2 June 1941

Consolidated Aircraft Corporation Model LB-30, Liberator B Mk.II, AL503 (SDASM Archives)

2 June 1941: Great Britain had been at war with Germany for 21 months. Its need for military equipment far exceeded the capacity of British industry, so the Empire looked across the North Atlantic Ocean to its former colonies, the United States of America.

The Royal Air Force ordered 140 Liberator B Mk.II bombers from Consolidated Aircraft Corporation of San Diego, California. The Consolidated Model LB-30 was a variant of the U.S. Army Air Corps B-24 four-engine long-range heavy bomber, but was built expressly for the RAF and had no direct Air Corps equivalent.

AL503 was the first Liberator Mk.II. It had made its first flight 26 May 1941, and was ready to be turned over to the Royal Air Force.

AL503 crashed on its acceptance flight, 2 June 1941. The aircraft was destroyed and all five on board were killed.

Consolidated LB-32, Liberator B Mk.II, AL503, photographed 2 June 1941—the same day it crashed. (Consolidated Aircraft Corporation)
Consolidated Model LB-30, Liberator B Mk.II, AL503, photographed 2 June 1941—the same day it crashed. The four-gun upper turret is visible. The bomb bay is open. (Consolidated Aircraft Corporation)

The Associated Press reported the accident:

Big Bomber Made for Britain Crashes in San Diego Bay; Four Members of Crew Perish

SAN DIEGO, Calif., June 2—(AP)—A $250,000 four-motored Consolidated bomber crashed and sank in San Diego Bay today, shortly after taking off from Lindbergh Field. Consolidated Aircraft Corp. officials said four of the crew members apparently perished.

The 25-ton craft was camouflaged and ready for delivery to Great Britain.

William B. Wheatley, 39, Chester, N.Y., chief test pilot for the Consolidated Aircraft Corp., apparently was at the controls. The Navy had taken over rescue operations, and details and names of crew members were not immediately available.

Witnesses said the huge plane left the airport on what appeared to be a normal takeoff, but that the bomber pulled up steep into a vertical climb instead of leveling off. At about 500 feet the plane apparently was in a stall.

The bomber then fell off to the left, and nosed down and the pilot, using the throttle appeared to have recovered. This difficulty was experienced over the airport, but by the time the pilot apparently had regained control of the craft it was flying over the water an an altitude of about 100 feet, the bomber again fell off to the left and the wing struck the water.

A Consolidated spokesman said the crash had “evidence of sabotage.”

The spokesman said the $250,000, 25-ton land bomber had been “thoroughly tested, and things like that just don’t happen.”

Believed dead were:

William Wheatley, 39, Chester, N.Y., chief test pilot for the company.
Allen T. Austen, 28, Kansas City, Mo., assistant test pilot.
Bruce K. Craig, 27, Chicago, engineer.
William H. Rieser, 33, Cambridge, Mass.
Lewis M. McAannon, 25, Woodstock, Ill., chief mechanic, was seriously injured. ¹

The bodies of Wheatley, Craig and Austin had not been recovered from the shattered bomber.

The impact with the water shattered the bomber, witnesses said, and it sank. Navy and small fishing vessels went to the rescue. The plane went down in an area between the San Diego shoreline and the naval air station.

The bomber, called “Liberator” by the Royal Air Force, was of all-metal construction, and its type is regarded as one of the most advanced military weapons. The Liberator can travel 230 miles an hour with a full bomb load over a 3,000 mile range. Orders for the huge land bomber originally were placed by the French, then taken over by the British.

The first B-24 was delivered to the British last Feb. 15 when the craft Consolidated Aircraft officials said established a record non-stop transcontinental flight of 9 hours, 57 minutes for planes of more than 5,000 pounds gross weight.

—The Eugene Guard, Vol. 50, No. 152, Monday, June 2, 1941, at Page 1 Column 6 and Page 2, Column 2

This aerial photograph of Lindbergh Field, San Diego, California, shows the location of the PB4Y-2 crash site, and nearby, the position where the outer wing panel was found. (U.S. Navy)
This is a 1944 aerial photograph of Lindbergh Field, San Diego, California, part of an investigation of the crash of a brand-new Consolidated PB4Y-2 Privateer. The Pacific Ocean is at the upper left corner of the image. (U.S. Navy)

The Consolidated B-24 had first flown 29 December 1939. Chief Test Pilot Bill Wheatley was in command. Designed as a long-range heavy bomber for the U.S. Army Air Corps, it was a high-wing, four-engine monoplane with dual vertical fins and rudders. It had retractable tricycle landing gear. The bomber was flown by two pilots, with the crew including a navigator, bombardier, radio operator and several gunners.

