A North American Aviation B-25B Mitchell medium bomber revs its engines, awaiting the signal to launch from the flight deck officer. (U.S. Navy)With flight deck personnel dropping to the deck to avoid its turning propellers, a North American B-25B Mitchell medium bomber starts its takeoff roll aboard USS Hornet (CV-8), 18 April 1942. (U.S. Navy)Fleet Admiral William F. Halsey, United States Navy
18 April 1942: Task Force 16, under the command of Vice Admiral William F. Halsey, Jr., U.S. Navy, approached the Japanese islands on a daring top secret joint Army-Navy attack.
Planning for the attack began in January 1942 under orders from Admiral Earnest J. King, Commander-in-Chief United States Fleet. Captain Donald B. Duncan, U.S. Navy, was responsible for the plan.
The operation was carried out by Task Force 16 under the command of Vice Admiral William F. Halsey, Jr., United States Navy. Task Force 16 consisted of two aircraft carriers, USS Enterprise (CV-6) and USS Hornet (CV-8), four cruisers, eight destroyers and two oilers. There were two air groups, consisting of eight squadrons of 54 fighters, 72 dive bombers, 36 torpedo bombers, and one squadron of of 16 medium bombers. Lieutenant Colonel James Harold (“Jimmy”) Doolittle, U.S. Army Air Corps, commanded the Strike Group of North American Aviation B-25 Mitchell bombers aboard Hornet.
With the land-based Army bombers secured to Hornet‘s flight deck, her own fighters had been struck below. The air group from Enterprise provided Combat Air Patrol for the task force. The plan was to bring the B-25s within 400 miles (645 kilometers) of Japan, have them take off and carry out the attack, then fly on to airfields in Chinese territory.
A U.S. Army Air Corps B-25B Mitchell medium bomber is launched from USS Hornet (CV-8), 18 April 1942. (U.S. Navy)Lieutenant Colonel James H. (“Jimmy”) Doolittle, U.S. Army Air Corps, flies a North American Aviation B-25B Mitchell medium bomber off the deck of USS Hornet (CV-8), 18 April 1942. His was the first bomber to takeoff. (U.S. Navy)
At 0500 hours, the task force was sighted by a Japanese picket boat while still over 700 miles (1,127 kilometers) away from Tokyo. At 0644 another vessel was spotted by the task force. Fearing that surprise had been lost, Admiral Halsey ordered the bombers launched while still 623 miles (1,003 kilometers) from land.
A North American Aviation B-25B Mitchell medium bomber takes off from USS Hornet (CV-8). The airplane’s nose wheel has lifted clear of the flight deck while the ship’s bow pitches down in heavy seas. (U.S. Navy)Lt. Col. James H. Doolittle, USAAC, aboard USS Hornet, April 1942. (U. S. Air Force)
The sixteen B-25s were successfully launched from Hornet and headed for their assigned targets. The lead airplane, B-25B serial number 40-2344, was flown by Lieutenant Colonel Doolittle.
Single B-25s attacked targets in the cities of Tokyo, Nagoya, Osaka and Kobe.The first bombs were dropped on Tokyo at 1215 local time. This was the first offensive operation carried out by the United States of American against the Empire of Japan during World War II.
The actual destructive effect of the attack was minimal. It had been hoped that there would be psychological effects on the citizenry, however the arrival of the American bombers coincided with an ongoing air raid drill, and many thought it was all part of the drill.
Militarily, however, the attack was a stunning success. Four Japanese fighter groups, needed elsewhere, were pinned down at home, waiting for the next attack.
A B-25 is airborne over the bow of USS Hornet (CV-8). (U.S. Navy)
Not a single B-25 was lost over Japan. One landed in Vladivostok where the crew and airplane were interred by the “neutral” Soviets, but they eventually were able to get home. The rest continued on toward China, though without enough fuel to reach their planned destinations. Four B-25s made crash landings, but the crews of the others bailed out into darkness as their planes ran out of gas.
Routes of ten of the sixteen B-25s. Lieutenant Colonel Doolittle’s airplane, 40-2344, enters the chart at the upper right corner, the exits to upper left. (United States Army)Yokosuka Naval Base photographed from an American B-25 bomber, 18 April 1942. (National Archives and Records Administration, 342-FH-#A-3028-9302)The wreckage of Jimmy Doolittle’s North American Aviation B-25B Mitchell bomber, 40-2344, China, April 1942. (Smithsonian.com)Lieutenant Colonel James Harold Doolittle (just right of center) with his crew in China following the 18 April 1942 air raid on Japan. Left to right, Staff Sergeant Fred A. Braemer; Staff Sergeant Paul J. Leonard; Lieutenant Richard E. Cole; Lieutenant Colonel Doolittle; and Lieutenant Henry A. Potter. (United States Navy, Naval History and Heritage Command NH 97502)
Five of the airmen were killed. Eight were captured by the Japanese, two of whom were executed by a military court, and another died in prison.
