23 April 1915

Lieutenant Commander Patrick Neison Lynch Bellinger, United States Navy.

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

Burgess-Dunne Model BD-5, U.S. Navy serial number AH-10.
Burgess-Dunne hydroaeroplane, U.S.N. serial number AH-10. (United States Navy)
Lieutenant John William Dunne, Wiltshire Regiment, British Army. (The Sketch, 19 May 1909)

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.[6][7] 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.[8] 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.

Alsomitra macrocarpa seed. (Scott Zona/Wikipedia)

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.

Burgess-Dunne Hydroaeroplane, 1914. (FLIGHT First Aero Weekly in the World, No. 286 (Vol. VI, No. 25), 19 June 1914 at page 645.)

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.)

Burgess-Dunne AH-10 hydroaeroplane at Naval Air Station Pensacola, Florida, circa 1917. (National Naval Aviation Museum)

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 commanding officer of the C-class submarine, C-4 (SS-15). He was then trained as an airplane pilot. Lieutenant Bellinger was Naval Air Pilot No. 4.

United States Navy Submarine C-4, circa 1912–1914. (U.S. Navy NH92096)

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.

Lieutenant Commander Bellinger, United States Navy, circa 1919.

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.

Lieutenant Commander Patrick N. L. Bellinger, U.S. Navy. (Portrait by Harris & Ewing, Washington D.C., 18 January 1920)

© 2019, Bryan R. Swopes

22 April 1962

Jackie Cochran in the cockpit of The Scarlett O'Hara, a record-setting Lockheed L-1329 JetStar, N172L. (FAI)
Jackie Cochran in the cockpit of The Scarlett O’Hara, a record-setting Lockheed L-1329 JetStar, N172L at Hanover-Langenhagen Airport, 22 April 1962. (FAI)

22 April 1962: 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 first production Lockheed JetStar, c/n 5001, in service with the Federal Aviation Administration, registered N1. (bizjets101)

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.

Lockheed L-1329 JetStar (FAI)

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.

Lockheed L-1329 JetStar, N814NA, NASA 4, on static display at Edwards Air Force Base, California. (NASA)
Lockheed L-1329 JetStar, N814NA, NASA 4, on static display at the Joe Davies Heritage Airpark, Palmdale, California. (NASA)

© 2016, Bryan R. Swopes

22 April 1912

Denys Corbett-Wilson at Fishguard, Wales, 22 April 1912. (VisitWexford)

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.

Lieutenant Denys Corbett-Wilson

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.

Denys Corbett Wilson's Blériot XI was slightly damaged after running out of room for landing at Crane, Wexford, ireland, 22 April 1912. (Corbett Wilson collection)
Denys Corbett-Wilson’s Blériot XI was slightly damaged after running out of room for landing at Crane, Wexford, Ireland, 22 April 1912. (Corbett-Wilson collection)

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, tractor 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.

Denys Corbett Wilson with a Bleriot XI-2 at Highcliffe, near Christchurch, New Zealand, 18 June 1913. This version o fteh airplane is powered by an air-cooled Gnome 7 cylinder rotary engine producing 80 horsepower.
Denys Corbett-Wilson with a Blériot XI-2 at Highcliffe, near Christchurch, Dorset, 18 June 1913. This version of the airplane is powered by an air-cooled 487.140-cubic-inch (7.983 liter) Gnome Omega 7-cylinder rotary engine, producing 50 horsepower at 1,200 r.p.m. (Christchurch History Society)

© 2017, Bryan R. Swopes

21 April 1972, 02:23:35 UTC, T + 104:29:35

Apollo 16 Lunar Module Orion at the Descartes Highlands.
Apollo 16 Lunar Module Orion at the Descartes Highlands.

21 April 1972, 02:23:35 UTC: Lunar Module Orion (LM-11) touched down on the surface of the Moon at the Descartes Highlands. On board were the Mission Commander, Captain John Watts Young, United States Navy, and Lunar Module Pilot Lieutenant Colonel Charles M. Duke, Jr., United States Air Force. They were the ninth and tenth humans to stand on the Moon.

Technical problems delayed Orion‘s descent for three orbits. Lieutenant Commander Thomas K. (Ken) Mattingly II, U.S.N., the Command Module Pilot, remained in lunar orbit aboard Casper (CSM-113).

As they neared the surface they started to see dust blowing at about 80 feet (24 meters). The lunar module hovered briefly before continued downward.

104:29:22 Duke: Okay, 2 down. Stand by for contact. Come on, let her down. You leveled off. (Pause) Let her on down. Okay, 7. . . 6 percent [fuel remaining]. Plenty fat.

104:29:36 Duke: Contact! Stop. (Pause while they drop to the surface) Boom.

During a debriefing, John Young said,

“When we got the Contact light, I counted ‘one-potato’ and shut the engine down. The thing fell out of the sky the last three feet. I know it did. I don’t know how much we were coming down, maybe a foot a second.”  ¹

Teh surface of the Moon as seen through the window of the Lunar Module, shortly after landing. (NASA)
The surface of the Moon as seen through the window of the Lunar Module, shortly after landing. (NASA)

Young and Duke remained on the surface for 2 days, 23 hours, 2 minutes, 12 seconds. ² During that time, they performed three EVAs totaling 20 hours, 14 minutes, 14 seconds. ³ They drove their Lunar Roving Vehicle 16.6 miles (26.7 kilometers).

