B-25 Mitchell bombers aboard USS Hornet (CV-8), with USS Gwin (DD-433) and USS Nashville (CL-43), somewhere in the Pacific, April 1942. (U.S. Navy)
2 April 1942: After loading sixteen North American Aviation B-25B Mitchell medium bombers and their crews of the 17th Bombardment Group (Medium) at NAS Alameda, the recently commissioned United States Navy aircraft carrier USS Hornet (CV-8) departed San Francisco Bay with her escorts and headed for a secret rendezvous with Vice Admiral William F. Halsey, Jr., and Task Force 16.
The new carrier was under command of Captain Marc A. Mitscher. The strike group was commanded by Lieutenant Colonel James H. (“Jimmy”) Doolittle, U.S. Army Air Corps. Until the second day at sea, only six U.S. military officers knew of the mission.
The photograph above shows some of the bombers secured on Hornet‘s flight deck. An escorting destroyer, USS Gwin (DD-433) is closing from astern, with light cruiser USS Nashville (CL-43) in the distance. Two more ships are on the horizon.
USS Hornet (CV-8), Captain Marc A. Mitscher, U.S.N., commanding, 27 October 1942. The aircraft carrier is painted in Measure 12 camouflage, Sea Blue 5-S, Ocean Gray 5-O and Haze Gray 5-H. (U.S. Navy)
USS Hornet was a brand new Yorktown-class aircraft carrier, commissioned 20 October 1941. It had just completed its shakedown cruise in the Atlantic when it was sent west for this mission.
The ship was 824 feet, 9 inches (251.384 meters) long, overall, with a maximum width of 114 feet (34.747 meters). Hornet‘s dimensions at the waterline (full load displacement) were 761 feet (232 meters) long with a beam of 83 feet, 3 inches (25.375 meters). Its draft was 28 feet (8.5 meters).
The flight deck had two hydraulic catapults, and three elevators for bringing aircraft up from the hangar deck. A third catapult was on the hangar deck, launching aircraft laterally.
Powered by four geared steam turbines driving four propeller shafts, Hornet‘s engines produced 120,000 shaft horsepower. The carrier’s maximum speed was 33.84 knots (39.94 miles per hour/62.67 kilometers per hour), and maximum range, 12,500 nautical miles (14,385 kilometers).
A 17th Bombardment Group North American Aviation B-25B Mitchell medium bomber tied down on the flight deck of U.S.S. Hornet (CV-8). An escorting destroyer, USS Gwin, (DD-433 ), Commander John S. Higgins, U.S.N., commanding, closes on the carrier’s right rear quarter. The sixteen Army bombers used all the space available on Hornet’s flight deck.(U.S. Navy)
The aircraft carrier’s primary armament was its air wing, consisting of a squadron each of Grumman F4F Wildcat fighters, Douglas SBD Dauntless dive bombers and Douglas TBD Devastator torpedo bombers. For the Halsey-Doolittle Raid, Hornet‘s air wing was stored on the hangar deck and unavailable.
“To make room for the Army bombers, Hornet had struck her own planes below. Wildcats and Devastators, with wings folded, and dismantled SBDs were packed into every available space, even hung from the overhead. So, except for her few guns, the carrier was defenseless until she rendezvoused with Task Force 16. . . .”
—History of United States Naval Operations in World War II, Volume III, The Rising Sun in the Pacific, by Samuel Eliot Morison, Little, Brown & Company, Boston, 1988, Chapter XX at Page 392.
For defense, the ship was lightly armored, with 2.5–4 inches (6.35–10.2 centimeters) of belt and deck armor. She also carried eight 5-inch, 38-caliber (5″/38) dual-purpose guns in single mounts, thirty 20mm Oerlikon autocannon, twenty water-cooled 1.1-inch, 75-caliber (1.1″/75) guns in four-gun mounts, and twenty-four Browning .50-caliber (12.7 millimeter) machine guns.
Including the ship’s air wing, the complement was 2,919 men.
USS Hornet fought at the Battle of Midway, June 3–7, 1942. She was sunk at the Battle of the Santa Cruz Islands, 26 October 1942, having been hit by two airplanes, 8 bombs, 16 torpedoes and an unknown number of 5-inch shells.¹
USS Hornet (CV-8) at Pearl Harbor, Hawaii, following the Halsey-Doolittle Raid, 1942. The ship is painted in Measure 12 (Modified) camouflage with splotches, with Navy Blue 5-N, Sea Blue 5-S, Ocean Gray 5-O and Haze Gray 5-H coloration.