Captain Edward J. York’s North American Aviation B-25B Mitchell, 40-2242, Aircraft 8, interned about 40 miles (25 miles) west of Vladivostok, Primorsky Krai, Union of Soviet Socialist Republics.1st Lieutenant Robert L. Hite, USAAC, co-pilot of Aircraft 16, “Bat Out of Hell,” was captured by the Japanese after bailing out over China, and was held as a prisoner of war for 3½ years. (U.S. Air Force)
For his leadership in the air raid, James Harold Doolittle was promoted to the rank of Brigadier General, and was awarded the Medal of Honor by President Franklin D. Roosevelt. General Doolittle’s Medal is in the collection of the National Air and Space Museum.
President Franklin D. Roosevelt presents the Medal of Honor to Brigadier General James Harold Doolittle in a ceremony at The White House, 19 May 1942. The President is seated at left. Standing, left to right, are Lieutenant General Henry H. Arnold, Chief of the Army Air Forces; Mrs. Doolittle; Brigadier General Doolittle; and General George Catlett Marshall, Jr., Chief of Staff, United States Army. (Franklin D. Roosevelt Library and Museum, Photographic Collection, NPx. 65-696)
CITATION:
The President of the United States of America, in the name of Congress, takes pleasure in presenting the Medal of Honor to Brigadier General [then Lieutenant Colonel] James Harold Doolittle (ASN: 0-271855), United States Army Air Forces, for conspicuous leadership above the call of duty, involving personal valor and intrepidity at an extreme hazard to life while Commanding the First Special Aviation Project in a bombing raid of Tokyo, Japan, on 18 April 1942. With the apparent certainty of being forced to land in enemy territory or to perish at sea, General Doolittle personally led a squadron of Army bombers, manned by volunteer crews, in a highly destructive raid on the Japanese mainland.
War Department, General Orders No. 29 (June 9, 1942), Amended by Department of the Army G.O. No. 22 (1959) & No. 4 (1960)
The Medal of Honor awarded to Brigadier General James Harold Doolittle, Air Corps, United States Army, in the collection of the Smithsonian Institution National Air and Space Museum, (NASM A19600049000)
Omega Speedmaster Professional Chronograph worn by Jack Swigert during the Apollo 13 mission.
17 April 1970: Because of the unusual configuration of the Apollo 13 Command Module, Service Module and Lunar Module “stack” during the coast from the Moon back to Earth, an additional, unplanned, Mid-Course Correction burn, MCC-7, had to be carried out. The damage to the Service Module prevented the use of its 21,900 pounds thrust (97.42 kilonewtons) Aerojet General Service Propulsion System engine. It was necessary to use the LM’s Space Technology Laboratories (TRW) VTR-10 Descent Propulsion System engine. The DPS engine produced 10,500 pounds of thrust (46.71 kilonewtons). The maneuver had to be carried out manually by the astronauts from the LM’s cockpit.
Mission Commander Lovell visually aligned the spacecraft with the LM’s Reaction Control System thrusters, by sighting the Earth in his window of the LM. Once aligned, LM pilot Fred Haise conducted the burn, which was timed by CM pilot Jack Swigert.
Swigert timed the burn using his NASA-issued Omega Speedmaster Professional Chronograph, a very accurate manual wristwatch.
The Mid Course Correction ignition commenced at T+137:39:51.5 and the engine was cutoff at T+137:40:13.0 (12:52:51–12:53.13 UTC), for a duration of 21.5 seconds.
MCC-7 was performed at EI-5 hours (137:39 GET). The same manual piloting technique used for MCC-5 was used for control during MCC-7. This was manual crew pitch and roll control with the TTCA and automatic yaw control by the AGS. MCC-7 was performed with LM RCS using the +X translation push button. It steepened the flight path angle at EI to -6.49 degrees. After MCC-7, the crew maneuvered the spacecraft to the SM separation attitude. The CM re-entry RCS system was activated and a firing test of the thrusters was successful.
—“Apollo 13 Guidance, Navigation, and Control Challenges” by John L. Goodman, United Space Alliance. American Institute of Astronautics AIAA 2009-6455 at Page 23.
