating in 1968.

Fulop joined the United States Air Force, 14 May 1969. He was trained as a B-52 navigator. Later selected for flight training, Captain Fulop was assigned to Class 73-06 at Laughlin Air Force Base, Del Rio, Texas. He was an Outstanding Graduate and was awarded his pilot’s wings, 26 February 1973. Captain Fulop was then assigned to a McDonnell Douglas F-4 Phantom II squadron at Homestead Air Force Base, Florida.

On 20 December 1969, Charles Fulop married Miss Cheryl P. Lewis at Sacramento, California. They would have two daughters, Michelle and Kelley.

Major Fulop was buried in the Veteran’s Court at Saint Mary’s Catholic Cemetery, Sacramento, California.

Republic F-105G Thunderchief 63-9320 Wild Weasel at the National Museum of the United States Air Force. This is the sister ship of Thud 71. (U.S. Air Force)

The F-105 was the largest single-seat, single-engine combat aircraft in history. It was designed as a Mach 2+ tactical nuclear strike aircraft and fighter-bomber. The fuselage of the F-105B incorporated the “area rule” which gave the Thunderchief its characteristic “wasp waist” shape. The F-105F was a two-place variant, flown by a pilot and a weapons system operator. Its high speed, low radar cross-section, and heavy bomb load capacity made it a good candidate for the “Wild Weasel” mission: locating and attacking enemy radar and surface-to-air missile installations.

The F-105F/G Thunderchief was 67 feet (20.422 meters) long with a wingspan of 34 feet, 11 inches (10.643 meters) and overall height of 20 feet, 2 inches (6.147 meters). Its wings were swept 45° at 25% chord. The angle of incidence was 0° and there was no twist. The wings had 3° 30′ anhedral. The total wing area was 385 square feet (35.8 square meters). Modified to the Wild Weasel III configuration, it had an empty weight of 31,279 pounds (14,188 kilograms), and a maximum takeoff weight of 54,580 pounds (24,757 kilograms).

Republic F-105G Wild Weasel III 63-8320, sister ship of Major Fulop’s 63-8321. (U.S. Air Force)

The Thunderchief was powered by one Pratt & Whitney J75-P-19W engine. The J75 is a two-spool axial-flow afterburning turbojet with water injection. It has a 15-stage compressor section (8 low- and and 7 high-pressure stages) and 3-stage turbine section (1 high- and 2 low-pressure stages.) The J75-P-19W is rated at 14,300 pounds of thrust (63.61 kilonewtons), continuous power; 16,100 pounds (71.62 kilonewtons), Military Power (30-minute limit); and Maximum Power rating of 24,500 pounds (108.98 kilonewtons) with afterburner (15-minute limit). The engine could produce 26,500 pounds of thrust (117.88 kilonewtons) with water injection, for takeoff. The J75-P-19W is 21 feet, 7.3 inches (6.586 meters) long, 3 feet, 7.0 inches (1.092 meters) in diameter, and weighs 5,960 pounds (2,703 kilograms).

The F-105G Wild Weasel III had a cruising speed of 514 knots (592 miles per hour/952 kilometers per hour). Its maximum speed was 681 knots at Sea Level—0.78 Mach—and  723 knots (832 miles per hour/1,339 kilometers per hour) at 36,000 feet (10,973 meters)—Mach 1.23. It could climb to 30,000 feet (9,144 meters) in 28.0 minutes. The F-105G’s combat ceiling was 43,900 feet (13,381 meters), and it had a combat radius of 391 nautical miles (450 statute miles/724 kilometers). The maximum ferry range, with external fuel tanks, was 1,623 nautical miles (1,868 statute miles/3,006 kilometers).

A Republic F-105G Wild Weasel III, serial number 62-4423, of the 6010th Wild Weasel Squadron, takes of from Korat Royal Thai Air Base, circa 1971. The modified Thunderchief is armed with an AGM-45 Shrike on the outboard hardpoint, and an AGM-78 Standard HARM on the right inboard hardpoint. (U.S. Air Force)

The Wild Weasel III was armed with one M61A1 Vulcan 20 mm six-barrel rotary cannon with 581 rounds of ammunition, one AGM-78 Standard High-Speed Anti-Radiation Missile (HARM),  and two AGM-45A Shrike anti-radiation missiles.

