Tag Archives: Mackay Trophy

28 September 1921

Lieutenant John A. Macready dressed for high altitude flight. (U.S. Air Force)
First Lieutenant John A. Macready dressed for high altitude flight. (U.S. Air Force)
Lieutenant John A. Macready, Air Service, United States Army. (U.S. Air force)
Captain John Arthur Macready, Air Service, United States Army, circa 1918. (U.S. Air Force)

28 September 1921: At McCook Field, Ohio, First Lieutenant John Arthur Macready, Air Service, United States Army, flew a turbo-supercharged Packard Lepère L USA C. II biplane, serial number S.C. 40015, to a world record altitude of 40,800 feet (12,436 meters). He won his first of three Mackay Trophies for this flight.

John A. Macready graduated from Stanford University in 1913 with a degree in economics. He enlisted in the Aviation Section, Signal Corps, U.S. Army, as a Private 1st Class, 16 July 1917. On 27 December 1917, he was commissioned as a 1st lieutenant in the Aviation Section, Signal Officers Reserve Corps. Lieutenant Macready became a flight instructor at Brooks Field, Texas, where he wrote the standard instructional text. On 11 October 1918, Lieutenant Macready was promoted to the rank of captain. After World War I, he became an engineering test pilot at McCook Field near Dayton, Ohio. He reverted to his permanent rank of first lieutenant, 18 September 1920. In 1923, Macready graduated from the Aeronautical Engineer Course, Air Service Engineering School.

For six years John Macready was responsible for testing turbosuperchargers, which enabled aircraft engines to produce continuous power at increasing altitudes. It was while testing these that he established his altitude record.

Lt. John A. Macready with his Packard Lepère L USA C.II. (San Diego History Center)

During a 35 hour, 18 minute endurance flight at Rockwell Field, San Diego, California, 5–6 October 1922, John Macready and Oakley G. Kelly pioneered the use of inflight refueling from another aircraft. Also, he and Kelly made the first non-stop transcontinental flight when they flew a Fokker T-2 across the United States from Roosevelt Field, Long Island, New York, to Rockwell Field in 26 hours, 50 minutes, 38.6 seconds, 2–3 May 1923. Macready won his second and third Mackay Trophies for these achievements. He is the only man to have won it three times.

The Packard Lepère L USA C.II was a World War I biplane designed by French aeronautical engineer Captain Georges Lepère and built by the Packard Motor Car Company of Detroit, Michigan. It was to have been a two-place fighter, light bomber and observation aircraft armed with four machine guns.

The Packard Lepère was 25 feet, 3-1/8 inches (7.699 meters) long. The upper and lower wings had an equal span of 41 feet, 7¼ inches (12.681 meters), and equal chord of 5 feet, 5¾ inches (1.670 meters). The vertical gap between the wings was 5 feet, 5/8-inch (1.527 meters) and the lower wing was staggered 2 feet, 15/16-inch (0.633 meters) behind the upper wing. The wings’ incidence was +1°. Upper and lower wings were equipped with ailerons, and had no sweep or dihedral. The height of the Packard Lepère, sitting on its landing gear, was 9 feet, 7 inches (2.921 meters). The Packard Lepère had an empty weight of 2,561.5 pounds (1,161.9 kilograms) and its gross weight was 3,746.0 pounds (1,699.2 kilograms).

The fuselage was a wooden structure with a rectangular cross section. It was covered with three layers of veneer, (2 mahogany, 1 white wood) with a total thickness of 3/32-inch (2.38 millimeters). The fuselage had a maximum width of 2 feet, 10 inches (0.864 meters) and maximum depth of 4 feet, 0 inches (1.219 meters).

The wings were also of wooden construction, with two spruce spars and spruce ribs. Three layers of wood veneer covered the upper surfaces. Heavy bracing wires were used. These had an airfoil cross-section and actually provided additional lift. The interplane struts were unusual in that they were fully-framed units.

The Packard Lepère was powered by a water-cooled, normally-aspirated, 1,649.336-cubic-inch-displacement (27.028 liter) Liberty L-12 single overhead cam (SOHC) 45° V-12 engine with a compression ratio of 5.4:1. The Liberty produced 408 horsepower at 1,800 r.p.m. The L-12 as a right-hand tractor, direct-drive engine and it turned turned a two-bladed, fixed-pitch wooden propeller. The Liberty 12 was 5 feet, 7.375 inches (1.711 meters) long, 2 feet, 3.0 inches (0.686 meters) wide, and 3 feet, 5.5 inches (1.054 meters) high. It weighed 844 pounds (383 kilograms).