¹ The research vessel R/V Petrel located the wreck of USS Hornet on the sea floor in January 2019. The ship lies at a depth of 5,330 meters (17,487 feet).
Messerschmitt Me 262 A-1 WNr. 111711 (U.S. Air Force)
31 March 1945: Messerschmitt Aktiengesellschaft test pilot and technical inspector Hans Fay (1888–1959) defected to the Allies at Frankfurt/Rhein-Main Airfield, Frankfurt, Germany.
He brought with him a brand-new Messerschmitt Me 262 A-1 twin-engine jet fighter.
Fay had been waiting for an opportunity to bring an Me 262 to the Americans, but feared reprisals against his parents. When he learned that the U.S. Army controlled their town, he felt that it was safe to go ahead with his plan.
On 31 March, Fay was ordered to fly one of twenty-two new fighters from the Me 262 assembly factory at Schwäbisch-Hall to a safer location at Neuburg an der Donau, as they were in danger of being captured by advancing Allied forces. His airplane was unpainted other than low visibility Balkenkreuz markings on the wings and fuselage, and standard Luftwaffe markings on the vertical fin. Fay was the fourth to take off, but instead of heading east-southeast toward Neuburg, he flew north-northwest to Frankfurt, arriving there at 1:45 p.m.
Hans Fay’s Messerschmitt Me 262 A-1 at Frankfurt Airfield. (U.S. Air Force)
The Messerchmitt Me 262 Schwalbe was the first production jet fighter. It was a single-place, twin-engine airplane with the engines placed in nacelles under the wings. It was 10.6 meters (34 feet, 9.3 inches) long with a wingspan of 12.51 meters (41 feet, 5.2 inches) and overall height of 3.85 meters (12 feet, 7.6 inches). According to Fay, the fighter’s empty weight was 3,760 kilograms (8,289 pounds) and the maximum gross weight was 7,100 kilograms (15,653 pounds) at engine start.¹
The Me-262 wings had 6° dihedral. The leading edges were swept aft to 20°, while the trailing edges of the inner panels swept forward 8½° to the engine nacelle, then outboard of the engines, aft 5°. The purpose of the sweep was to keep the airplane’s aerodynamic center close to the center of gravity, a technique first applied to the Douglas DC-2. The total wing area was 21.7 square meters (233.6 square feet).
Messerschmitt Me 262A-1 WNr. 111711 at Frankfurt Airfield. (U.S. Air Force)
The Me 262 A-1 was powered by two Junkers Jumo TL 109.004 B-1 turbojet engines. The 004 was an axial-flow turbojet with an 8-stage compressor section, six combustion chambers, and single-stage turbine. The 004 engine case was made of magnesium for light weight, but this made it vulnerable to engine fires. The engine was designed to run on diesel fuel, but could also burn gasoline or, more commonly, a synthetic fuel produced from coal, called J2. The engine was first run in 1940, but was not ready for production until 1944. An estimated 8,000 engines were built. The 004 B-1 idled at 3,800 r.p.m., and produced 1,984 pounds of thrust (8.825 kilonewtons) at 8,700 r.p.m. The engine was 2 feet, 10 inches (0.864 meters) in diameter, 12 feet, 8 inches (3.861 meters) long, and weighed 1,669 pounds (757 kilograms).
24 March 1946: The Jumo 004 was tested at the NACA Aircraft Engine Research Laboratory, Cleveland, Ohio. The axial-flow compressor section is visible. (NASA)
During interrogation, Hans Fay said that for acceptance, the production Me 262 was required to maintain a minimum of 830 kilometers per hour (515 miles per hour) in level flight, and 950 kilometers per hour (590 miles per hour) in a 30° dive. The fighter’s cruise speed was 750 kilometers per hour (466 miles per hour).
A number of factors influenced the Me 262’s maximum range, but Fay estimated that the maximum endurance was 1 hour, 30 minutes. U.S. Air Force testing establish the range as 650 miles (1,046 kilometers) and service ceiling at 38,000 feet (11,582 meters).
