Category Archives: Aviation

Medal of Honor, First Lieutenant Donald Dale Pucket, United States Army Air Corps

First Lieutenant Donald Dale Pucket, U.S. Army Air Corps (1915–1944). (Longmont Museum)

MEDAL OF HONOR

PUCKET, DONALD D. (Air Mission)

Rank and organization: First Lieutenant, U.S. Army Air Corps, 98th Bombardment Group.

Place and date: Ploesti Raid, Rumania, 9 July 1944.

Entered service at: Boulder, Colo. Birth: Longmont, Colo.

G.O. No.: 48, 23 June 1945.

Citation: He took part in a highly effective attack against vital oil installation in Ploesti, Rumania, on 9 July 1944. Just after “bombs away,” the plane received heavy and direct hits from antiaircraft fire. One crewmember was instantly killed and 6 others severely wounded. The airplane was badly damaged, two engines were knocked out, the control cables cut, the oxygen system on fire, and the bomb bay flooded with gas and hydraulic fluid. Regaining control of his crippled plane, 1st Lt. Pucket turned its direction over to the copilot. He calmed the crew, administered first aid, and surveyed the damage. Finding the bomb bay doors jammed, he used the hand crank to open them to allow the gas to escape. He jettisoned all guns and equipment but the plane continued to lose altitude rapidly. Realizing that it would be impossible to reach friendly territory he ordered the crew to abandon ship. Three of the crew, uncontrollable from fright or shock, would not leave. 1st Lt. Pucket urged the others to jump. Ignoring their entreaties to follow, he refused to abandon the 3 hysterical men and was last seen fighting to regain control of the plane. A few moments later the flaming bomber crashed on a mountainside. 1st Lt. Pucket, unhesitatingly and with supreme sacrifice, gave his life in his courageous attempt to save the lives of 3 others.

Medal of Honor
Medal of Honor
Donald D. Pucket, 1938. (The Coloradan)

Donald Dale Pucket was born at Longmont, Colorado, 15 December 1915. He was the son of Roy A. Pucket, an automotive mechanic, and Lula M. (Gilmore?) Pucket.

Pucket attended the University of Colorado at Boulder where he studied business. He was president of the Board of Directors of the School of Business, and a member of the Delta Sigma Pi (ΔΣΠ) fraternity. During his senior year, he was the fraternity’s president and headmaster. Pucket graduated in 1938. Pucket was employed by a finance company as an insurance inspector.

On 16 September 1939, Donald Dale Pucket married Miss Lorene Edna Joyce, a public school teacher, at Denver, Colorado. They rented a home at 2705 High Street, Pueblo, Colorado.

In 1940, as required, Pucket registered for the Draft (conscription for military service). His registration shows that he was 5 feet, 8 inches (172.7 centimeters) tall and weighed 158 pounds (71.7 kilograms). He had brown hair and brown eyes.

Pucket enlisted as an aviation cadet in the United States Army Air Forces at Denver, Colorado, 25 November 1942 and was trained as a bomber pilot. He was commissioned a second lieutenant, U.S. Army Air Corps, in October 1943. Lieutenant Pucket was assigned to the 343rd Bombardment Squadron (Heavy), 98th Bombardment Group (Heavy), as a B-24 Liberator pilot and deployed to the Mediterranean Theater of Operations in April 1944. He was promoted to the rank of First Lieutenant in June 1944. He was killed in action during an attack against the oil refineries at Ploesti, Romania, 9 July 1944.

Lieutenant Pucket’s remains were eventually returned to the United States. On 31 October 1950, Lieutenant Pucket’s remains were interred in a group grave with those of five members of his crew, at the Jefferson Barracks National Cemetery, Lemay, Missouri. They were: Staff Sergeant Herschel K. Devore, Technical Sergeant Ilas B. Dye, Staff Sergeant Leon Fournas, Staff Sergeant Lawrence L. Hood and Staff Sergeant Jack C. Rathbun.

In addition to the Medal of Honor, First Lieutenant Donald Dale Pucket, United States Army Air Corps, was awarded the Distinguished Flying Cross, the Air Medal with 2 oak leaf clusters (three awards), and the Purple Heart.