The engine coolant radiator was positioned horizontally in the center section of the Lepère’s upper wing. Water flowed through the radiator at a rate of 80 gallons (303 liters) per minute.

Packard Lepère LUSAC 11 P53, left profile. The turbocharger is mounted above the propeller driveshaft.
Packard Lepère L USA C.II S.C. 40013, McCook Field project number P53, left profile. The turbocharger’s turbine housing is mounted above the propeller driveshaft. (U.S. Air Force)

The Packard Lepère had a maximum speed of 130.4 miles per hour (209.9 kilometers per hour) at 5,000 feet (1,524 meters), 127.6 miles per hour (205.4 kilometers per hour) at 10,000 feet (3,048 meters), 122.4 miles per hour (197.0 kilometers per hour) at 15,000 feet (4,572 meters), 110.0 miles per hour (177.0 kilometers per hours) at 18,000 feet (5,486 meters) and 94.0 miles per hour (151.3 kilometers per hour) at 20,000 feet (6,096 meters). Its cruising speed was 112 miles per hour (180 was kilometers per hour). The airplane could climb to 5,000 feet in 4 minutes, 24 seconds, and to 20,000 feet in 36 minutes, 36 seconds. In standard configuration, the Packard Lepère had a service ceiling of 20,200 feet (6,157 meters). Its range was 320 miles (515 kilometers).

The fighter’s armament consisted of two fixed M1918 Marlin .30-caliber aircraft machine guns mounted on the right side of the fuselage, synchronized to fire forward through the propeller arc, with 1,000 rounds of ammunition, and two M1918 Lewis .30-caliber machine guns on a flexible mount with 970 rounds of ammunition.

The Air Service had ordered 3,525 of these airplanes, but when the War ended only 28 had been built. The contract was cancelled.

Six Packard Lepères were used for flight testing at McCook Field, Dayton, Ohio, assigned project numbers P 44, P 53, P 54, P 65, P 70 and P 80. One of these, flown by Major Rudolph W. Schroeder, set two Fédération Aéronautique Internationale (FAI) World Records for Altitude at 9,455 meters (31,020 feet), 18 September 1918.¹ On 6 September 1919, Schroeder flew a Packard Lepère to 8,616 meters (28,268 feet) while carrying a passenger. This set two more World Altitude Records.² Flying P 53, A.S. 40015, he set a fifth FAI altitude record of 10,093 meters (33,114 feet), 27 February 1920.³ On 28 September 1921, Captain John A. Macready flew P 53 to an altitude of 40,800 feet (12,436 meters). On 13 October 1922, 1st Lieutenant Theodore J. Koenig flew P 53 to win the Liberty Engine Builders’ Trophy Race at Selfridge Field, near Mount Clemens, Michigan. Koenig completed ten laps of the triangular racecourse in 2:00:01.54, at an average speed of 128.8 miles per hour (207.3 kilometers per hour).

The only Packard Lepère in existence, serial number A.S. 42133, is in the collection of the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.

Lieutenant John A Macready flew this turbosupercharged Packard Lepère L USA C.II, S.C 40013, McCook Field project number P53, to an altitude of 40,800 feet, 28 September 1921. (U.S. Air Force)
Barograph chart showing Lieutenant Macready’s record altitude of 40,800 feet (12,192 meters), 28 September 1921. (Sally Macready Wallace via www.earlyaviators.com)

¹ FAI Record File Number 15463

² FAI Record File Number 15671

³ FAI Record File Number 8229

© 2017, Bryan R. Swopes

7 September 1956

Captain Iven Carl Kincheloe, Jr., United States Air Force
Captain Iven Carl Kincheloe, Jr., United States Air Force

7 September 1956: At Edwards Air Force Base, California, test pilot Captain Iven Carl Kincheloe, Jr., U.S. Air Force, flew the Bell X-2 rocketplane, serial number 46-674, to a speed of Mach 1.7 and an altitude of 126,200 feet (38,465 meters). He was the first pilot to fly above 100,000 feet (30,480 meters) and was called “The First of the Spacemen.”