Omega Speedmaster Professional “Moon Watch.” (Omega)
The Omega Speedmaster Professional Chronograph is a manual-winding analog wrist watch produced by Omega, a luxury brand of Société Suisse pour l’Industrie Horlogère, (SSIH) and now a part of the SWATCH Group. The case is made of stainless steel and has a diameter of 48 millimeters (1.89 inches). The Speedmaster Professional, which is also known as the “Moon Watch,” or “Speedy” to watch collectors, features a stop watch function and three sub dials for recording hours, minutes and seconds. The chronograph has a black dial with tritium-painted hands and hour marks. The bezel has a tachymeter for calculating speed based on time. When fully wound, the Speedmaster can run for up to 48 hours. The chronograph is water resistant to a depth of 50 meters (164 feet).
The Speedmaster’s crystal is not glass, but “hesalite,” a clear, scratch-resistant plastic. There had been concern that if a crystal broke during a space flight, glass fragments could be scattered throughout the weightless environment of the spacecraft, presenting a danger to the astronauts.
Description of the Omega Speedmaster Professional Chronograph in a NASA Manual. (NASA)
NASA provided Omega Speedmaster Professional Chronographs to Gemini and Apollo Program astronauts. Each watch was engraved with NASA’s two-digit serial number, and could be equipped with an adjustable length Velcro strap which allowed the watch to be worn on the outside of the space suit. NASA also assigned an equipment part number.
Jack Swigert’s watch, p/n SEB12100039-002, was NASA’s number 69. It is in the collection of the Smithsonian Institution National Air and Space Museum, as Catalog Number 1977-1181.000. In 2016, the watch was on display at the University of Colorado.
Astronaut Jack Swigert prepares to board the Apollo 13 Command Module. He is wearing his Omega Speedmaster Professional Chronograph on his left arm. NASA space suit technician Clyde Teague is at left. (NASA)
Geraldine Fredritz Mock with her Cessna 180, N1538C, at Columbus, Ohio, 19 March 1964. (National Air and Space Museum, Smithsonian Institution)
19 March–17 April 1964: Geraldine Fredritz (“Jerrie”) Mock landed her 1953 Cessna 180, Spirit of Columbus, N1538C, at Columbus, Ohio, completing a circumnavigation of the Earth she had begun at 9:31 a.m., 19 March 1964. Mock was the first woman to complete a circumnavigation by air.¹ Her journey covered 23,103 miles (36,964 kilometers). The total elapsed time was 29 days, 11 hours, 59 minutes. The flight set a Fédération Aéronautique Internationale (FAI) World Record for Speed Around the World, Eastbound, of 52.75 kilometers per hour (32.78 miles per hour).²
Geraldine Mock’s route of flight. (Smithsonian Institution National Air and Space Museum, NASM-9A11714)
Jerrie Mock held twenty-two FAI world records, set between 1964 and 1969.
Jerrie Mock in the cockpit of her Cessna 180.
Cessna 180 serial number 30238 was built by the Cessna Aircraft Company, Inc., Wichita, Kansas, in 1953, and registered N1538C, the first year of production for the model. It was the 238th of 640 Model 180s that were built during the first year of production. 6,193 were built by the time production came to an end in 1986. N1538C was purchased for Jerrie Mock in 1963, with a total of 990 hours on the engine and airframe. The passenger seats were removed and replaced with additional fuel tanks. Additional radios and instruments were installed.
The prototype Cessna 180, N41697. (Ed Coates Collection)
The Cessna Model 180 is an all-metal, four-place, single-engine, high-wing monoplane with fixed landing gear. It is 25 feet, 6 inches (7.772 meters) long with a wingspan of 36 feet, 2 inches (11.024 meters) and height of 7 feet, 6 inches (2.286 meters). If the optional rotating beacon is installed, the height is increased to 7 feet, 9 inches (2.362 meters). The Cessna 180 has an approximate empty weight of 1,525 pounds (692 kilograms), depending on installed equipment, and the maximum gross weight is 2,800 pounds (1,270 kilograms).
Cessna 180 three-view illustration with dimensions. (Cessna)
Spirit of Columbus is powered by an air-cooled, normally-aspirated 471.239-cubic-inch-displacement (7.722 liter) Continental O-470-A horizontally-opposed six-cylinder overhead valve (OHV) direct-drive engine with a compression ratio of 7:1. This engine is rated at 225 horsepower at 2,600 r.p.m., burning 80/87 aviation gasoline, and turns a two-bladed constant speed propellerwith a diameter of 6 feet, 10 inches (2.083 meters).
The airplane has a cruise speed of 162 miles per hour (261 kilometers per hour) at 6,500 feet (1,981 meters), and its maximum speed is 170 miles per hour (274 kilometers per hour) at Sea Level. Its service ceiling is 19,600 feet (5,974 meters). The Cessna 180 has a maximum fuel capacity of 84 gallons (318 liters), giving it an optimum range of 1,215 miles (1,955 kilometers) at 10,000 feet (3,048 meters) and 121 miles per hour (195 kilometers per hour).