Lt. Walter J. McAuley, Jr.
The Me 262 A-1 was armed with four Rheinmetall-Borsig MK 108 30 mm autocannons with a total of 360 rounds of ammunition. (The Me 262 A-2 had just two autocannons with 160 rounds.) It could also be armed with twenty-four R4M Orkan 55 mm air-to-air rockets. Two bomb racks under the fuselage could each be loaded with a 500 kilogram (1,102 pounds) bomb.
1,430 Me 262s were produced. They entered service during the summer of 1944. Luftwaffe pilots claimed 542 Allied airplanes shot down with the Me 262.
Hans Fay’s Messerschmitt Me 262 A-1, WNr. 111711, was transported to the United States and was tested at Wright Field, Dayton, Ohio.
711 was lost during a test flight, 20 August 1946, when one of its engines caught fire. The test pilot, Lieutenant Walter J. “Mac” McAuley, Jr., U.S. Army Air Corps, safely bailed out. The Me 262 crashed 2 miles (3.2 kilometers) east of Lumberton, Ohio, and was completely destroyed.
Messerschmitt Me 262A-1 Schwalbe WNr. 111711. (U.S. Air Force)
Walter J. McAuley, Jr.,² was born 10 March 1917 at Fort Worth, Texas. He was the fourth child of Walter J. McAuley and Lola Mahaffey McAuley. Walter attended Texas A&M College at College Station, Texas. While there, he also worked as a mechanic. He graduated with a bachelor of science degree in 1941.
McAuley had brown hair, blue eyes, was 5 feet, 9 inches (1.75 meters) tall and weighed 160 pounds (75.6 kilograms).
McAuley enlisted as a seaman, second class, United States Naval Reserve, and served from 11 April to 3 December 1941. He transferred to the U.S. Army as a private, Air Corps Enlisted Reserve Corps (A.C.E.R.C.), 2 May 1942. Private McAuley was accepted as an aviation cadet, Air Corps, 18 October 1942.
Aviation Cadet McAuley was commissioned as a second lieutenant, Army of the United States (A.U.S.), 29 July 1943, and placed on active duty. He was promoted to first lieutenant, A.U.S., one year later, 1 August 1944.
Lieutenant McAuley was promoted to captain, Air-Reserve, 30 July 1947. On 10 July 1947, he received a permanent commission as a first lieutenant, Air Corps, United States Army. His date of rank was retroactive to 10 March 1945.
After the establishment of the United States Air Force, Lieutenant McAuley was transferred to the new service. He was number 6,626 on the register of Air Force first lieutenants.
McCauley rose to the rank of lieutenant colonel in the U.S. Air Force. He was released from duty 31 December 1962.
Walter J. McAuley Jr., married Miss Mary Elizabeth Sloss, 8 May 1943. They divorced 25 March 1969. He then married Lillian R. Zwickl, 3 April 1969. They also divorced, 10 September 1971.
Lieutenant Colonel McAuley died 11 March 1985. He was buried at Greenwood Memorial Park, Fort Worth, Texas.
Messerschmitt Me 262A-1 WNr. 111711 at Wright Field. (U.S. Air Force)
¹ A technical report from RAE Farnborough gave the empty weight of the Me 262 as 11,120 pounds (5,044 kilograms). Its “all up weight,” less ammunition, was 14,730 pounds (6,681 kilograms).
North American Aviation B-25B Mitchell 40-2291 at Eglin Field, Florida, March 1942. (U.S. Air Force)
27 March 1942: After three weeks of intensive training at Eglin Field, Florida, twenty-two North American Aviation B-25B Mitchell twin-engine medium bombers of the 34th Bombardment Squadron (Medium), 17th Bombardment Group (Medium), U.S. Army Air Force, under the command of Lieutenant Colonel James Harold Doolittle, completed a two-day, low-level, transcontinental flight, and arrived at the Sacramento Air Depot, McClellan Field, California, for final modifications, repairs and maintenance before an upcoming secret mission: The Halsey-Doolittle Raid.
