23 April 1941: At North American Aviation’s Inglewood, California factory, test pilot Louis S. Wait takes the very first production Mustang Mk.I, AG345, (c/n 73-3098) for its first flight.
The Royal Air Force had contracted with NAA to design and build a new fighter with a 1,200 horsepower Allison V-1710 supercharged 12-cylinder engine. The first order from the British Purchasing Commission was for 320 airplanes, and a second order for another 300 soon followed.
The Mustang Mk.I (NAA Model NA-73) was a single-place, single-engine fighter primarily of metal construction with fabric control surfaces. It was 32 feet, 3 inches (9.830 meters) long with a wingspan of 37 feet, 5/16-inches (11.373 meters) and height of 12 feet, 2½ inches (3.721 meters). The airplane’s empty weight was 6,280 pounds (2,849 kilograms) and loaded weight was 8,400 pounds (3,810 kilograms).
The Mustang Mk.I was powered by a liquid-cooled, supercharged 1,710.597-cubic-inch-displacement (28.032 liter) Allison Engineering Company V-1710-F3R (V-1710-39) single overhead cam (SOHC) 60° V-12 engine with a compression ratio of 6.65:1. The -F3R had a Maximum Continuous Power rating of 880 horsepower at 2,600 r.p.m. at Sea level, and 1,000 horsepower at 11,000 feet (3,353 meters). It was rated at 1,150 horsepower at 3,000 r.p.m. for Take Off and Military Power. The Allison V-12 drove a 10 foot, 9 inch (3.277 meter) diameter, three-bladed Curtiss Electric constant-speed propeller through a 2.00:1 gear reduction. The V-1710-F3R was 7 feet, 4.38 inches (2.245 meters) long, 3 feet, 0.54 inches (0.928 meters) high, and 2 feet, 5.29 inches (0.734 meters) wide. It weighed 1,310 pounds (594 kilograms).
The Mustang Mk.I had a cruise speed of 311 miles per hour (500.5 kilometers per hour) at 75% power, and a maximum speed of 384 miles per hour (618 kilometers per hour) at 19,000 feet (5,791 meters). The airplane could reach 20,000 feet (6,096 meters) in 8.80 minutes. The service ceiling was 32,000 feet (9,754 meters) and its range was 640 miles (1,030 kilometers).
The Mk.I was equipped with four Browning AN-M2 .50-caliber machine guns, with one in each wing and two mounted in the nose under the engine. Four Browning .303 Mk.II machine guns were also installed, with two in each wing.
The Mk.I was 30 m.p.h. (48 kilometers per hour) faster than its contemporary, the Curtiss P-40 Warhawk, though both used the same engine. Below 15,000 feet (4,572 meters), the Mustang was also 30–35 m.p.h (48–56 kilometers per hour) faster than a Supermarine Spitfire, which had the more powerful Roll-Royce Merlin V-12.
Two Mustang Mk.Is, AG348 and AG354, were taken from the first RAF production order and sent to Wright Field for testing by the U.S. Army Air Force. These airplanes, assigned serial numbers 41-038 and 41-039, were designated XP-51. They would be developed into the legendary P-51 Mustang. In production from 1941 to 1945, a total of 16,766 Mustangs of all variants were built.
AG345 was retained by North American Aviation for long term testing. It was stricken off charge 3 December 1946.
23 April 1918: at 09:55 a.m., near Saint-Gobain, France, 1st Lieutenant Paul Frank Baer, 103rd Aero Squadron (Pursuit), shot down an enemy Albatross C two-place biplane. This was Baer’s fifth victory in aerial combat, making him the first American “ace.” ¹
Paul Frank Baer was born 29 January 1894 at Fort Wayne, Indiana, the fourth of four children of Alvin E. Baer, a railroad engineer, and Emma B. Parent Baer.
In 1916, Paul Baer served under Brigadier John J. General Pershing during the Mexican Expedition to capture the outlaw and revolutionary Francisco (“Pancho”) Villa.
He then went to France and enlisted the Aéronautique Militaire, in 20 February 1917. He was sent for flight training at the Avord Groupemant des Divisions d’Entrainment (G.D.E.). He graduated as a pilot, 15 June 1917, with the rank of corporal. After flight training, Corporal Baer was assigned to Escadrille SPA 80, under the command of Capitaine Paul Ferrand, 14 August 1917 to 20 January 1918, flying the SPAD S.VII C.1 and SPAD S.XIII C.1. Baer was next transferred to Escadrille N. 124, the EscadrilleAméricaine, under Georges Thénault. This unit was equipped with the Nieuport-Delâge Ni-D 29 C1.