The Royal Air Force Liberator B. Mk.I was essentially a B-24A. The Liberator Mk.II, though,  was lengthened by extending the nose in front of the cockpit by 3 feet (0.914 meters). It was equipped with two power-operated gun turrets, one at the top of the fuselage, just aft of the wing, and a second at the tail.

The Liberator Mk.II was 66 feet, 4 inches (20.218 meters) long with a wingspan of 110 feet, 0 inches (33.528 meters) and overall height of 18 feet, 0 inches (5.486 meters). It was heavier than the Mk.I as a result of the longer fuselage and the heavy power turrets. The maximum gross weight was 64,250 pounds (29,143 kilograms).

Consolidated LB30 Liberator II
Consolidated Model LB-30, Liberator B Mk.II

The LB-30/Mk.II was powered by four air-cooled, supercharged 1,829.4-cubic-inch-displacement (29.978 liter) Pratt & Whitney Twin Wasp S3C4-G (R-1830-33) two-row fourteen-cylinder radial engines. These had a normal power rating of 1,100 horsepower at 2,550 r.p.m. to 6,100 feet (1,859 meters) and 1,000 horsepower at 2,700 r.p.m at 14,500 feet. The takeoff/military power rating was 1,200 horsepower at 2,700 r.p.m. to 5,000 feet (1,524 meters). The engines drove three-bladed Curtiss Electric variable-pitch propellers through a 2:1 gear reduction. The R-1830-33 was 4 feet, 0.06 inches (1.221 meters) in diameter and 5 feet, 3.48 inches (1.612 meters) long. It weighed 1,480 pounds (671 kilograms).

The Liberator Mk.II had a maximum speed of 263 miles per hour (423 kilometers per hour) at 15,000 feet (4,572 meters). Its service ceiling was 24,000 feet (7315 meters).

As was common with British bombers, the Liberator Mk.II was defended by Browning .303 Mk.II (7.7 × 56 mm) machine guns. Four were installed in the upper power turret and another four guns in the tail turret. Left and right waist positions each had two guns. One gun was mounted at the nose and one in the belly of the aircraft. This was a total of fourteen. The tail turret carried 2,200 rounds of ammunition and the top turret had 600 rounds.

Prime Minister Churchill's personal transport, "Commando," teh second Consolidated LB30 Liberator Mark II, AL504 © IWM (CH 14142)
Prime Minister Churchill’s personal transport, “Commando,” the second Consolidated LB30 Liberator Mark II, AL504. Its fuselage has been lengthened and tail surfaces from the PB4Y-2 Privateer installed. © IWM (CH 14142)

The second Liberator Mk.II, AL504, became the personal transport of Prime Minister Winston Churchill, who named it Commando. In 1944, the aircraft was modified to the single vertical fin configuration of the PB4Y-2 Privateer. Commando disappeared over the Atlantic in 1945.

William Ballentine Wheatley. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

William Ballantine Wheatley was born at Chester, New York, 17 December 1902, the first of three children of William A. Wheatley, a public school superintendent, and Mabel Ballantine Wheatley. He was twice married, first, about 1927, to Esther Leary Wheatley, of Massachussetts. They had two children, Mary and William Thomas Wheatley. His second marriage was to Miss Grace Lenore Ray, 18 April 1935, at Washington, D.C. They would have a son, John, and two daughters, Grace and Charlotte Wheatley.

After two years of college, Wheatley joined the U.S. Army Air Corps as an aviation cadet, 3 March 1925. He trained as a pilot at Brooks Field, Texas, and was commissioned as a 2nd lieutenant, 13 March 1926. On 4 May 1927, Lieutenant Wheatley was assigned to the 118th Observation Squadron, 43rd Division, Air Service, at Hartford, Connecticut, as a pilot and observer. He served in the Air Corps Reserve until 1937.

In 1928, Wheatley went to work for the Pratt & Whitney Aircraft Company as a test pilot. He was an air mail pilot in 1928-1929, and then, in February 1929, he became a test pilot for Reuben H. Fleet’s Consolidated Aircraft Corporation at Buffalo, New York. In 1935, Consolidated moved to its new headquarters at Lindbergh Field, San Diego, California. Wheatley moved with it. He and his family lived in a 3 bedroom home about three miles northeast of the airport. In 1940, his salary as chief test pilot of Consolidated was $50,000 per year. ²

Following Wheatley’s death, Beryl Arthur Erickson was assigned as chief test pilot for Consolidated.

