Boeing B-17G-75-BO Flying Fortress 43-37877 on fire and going down near Merseburg, Germany, 1314 GMT, 30 November 1944. (American Air Museum in Britain UPL 30040)
30 November 1944: In another iconic photograph from World War II, this Boeing B-17 Flying Fortress, B-17G-75-BO 43-37877, of the 836th Bombardment Squadron (Heavy), 487th Bombardment Group (Heavy), was hit by anti-aircraft artillery just after bomb release near Merseburg, Sachsen-Anhalt, Germany, at 1314 GMT, 30 November 1944.
43-37877 was crewed by 1st Lieutenant Lloyd W. Kersten, Pilot; 1st Lieutenant Henry E. Gerland, Co-Pilot; 1st Lieutenant James Hyland, Navigator; 1st Lieutenant Warren R. Ritchhart, Bombardier; Technical Sergeant Arnold R. Shegal, Flight Engineer/Gunner; Staff Sergeant Everett S. Morrison, Ball Turret Gunner; Staff Sergeant Joseph M. Miller, Gunner; Staff Sergeant Maurice J. Sullivan, Tail Gunner.
The B-17 crashed near Halle, Sachsen-Anhalt. Seven of the crew were killed. Two, Lieutenants Hyland and Richart, were captured and held as prisoners of war.
43-37877 was built by the Boeing Airplane Company at its Plant II, south of downtown Seattle, Washington. It was delivered to the United Air Lines Modification Center at Cheyenne, Wyoming, on 31 May 1944. After completion of modifications, on 12 June the B-17 was flown to Hunter Army Air Field at Savannah, Georgia, and then on 3 July, to Dow Army Air Field at Bangor, Maine, where it was positioned to be ferried across the north Atlantic Ocean to England.
On 19 June the new bomber was assigned to the 379th Bombardment Group (Heavy), which was based at RAF Kimbolton (U.S. Army Air Force Station 117), west of Huntingdon in Cambridgeshire. Then on 4 July 1944, B-17G 43-32877 was reassigned to the 836th Bombardment Squadron (Heavy), 487th Bombardment Group (Heavy) at RAF Lavenham (AAF-137), north of Sudbury in Suffolk, England..
43-37877 was not camouflaged. It was marked with a white letter P in a black square on the vertical fin, indicating the 487th Bomb Group, along with a partial serial number, 333787. The side of the fuselage was marked 2G ✪ E, indicating that it was assigned to the 836th Bomb Squadron. The wing tips, vertical fin and rudder, and horizontal stabilizer and elevators were painted yellow.
Two B-17G Flying Fortresses of the 836th Bombardment Squadron (Heavy), sometime between 6 January–14 April 1945. In the foreground, marked 2G-P, is a Lockheed Vega-built B-17G-80-VE Flying Fortress, serial number 44-8768. The farther airplane is identified 2G-M. It may be 44-8312. (American Air Museum in Britain, Roger Freeman Collection FRE 8542)
Lieutenant Commander William T. Amen, U.S. Navy, Commanding Officer of Fighter Squadron VF-111, is congratulated on his air to air victory after returning to the aircraft carrier USS Philippine Sea (CV-47). (U.S. Navy)
9 November 1950: The first jet vs. jet air-to-air victory which can be confirmed from both sides occurred when Lieutenant Commander William T. Amen, United States Navy, flying a Grumman F9F-2B Panther, Bu. No. 127184, shot down a Soviet Mikoyan-Gurevich MiG-15 over Korea.
Captain Mikhail Fedorovich Grachev, 139th Guards Fighter Aviation Regiment, led a squadron of MiG-15 fighters from their base at Antung, China to intercept U.S. Navy Douglas AD Skyraiders which were attacking bridges across the Yalu River, which marked the border between China and Korea.
Russian technicians service a MiG-15bis of the 351st Fighter Aviation Regiment at Antung Air Base, China, mid-1952. (Unattributed)
An escorting group of Grumman F9F-2B Panther fighters, assigned to Fighter Squadron 111 (VMF-111, “Sundowners”) aboard the Essex-class aircraft carrier, USS Philippine Sea (CV-47) went after the MiGs as they dove on the Skyraiders. The Soviet flight broke up into single aircraft, or pairs, and did not counterattack with any organization. Visibility was poor, and airplanes would disappear then reappear in the clouds.