After the United States entered the War, Baer was transferred to the 103rd Aero Squadron, American Expeditionary Forces, and commissioned as a 1st Lieutenant with a date of rank retroactive to 5 November 1917. At that time, the 103rd was under the command of Major William Thaw II, and was operating near La Cheppe, France, flying the SPAD S.VII C.1 chasseur.
Lieutenant Baer is officially credited with 9 victories, and claimed an additional 7. After shooting down his ninth enemy airplane on 22 May 1918, Baer and his SPAD S.XIII C.1 were also shot down. He was seriously injured and was captured by the enemy near Armentières and held as a Prisoner of War. At one point, Baer was able to escape for several days before being recaptured.
For his service in World War I, 1st Lieutenant Paul Frank Baer was awarded the United States’ Distinguished Service Cross with one oak leaf cluster (a second award). He was appointed Chevalier de laLégion d’honneur by Raymond Poincaré, the President of France. He was also awarded the Croix de Guerre with seven palms.
After World War I, Baer, as a “soldier of fortune,” organized a group of pilots to fight against “the Bolsheviks” in Poland. He returned to the United States, departing Boulogne-sur-mer aboard T.S.S. Nieuw Amsterdam, and arriving at New York City, 4 November 1919. He then flew as a test pilot, an air mail pilot in South America, and worked as an aeronautical inspector for the U.S. Department of Commerce, based at Brownsville Airport, Texas. In 1930, he was employed as a pilot for the China National Aviation Corporation.
Baer was flying from Nanking to Shanghai for with an amphibious Loening Air Yacht biplane, named Shanghai. The airplane crashed after striking the mast of a boat on the Huanpu River. He died at the Red Cross Hospital at Shanghai, China, at 9:00 a.m., 9 December 1930. A Chinese pilot, K. F. Pan, and an unidentified female passenger were also killed. General Hsiung Shih-hui and four other passengers on board were seriously injured.
Paul Baer’s remains were returned to the United States aboard S.S. President McKinley and were buried at the Lindenwood Cemetery in Fort Wayne, Indiana.
In 1925 a new airport was opened in Fort Wayne and named Paul Baer Municipal Airport. During World War II, the airport was taken over by the military and designated Baer Army Airfield. It is now Fort Wayne International Airport (FWA).
¹ TDiA would like to thank CMSgt Bob Laymon USAF (Ret.) (AKA, “Scatback Scribe”) for pointing out that while Lt. Baer was the first American to become an ace flying in the American service, that,
23 April 1915: Lieutenant Patrick Neison Lynch Bellinger, United States Navy, flew a Burgess-Dunne hydroaeroplane to an altitude of 10,000 feet (3,048 meters) over Pensacola Bay, Florida.
The Aero Club of America certified Lieutenant Bellinger’s record:
Homolgation of the altitude record made by Lieut. P. N. L. Bellinger at Pensacola Bay, Fla., on April 23rd last has been officially recognized and awarded as follows: American altitude record, aviator alone, hydroaeroplane, 10,000 feet. This height was reached in one hour, nineteen minutes. It is interesting to note the climbing record in connection with this flight, 6,000 feet being attained in 24 minutes and 8,000 feet in 41 minutes.
—Flying, Vol. IV, No. 5, June, 1915, The Aero Club of America, Club News, Page 554 at Column 1
The Burgess-Dunne Model BD-5, U.S. Navy serial number AH-10, was a licensed variant of the British Short Brothers-built Dunne D.5. The configuration was designed by Lieutenant John William Dunne, F.R.Ae.S., and was based on his observations of the Roemer’s Alsomitra macrocarpa seeds, although his design essentially reversed the aerodynamic features of the seed.
According to Wikipedia:
The seed or samara of this species is unusual in having two flat bracts extending either side of the seed to form a wing-like shape with the seed embedded along one long edge and the wings angled slightly back from it. As the seed ripens the wings dry and the long edge furthest from the seed curls slightly upwards. When ripe, the seed drops off and its aerodynamic form allows it to glide away from the tree. The wing spans some 13 cm and can glide for great distances. The seed moves through the air like a butterfly in flight — it gains height, stalls, dips and accelerates, once again producing lift, a process termed phugoid oscillation. In the past it was often found on the decks of ships at sea.