The X-2 was a joint project of the U.S. Air Force and NACA (the National Advisory Committee for Aeronautics, the predecessor of NASA). The rocketplane was designed and built by Bell Aircraft Corporation of Buffalo, New York, to explore supersonic flight at speeds beyond the capabilities of the earlier Bell X-1 and Douglas D-558-2 Skyrocket. In addition to the aerodynamic effects of speeds in the Mach 2.0–Mach 3.0 range, engineers knew that the high temperatures created by aerodynamic friction would be a problem, so the aircraft was built from Stainless Steel and K-Monel, a copper-nickel alloy.

The Bell Aircraft Corporation X-2 was 37 feet, 10 inches (11.532 meters) long with a wingspan of 32 feet, 3 inches (9.830 meters) and height of 11 feet, 10 inches (3.607 meters). Its empty weight was 12,375 pounds (5,613 kilograms) and loaded weight was 24,910 pounds (11,299 kilograms).

The X-2 was powered by a throttleable Curtiss-Wright XLR25-CW-1 rocket engine that produced 2,500–15,000 pounds of thrust (11.12–66.72 kilonewtons) burning alcohol and liquid oxygen. The engine used two rocket chambers and had pneumatic, electrical and mechanical controls. The smaller chamber could produce a maximum 5,000 pounds of thrust, and the larger, 10,000 pounds (22.24 and 44.48 kilonewtons, respectively).

Professor Robert H. Goddard, “The Father of Modern Rocketry,” authorized Curtiss-Wright to use his patents, and his rocketry team went to work for the Curtiss-Wright Rocket Department. Royalties for use of the patents were paid to the Guggenheim Foundation and Clark University. Professor Goddard died before he could also make the move to Curtiss-Wright.

Rather than use its limited fuel capacity to take off and climb to altitude, the X-2 was dropped from a modified heavy bomber as had been the earlier rocketplanes. A four-engine Boeing B-50A Superfortress bomber, serial number 46-011, was modified as the ”mothership.” A second Superfortress, B-50D-95-BO 48-096, was also modified to carry the X-2, and was redesignated EB-50D

The launch altitude was 30,000 feet (9,144 meters). After the fuel was exhausted, the X-2 glided to a touchdown on Rogers Dry Lake at Edwards Air Force Base.

The Bell X-2 carried by Boeing EB-50D Superfortress 48-096. (U.S. Air Force)
A Bell X-2 carried by Boeing EB-50D Superfortress 48-096. (U.S. Air Force)

Iven Kincheloe was awarded the Mackay Trophy for this flight. His altitude record remained unbeaten until the X-15 Project.

Iven Kincheloe stands in front of the Bell X-2 and the entire support team at Edwards Air Force Base. The "mothership" is a highly-modified Boeing EB-50D Superfortress. Chase aircraft are a North American F-86 Sabre, Lockheed T-33 Shooting Star, North American F-100 Super Sabre. The rescue helicopter is a Sikorsky H-19.
Iven Kincheloe stands in front of the Bell X-2 and the entire support team at Edwards Air Force Base. The “mothership” is a highly-modified Boeing EB-50D Superfortress. Chase aircraft are a North American F-86 Sabre, Lockheed T-33 Shooting Star, North American F-100 Super Sabre. The rescue helicopter is a Sikorsky H-19. (NASA)

© 2017, Bryan R. Swopes

5 September 1983

Captain Robert J. Goodman's Boeing KC-135A Stratotanker refuels and tows a crippled McDonnell Douglas F-4E Phantom II over the North Atlantic. (U.S. Air Force)
Captain Robert J. Goodman’s Boeing KC-135A Stratotanker refuels and tows a crippled McDonnell Douglas F-4E Phantom II over the North Atlantic. (U.S. Air Force)

5 September 1983: A Strategic Air Command Boeing KC-135A Stratotanker of the 42nd Air Refueling Squadron, Loring  AFB, Maine, was sent to rendezvous with a flight of McDonnell Douglas F-4E Phantom II fighter bombers crossing the Atlantic Ocean enroute to Europe. As they began to refuel the fighters, one F-4E began to lose power in one of its engines, and also lost part of its hydraulic system. The Phantom’s pilot had difficulty maintaining speed and altitude as he tried to hook up with the tanker, and the second engine began to overheat. The two aircraft flew at just above the Stratotanker’s landing speed so that the Phantom could keep up, but as it slowed further, the Phantom’s angle of attack had to increase to maintain lift. This exceeded the mechanical limits of the refueling boom and the two airplanes separated without the fighter having received a full fuel load.