¹ Lewis McCannon also died as a result of the crash.

² Approximately equivalent to $1,119,814 U.S. dollars in 2024.

© 2018 Bryan R. Swopes

2 June 1937

Fred Noonan and Amelia Earhart board the Electra at San Juan, Puerto Rico, 2 June 1937. (Bettmann/CORBIS)

2 June 1937: After an overnight stay at San Juan, Puerto Rico, Amelia Earhart and Fred Noonan continued on Leg 6 of their around-the-world flight, to Caripito, Venezuela, approximately 611 miles (984 kilometers) southeast. They arrived at 1:18 p.m., local time.

“I rolled out of bed at a quarter of four in the morning, hoping to make a dawn take-off from San Juan, but actually the Electra did not lift her wheels from the runway until nearly seven o’clock, with the sun well above the horizon. . . I flew at 8,000 feet most of the way, bucking head winds of probably thirty miles an hour. . . The coast of Venezuela in the hazy distance was my first glimpse of South America. As we drew near I saw densely wooded mountains and between them wide valleys of open plains and jungle. I had never seen a jungle before. . .  close-knit tropic jungles are in a pilot’s eyes about the least desirable of all possible landing places. . . A muddy river wound through the mountain pass we followed, a reddish-brown snake crawling among tight-packed greenery. A few miles inland lay the red-roofed town of Caripito, with squat oil tanks on the outskirts. There was a splendid airfield, with paved runways and a well-equipped hangar. It is managed jointly by Pan American Airways and the Standard Oil Company.

—Amelia Earhart

Amelia Earhart is greeted on her arrival at Caripito, Venezuela, 2 June 1937.
Great Circle route from Isla Grande Airport, San Juan, Puerto Rico, to Maturin, Venezuela, location of the closest existing airport to Caripito. 548 nautical miles (630 statute miles/1,014 kilometers). (Great Circle Mapper)

© 2019, Bryan R. Swopes

1 June 1978

A Republic F-105F Thunderchief (foreground) and nine F-105Ds of the U.S. Air Force Reserve 465th Tactical Fighter Squadron, 507th Tactical Fighter Group (later 301st TFW), on the flight line at Tinker Air Force Base, Oklahoma (USA), on 1 June 1978. (Camera Operator: Rick Diaz - U.S. Defense Visual Information Center photo DF-ST-86-12883)
Ten Republic F-105 Thunderchiefs (eight F-105Ds and two, two-place F-105Fs) of the U.S. Air Force Reserve 465th Tactical Fighter Squadron, 507th Tactical Fighter Group (later 301st TFW), on the flight line at Tinker Air Force Base, Oklahoma (USA), on 1 June 1978. (Camera Operator: Rick Diaz – U.S. Defense Visual Information Center photo DF-ST-86-12883)

31 May–1 June 1967

Left to Right: Major Herbert Zehnder, USAF; Igor Sikorsky; Major Donald B. Murras, USAF, at Le Bourget, 1 June 1967.
Major Herbert R. Zehnder, USAF; Igor Sikorsky; Major Donald B. Murras, USAF, at le Bourget, 1 June 1967. (Sikorsky Historical Archives)

At 0105 hours, 31 May 1967, two Sikorsky HH-3E Jolly Green Giant helicopters, 66-13280 and 66-13281, from the 48th Aerospace Rescue and Recovery Squadron, United States Air Force, took off from Floyd Bennett Field, New York, and flew non-stop across the Atlantic Ocean to the Paris Air Show. They arrived at Le Bourget at 1351 hours, 1 June.

“H-211,” one of two 48th ARRS Sikorsky HH-3E Jolly Green Giant helicopters, lands at Le Bourget after a non-stop trans Atlantic flight, 1 June 1967. (Sikorsky Historical Archives)

The flight covered 4,271 miles (6873.5 kilometers) and took 30 hours, 46 minutes. Nine in-flight refuelings were required from Lockheed HC-130P Combat King tankers. The aircraft commanders were Major Herbert Zehnder and Major Donald B. Murras. Each helicopter had a crew of five.

Flight crews of the two 48th ARRS Sikorsky HH-3E Jolly Green Giant helicoptersat Le Bourget after a non-stop trans Atlantic flight, 1 June 1967. Major Zehnder is in the back row, at left.