Captain Grachev made a quick left turn, then reversed and rolled over into a dive. His two wingmen could not stay with him and visual contact was lost.
Bill Amen saw Grachev’s diving MiG-15 and, following him down, fired his four 20 mm cannon. Amen’s wingman saw the MiG crash into a wooded slope and burn. Grachev did not return from his mission and is presumed to have been killed in the crash.
USS Philippine Sea (CV-47) with Douglas AD Skyraiders and Grumman F9F Panthers on the flight deck, off the coast of Korea. Philippine Sea was a “long-hull” Essex-class ship, sometimes called the Ticonderoga-class. (U.S. Navy)
The Grumman F9F-2 Panther was a single-seat, single-engine turbojet powered fighter designed for operation from the U.S. Navy’s aircraft carriers. It was 38 feet, 5⅜ inches (11.719 meters) long, with a wingspan of 38 feet, 0 inches (11.528 meters)— not including wing tanks. Its overall height was 11 feet, 4 inches (3.454 meters). The wings could be hydraulically folded to reduce the span for storage aboard ship. The Panther weighed 9,303 pounds (4,220 kilograms) empty, and had a gross weight of 19,494 pounds (8,842 kilograms).
The F9F-2 was powered by a Pratt & Whitney Turbo Wasp JT6 (J42-P-8) turbojet engine which produced 5,000 pounds of thrust (22.241 kilonewtons) at Sea Level. The J42 was a license-built version of the Rolls-Royce Nene. The engine used a single-stage centrifugal-flow compressor, 9 combustion chambers and a single-stage axial-flow turbine. The engine weighed 1,715 pounds (778 kilograms).
Interestingly, the MiG-15 was powered by an un-licensed, reverse-engineered version of the Nene, the Klimov VK-1.
The Panther had a maximum speed of 575 miles per hour (925 kilometers per hour) at Sea Level. Its service ceiling was 44,600 feet (13,594 meters), and the range was 1,353 miles (2,177 kilometers).
The Panther was armed with four M3 20 mm autocannon placed in the nose, with 760 rounds of ammunition. It could carry up to 3,000 pounds (1,361 kilograms) of bombs or eight 5-inch (12.7 centimeters) rockets on four hardpoints under each wing.
The XF9F-2 prototype first flew 21 November 1947. 1,382 were produced and remained in service with the U.S. Navy and Marine Corps until 1958. A swept wing version, the F9F-6 through F9F-9J Cougar, was also produced.
For his service with VF-111 in combat from 5 August 1950 to 1 February 1951, Lieutenant Commander Amen was awarded the Distinguished Flying Cross.
F9F-2 Bu. No. 127184 was part of a group of 28 Grumman F9F panthers that were sold to the Argentine Navy. It was transferred in April 1963.
A Grumman F9F-2 Panther of Fighter Squadron 111 drops bombs over Korea, circa 1952. It is painted overall Glossy Sea Blue with red accents at the nose and tail. This is similar in appearance to the Panther flown by Lieutenant Commander William T. Amen, 9 November 1950. (U.S. Navy)
This painting by famed aviation artist Keith Ferris depicts 1st Lieutenant Russell Brown’s Lockheed F-80C Shooting Star as he shot down an enemy Mikoyan-Gurevich MiG 15 over Korea, 8 November 1950. (Keith Ferris)
8 November 1950: First Lieutenant Russell J. Brown, United States Air Force, 16th Fighter Interceptor Squadron, 51st Fighter Interceptor Wing, is credited with shooting down a Russian-built Mikoyan-Gurevich MiG 15 jet fighter near the Yalu River while flying a Lockheed F-80C-10-LO Shooting Star. This may have been the very first time that a jet fighter had been shot down by another jet fighter.
Sources vary, reporting the serial number of Lieutenant Brown’s fighter as 49-713 or 49-717.
A contemporary newspaper quoted Brown:
1st Lieutenant Russell J. Brown. (Air Force Times)
Brown gave a colorful description of the fight in history’s first jet-versus-jet battle last week. He said:
“We had just completed a strafing run on Sinuiju antiaircraft positions and were climbing when we got word that enemy jets were in the area.