65 F-105Fs were converted to the F-105G Wild Weasel III configuration. Republic Aviation Corporation built 833 F-105 Thunderchief fighter bombers at its Farmingdale, New York, factory. 334 of them were lost in combat during the Vietnam War.

Thud 71’s sister ship, Republic F-105G Thunderchief 63-8320, shot down three enemy MiG fighters. It is on display at the National Museum of the United States Air Force, Wright Patterson Air Force Base, Ohio.

Republic F-105F-1-RE Thunderchief (converted to F-105G Wild Weasel III) 63-8320 at the National Museum of the United States Air Force, Wright-Patterson AFB. (U.S. Air Force)
Republic F-105F-1-RE Thunderchief (converted to F-105G Wild Weasel III) 63-8320 at the National Museum of the United States Air Force, Wright-Patterson AFB. (U.S. Air Force)

© 2021, Bryan R. Swopes

2 March 1969

Aérospatiale Concorde 001 first flight, at Toulouse, 2 March 1969, test pilot André Edouard Turcat.
Aérospatiale Concorde 001 first flight, at Toulouse, 2 March 1969, test pilot André Edouard Turcat.

2 March 1969: Just three weeks after the prototype Boeing 747, City of Everett, made its first flight at Seattle, Washington, the first supersonic airliner prototype, Aérospatiale-BAC Concorde Aircraft 001, registration F-WTSS, made its first flight, taking off from Runway 33 at the Aéroport de Toulouse-Blagnac, Toulouse, France.

On the flight deck were André Édouard Marcel Turcat, Henri Perrier, Michel Retif and Jacques Guinard.

The flight lasted 27 minutes. Throughout the flight, the “droop nose” and landing gear remained lowered.

Concorde was the only commercial airliner capable of cruising at supersonic speeds.

The flight test crew of Concorde 001. Left to right, Andre Edouard Turcat, Henri Perrier, Michel Retif and Jacques Guinard. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
The flight test crew of Concorde 001. Left to right, André Edouard Turcat, Henri Perrier, Michel Retif and Jacques Guinard. (Photograph courtesy of Neil Corbett, Test & Research Pilots, Flight Test Engineers)

There were two Concorde prototypes (the British Aerospace Corporation built Concorde 002) followed by two pre-production developmental aircraft and sixteen production airliners.

Aérospatiale-BAC Concorde 001, F-WTSS. (Aérospatiale)

Concorde 001 is 51.80 meters (169 feet, 11.4 inches) long, with a wingspan of 23.80 meters (78 feet, 1 inch). Its fuselage has a maximum height of 3.32 meters (10 feet, 10.7 inches) and maximum width of 2.88 meters (9 feet, 5.4 inches) max internal height 1.96 m (6 feet, 5.2 inches). The prototype’s empty weight is 78,700 kilograms (173,504 pounds), and the maximum takeoff weight is 185,000 kilograms (407,855 pounds). (Pre-production and production Concorde weights and dimensions vary.)

The Concorde is powered by four Rolls-Royce/SNECMA Olympus 593 Mk.610 engines. The Mk. 610 is a two-spool, axial-flow turbojet with afterburner. The compressor section as 14 stages (7 low- and 7 high-pressure stages). Two-stage turbine has 1 high- and 1 low-pressure stage. The engine has a maximum continuous power rating of 28,800 pounds of thrust (128.11 kilonewtons). It is rated at 37,080 pounds (164.94 kilonewtons) for takeoff (5 minute limit). During takeoff, the afterburners produce approximately 20% of the total thrust. The Olympus 593 Mk.613 is 1.212 meters (3.976378 feet) in diameter, 4.039 meters (13.251312 feet)long, and weighs 3,175 kilograms (7,000 pounds).

Production Concordes were certified for a maximum operating cruise speed of Mach 2.04, and a maximum operating altitude of 60,000 feet (18.288 meters). The maximum range 3,900 was nautical miles (4,488 statute miles/7,223 kilometers).

Concorde 001 made 397 flight during flight testing. It accumulated a total of 812 hours, 19 minutes of flight time, of which 254 hours, 49 minutes were supersonic.

Today, Concorde 001 is displayed at the Musée de l’Air et de l’Espace, Aéroport de Paris – Le Bourget.