The B-25 had made its first flight 19 October 1940 with test pilot Vance Breese and engineer Roy Ferren in the cockpit. It was a mid-wing airplane with twin vertical tails and retractable tricycle landing gear. The first 8–10 production airplanes were built with a constant dihedral wing. Testing at Wright Field showed that the airplane had a slight tendency to “Dutch roll” so all B-25s after those were built with a “cranked” wing, using dihedral for the inner wing and anhedral in the wing outboard of the engines. This gave it the bomber’s characteristic “gull wing” appearance. The two vertical stabilizers were also increased in size.
A 34th Bombardment Squadron B-25B Mitchell bomber at Mid-Continent Airlines, Minneapolis, Minnesota, for modifications, January–February 1942. (U.S. Air Force)
The B-25B Mitchell was operated by a crew of five: two pilots, a navigator, bombardier and radio operator/gunner. It was 53 feet, 0 inch (16.154 meters) long with a wingspan of 67 feet, 7.7 inches (20.617 meters) and overall height of 15 feet, 9 inches (4.801 meters). The The B-25B had an empty weight of 20,000 pounds (9,072 kilograms) and the maximum gross weight was 28,460 pounds (12,909 kilograms).
The B-25B was powered by two air-cooled, supercharged, 2,603.737-cubic-inch-displacement (42.668 liter) Wright Aeronautical Division Cyclone 14 GR2600B665 (R-2600-9) two-row 14-cylinder radial engines with a compression ratio of 6.9:1. The engines had a Normal Power rating of 1,500 horsepower at 2,400 r.p.m., and 1,700 horsepower at 2,600 r.p.m. for takeoff, burning 100-octane gasoline. These engines (also commonly called “Twin Cyclone”) drove three-bladed Hamilton Standard Hydromatic variable-pitch propellers through 16:9 gear reduction. The R-2600-9 was 5 feet, 3.1 inches (1.603 meters) long and 4 feet, 6.26 inches (1.378 meters) in diameter. It weighed 1,980 pounds (898 kilograms).
“On a low level training mission early in 1942 B-25 40-2297 would be airplane number 14 for the Doolittle Raid on Tokyo — This image was taken before the modification to the troublesome ventral turret. Pilot Major J.A. Hilger, Co-Pilot 2nd Lt. Jack A. Sims, Navigator 2nd Lt. James H. Macie, Jr., Bombardier S/Sgt. Jacob Eierman, Engineer/Gunner S/Sgt. Edwin V. Bain” —HISTORYNET
The medium bomber had a maximum speed of 322 miles per hour (518 kilometers per hour) at 15,000 feet (4,572 meters) and a service ceiling of 30,000 feet (9,144 meters).
It could carry a 3,000 pound (1,361 kilograms) bomb load 2,000 miles (3,219 kilometers). Defensive armament consisted of a single Browning M2 .30-caliber machine gun mounted in the nose, two Browning M2 .50-caliber machine guns in a power dorsal turret, and two more .50s in a retractable ventral turret. (The lower turrets were removed from all of the Doolittle B-25s.)
North American Aviation, Inc., built 9,816 B-25s at Inglewood, California, and Kansas City, Kansas. 120 of these were B-25Bs.
North American Aviation B-25 Mitchell medium bombers being assembled at the Kansas City bomber plant, October 1942. (Alfred T. Palmer, Office of War Information)
Stammlager Luft III prison in Province of East Silesia, World War II. (Muzeum Obózow Jenieckich W Żaganiu)
24 March 1944: At about 2230 hours, the first of 76 Allied prisoners of war interred at Stammlager LuftIII (Stalag Luft III) began to escape through a 30-foot-deep (9 meters), 320-foot-long (98 meters) tunnel, code-named “Harry.”
Aerial reconnaissance image of Stalag Luft III, 17 September 1944. (American Air Museum in Britain UPL 36335)
The prison, located just south of Sagan (Żagań) in East Silesia (now a part of Poland) was specially constructed to house captured Royal Air Force and other Allied airmen, and was controlled by the German air force, the Luftwaffe. Prior to this escape, the German captors had discovered at least 98 tunnels at the prison.
Popularly known as “The Great Escape,” this was the subject of a 1950 book, The Great Escape, by Paul Brickhill, who was a POW at the prison. His book was adapted into a very popular motion picture, “The Great Escape,” in 1963.