[Note: Records available online do not indicate the specific variant or serial number of the B-24 Liberator flown by 1st Lieutenant Pucket, however research revealed that there were two B-24s lost by the 98th Bombardment Group on 9 July 1944. They were both North American/Dallas-built B-24G-15-NT Liberators, serial numbers 42-78346 and 42-78348. The B-24 in the photograph below is their sister ship, 42-78349.] ¹

North American B-24G-15-NT Liberator 42-78349, four-engine heavy bomber. (U.S. Air Force)
North American Aviation B-24G-15-NT Liberator 42-78349, four-engine heavy bomber. (U.S. Air Force)
North American B-24G-15-NT Liberator 42-78349, four-engine heavy bomber. (U.S. Air Force)

¹ UPDATE: Information provided by Lieutenant Colonel Jonathan B. Ott, United States Army, indicates that Lieutenant Pucket’s bomber was North American Aviation B-24G-15-NT Liberator 42-78346. Thank you very much, Colonel Ott.

© 2017, Bryan R. Swopes

9 July 1910

Walter Richard Brookins. (Empire State Aerosciences Museum)
Brookins’ Wright Flyer over the Atlantic City pier, 9 July 1910.

9 July 1910: Walter Richard Brookins flew his Wright Flyer to an altitude of 6,175 feet (1,882 meters) at the Atlantic City Aero Meet at Atlantic City, New Jersey, becoming the first pilot to fly higher than one mile. He broke his own altitude record of 4,380 feet (1,335 meters) set at Indianapolis, Indiana, less than a month earlier.

Brookins took off in a Wright Model A at 6:07:30 p.m. The ascent took just over 56 minutes as he made a gradual climb in 2-mile circles. The altitude was recorded by a Richard Frères recording aneroid barometer (or barograph), serial number 48188, which had a measurement range of 0–5,000 meters (0–16,404 feet). The descent from the record altitude took approximately seven minutes, as Brookins circled in a steeply-banked spiral and landed at 7:11 p.m.

In addition to the barograph carried aboard the Wright Flyer, a team of engineers and surveyors from the civil engineering firm of Ashmead & Hackney of Atlantic City measured the height of Brookins’ airplane by triangulation, using transits set up approximately 2½ ¹ miles (4 kilometers) apart. At 7:03:55 p.m., Brookins’ crossed the surveyors’ base line.

Civil engineers’ trianglulation measurements. Altitude: 6,175.48 feet (1,882.29 meters).  (American Engineer)

The engineering team reported:

“Gentlemen, —We beg leave to report that we have determined the height of the undersides of the runners of the Wright biplane occupied by Mr. Walter R. Brookins at the time of crossing the established base line between the two instrument stations (7h. 03m. 55s. p.m., July 9th, 1910) to have been 6,175 ft. (nearest even ft.) above sea-level.”

Flight, No. 86 (Vol. II, No. 34.), 20 August 1910, at Page 677, Column 2

Brookins was awarded a prize of $5,000.00 offered by the Atlantic City Aero Club.

Walter Richard Brookins (Library of Congress)

A contemporary newspaper reported the event:

BROOKINS BREAKS ALTITUDE RECORD

     Atlantic City, July 9.—Walter Brookins, in a Wright biplane, broke the world’s altitude record here this evening, when he attained a height of 6,175 feet. He used his last drop of gasoline at his highest altitude and was still climbing when his engine missed explosions. The daring aviator brought his machine back to level to get the last drop of fuel out of the storage tank to reach the line of vision of engineers on the beach. Reaching the imaginary line, Brookins started to glide to earth and his engine stopped entirely when he was at 5,600 feet and still over the ocean. His circling glide to the beach which the crown believed to be a bit of fancy flying was done to save himself from diving into the sea.

     Brookins was ready to collapse when he reached the ground and did not tell of his plight in the air until midnight, after he had partly recovered.

     Officials at midnight gave 6,175 feet as the exact height of the flight from calculations of engineering experts. The barograph record is 6,200 feet, leaving but 25 feet difference. It is expected that the record will stand without protest.

Wins $5,000 Prize.

     By his feat today Brookins wins the $5,000 prize offered by the Atlantic City Aero Club for breaking the world’s record, unless a higher altitude is reached here before the end of the present meet.

     Brookins spent one hour, two minutes, 35 15-100 seconds in the air, according to the official timing of Chairman Henry M. Neely and Recorder Augustus Post, of the Contest Committee of the National Council of the Aero Club of America. About 57 minutes of this time was made in a circling ascent, the rush of over a mile to the ground consuming less than seven minutes.

     Fear that Brookins at his highest point had not crossed the line of vision of the expert engineers in charge of securing his height by triangulation startled officials and spectators until it was discovered that the failure to secure a record of his crossing the imaginary line on which his record will be based was on two swings at a much lower altitude than at the final highest point.

Makes Final Start at 6.08 P. M.

     Brookins, after waiting all day for the brisk southerly wind to die out, made a practice spin of a little over 15 minutes, reaching an altitude of 1,900 feet. His final start was made at 6.08 o’clock p. m., with the weather absolutely clear and much of the force of the wind gone in the lower altitudes.