Aérospatiale-BAC Concorde 001, F-WTSS. (Aérospatiale)
Aérospatiale-BAC Concorde 001, F-WTSS. (Aérospatiale)

André Édouard Marcel Turcat was born 23 October 1921 at Marseille, Bouches-du-Rhône, Provence-Alpes-Côte d’Azur, France. André was the son of Emile Gaston Turcat and Claire Victoria Jeane Marie Françoise Fleury Turcat. His uncle, Léon Turcat, was co-founder of Ateliers de Construction d’Automobiles Turcat-Méry SA, a manufactuers of grand prix race cars. He was educated at l’École Polytechnique in Palaiseau, a suburb southwest of Paris.

Turcat

During World War II, Turcat served in the Forces Aériennes Françaises Libres, (the  Free French Air Force).

On the day that World War II ended in Europe, 8 May 1945, André Turcat married Mlle Elisabeth Marie (“Julie”) Borelli in Marseille. They would have four children. One, a daughter, died in infancy.

Andre Turcat remained in the Armée de l’air after the war. He flew the Douglas C-47 Skytrain during the First Indochina War. He was awarded the Croix de Guerre des théâtres d’opérations extérieures.

In 1950, Turcat was admitted to the École du personnel navigant d’essais et de réception (EPNER), the test pilot school at Brétigny-sur-Orge, France. He served as director of EPNER, 1952–53.

In 1954, Major Turcat resigned from the Armée de l’air and became the chief test pilot at Société Française d’Etude et de Construction de Matériel Aéronautiques Spéciaux (SFECMAS) (later, Nord-Aviation), flight-testing the Nord 1500 Griffon. He made the first flight of the Nord 1500-01 Griffon, 20 September 1955. He flew the Griffon II, a mixed-propulsion aircraft powered by a turbojet and a ramjet engine, beginning with its first flight, 23 January 1957.

Flying a Griffon, Turcat set three Fédération Aéronautique Internationale (FAI) World Records for Time to Altitude, 16 February 1957: 6,000 meters, 1:17.05;¹ 9,000 meters, 1:33.75;² and 12,000 meters, 2:17.70.³

Turcat reached Mach 2.19 with the Griffon II, for which he was awarded the Harmon Trophy for 1958. The trophy was presented by Richard M. Nixon, 37th President of the United States.

On 25 February 1959, Turcat flew the Griffon II to set an FAI World Record for Speed Over a Closed Circuit of 100 Kilometers, with an average speed of 1,643.00 kilometers per hour (1.015.32 miles per hour).⁴ The Académie des Sports awarded him its Prix Robert Peugeot for the greatest feat accomplished by French athletes in motorsports.

André Edouard Marcel Turcat (fifth from right) with the Nord 1500-02 Griffon, circa January 1957

Turcat joined Sud-Aviation as chief pilot for the Concorde.

Turcat and British Aerospace chief test pilot Ernest Brian Trubshaw, C.B.E., M.V.O., shared the 1970 Harmon Trophy, and in 1971, the Iven C. Kincheloe Award of the Society of Experimental Test Pilots, Iven C. Kincheloe Award for their outstanding professional accomplishments in flight testing.

André Turcat and Brian Trubshaw.

After 740 flight hours in Concorde, Andre Turcat retired from Aérospatiale, 31 March 1976. He never flew an airplane again.

As a politician, M. Turcat served as deputy mayor of Toulouse, 1971–77; and as a member of the European Parliament, 1980–81.

In 1983, Turcat founded l’Académie nationale de l’air et de l’espace (ANAE) and served as its first president.

In 1990 Turcat earned a doctorate degree in the study of Christian art. He was the author of Pilote d’essais (Ciels du monde t.1); Concorde: Essais d’hier, betailles d’aujourd’hui, 30 and de réve; Les plus beaux textes de la Bible; Moi, Etienne Jamet, alias Esteban Jamete: Sculpteur français de la Renaissance en Espagne comdamné par l’Inquisition; and Une épopeé française.

During his aviation career, Turcat flew more than 6,500 hours in 110 different aircraft. He had been awarded the Médaille de l’Aéronautique. The United Kingdom had appointed him Commander of the Most Excellent Order of the British Empire (C.B.E.). In 2005 Andre Turcat was named Grand Officier Ordre national de la Légion d’honneur.

André Édouard Marcel Turcat died at his home in Aix-en-Provence, 3 January 2016 at the age of 94 years.

André Édouard Marcel Turcat (FlightGlobal)

¹ FAI Record File Number 8611

² FAI Record File Number 8612

³ FAI Record File Number 8613

© 2019, Bryan R. Swopes