LCOL Robert J. Goodman, USAF (1943–2011). (U.S. Air Force)
LCOL Robert J. Goodman, USAF (1943–2011). (U.S. Air Force)

The crew of the F-4E was in serious danger. It was unlikely that the airplane could remain in the air for much longer. It was decided to head for Gander, Newfoundland, the closest place to land, 500 miles (806 kilometers) away. Captain Robert J. Goodman, U.S. Air Force, aircraft commander of the Stratotanker, decided to escort the crippled fighter which continued to lose altitude. It was necessary to try to refuel it three more times, and on occasion, the tanker actually towed the fighter back to altitude.

With the help of the tanker, the Phantom II finally arrived at Gander and landed safely.

For their efforts to save the lives of the crew of the F-4E, Captain Goodman and his crew, Captain Michael F. Clover, 1st Lieutenant Karol F. Wojcikowski and Staff Sergeant Douglas D. Simmons, Crew E113, were awarded the Mackay Trophy “For outstanding achievement while on a routine refueling mission involving F-4E aircraft, saving a valuable aircraft from destruction and its crew from possible death.

SAC Crew E113, left to right: 1st Lieutenant Karol F. Wocjikowski, Captain Michael F. Clover, Captain Robert J. Goodman and Staff Sergeant Douglas D. Simmons. (U.S. Air Force)

The Mackay Trophy which is awarded annually for “the most meritorious flight of the year by an Air Force person, persons, or organization.” It is kept at the Smithsonian Institution, National Air and Space Museum.

The Mackay Trophy.
The Mackay Trophy.

© 2015, Bryan R. Swopes

23 August 1937

Captain Carl J. Crane, Captain George V. Holloman and Mr. Raymond K. Stout with the C-14B, 31-381. (United States Air Force 090176-F-1234K-007)

23 August 1937: The first completely automatic landing of an airplane took place at Patterson Field, near Dayton, Ohio. With Captain George Vernon Holloman in the cockpit, and Captain Carl Joseph Crane and Mr. Raymond K. Stout in the cabin, a Fokker Y1C-14B, Army serial number 31-381, departed Wright Field then automatically intercepted a series of four radio beacons, initiated a descent, and landed at nearby Patterson Field and braked to a stop, all without any input from the pilot.

The two military officers were each awarded the Distinguished Flying Cross and the Mackay Trophy.

14 October 1938. Secretary of War Harry Hines Woodring (left) pins gold medal on Carl J. Crane (center) and George V. Holloman (right). “War Secretary presents Army Flyers with Mackay Trophy. Washington, D.C. Oct. 14.” (Library of Congress)

The President of the United States of America, authorized by Act of Congress, July 2, 1926, takes pleasure in presenting the Distinguished Flying Cross to Captain (Air Corps) George V. Holloman, U.S. Army Air Corps, for extraordinary achievement while participating in aerial flights in connection with the design and development of the airplane automatic landing system which made possible the first complete automatic airplane landing in history. Over the period of two years during which this system was under development, Captain Holloman, with utter disregard of his personal safety, performed virtually all of the great amount of flight testing which was required for the numerous items of equipment which go to make up the complete automatic landing assembly, and when finally on 23 August 1937, the first experimental automatic landing flights were made, he was in the cockpit of the airplane used for this purpose. The engineering skill, judgment, and resourcefulness displayed by Captain Holloman, and his courage in performing hundreds of test flights with highly experimental equipment, contributed largely to the ultimate successful development of the automatic landing system.

General Orders: War Department: American Decorations, 1940 (Supplement IV-1940)

Action Date: August 23, 1937

Service: Army Air Forces

Rank: Captain

A contemporary aviation publication stated:

After two years of research and preparation daring pilots and engineers of the Army Air Corps in 1937 began to make automatic “blind” landings without any control from the occupants of the airplane or observers on the surface. On Monday, August 23, a day when the air was bumpy and the wind decidedly adverse, a big Army plane swung over the horizon near Wright Field, at Dayton, O., and glided straight down on the runway, rolling a few yards and then coming to a stop as if it had been at all times in the hands of an expert pilot. But nobody had anything to do with this landing; There were three men in the Army’s cargo plane, and they were the three experts who had developed the apparatus. Like true scientists they had gone up and come down on this test to see for themselves just how their creation would work. . . .