     His rise was made from alongside one of the ocean piers, He pointed his machine to the west and then swung out over the ocean, where he started his spiral flight over the ocean and city.

     News that Brookins was really attempting to break the altitude record reached hotels and city people, and when he reached a height of 1,520 feet the greater part of the city was on the beach. It is calculated that nearly 100,000 people watched the flight and cheered Brookins when he descended at 7.11 p. m.

     Men and women in the great throng threw up hats and handkerchiefs and the police had trouble keeping back the crown until Brookins made a run from his machine to his dressing room on the pier.

Waves Roses to Cheering Crowd.

Miss Eva Goffyn, sister of Frank Goffyn, Brookins’ fellow aviator, pushed a bunch of roses into his hands which he waved to the cheering crowd as he mounted to the deck of the pier.

     Brookins declined to receive callers and rested for 10 minutes before he left for his hotel in an automobile. He again went into seclusion, after stating that he found the air currents steady at his highest altitude and that he turned toward the earth when his aneroid barometers showed an altitude of over 6,000 feet.

     Glenn Curtiss made several short flights while Brookins was preparing to ascend for his final trial, but descended without attempting any altitude flight over the 50-mile course which he expects to cover tomorrow.

THE READING EAGLE, Vol. 43, No. 164 Sunday 10 July, Page 1 at Column 3

Recording baraograph chart of Brookins’ altitude record indicates 6,200 feet (1,890 meters). (American Machinist)

The Wright Model A, produced from 1907 to 1909, was the world’s first series production airplane. It was slightly larger and heavier than the Wright Flyer III which had preceded it. It was a two-place, single-engine canard biplane built of a wooden framework braced with wires and covered with muslin fabric. A new system of flight controls allowed the pilot to sit upright rather than lying prone on the lower wing.

The dual horizontal elevators were placed forward and the dual vertical rudders aft. The biplane was 31 feet (9.449 meters) long with a wingspan of 41 feet (12.497 meters). The wings had a chord of 6.6 feet, and vertical separation of 6 feet. The airplane had an empty weight of approximately 800 pounds (363 kilograms).

A Wright vertical four-cylinder engine at teh Smithsonian Institution National Air and Space Museum. (Sanjay Acharya/Wikipedia)
A Wright vertical inline four-cylinder engine at the Smithsonian Institution National Air and Space Museum. (Sanjay Acharya/Wikipedia)

The Model A was powered by a single water-cooled, fuel-injected, 240.528 cubic-inch-displacement (3.942 liter) Wright vertical overhead-valve inline four-cylinder gasoline engine with 2 valves per cylinder and a compression ratio of 4.165:1. It produced 32 horsepower at 1,310 r.p.m. During three years of production (1908–1911) Wright “4-40” engines were built that operated from 1,3525 to 1,500 r.p.m. Power output ranged from 28 to 40 horsepower. These engines weighed from 160 to 180 pounds (72.6–81.6 kilograms).

Two 8½ foot (2.591 meters) diameter, two-bladed, counter-rotating propellers, driven by a chain drive, are mounted behind the wings in pusher configuration. They turned 445 r.p.m.

The Wright Model A  could fly 37 miles per hour (kilometers per hour).

Walter R. Brookins and his Wright Model A at Atlantic City, New Jersey, 9 July 1910.

Walter Richard Brookins was born at Dayton, Ohio, 17 July 1888. He was the second of four children of Noah Holsapple Brookins, a salesman, and Clara Belle Spitler Brookins.

Brookins, then working as a chauffeur, married Miss Grace M. Miller, a governess, on 7 February 1907, in Hamilton County, Ohio. They divorced 18 May 1911, in Cincinnati, Ohio. (An earlier divorce decree, issued in Dayton in 1910, was set aside.)

Walter Richard Brookins was the first civilian pilot trained by Orville Wright. He was in a group of five pilots trained for the Wright Brothers’ Exhibition Team at their training camp at what is now Maxwell Air Force Base, Montgomery, Alabama.

Brookins was then hired as an instructor and finished training the last two men in the group. He was given a two-year contract with a salary of $20.00 per week, plus $50.00 per day for each flying day. Any prize money won—such as the $5,000 prize at Atlantic City—was turned over to the company.

All-In-One Liquid Measure. (Automobile Trade Journal)

From May 1919, Brookins, with his brother Earl, owned and operated the Brookins Manufacturing Company, Inc., in Dayton, which produced their invention, the All-In-One Liquid Measure. The first version was patented in 1924, and improvements followed.