“Then we saw them across the Yalu, doing acrobatics.
“Suddenly they came over at about 400 miles an hour. We were doing about 300. They broke formation right in front of us at about 18,000 or 20,000 feet. They were good looking planes—shiny and brand, spanking new.”
—INS, Tokyo, November 13
Soviet records reported no MiG 15s lost on 8 November. Senior Lieutenant Kharitonov, 72nd Guards Fighter Aviation Unit, reported being attacked by an F-80 under circumstances that suggest this was the engagement reported by Lieutenant Brown, however Kharitonov succeeded in evading the American fighter after diving away and jettisoning his external fuel tanks.
A Soviet MiG 15 pilot, Lieutenant Khominich, also of the 72nd Guards, claimed shooting down an American F-80 on 1 November, but U.S. records indicate that this fighter had been destroyed by anti-aircraft fire.
What is clear is that air combat had entered the jet age, and that the Soviet Union was not only supplying its swept wing MiG 15 to North Korea and China, but that Soviet Air Force pilots were actively engaged in the war in Korea.
Russian technicians service a MiG 15bis of the 351st IAP at Antung Air Base, China, mid-1952. (Unattributed)
The Mikoyan-Gurevich MiG 15 is a single-seat, single engine turbojet-powered fighter interceptor, designed to attack heavy bombers. Designed for high sub-sonic speed, the leading edges of the wings and tail surfaces were swept to 35°. The wings were very thin to minimize aerodynamic drag.
The fighter was 10.102 meters (33 feet, 1.7 inches) long, with a wingspan of 10.085 meters (33 feet, 1 inch). Its empty weight was 3,253 kilograms (7,170 pounds) and takeoff weight was 4,963 kilograms (10,938 pounds).
The Rolls-Royce Nene I and Nene II jet engines had been used in the three MiG 15 prototypes. The British engines were reverse-engineered by Vladimir Yakovlevich Klimov and manufactured at Factory No. 45 in Moscow as the Klimov VK-1. The VK-1 used a single-stage centrifugal-flow compressor, 9 combustion chambers and a single-stage axial-flow turbine. It produced a maximum 26.5 kilonewtons of thrust (5,957 pounds of thrust). The VK-1 was 2.600 meters (8 feet, 6.4 inches) long, 1.300 meters (4 feet, 3.2 inches) in diameter, and weighed 872 kilograms (1,922 pounds).
The MiG 15 had a maximum speed of 1,031 kilometers per hour (557 knots/641 miles per hour) at 5,000 meters (16,400 feet) and 1,050 kilometers per hour (567 knots/652 miles per hour) at Sea Level.
Armament consisted of one Nudelman N-37 37 mm cannon and two Nudelman-Rikhter NR-23 23 mm cannon.
MIG 15 Red 2057. A North Korean Peoples’ Air Force Mikoyan-Gurevich MiG 15bis in a hangar at Kimpo Air Base, Republic of South Korea. A defecting North Korean pilot, Lieutenant No Kum-Sok, flew it to Kimpo on 21 September 1953. It was taken to Okinawa, examined and test flown by U.S.A.F. test pilots, including Major Charles E. (“Chuck”) Yeager. This MiG 15 is in the collection of the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio. (U.S. Air Force).
The Lockheed P-80 Shooting Star was the United States’ first operational jet fighter. It was redesignated F-80 in 1948. It was a single-seat, single-engine airplane, designed by a team of engineers led by Clarence L. (“Kelly”) Johnson. The prototype XP-80A, 44-83020, nicknamed Lulu-Belle, was first flown by test pilot Tony LeVier at Muroc Army Air Field (now known as Edwards Air Force Base) 8 January 1944. The P-80A entered production in 1945. Improved versions, the P-80B and P-80C (F-80C) followed.
Lockheed F-80C-10-LO Shooting Star 49-432 on display at the Air Force Armaments Museum, Eglin Air Force Base, Florida. The fighter is marked as F-80C-10-LO 49-713, assigned to the 16th Fighter Squadron, 51st Fighter Interceptor Group, Kimpo, Korea, 1950.
The F-80C was 34 feet, 5 inches (10.490 meters) long with a wingspan of 38 feet, 9 inches (11.811 meters) and an overall height of 11 feet, 3 inches (3.429 meters). It weighed 8,420 pounds empty (3,819 kilograms) and had a maximum takeoff weight of 16,856 pounds (7,645 kilograms).