The seed’s relative stability in pitch and roll inspired Igo Etrich, a pioneer of early aviation. The contemporary pioneer J.W. Dunne also studied the seed but discarded it as inspiration because it was not directionally stable.
The BD-5 was a two-place, single-engine, four-bay biplane with a single pontoon and wingtip-mounted floats. The wings were swept 30° and the lower wing was staggered significantly behind the upper. Both wings had anhedral, and the upper wing had slightly more area and a negative twist. There was no tail, rudder or elevators. The ailerons also acted as elevators. The design was very stable and it could not be forced into a stall.
The Burgess-Dunne was 24 feet, 8 inches (7.518 meters) long, with a wingspan of 46 feet, 0 inches (14.021 meters). The wings have a chord of 6 feet, 0 inches (1.829 meters) vertical gap between the wings was 6 feet, 0 inches (1.829 meters). The total wing area is 545 square feet (50.63 square meters). The airplane’s empty weight was 1,450 pounds (658 kilograms), and it had a gross weight of 1,700 pounds (771 kilograms).
The pontoon had a single hydrodynamic step. It was 17 feet, 8 inches (5.385 meters) long, 3 feet, 1 inch (0.940 meters) wide and had a maximum depth of 1 foot, 2 inches (0.356 meters).
The airplane was powered by a water-cooled, normally-aspirated 567.450-cubic-inch-displacement (9.299 liter) Curtiss OXX-2 overhead valve 90° V-8 engine with dual ignition. It had two valves per cylinder, a compression ratio of 4.92:1, and produced 100 horsepower at 1,400 r.p.m. The OXX-2 was a direct-drive engine and turned a two-bladed, 8 foot (2.4 meter) diameter propeller in a pusher configuration.
The Burgess-Dunne had a fuel capacity of 22 Imperial gallons (100 liters) and carried 4 gallons (18 liters) of lubricating oil.
During flight testing, the Burgess-Dunne Hydroaeroplane averaged 58.75 miles per hour (94.55 kilometers per hour) ground speed over a triangular course with a 10 knot wind (11.5 miles per hour, or 5.4 meters per second).
One Burgess-Dunne had been ordered by the Navy on 5 December 1914. The cost was $5,000.00, less engine. It was delivered in April, 1915. After being flown to the altitude record, AH-10 was used for artillery spotting at Fort Monroe, Virginia. It was the first U.S. Navy aircraft to be armed with a machine gun, a .30-caliber Benét-Mercié machine rifle, and bomb racks.
On 7 March 1916, AH-10 was damaged in a collision with a sailing vessel off Mobile, Alabama. The pilot, Lieutenant Edward Orrick McDonnell, U.S. Navy, was not hurt. After repair, the airplane was returned to service. (Lieutenant McDonnell had been awarded the Medal of Honor for his actions at the Battle of Veracruz, 21–22 April 1914. He rose to the rank of Vice Admiral.)
Patrick Neison Lynch Bellinger was born 8 October 1885 at Cheraw, South Carolina. He was the son of Carnot Ambrose Bellinger and Eleanor Lynch Bellinger.
A 1907 graduate of the U.S. Naval Academy, Annapolis, Maryland, he served at sea aboard the battleship USS South Carolina (BB-26) before being assigned as captain of the C-class submarine, C-4 (SS-14). He was then assigned to aviation. Lieutenant Bellinger was Naval Air Pilot No. 4.
During the Veracruz campaign, 1914, Lieutenant Bellinger flew reconnaissance over enemy lines. It was here that a United States military airplane first came under enemy fire. He was nominated for the Medal of Honor for his actions there.
In 1919 he was awarded the Navy Cross, “For distinguished service in the line of his profession as commanding officer of the seaplane NC-1 which made a long overseas flight from Newfoundland to the vicinity of the Azores in May 1919.”
Lieutenant Commander Bellinger married Elsie McKeown of Pennsylvania, 24 July 1915. She died at Washington, D.C., 9 February 1920. He married his second wife, Miriam Georgia Benoist, 14 April 1921.