Brookins married Mary Lamke, a secretary at McCook Field, Dayton, 12 April 1921. She held the position of corporate treasurer for the company. They remained together until his death.

In 1930, Brookins was self-employed in the financial industry. He and Mary relocated to California, living in Beverly Hills.

Brookins partnered with David R. Davis ² to form Brookins-Davis Aircraft Corporation, Los Angeles. In 1931 the company had applied for a patent for an airfoil profile designed by Davis, and which would become known as the “Davis Wing.”  The patent was issued 1934. Mrs. Brookins had known Major Reuben Hollis Fleet at McCook Field. (Fleet was the founder and president of the Consolidated Aircraft Corporation.) This led to meetings between Brookins, Davis and Fleet which resulted in the airfoil being licensed to Consolidated. It was used on the B-24 Liberator and B-32 Dominator heavy bombers.

Walter Richard Brookins died at Los Angeles, California, on 29 April 1953. His ashes were interred at the Portal of the Folded Wings, Valhalla Memorial, North Hollywood, California, 17 December 1953.

The Portal of the Folded Wings at Valhalla Memorial Park, North Hollywood, California. The remains of many pioneers of aviation are interred here. (Dignity Memorial)

¹ The actual length of the base line was 13,394.29 feet (4,082.58 meters). Brookins’ trangulated altitude was 6,175.48 feet (1,882.29 meters).

² Davis had previously co-founded the Davis-Douglas Company, which would become the Douglas Aircraft Company.

© 2018, Bryan R. Swopes

8 July 2011, 15:29:03 UTC, T minus Zero

The flight crew of Atlantis, STS-135. Left to right: COL Rex J. Waldheim, USAF, LCOL Douglas G. Hurley, USMC, CAPT Christopher J. Ferguson, USN, and Sandra Hall Magnus, Ph.D. (NASA)

8 July 2011: At 11:29:03 a.m., Eastern Daylight Time, the Space Shuttle Atlantis (OV-104) was launched on Mission STS-135 from Launch Complex 39A at the Kennedy Space Center, Cape Canaveral, Florida. This was the very last of 135 flights for the United States space shuttle program. The mission was to carry assembly modules and supplies to the International Space Station in Low Earth Orbit. The mission had a total elapsed time of 12 days, 18 hours, 28 minutes, 50 seconds. Atlantis arrived at the Shuttle Landing Facility 21 July 2011 at 09-57 UTC.

The mission commander was Captain Christopher J. Ferguson, U.S. Navy, on his third space flight. Atlantis‘ pilot for STS-135 was Lieutenant Colonel Douglas G. Hurley, United States Marine Corps, on his second shuttle flight. Mission specialists were Sandra Hall Magnus, Ph.D. and Colonel Rex J. Waldheim, U.S. Air Force. This was Dr. Magnus’ third space flight. She spent a total of 157 days, 8 hours, 42 minutes in space. Colonel Waldheim, the mission flight engineer, was on his third shuttle mission.

Shuttle Orbiter Atlantis first flew 3 October 1985 and made 33 space flights. It spent 306 days, 14 hours, 12 minutes, 43 seconds in space. Atlantis orbited the Earth 4,848 times and traveled miles 125,935,769 (202,673,974 kilometers) When it was retired at the end of STS-135, Atlantis had flown just one-third of its designed operational life. The space ship is on display at the Kennedy Space Center.

Space Shuttle Atlantis (STS-135) launch from Launch Complex 39A, Kennedy Space Center, Cape Canaveral, Florida, 15:29:03 UTC, 8 July 2011. (NASA)

© 2020, Bryan R. Swopes

8 July 1980

The prototype Strike Eagle, a modified F-15B-4-MC, 71-0291, banks away to show a full load of bombs and its conformal fuel tanks. (U.S. Air Force)

8 July 1980: The prototype McDonnell Douglas F-15 Strike Eagle, a fighter-bomber variant converted from the second two-seat F-15B Eagle trainer, F-15B-4-MC 71-0291, made its first flight. Originally designated TF-15A, -0291 first flew nearly seven years earlier, 18 October 1973.

The Strike Eagle was begun as a private venture by McDonnell Douglas. Designed to be operated by a pilot and a weapons system officer (WSO), the airplane can carry bombs, missiles and guns for a ground attack role, while maintaining its capability as an air superiority fighter. It’s airframe was a strengthened and its service life doubled to 16,000 flight hours. The Strike Eagle became an Air Force project in March 1981, and  went into production as the F-15E. The first production model, 86-0183, made its first flight 11 December 1986.