The AIRCRAFT YEAR BOOK FOR 1938, Howard Mingos, Editor, Aeronautical Chamber of Commerce of America, Inc., New York, 1938, Chapter II at Pages 43–50

Diagram from Patent Application No. US358438A

The automatic landing system used a barometric altimeter, a radio compass and Sperry Autopilot. The pilot would fly the airplane to a predetermined altitude at a distance greater than 20 miles (32 kilometers) from the airfield. When the system was activated, the airplane automatically maintained this altitude and turned toward the outermost beacon. (Turns of up to 180° were demonstrated.)

As the airplane passed over each of the three outer beacons, the radio compass frequency would change to that of the next successive beacon, and the airplane homed in on it. Coupled with the altimeter, the system prevented the airplane from descending below the minimum altitude until it had passed the innermost beacon.

When passing over the innermost beacon, the engine was automatically throttled back to begin a controlled descent. It then set the throttle to maintain a preset rate of descent and glide slope angle until ground contact was made. Switches in the landing gear signaled the system to bring the engine to idle and apply the brakes.

During testing all of the landings were made with a crosswind.

Y1C-14B (U.S. Air Force 097014-F-1234K-035)

The Fokker Y1C-14B was a variant of the F-14 commercial transport. It was a single-engine parasol-wing monoplane with conventional fixed landing gear. The airplane was flown by a single pilot in an open cockpit and could carry up to six passengers in its enclosed cabin. It was 43 feet, 3 inches (13.183 meters) long, with a wingspan of 59 feet, 0 inches (17,983 meters) and height of 12 feet, 0 inches (3.658 meters). The airplane’s maximum takeoff weight was 7,341 pounds (3,330 kilograms).

Fokker Y1C-14B 31-381, Wright Field. (United States Air Force 050406-F-1234P-036)

The Y1C-14B differed from the C-14A with the installation of an air-cooled, 1,690.537-cubic-inch-displacement (27.703 liters) Pratt & Whitney R-1690-5 nine-cylinder radial engine. This engine was direct-drive and had a compression ratio of 5:1. Burning 73-octane gasoline, it was rated at 525 horsepower at 1,900 r.p.m. at Sea Level. The R-1690-5 was 3 feet, 8.78 inches (1.137 meters) long, 4 feet, 6.43 inches (1.383 meters) in diameter and weighed 850 pounds (386 kilograms). This engine was sold commercially as the Pratt & Whitney Hornet A2.

Y1C-14B (U.S. Air Force 097014-F-1234K-036)

The Y1C-14B had a cruise speed of 133 miles per hour (214 kilometers per hour) and maximum speed of 150 miles per hour (241 kilometers per hour). The service ceiling was 14,300 feet (4,359 meters). Its range was 675 miles (1,086 kilometers).

Atlantic Aircraft Y1C-14B (U.S. Air Force 097014-F-1234K-037)

© 2019, Bryan R. Swopes

20 August 1955

Colonel Horace A. Hanes with North American Aviation F-100C Super Sabre 53-1709, at Edwards AFB after setting a supersonic speed record, 20 August 1955. (U.S. Air Force)

20 August 1955: Colonel Horace A. Hanes, United States Air Force, flew the first North American Aviation F-100C-1-NA Super Sabre, 53-1709, to Mach 1.246 at 40,000 feet (12,192 meters), setting a new Fédération Aéronautique Internationale (FAI) speed record of 1,323.312 kilometers per hour (822.268 miles per hour) over a measured 15/25-kilometer course at Edwards Air Force Base, California.¹

This was the first supersonic world speed record. It was also the first speed record set at high altitude. Previously, all speed records were set very close to the ground for measurement purposes, but with ever increasing speeds this practice was becoming too dangerous.

For his accomplishment, Colonel Hanes was awarded the Mackay Trophy.

North American Aviation F-100C-1-NA Super Sabre 53-1709, FAI World Speed Record holder. (U.S. Air Force)
North American Aviation F-100C-1-NA Super Sabre 53-1709, FAI World Speed Record holder. (U.S. Air Force)

The North American Aviation F-100C Super Sabre was a single-seat, single-engine swept wing fighter. In addition to its air superiority role, the F-100C was also capable of ground attack.