Bellinger progressively rose in rank and responsibility. As rear admiral, he commanded Patrol Wing 2 at Pearl Harbor at the time of the surprise attack by the Imperial Japanese Navy. During World War II, he was promoted to the rank of Vice Admiral and served as Commander Air Force, Atlantic Fleet. Vice Admiral Bellinger retired from the Navy in 1947.
Vice Admiral Patrick Neison Lynch Bellinger, United States Navy (Retired), died 29 May 1962 at the Chesapeake & Ohio Hospital, Clifton Forge, Virginia. He is buried at the Arlington National Cemetery.
22 April 1961: Jackie Cochran set 18 Fédération Aéronautique Internationale (FAI) records in one day flying a Lockheed L-1329 JetStar, construction number 5003, FAA registration N172L, and named The Scarlett O’Hara. The route of her flight was New Orleans–Boston–Gander–Shannon–London–Paris–Bonn, with refueling stops at Gander and Shannon.
According to the U.S. Centennial of Flight Commission, Jackie Cochran “…set more speed and altitude records than any other pilot.”
The following are the FAI records that she set on 22 April 1961:
4609, 4615: Speed over a recognized course, Gander, NF (Canada)–Shannon (Ireland): 829.69 kilometers per hour (515.546 miles per hour)
4611, 4616: Speed over a recognized course, Gander, NF (Canada)–London (UK): 749.11 kilometers per hour (465.475 miles per hour)
4612, 4617: Speed over a recognized course, Gander, NF (Canada)–Paris (France): 746.22 kilometers per hour (463.680 miles per hour)
4613, 4618: Speed over a recognized course, Gander, NF (Canada)–Bonn (FRG): 728.26 kilometers per hour (452.520 miles per hour)
4638: Speed over a recognized course, Boston, MA (USA)–Gander, NF (Canada): 816.32 kilometers per hour (507.238 miles per hour)
4639, 4640: Speed over a recognized course, Boston, MA (USA)–Shannon (Ireland): 565.45 kilometers per hour (351.354 miles per hour)
4641, 4642: Speed over a recognized course, Boston, MA (USA)–London (UK): 558.50 kilometers per hour (347.036 miles per hour)
4643, 4644: Speed over a recognized course, Boston, MA (USA)–Paris (France): 564.88 kilometers per hour (351.000 miles per hour)
4645, 4646: Speed over a recognized course, Boston, MA (USA)–Bonn (FRG): 562.56 kilometers per hour (349.559 miles per hour)
12322: Distance, New Orleans, LA (USA)–Gander, NF (Canada): 3,661.33 kilometers (2,275.045 miles)
The Lockheed L-1329 JetStar was the first in a category of small-to-medium-sized jet transports that would become known as the “business jet.” Like many Lockheed airplanes, it was designed by a team led by Clarence L. “Kelly” Johnson, and he retained the first prototype as his personal transport.
The JetStar is operated by two pilots and can be configured for 8 to 10 passengers. The airplane is 60 feet, 5 inches (18.41 meters) long with a wingspan of 54 feet, 5 inches (16.59 meters) and overall height of 20 feet, 5 inches (6.22 meters). The leading edge of the wings are swept to 30°. The JetStar has an empty weight of 24,750 pounds (11,226 kilograms) and maximum takeoff weight (MTOW) of 44,500 pounds.
The two prototype JetStars were powered by two Bristol Siddeley Orpheus engines, but the production models were powered by four Pratt & Whitney JT12A-8 turbojets engines which produced 3,300 pounds of thrust, each. The JetStar 731 was a modification program to replace the turbojet engines with quieter, more efficient and more powerful Garrett AiResearch TFE731 turbofan engines which increased thrust to 3,700 pounds per engine. New production JetStar II airplanes were equipped with these turbofans.
The JetStar’s cruise speed is 504 miles per hour (811 kilometers per hour) and its maximum speed is 547 miles per hour (883 kilometers per hour) at 30,000 feet (9,145 meters). The service ceiling is 43,000 feet (13,105 meters) and range is 2,995 miles (4,820 kilometers).
The Lockheed JetStar was in production from 1957 to 1978. 204 were built as civil JetStars and military C-140A Flight Check and C-140B and VC-140B JetStar transports.