Major Zehnder, in H-211, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Recognized Course for helicopters, with an average speed of 189.95 kilometers per hour (118.03 miles per hour). This record still stands.¹

The route of the two 48th ARRS Sikorsky HH-3E Jolly Green Giant helicopters from New York to Paris. (Sikorsky Archives News, July 2017)
Lieutenant Colonel Travis Wofford, United States Air Force.
Lieutenant Colonel Travis Wofford, United States Air Force.

Both Jolly Green Giants, serial numbers 66-13280 and 66-13281, were later assigned to the 37th Air Rescue and Recovery Squadron. Both were lost in combat during the Vietnam War.

66-13280, “Jolly Green 27” crashed at Kontum, Republic of South Vietnam, 15 April 1970. The pilot, Captain Travis H. Scott, Jr., was killed, and flight engineer Gerald E. Hartzel later died of wounds. The co-pilot, Major Travis Wofford, was awarded the Air Force Cross and the Cheney Medal for his rescue of the crewmembers from the burning helicopter. Captain Scott was posthumously awarded the Air Force Cross.

66-13281, “Jolly Green 28,” was shot down over Laos, 24 October 1969. The crew was rescued and the helicopter destroyed to prevent capture. The pararescueman, Technical Sergeant Donald G. Smith, was awarded the  Air Force Cross for the rescue of the pilot of “Misty 11.” He was also awarded the Airman’s Medal.

Master Sergeant Donald G. Smith, United States Air Force.
Master Sergeant Donald G. Smith, United States Air Force.

Major Herbert Zehnder flew another Sikorsky HH-3E, 65-12785, to intentionally crash land inside the Sơn Tây Prison Camp, 23 miles (37 kilometers) west of Hanoi, North Vietnam. He was awarded the Silver Star.

The SH-3A Sea King (Sikorsky S-61) first flew 11 March 1959, designed as an anti-submarine helicopter for the U.S. Navy. The prototype was designated XHSS-2 Sea King. In 1962, the HSS-2 was redesignated SH-3A Sea King. Many early production aircraft were upgraded through SH-3D, SH-3G, etc. In addition to the original ASW role, the Sea Kings have been widely used for Combat Search and Rescue operations. Marine One, the call sign for the helicopters assigned to the President of the United States, are VH-3D Sea Kings.

A Sikorsky HH-3E Jolly Green Giant (66-13290) of the 37th Air Rescue and Recovery Squadron, hovering in ground effect at Da Nang, Republic of South Vietnam, 1968. (U.S. Air Force)

The Sikorsky HH-3E (Sikorsky S-61R) earned the nickname Jolly Green Giant during the Vietnam War. It is a dedicated Combat Search and Rescue (CSAR) helicopter flown by the U.S. Air Force, based on the CH-3C transport helicopter. The aircraft is flown by two pilots and the crew includes a flight mechanic and gunner. It is a large twin-engine helicopter with a single main rotor/tail rotor configuration. It has retractable tricycle landing gear and a rear cargo ramp. The rear landing gear retracts into a stub wing on the aft fuselage. The helicopter has an extendable inflight refueling boom.

The HH-3E is 72 feet, 7 inches (22.123 meters) long and 18 feet, 10 inches (5.740 meters) high with all rotors turning. The main rotor has five blades and a diameter of 62 feet (18.898 meters). Each blade has a chord of 1 foot, 6.25 inches (0.464 meters). The main rotor turns at 203 r.p.m., counter-clockwise, as seen from above. (The advancing blade is on the right.) The tail rotor also has five blades and has a diameter of 10 feet, 4 inches (3.150 meters). The blades have a chord of 7–11/32 inches (0.187 meters). The tail rotor turns clockwise as seen from the helicopter’s left. (The advancing blade is below the axis of rotation.) The tail rotor turns 1,244 r.p.m.

A Sikorsky HH-3E Jolly Green Giant refuels in flight from a Lockheed HC-130 Combat King. (U.S. Air Force)
A Sikorsky HH-3E Jolly Green Giant refuels in flight from a Lockheed HC-130 Combat King. (U.S. Air Force)

The HH-3E has an empty weight of 13,341 pounds (6,051 kilograms). The maximum gross weight is 22,050 pounds (10,002 kilograms).

The Jolly Green Giant is powered by two General Electric T58-GE-5 turboshaft engines, which have a Maximum Continuous Power rating of 1,400 shaft horsepower, each, and Military Power rating of 1,500 shaft horsepower. The main transmission is rated for 2,500 horsepower, maximum.