The F-100C was 47.8 feet (14.57 meters) long (excluding pitot boom) with a wingspan of 38.8 feet (11.83 meters) and overall height of 15.5 feet (4.72 meters). The wings were swept aft 45° at 25% chord. The wings’ angle of incidence was 0° and there was no dihedral or twist. The total wing area was 385 square feet (35.8 square meters). The fighter had an empty weight of 19,197 pounds (8,708 kilograms), and maximum gross weight of 35,618 pounds (16,156 kilograms).

The F-100C was powered by a Pratt & Whitney J57-P-7 engine. The J57 was a two-spool axial-flow turbojet which had a 16-stage compressor section (9 low- and 7 high-pressure stages) and a 3-stage turbine (2 high- and 1 low-pressure stages). Its continuous power rating was 8,000 pounds of thrust (35.586 kilonewtons). The Military Power rating was 9,700 pounds (43.148 kilonewtons) (30-minute limit). Maximum power was 14,800 pounds (43.148 kilonewtons) with afterburner (5-minute limit). The engine was 20 feet, 9.7 inches (6.342 meters) long, 3 feet, 3.9 inches (1.014 meters) in diameter, and weighed 5,075 pounds (2,303 kilograms).

F-100C-1-NA Super Sabre 53-1709 at the North American Aviation, Inc., facility at Air Force Plant 42, near Palmdale, California. (Super Sabre Society)

The F-100C had a maximum speed of 756 knots (870 miles per hour/1,400 kilometers per hour) at 35,000 feet (10.668 meters). The service ceiling was 46,900 feet (14,295 meters). The maximum ferry range was 1,630 nautical miles (1,876 statute miles/3,019 kilometers).

The F-100C Super Sabre was armed with four 20 mm M-39 revolver cannon with 200 rounds of ammunition per gun. It could carry 14 unguided 2.75 inch (70 mm) Folding Fin Aerial Rockets in two 7-round pods. It could be loaded with four 1,000-pound, or six 750-pound bombs on underwing hard points. For tactical nuclear strike, the Super Sabre could be armed with a single MK-7 “Special Store.”

NASA 703, the World Record-setting North American Aviation F-100C Super Sabre, parked on the dry lake at Edwards Air Force Base. (NASA)
NASA 703, the World Record-setting North American Aviation F-100C-1-NA Super Sabre, N703NA, parked on the dry lake at Edwards Air Force Base, California. (NASA)

After being used in Air Force testing at Edwards Air Force Base, 53-1709 was transferred to the National Advisory Committee for Aeronautics (NACA) High-Speed Flight Station, also located at Edwards AFB. The F-100 was identified as NACA 703 and assigned civil registration N703NA. It was used for variable stability testing at the Ames Flight Research Center, Moffett Field, California, from 4 September 1956 to 2 November 1960, and 11 March 1964 until 21 March 1972. At some point its tail surfaces were upgraded to those of the F-100D series.

Today, the FAI world-record setting F-100C is displayed at the Castle Air Museum, marked as F-100D 55-2879.

World-record-setting North American Aviation F-100C-1-NA Super Sabre 53-1709 and the NACA (NASA after 1958) F-100C Variable Stability Team at the Ames Flight Research Center. Left to right: Don Heinle, Mel Sadoff, Dick Bray, Walt MacNeill, G. Allan Smith,Jack Ratcliff, John Foster, Jim Swain, Howard Clark, Don Olson, Dan Hegarty, Gil Parra, Eric Johnson and Fred Drinkwater. (NASA)
Horace A. Hanes, 1937. (The Index)

Horace Albert Hanes was born at Fayette, Illinois, 1 March 1916, the first of two children of Albert Lee Hanes, a farmer, and Martha Elizabeth Jones Hanes. Hanes grew up in Bellflower, Illinois. He attended Normal Community High School at Normal, Illinois, graduating in 1933, and then Illinois State Normal University, also located in Normal. He participated in basketball and track and field. He graduated in 1938 with a bachelor of arts degree in education. He worked as a teacher and athletic coach.

Hanes married Miss Virginia Kumber, a school teacher, in Covington, Indiana, 9 October 1937. The ceremony was officiated by Rev. Lawrence P. Green.