The F-80C was powered by either a General Electric J33-GE-11, Allison J33-A-23 or J33-A-35 turbojet engine. The J33 was a development of an earlier Frank Whittle-designed turbojet. It used a single-stage centrifugal-flow compressor, eleven combustion chambers and a single-stage axial-flow turbine section. The J33-A-35 had a Normal Power rating of 3,900 pounds of thrust (17.348 kilonewtons) at 11,000 r.p.m., at Sea Level, and 4,600 pounds (20.462 kilonewtons) at 11,500 r.p.m., for Takeoff. It was 107 inches (2.718 meters) long, 50.5 inches (1.283 meters) in diameter, and weighed 1,820 pounds (826 kilograms).
The F-80C had a maximum speed of 594 miles per hour (516 knots/956 kilometers per hour) at Sea Level and 543 miles per hour (472 knots/874 kilometers per hour) at 25,000 feet (7,620 meters). The service ceiling was 46,800 feet (14,265 meters). The maximum range was 1,380 miles (2,221 kilometers).
The F-80C Shooting Star was armed with six Browning AN-M3 .50-caliber aircraft machine guns mounted in the nose.
A Lockheed F-80C Shooting Star of the 16th Fighter Interceptor Squadron, 51st Fighter Interceptor Wing, makes a JATO-assisted takeoff from an airfield in the Republic of South Korea, circa 1950. (U.S. Air Force)
Lockheed F-80C-10-LO Shooting Star 49-713, flown by Albert C. Ware, Jr., was lost 10 miles north of Tsuiki Air Base, Japan, 23 March 1951.
Lieutenant Russell L. Maughan, Air Service, United States Army (FAI)
27 October 1918:
MAUGHAN, RUSSELL L.
First Lieutenant (Air Service), U.S. Army
Pilot, 139th Aero Squadron, American Expeditionary Forces
Citation:
Distinguished Service Cross
The President of the United States of America, authorized by Act of Congress, July 9, 1918, takes pleasure in presenting the Distinguished Service Cross to First Lieutenant (Air Service) Russell L. Maughan, United States Army Air Service, for extraordinary heroism in action while serving with 138th Aero Squadron, U.S. Army Air Service, A.E.F., near Sommerance, France, 27 October 1918. Accompanied by two other planes, Lieutenant Maughan was patrolling our lines, when he saw slightly below him an enemy plane (Fokker type). When he started an attack upon it he was attacked from behind by four more of the enemy. By several well-directed shots he sent one of his opponents to the earth, and, although the forces of the enemy were again increased by seven planes, he so skillfully maneuvered that he was able to escape toward his lines. While returning he attacked and brought down an enemy plane which was diving on our trenches.
General Orders: War Department, General Orders No. 46 (1919), Amended Supplement 1
Action Date: October 27, 1918
Officers of the 139th Aero Squadron, at Belrain Aerodrome, France, November 1918. 1st Lieutenant Russell L. Maughan is at the center of the photograph, kneeling, in the second row. (U.S. Air Force)
Maughan is credited with four enemy aircraft destroyed while flying a SPAD S.XIII C.I fighter.
Russell Lowell Maughan was born at Logan, Utah, 28 March 1893. He was the sixth of eight children of Peter Weston Maughan, an accountant, and Mary Lucinda Naef Maughan. He attended Utah Agricultural College in Logan and graduated with a bachelor of science degree in 1917.
Maughan was commissioned as a second lieutenant in the U.S. Army Signal Officers Reserve Corps, 28 May 1917. He was promoted to first lieutenant, 8 January 1918. This commission was vacated 10 September 1920 and he was appointed a first lieutenant, Air Service, United States Army, retroactive to 1 July 1920.
On 14 August 1919, Maughan married Miss Ila May Fisher at Logan, Utah. They would have three children, but divorced sometime after 1940. His son, Russell L. Maughan, Jr., would become an cadet at the United States Military Academy (West Point) and be commissioned as an officer in the U.S. Air Force.
Following the War, Lieutenant Maughan became a test pilot at McCook Field, Ohio. In 1921, he was reassigned to the 91st Observation Squadron, based at the Presidio of San Francisco.