The JetStar flown by Jackie Cochran on her record setting flight from New Orleans to Bonn, construction number 5003, eventually was acquired by NASA and assigned to the Dryden Flight Test Center at Edwards Air Force Base, California. It was reregistered as N814NA, and used the call sign NASA 4. No longer in service, NASA 4 is on display at the Joe Davies Heritage Airpark at Air Force Plant 42, Palmdale, California.
22 April 1912: Departing at 5:47 a.m., Denys Corbett-Wilson flew his Blériot XI from Fishguard and Goodwick, Pembrokeshire, Wales, across St. George’s Channel and landed at Crane, near Enniscorthy, County Wexford, Ireland, 1 hour, 40 minutes later. This was the first crossing of the Irish Sea from England to Ireland by air.
Corbett-Wilson, having flown in heavy rain for the final half hour, with an erratic compass and misfiring engine, saw a field at Crane that he thought was suitable for landing his airplane. The area was too small, though, and he ran into heavy brush, slightly damaging the Blériot.
The damaged airplane was stored at the stables of Lord Donoughmore’s Estate. Many years later the estate was sold and the wreck was purchased. It was later donated to a museum in Kilkenny.
Denys Corbett-Wilson was born at Thames Ditton, Surrey, England, on Christmas Eve, 24 December 1882. He was the son of W.H.C. Wilson, Esq., Barrister-at-Law, and Ada Caroline Corbett-Wilson.
Corbett-Wilson learned to fly at Pau, France in 1911. A sportsman and “an intrepid rider to hounds,” he joined the Royal Flying Corps at the beginning of World War I and was commissioned a second lieutenant, Special Reserve, Royal Flying Corps. He served with No. 3 Squadron at Béthune, France, and was promoted to lieutenant in November 1914.
Lieutenant Denys Corbett-Wilson was killed in action while on a reconnaissance flight along the Western Front, 10 May 1915. His airplane, a Morane-Saulnier Type L, was struck by an artillery shell. He was buried with full military honors at Fournes-en-Weppes by the German Army.
The Blériot XI was a single-seat, single-engine monoplane, designed by Raymond Saulnier and built by Louis Charles Joseph Blériot. It was 24 feet, 11 inches (7.595 meters) long with a wingspan of 27 feet, 11 inches (8.509 meters) and overall height of 8 feet, 10 inches (2.692 meters). The wings had a chord of 6 feet (1.829 meters). The airplane had an empty weight of 507 pounds (229.9 kilograms).
In its original configuration, the airplane was powered by an air-cooled, 3.774 liter (230.273 cubic inches) R.E.P. two-row, seven-cylinder fan engine (or “semi-radial”) which produced 30 horsepower at 1,500 r.p.m., driving a four-bladed paddle-type propeller. The R.E.P. engine weighed 54 kilograms (119 pounds). This engine was unreliable and was soon replaced by an air-cooled 3.534 liter (215.676 cubic inch) Alessandro Anzani & Co., 60° (some sources state 55°) three-cylinder “fan”-type radial engine (or W-3) and a highly-efficient Hélice Intégrale Chauvière two-bladed fixed-pitch propeller, which had a diameter of 6 feet, 8 inches (2.032 meters).
The Anzani W-3 was a direct-drive, right-hand tractor engine which produced 25 horsepower at 1,400 r.p.m. It was 1.130 meters (3 feet 8.49 inches) long, 1.500 meters (4 feet, 11.01 inches) high, and 0.720 meters (2 feet, 4.35 inches) wide. The engine weighed 66 kilograms (145.5 pounds).
After 1910, the Blériot XI was often equipped with a Gnome rotary engine. This was a normally-aspirated, air-cooled, 7.983 liter (487.140-cubic-inch-displacement) Société des Moteurs Gnome Omega 7-cylinder rotary engine which produced 50 horsepower at 1,200 r.p.m. The direct-drive engine turned a two-bladed wooden propeller in a left-hand, pusher configuration. The Omega 7 is 79.2 centimeters (2 feet, 7.2 inches) long, 83.8 centimeters (2 feet, 9.0 inches) in diameter, and weighs 75.6 kilograms (166.7 pounds). The prototype of this engine is in the collection of the Smithsonian Institution National Air & Space Museum.
The Blériot XI had a maximum speed of 47 miles per hour (76 kilometers per hour) and the service ceiling was (3,280 feet) 1,000 meters.