Horace Hanes entered the U.S. Army Air Corps as an aviation cadet, 8 October 1938. He graduated from flight training 25 August 1939 and was commissioned as a second lieutenant, Air Reserve. Lieutenant Hanes was assigned to the 18th Pursuit Group at Wheeler Field, Oahu, Territory of Hawaii, which was equipped with Curtiss-Wright P-36 Hawk and P-40 Warhawk “pursuits.”

Curtiss-Wright P-40B Warhawks of the 44th Pursuit Squadron, 18th Pursuit Group. (U.S. Air Force)

Hanes was commissioned as a second lieutenant, Air Corps, United States Army, 1 July 1940. While retaining his permanent rank of second lieutenant, Hanes advanced to the rank of first lieutenant, Army of the United States (A.U.S.), 10 October 1941. He returned to the United States and served with the Air Training Command.

Lieutenant Hanes was promoted to captain, A.U.S. (A.C.), 1 March 1942, and placed in command of a P-47 Thunderbolt squadron based in Florida, the 312th Fighter Squadron, 338 Fighter Group. On 26 November 1942, Hanes was promoted to the rank of major, A.U.S. On 1 July 1943, Hanes was promoted to the permanent rank of first lieutenant, Air Corps, United States Army. He retained this permanent rank until after the war.

Lockheed P-38J-15-LO Lightning 43-28777, 71st Fighter Squadron, 1st Fighter Group. (U.S. Air Force)

Major Hanes was deployed to Europe in August 1943, commanding the 71st Fighter Squadron (Twin Engine), 1st Fighter Group, at Mateur Airfield, Tunisia. The 71st had been the first operational P-38 squadron. After flying 30 combat missions, Major Hanes’ P-38 went down over Yugoslavia in January 1944. For the next three months he evaded capture. Hanes returned to the United States in April 1944 and was assigned to command Punta Gorda Army Airfield, a fighter training base on the western coast of Florida.

Hanes was promoted to lieutenant colonel, A.U.S., 1 August 1944, and to colonel, A.U.S., 23 October 1945. In January 1946, Colonel Hanes assumed command of the 31st Fighter Group, which deployed to Giebelstadt Army Airfield in southwest Germany. The group operated P-51D Mustangs and the new Lockheed P-80B Shooting Star jet fighter. In 1947, Colonel Hanes took command of the 67th Tactical Reconnaissance Group at March Air Force Base, Riverside, California. The 67th was equipped with the Douglas RB-26 Invader and the Lockheed RF-80 Shooting Star.

From January to July 1949, Colonel Hanes attended the Armed Forces Staff College, and then was assigned as Chief of the Air Defense Division within the Directorate of Research and Development, Headquarters, U.S. Air Force. From July 1952 to June 1953, he attended the Air War College, Maxwell Air Force Base, Montgomery, Alabama, and then became Director of Flight Test at the Air Force Flight Test Center, Edwards Air Force Base. It was while at Edwards that Colonel Hanes set the world speed record. He remained at the AFFTC for four years.

Hanes took command of the 58th Fighter-Bomber Wing at Osan Air Base, Republic of South Korea, July 1957. The 58th flew the North American Aviation F-86F Sabre. He then spent three years in Japan as Deputy Chief of Staff, Operations, Fifth Air Force.

In July 1964, Brigadier General Hanes took command of the 9th Aerospace Defense Division at Ent Air Force Base, Colorado Springs, Colorado. On 24 September 1964, Hanes was promoted to the rank of major general, with his date of rank retroactive to 1 April 1960. After two years, Hanes returned to Europe as Assistant Chief of Staff, Operations, Supreme Headquarters, Allied Powers Europe.

Major General Hanes’ final assignment was as Vice Commander, Aerospace Defense Command. He  retired from the United States Air Force in 1973.

During his military Career, Major General Horace Albert Hanes, United States Air Force, was awarded the Distinguished Service medal, the Silver Star, Legion of Merit with oak leaf cluster (two awards), the Air Medal with five oak leaf clusters (six awards), the Air Force Commendation medal and the Air Force Outstanding Unit Award ribbon.

Major General Hanes died at his home in Bloomington, Indiana, 3 December 2002. He was buried alongside his wife, Virginia (who died in 1996) at the United States Air Force Academy Cemetery, Colorado Springs, Colorado.

Major General Horace Hanes, United States Air Force
Major General Horace Albert  Hanes, United States Air Force

¹ FAI Record File Number 8867

© 2018, Bryan R. Swopes