On 14 October 1922, Rusell Maughan won the Pulitzer Trophy Race at Selfridge Field, near Mount Clemens, Michigan, before a crowd of 200,000 spectators. He set two World Speed Record during the race with his Curtiss R-6: 330.41 kilometers per hour (205.31 miles per hour) over a distance of 100 kilometers,¹ and 331.46 kilometers per hour (205.96 miles per hour) over a distance of 200 kilometers).² On 29 March 1923, he set another World Speed Record, 380.75 kilometers per hour (236.587 miles per hour),³ again flying a Curtiss R-6.
Major General Mason Patrick, Chief of the Air Service, with Lieutenant Russell L. Maughan, 8 July 1924. (Library of Congress)
On 23 June 1924, Lieutenant Maughan flew a Curtiss PW-8 Hawk from Mitchel Field, Long Island, New York, to the Presidio of San Francisco on the west coast of California, in an elapsed time of 21 hours, 47 minutes including refueling stops enroute. This was the “Dawn-to-Dusk Flight.” For this transcontinental flight, Maughan was awarded the Distinguished Flying Cross.
On 1 October 1930, Maughan was promoted to captain. He served in the Philippine Islands from 1930 to 1935, acting as an advisor to the government until 1932. From 1932 to 1935, he served as the post operations officer. He and his family lived in Manila. They returned to the United States aboard SS Columbus, a Norddeutscher Lloyd passenger liner, arriving at New York City from Southampton, 18 August 1935.
Captain Maughan served as an aviation advisor to the governor general of the Philippine Islands, from 1935 to 1939. On 16 June 1936, Captain Maughan was promoted to major (temporary). That rank was made permanent 12 June 1939. He was promoted to lieutenant colonel, 11 March 1940. Just prior to World War II, Lieutenant Colonel Maughan was sent on a survey tour to identify suitable locations for airfields in Greenland.
During World War II, Lieutenant Colonel Maughan commanded the 60th Troop Carrier Group, a Douglas C-47 unit, 1941–42, and then, with the rank of colonel, he commanded the 51st Troop Carrier Wing during Operation Torch, the Allied invasion of North Africa.
On 25 October 1946, Colonel Maughan married Lois Rae Roylance at Las Vegas, Nevada. She was 21 years his junior. They lived in Portland, Oregon.
Colonel Maughan later commanded Lemoore Army Airfield, California, and Portland Air Force Base, Oregon.
Maughan was discharged from the U.S. Air Force, 30 November 1947, at the U.S. Army Hospital at Valley Forge, Pennsylvania. He died at the U.S. Air Force Hospital, Lackland Air Force Base, San Antonio, Texas, 21 April 1958, at the age of 65 years. He was buried at the Logan City Cemetery, Logan, Utah.
SPAD S.XIII at Air Service Production Center No. 2, Romorantin Aerodrome, France, 1918. (U.S. Air Force)
The Société Pour L’Aviation et ses Dérivés SPAD S.XIII C.1 was a single-seat, single-engine, two-bay biplane designed by Technical Director Louis Béchéreau. The chasseur was first flown by René Pierre Marie Dorme, 4 April 1917. It was constructed of a wooden framework and covered with doped fabric. Sheet metal panels covered the engine and cockpit.
The SPAD S.XIII was 20 feet, 4 inches (6.198 meters) long with the wings having an equal span of 26 feet, 3¾ inches (8.020 meters). It had an overall height of 7 feet, 6½ inches (2.299 meters). The total wing area was 227 square feet (21.089 square meters). The wings each had a chord of 4 feet, 7-1/8 inches (1.400 meters) with 0° dihedral and 1¼° stagger. The vertical gap between the upper and lower wings was 3 feet, 10½ inches (1.181 meters). The upper wing had a 1½° angle of incidence; the lower wing had 1° angle of incidence. There were ailerons on the upper wing only. They had a span of 7 feet, 3½ inches (2.222 meters) and chord of 1 foot, 7½ inches (0.495 meters). The horizontal stabilizer span was 10 feet, 2 inches (3,099 meters. Its maximum chord was 1 foot, 8¾ inches (0.527 meters). The vertical fin height was 2 feet, 7/8-inch (0.876 meters) and it was 3 feet, 11¼ inches (1.200 meters) long at the base. The rudder was 3 feet, 10-5/8 inches (1.184 meters) high with a maximum chord of 2 feet, 2 inches (0.660 meters).