The HH-3E has a cruise speed of 154 miles per hour (248 kilometers per hour) at Sea Level, and a maximum speed of 177 miles per hour (285 kilometers per hour), also at Sea Level. The service ceiling is 14,000 feet (4,267 meters). The HH-3E had a maximum range of 779 miles (1,254 kilometers) with external fuel tanks.

The Jolly Green Giant can be armed with two M60 7.62 mm machine guns.

Sikorsky built 14 HH-3Es. Many CH-3Cs and CH-3Es were upgraded to the HH-3E configuration. Sikorsky built a total of 173 of the S-61R series.

Sikorsky HH-3E Jolly Green Giant 67-14709 at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)
Sikorsky HH-3E Jolly Green Giant 67-14709 at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)

¹ FAI Record File Number 2092

© 2017, Bryan R. Swopes

1 June 1964

Jackie Cochran and Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)
Jackie Cochran and Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)

1 June 1964: At Edwards Air Force Base, in the high Mojave Desert of southern California, Jackie Cochran flew a Lockheed F-104G Starfighter, serial number 62-12222, over a 100 kilometer (62.137 miles) closed circuit without payload, averaging 2,097.27 kilometers per hour (1,303.18 miles per hour).¹ This new Fédération Aéronautique Internationale (FAI) speed record broke the one set a year earlier—2,038.70 kilometers per hour (1,266.79 miles per hour)—by Cochran’s friend and competitor, Jacqueline Auriol, who flew a Dassault Mirage IIIR delta-winged reconnaissance fighter at Istres, France. ²

Jackie Cochran taxiing Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)
Jackie Cochran taxiing Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)

Designed by the legendary Kelly Johnson as a Mach 2 interceptor, the Starfighter was used as a fighter bomber by Germany. The F-104G was most-produced version of the Lockheed Starfighter. It had a strengthened fuselage and wings, with hardpoints for carrying bombs, missiles and additional fuel tanks. Built by Lockheed, they were also licensed for production by Canadair, Dornier, Fiat, Fokker, Messerschmitt and SABCA.

The F-104G is a single-seat, single-engine fighter bomber, 54 feet 8 inches (16.662 meters) long with a wingspan of just 21 feet, 9 inches (6.629 meters) and overall height of 13 feet, 6 inches (4.115 meters). The empty weight is 14,000 pounds (6,350.3 kilograms) and loaded weight is 20,640 pounds (9,362.2 kilograms).

The F-104G was powered by a General Electric J79-GE-11A engine, a single-spool, axial-flow, afterburning turbojet, which used a 17-stage compressor section and 3-stage turbine. The J79-GE-11A is rated at 10,000 pounds of thrust (44.48 kilonewtons), and 15,800 pounds (70.28 kilonewtons) with afterburner. The engine is 17 feet, 4.0 inches (5.283 meters) long, 3 feet, 2.3 inches (0.973 meters) in diameter, and weighed 3,560 pounds (1,615 kilograms).

The maximum speed is 1,328 miles per hour (2,137.2 kilometers per hour). It has a combat radius of 420 miles (675.9 kilometers) or a ferry range of 1,630 miles (2,623.2 kilometers). The service ceiling is 50,000 feet (15,240 meters).

The Starfighter’s standard armament consists of a 20 mm General Electric M61A1 Vulcan 6-barreled Gatling gun, with 725 rounds of ammunition, and up to four AIM-9 Sidewinder air-to-air heat seeking missiles could be carried on the wingtips or under wing pylons. In place of missiles two wingtip fuel tanks and another two underwing tanks could be carried.

On NATO alert, the F-104G was armed with a B43 variable-yield nuclear bomb on the fuselage centerline hardpoint. The B43 could be set for explosive force between 170 kilotons and 1 megaton and was designed for high-speed, low-altitude, laydown delivery.

Jackie Cochran set three speed records with this F-104 in May and June 1964.³ Under the Military Assistance Program, the U.S. Air Force transferred it to the Republic of China Air Force, where it was assigned number 4322. It crashed 17 July 1981. The pilot, Yan Shau-kuen, ejected.

The record-setting Lockheed F-104G Starfighter, USAF serial number 62-12222, in service with the Republic of China Air Force as 4322.
The record-setting Lockheed F-104G Starfighter, USAF serial number 62-12222, in service with the Republic of China Air Force as 4322. (Detail from image International F-104 Society)

¹ FAI Record File Number 12389

² FAI Record File Number 12392

³ FAI Record File Numbers 12389, 13037, 13041

© 2019, Bryan R. Swopes