Squadron Leader Thomas Gresham Kirby-Green, RAF, and Flight Lieutenant Gordon Arthur Kidder, RCAF, were murdered by Gestapo agents near Zlín, Moravia, 29 March 1944. (This photograph may be of a reconstruction by the RAF Special Investigations Branch, circa 1946)
Cornelia Clark Fort with a Fairchild PT-19A Cornell trainer. (U.S. Air Force)
21 March 1943: Cornelia Clark Fort, a pilot in the Women’s Auxiliary Ferrying Squadron (the WAFS), was ferrying a new Vultee BT-13A Valiant basic trainer, serial number 42-42432, from the airplane factory at Downey, California, to an airfield in Texas. She was leading a flight of five BT-13s with the others being flown by inexperienced military pilots.
A flight of Vultee BT-13A Valiant basic trainers, 41-22226, 41-22666 and 41-23050. (Smithsonian Institution National Air and Space Museum NASM A19600288000a)
The left wing of Fort’s airplane was struck from behind by another airplane, BT-13A 42-42450, flown by Flight Officer Frank E. Stamme, Jr., U.S. Army Air Corps.
Fort’s BT-13 crashed approximately 10 miles (16 kilometers) south of Merkel, Texas, and Cornelia Fort was killed. Her body was found in the wreckage of the airplane. The canopy latches were still fastened.
The Associated Press reported:
Woman Ferry Pilot Killed
LONG BEACH, Calif., March 22. (AP)—The army air transport command’s ferrying division has announced the death of Cornelia Fort, twenty-three-year-old Nashville, Tenn., pilot.
Miss Fort was killed, the command said, on a routine ferrying flight yesterday at Merkel, Tex. She was the second woman to sign up with the women’s auxiliary ferrying squadron, and had had 1100 hours in the air.
Cause of the accident has not been learned, the command reported.
Fifteen months ago, a private flying instructor, Miss Fort was giving a lesson over Honolulu when the Japs attacked. Her surprised student almost piloted their plane into an enemy ship before she grabbed the controls, she related later.
Following her evacuation from the Hawaiian islands, she joined the auxiliary ferrying squadron and was stationed here. Miss Fort was the daughter of Cornelia Clark Fort of Fortland farms, near Nashville.
Cornelia Clark Fort was the first female pilot killed while on active duty with the United States military. She was 24 years old. Miss Fort was buried at the Mount Olivet Cemetery, Nashville, Tennesee.
Cornelia Clark Fort. (Tennessee State Library and Archives)
Cornelia Clark Fort was born into an affluent family in Nashville, Tennessee, 5 February 1919. She was the fourth of five children of Dr. Rufus Elijah Fort and Louise Clark Fort. Her father was a prominent surgeon who co-founded the National Life and Accident Insurance Company. The family lived at Fortland, an estate east of Nashville.
Cornelia Clark Fort. (1936 Milestones)
Cornelia attended the Ward-Belmont School in Nashville, then studied at the Ogontz School in Philadelphia. (Amelia Earhart had also attended Ogontz.) In 1937, Miss Fort transferred to Sarah Lawrence College, Yonkers, New York, where she studied Literature. She graduated 10 June 1939.
After taking a flight with a friend, Jack Caldwell, in January 1940, she pursued an interest in aviation, starting flight lessons the following day. Miss Ford had earned her pilot certificate and flight instructor certificate by June 1940. She was the first woman to become an instructor at Nashville. With the Civilian Pilot Training Program, she first went to Fort Collins, Colorado, where she taught for about three months, then went on to Honolulu, Territory of Hawaii.
On the morning of 7 December 1941, Cornelia Fort was practicing touch-and-goes with a student at John Rodgers Airport, near Honolulu.
Shortly before 8:00 a.m., Miss Fort saw a silver military-type airplane approaching her Interstate Cadet at high speed. She took over the flight controls from Mr. Suomala and put the trainer into a steep climb. The other airplane flew directly under, close enough that she felt the vibrations of its engine. She saw that its wings carried the “rising sun” insignia of the Empire of Japan.
Fort landed the Cadet at John Rogers Airport, which was being attacked by Japanese airplanes. Another trainer on the ground was destroyed by machine gunfire and its instructor killed.