The airplane had fixed wheeled landing gear which used rubber cords (bungie cords) for shock absorption. The wheel track was 4 feet, 10¾ inches (1.492 meters). A fixed skid was used at the tail.
The the S.XIII had an empty weight of 1,464 pounds (663 kilograms) and maximum takeoff weight of 1,863 pounds (845 kilograms).
The SPAD S.XIII C.1 was powered by a water-cooled, normally-aspirated 11.762 liter (717.769-cubic-inch-displacement) left-hand tractor ⁴ Hispano-Suiza 8B single-overhead-cam 90° V-8 engine, with a 5.3:1 compression ratio. The engine drove a fixed-pitch two-bladed laminated wood propeller through a 0.75:1 gear reduction. The Hispano-Suiza 8B was rated at 235 cheval vapeur (231.8 horsepower) at 2,300 r.p.m. It was 1.36 meters (4 feet, 5.5 inches) long, 0.86 meters (2 feet, 9.9 inches) wide, and 0.90 meters (2 feet, 11.4 inches) high. It weighed 236 kilograms (520.3 pounds).
The SPAD’s main fuel tank was behind the engine, with a gravity feed supply tank in the upper wing. The total fuel total capacity was about 30 gallons (114 liters). This was sufficient for two hours endurance at full throttle at 10,000 feet (3,048 meters), including climb.
The SPAD XIII had a maximum speed at Sea Level of 131.5 mph (211.6 kilometers per hour) at 2,300 rpm; and 105 mph (169 kilometers per hour) at its service ceiling of 18,400 feet (5,608 meters), at 2,060 r.p.m. The airplane’s absolute ceiling was 20,000 feet (6,096 meters).
The fighter was armed with two fixed, water-cooled, .303-caliber Vickers machine guns, or two air-cooled .30-caliber Marlin M1917 or M1918 aircraft machine guns, with 400 rounds of ammunition per gun, synchronized to fire forward through the propeller arc.
According to a report by the National Aeronautics and Space Administration,
. . .the SPAD XIII had the most favorable power loading of any of the aircraft considered and a high (for its day) wing loading. These characteristics coupled with a relatively low zero-lift drag coefficient and low drag area gave the SPAD the highest speed of any of the aircraft listed in the table. As shown by the data in figure 2.18, the climb characteristics of the SPAD were bettered only by three of the Fokker aircraft.
A total of 8,742 S.XIII C.1 fighters were built by nine different manufacturers. Only one, Société Kellner Frères Constructeurs serial number 4377, the oldest existing original airplane, is in flyable condition. It is in the collection of the Memorial-Flight Association at L’aérodrome de La Ferté-Alais (LFFQ)
The same type fighter flown by Lt. Maughan on 27 October 1918, this is SPAD S.XIII C.1 serial number 7689, Smith IV, after restoration at the Paul E. Garber Center, Smithsonian Institution National Air and Space Museum. (NASM)
¹ FAI Record File Number 15195
² FAI Record File Number 15196
³ FAI Record File Number 15194
⁴ The propeller rotates clock-wise, as seen from the front of the airplane.
Sergeant Joseph Frantz and Corporal Louis Quénault. (Unattributed)
5 October 1914: The first aerial combat between two airplanes took place during World War I over Jonchery, Reims, France.
A French Voisin III biplane of Escadrille VB24, flown by Sergeant Joseph Frantz with observer Corporal Louis Quénault, engaged a German Aviatik B.II flown by Oberleutnant Fritz von Zangen and Sergeant Wilhelm Schlichting of FFA 18.
Voisin III. (Unattributed)
The Voisin was armed with a Hotchkiss M1909 8mm machine gun. Corporal Quénault fired two 48-round magazines at the German airplane, whose crew returned fire with rifles. Quénault’s machine gun jammed and he continued to fire on the Aviatik with a rifle.
The German airplane crashed and von Zangen and Schlichting were killed.
This was the first air-to-air kill in the history of warfare.
Aviatik B.II No. B 558/15, Hangest-en-Santerre, France, circa 1915. (Unattributed)