The McDonnell Douglas F-15E Strike Eagle is a two-place twin-engine multi-role fighter. It is 63 feet, 9 inches (19.431 meters) long with a wingspan of 42 feet, 9¾ inches (13.049 meters) and height of 18 feet, 5½ inches (5.626 meters). It weighs 31,700 pounds (14,379 kilograms) empty and has a maximum takeoff weight of 81,000 pounds (36,741 kilograms). The F-15E is powered by two Pratt and Whitney F100-PW-229 turbofan engines which produce 17,800 pounds of thrust (79.178 kilonewtons) each, or 29,100 pounds (129.443 kilonewtons) with afterburner.

This McDonnell Douglas F-15E Strike Eagle is carrying AIM-7 Sparrow and AIM 9 Sidewinder air-to-air missiles, 2,000-pound laser guided bombs, targeting designators and jettisonable fuel tanks. (U.S. Air Force)
This McDonnell Douglas F-15E Strike Eagle is carrying AIM-7 Sparrow and AIM 9 Sidewinder air-to-air missiles, 2,000-pound laser-guided bombs, targeting designators and jettisonable fuel tanks. (U.S. Air Force)

The Strike Eagle has a maximum speed of Mach 2.54 (1,676 miles per hour, (2,697 kilometers per hour) at 40,000 feet (12,192 meters) and is capable of sustained speed at Mach 2.3 (1,520 miles per hour, 2,446 kilometers per hour). Its service ceiling is 60,000 feet (18,288 meters). The fighter-bomber has a combat radius of 790 miles (1,271 kilometers) and a maximum ferry range of 2,765 miles (4,450 kilometers).

Though optimized as a fighter-bomber, the F-15E Strike Eagle retains an air-to-air combat capability. The F-15E is armed with one 20mm M61A1 Vulcan 6-barrel rotary cannon with 512 rounds of ammunition, and can carry four AIM-9M Sidewinder heat-seeking missiles and four AIM-7M Sparrow radar-guided missiles, or a combination of Sidewinders, Sparrows and AIM-120 AMRAAM long range missiles. It can carry a maximum load of 24,500 pounds (11,113 kilograms) of bombs and missiles for ground attack.

71-0291 remained at McDonnell Douglas as a dedicated test aircraft. During that time it was painted in many different camouflage schemes. In these photographs, it is painted in the “European 1” camouflage.

71-0291 was retired from the active inventory in the early 1990s and was used for battle damage repair training at Warner Robins Air Force Base, Georgia. It is reported to be on display at the Royal Saudi Air Force Museum at Riyadh, Saudi Arabia, in RSAF colors and markings.

The prototype McDonnell Douglas F-15E Strike Eagle (modified from F-15B-4-MC 71-0291) is parked on the ramp at the McDonnell Douglas facility at St. Louis. (U.S. Air Force)
The prototype McDonnell Douglas F-15E Strike Eagle (modified from F-15B-4-MC 71-0291) is parked on the ramp at the McDonnell Douglas facility at St. Louis. This camouflage scheme is called European 1. (U.S. Air Force)

© 2017, Bryan R. Swopes

8 July 1953

New York Airways’ Sikorsky S-55A, N405A, at the East River heliport in the early 1950s. (This aircraft was destroyed following a tail rotor pylon attachment failure at Sarawak, Malaysia, 2 April 1964.)

8 July 1953: America’s first helicopter airline, New York Airways, began scheduled passenger service, operating flights between the three area airports—La Guardia, Idlewild and Newark. There were 16 flights per day at 90-minute intervals.

The first aircraft used was the Sikorsky S-55, a commercial variant of the military H-19 Chickasaw. It carried 8 passengers and a cargo of U.S. Mail. The mail contract actually was the source of 75% of NYA’s revenue.

As its popularity increased, New York Airways shifted to larger helicopters when they became available, adding three Sikorsky S-58s in 1956. In 1958, the fleet was changed to the Vertol V-44 tandem-rotor helicopter, a commercial model of the Piasecki H-21 Shawnee. In 1962 the turbine-powered Boeing Vertol BV 107-II replaced the earlier helicopters. NYA’s final aircraft was the twin-turbine Sikorsky S-61.

On 16 May 1977, the landing gear of a S-61L failed while on the roof top heliport of the Pan Am building in Manhattan. The helicopter rolled over and spinning rotor blades killed four waiting passengers. Broken blades then fell to the street, fifty-nine stories below, killing a pedestrian and injuring several others.

With its reputation severely damaged and fuel prices escalating, New York Airways filed for bankruptcy in 1979. It’s surviving helicopters are operated today by Columbia Helicopters, Inc., Aurora, Oregon.

© 2016, Bryan R. Swopes