“WAFS WELCOMED—Mrs. Nancy H. Love (left), commander, is shown in this photo greeting Women’s Auxiliary Ferrying Command recruits at New Castle, Del. The fledglings are, left to right, Cornelia Fort, Helen Clark, Aline Rhonie and Betty Gillies.” (AP Wirephoto, The Evening Sun (Baltimore, Maryland), Vol. 65—No. 137, Thursday, 24 September 1942, Page 28, Columns 5–8)
Following the attack on Pearl Harbor, all civilian aircraft were grounded. Cornelia Fort was able to return to the mainland United States in early 1942. In September she was one of the first 25 women accepted into the Women’s Auxiliary Ferrying Squadron. Miss Fort was assigned to the 6th Ferrying Group based at Long Beach, California.
Pilots of the Women’s Auxiliary Ferrying Squadron at Long Beach Army Airfield, 7 March 1943. Left to right, Barbara Towne, Cornelia Clark Fort, Evelyn Sharp, Barbara Erickson and Bernice Batten. The airplane is a Vultee BT-13 Valiant. (Image Courtesy of the WASP Archive, The TWU Libraries’ Woman’s Collection, Texas Woman’s University, Denton, Texas)
Air & Space/Smithsonian quoted from a letter written by Fort in a January 2012 article:
“I dearly loved the airports, little and big. I loved the sky and the airplanes, and yet, best of all I loved the flying. . . I was happiest in the sky at dawn when the quietness of the air was like a caress, when the noon sun beat down, and at dusk when the sky was drenched with the fading light.”
—Cornelia Clark Fort, 1942.
Cornelia Clark Fort’s military identification card. (Nashville Public Library)
Frank Edward Stamme, Jr., was born at Dorchester, Illinois, 3 January 1920. He was the first of four children of Frank Edward Stamme, a machinist, and Bertha Catherine Peters Stamme.
Stamme enlisted as a private in the U.S. Army Air Corps at San Francisco, California, 5 November 1941. He had brown hair, gray eyes, was 6 feet, 1 inch (1.85 meters) tall and weighed 159 pounds (72 kilograms). At the time of the collision, he had approximately 250 hours flight time. Stamme was released from military service 16 January 1947. He died 19 February 1987 at San Pablo, California.
Vultee BT-13A Valiant 42-43130, the same type aircraft flown by Cornelia Fort and Frank Stamme, 21 March 1943. (U.S. Air Force)
The Vultee BT-13A Valiant was an all-metal, two-place, single engine, low-wing monoplane with fixed landing gear. The airplane was 28 feet, 10 inches (8.788 meters) long with a wingspan of 42 feet, 0 inches (12.802 meters) and height of 11 feet, 4-3/8 inches (3.464 meters). It had an empty weight of approximately 3,375 pounds (1,531 kilograms) and “maximum recommended flying weight” of 4,745 pounds (2,152 kilograms).
The BT-13A was powered by an air-cooled, supercharged, 986.749-cubic-inch-displacement (16.170 liter) Pratt & Whitney R-985-AN-1, -AN-3, or R-985-25 nine-cylinder radial engine. These engines had a compression ratio of 6:1, with Normal Power ratings from 420 horsepower at 2,200 r.p.m. at Sea Level to 450 horsepower at 2,300 r.p.m., and 440 horsepower to 450 horsepower at 2,300 r.p.m. for Takeoff. They were direct-drive engines which turned a two-bladed variable-pitch propeller. These engines were 3 feet, 6.38 inches (1.076 meters) long, 3 feet, 9.75 inches (1.162 meters) in diameter and weighed from 648 to 685 pounds (294–311 kilograms).
The BT-13A had a maximum speed (VNE) of 230 miles per hour (370 kilometers per hour). The service ceiling was 21,650 feet (6,599 meters) and range was 725 miles (1,167 kilometers).
Vultee built 9,525 BT-13 and BT-15 Valiant basic trainers between 1940 and 1945. Of these, 7,037 were the BT-13A and SNV-1 variant. By the end of World War II, the Vultee Valiant was considered obsolete and was replaced in U.S. service by the North American AT-6 Texan.
![A drawing showing the proposed route of one of the escape tunnels, by wartime artist Ley Kenyon, a prisoner-of-war in Stalag Luft III at the time of the Great Escape in March 1944 [Picture: from the original drawings of Ley Kenyon 1943] (GOV.UK)](https://static.thisdayinaviation.com/wp-content/uploads/tdia/2016/03/ODD_5948.jpg.webp)