Looking northeast at John Young with the LRV, 22 April 1972. (Charles M. Duke, Jr./NASA)
Looking northeast at John Young with the LRV, 22 April 1972. (Charles M. Duke, Jr./NASA)

A remote television camera was placed on the surface and captured color images of the Lunar Module Ascent Stage departing the Moon for lunar orbit at 01:25:47 UTC, 24 April 1972. ⁴

Ascent Stage launch, 01;25:47 UTC, 24 April 1972. (NASA)
Ascent Stage launch, 01:25:47 UTC, 24 April 1972. (NASA)

¹ FAI Record File Number 2301. Greatest Mass Landed on a Celestial Body: 8 257,6 kilograms (18,204.9 pounds)

² FAI Record File Number 2303. Duration of Stay on the Surface of a Celestial Body: 71 hours, 02 minutes, 13 seconds

³ FAI Record File Number 17099: Duration Extravehicular Stay on the Surface of Moon or Planet: 39 hours, 47 minutes, 3 seconds [TDiA note: EVA 1, 118:53:38—126:04:40, 7 hours, 11 minutes, 2 seconds. EVA 2, 142:39:35—150:02:44, 7 hours, 23 minutes, 9 seconds. EVA 3, 165:31:28—171:11:31, 5 hours, 40 minutes, 3 seconds. Total of EVAs 1, 2 and 3: 20 hours, 14 minutes, 14 seconds.]

⁴ FAI Record File Number 17098: Greatest Mass Lifted to Lunar or Planetary Orbit from the Lunar or Planetary Surface: 4 965,5 kilograms (10,947.05 pounds)

© 2019, Bryan R. Swopes

20–21 April 1964

Lockheed L-100 Hercules N1130E, in flight. Both outboard engines are shut down and the propellers feathered. (Lockheed Martin)

20–21 April 1964: Nearly ten years after the first flight of the Lockheed YC-130 Hercules prototype, the Lockheed Model 382, serial number 3946, the commercial version of the military C-130E, made the longest first flight in history when it flew for 25 hours, 1 minute, after taking off from Marietta, Georgia.

The flight crew, led by Chief Production Pilot Joe Garrett, flew the Hercules in a racetrack pattern over Georgia and Alabama, and for all but 36 minutes of the flight, the outboard engines were shut down and their propellers feathered.

The Lockheed Model 382 was certified by the Federal Aviation Administration 16 February 1965.

Lockheed personnel celbrate the 25 hour, 1 minute first flight of the commercial L100 Hercules. (Lockheed Martin)
Lockheed personnel celebrate the 25 hour, 1 minute first flight of the commercial L-100 Hercules. (Lockheed Martin)

The L-382 was powered by four Allison 501-D22 turboprop engines, rated at 3,755 shaft horsepower at 13,820 r.p.m., and driving four-bladed Hamilton Standard Hydromatic constant-speed, reversible-pitch propellers with a diameter of 13 feet, 6 inches (4.115 meters). at 1,020 r.p.m.

Maximum operating altitude 32,600 feet (9.936 meters)

N1130E at Fairbanks, leased to Alaska Airlines. (Lockheed Martin)
N1130E at Fairbanks, leased to Alaska Airlines, 1965. (Lockheed Martin)

N1130E was retained by Lockheed as a demonstrator, however it was briefly leased to Alaska Airlines in March 1965, and returned the following month.

The L-382 was converted to the L382E-44K-20 standard in April 1968, with a 5 foot, 0 inch (1.524 meters) segment added to the fuselage behind the cockpit, and a 3 foot, 4 inch (1.016 meter) section behind the wing.

N1130E's fuselage was cut in two places to accommodate an 8 foot, 4 inch ( meter) stretch. (Lockheed Martin)
N1130E’s fuselage was cut in two places to accommodate an 8 foot, 4 inch (2.540 meter) stretch. (c-130hercules.net)
N1130E after conversion to the L100-20 configuration, at Lockheed-Burbank Airport, 1968. (Unattributed)
N1130E after conversion to the L100-20 configuration, at Lockheed-Burbank Airport, 1968. (c-130hercules.net)

N1130E was leased to Delta Air Lines in October 1968, and returned after six months.

Lockheed sold N1130E to Pepsico Airlease Corporation, who leased the freighter to Flying W Airways. It was reregistered as N50FW. In March 1973 Pepsico sold it to Philippine Aerotransport and it was operated for the Philippine government, first as PI-97, then RP-97, and finally, RP-C97. The Hercules was placed in storage in March 1981. With a total flight time of 13,144.8 hours, it was scrapped 18 February 2014.

The first commercial Lockheed L-100, s/n 3946, in service with the Republic of the Philippines. (Ken Fielding via flickr)
The first commercial Lockheed L-100, s/n 3946, in service with the Republic of the Philippines. (Ken Fielding via flickr)

After 71 years, the Lockheed Hercules remains in production, and both military and civil versions are in service worldwide.

Lockheed Martin Model 382J Super Hercules (Lockheed Martin)
Lockheed Martin Model 382J Super Hercules, N100J. (Lockheed Martin)

© 2018, Bryan R. Swopes