An early production Cessna 180, N2824A. (Cessna)
After her around the world flight, Jerrie Mock never flew Spirit of Columbus again. Cessna exchanged it for a new six-place P206 Super Skylane, N155JM. For many years N1538C was hanging over a production line at the Cessna factory. Today, Mock’s Cessna 180 is on display at the Steven F. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum.
Jerrie Mock with her Cessna P206, N155JM. (FAI)
On 4 May 1964, President Lyndon B. Johnson presented Jerrie Mock with the Federal Aviation Agency Gold Medal for Distinguished Service, and the Fédération Aéronautique Internationale awarded her its Louis Blériot Silver Medal.
President Lyndon Johnson bestows the FAA Gold Medal for Distinguished Service on Geraldine Mock, 4 May 1964. (UPI)
Geraldine Lois Fredritz was born 22 November 1925 at Newark, Ohio. She was the first of three daughters of Timothy J. Fredritz, a clerk for a power company, and Blanche M. Wright Fredritz. Jerrie Fredritz graduated from Newark High School in 1943, then studied aeronautical engineering at Ohio State University, Columbus, Ohio. She was a member of the Phi Mu (ΦΜ) sorority.
Miss Fredritz married Russell Charles Mock, 21 March 1945, in Cook County, Illinois. They would have three children, Valerie, Roger and Gary.
Jerrie Mock wrote about her around-the-world flight in Three Eight Charlie, published by Lippincott, Philadelphia, Pennsylvania, 1970.
Geraldine Fredritz Mock died at Qunicy, Florida, Monday, 30 September 2014, at the age of 88 years. She had requested that her ashes be spread over the Gulf of Mexico.
1953 Cessna 180, N1538C, Spirit of Columbus, on display at the Steven F. Udvar-Hazy Center. (National Air and Space Museum, Smithsonian Institution)
¹ The international organization for flight records, the Fédération Aéronautique Internationale, requires that a circumnavigation cross all meridians in one direction and be at least the length of the Tropic of Cancer, 22,858.729 miles (36,787.559 kilometers).
The first Lockheed F-104A Starfighter, 55-2956, is towed out of its hangar at Air Force Plant 42, Palmdale, California, 17 April 1956. (Lockheed Martin)
17 April 1956: Lockheed Aircraft Corporation rolled out the very first production F-104A Starfighter, 55-2956, at Air Force Plant 42, Palmdale, California. This airplane, one of the original seventeen pre-production YF-104As, incorporated many improvements over the XF-104 prototype, the most visible being a longer fuselage.
Once the configuration was finalized, 55-2956 was the first YF-104A converted to the F-104A production standard. In this photograph, the F-104’s secret engine intakes are covered by false fairings.
Lockheed F-104A Starfighter 55-2956 rollout at Palmdale, 17 April 1956. (Lockheed Martin)
The Lockheed F-104A Starfighter was a single-place, single-engine supersonic interceptor. It was designed by a team lead by the legendary Clarence L. “Kelly” Johnson. The F-104A was 54 feet, 8 inches (16.662 meters) long with a wingspan of 21 feet, 9 inches (6.629 meters) and overall height of 13 feet, 5 inches (4.089 meters). It had an empty weight of 13,184 pounds (5,980.2 kilograms), combat weight of 17,988 pounds (8,159.2 kilograms), gross weight of 22,614 pounds (10,257.5 kilograms) and a maximum takeoff weight of 25,840 pounds (11,720.8 kilograms). Internal fuel capacity was 897 gallons (3,395.5 liters).
The F-104A was powered by a single General Electric J79-GE-3A engine, a single-spool axial-flow afterburning turbojet, which used a 17-stage compressor and 3-stage turbine. The J79-GE-3A is rated at 9,600 pounds of thrust (42.70 kilonewtons), and 15,000 pounds (66.72 kilonewtons) with afterburner. The engine is 17 feet, 3.5 inches (5.271 meters) long, 3 feet, 2.3 inches (0.973 meters) in diameter, and weighs 3,325 pounds (1,508 kilograms).
The F-104A had a maximum speed of 1,037 miles per hour (1,669 kilometers per hour) at 50,000 feet (15,240 meters). Its stall speed was 198 miles per hour (319 kilometers per hour). The Starfighter’s initial rate of climb was 60,395 feet per minute (306.8 meters per second) and its service ceiling was 64,795 feet (19,750 meters).
Lockheed F-104A-5-LO Starfighter 56-737 launches two AIM-9B Sidewinder infrared-homing air-to-air missiles. (U.S. Air Force)
Armament was one General Electric M61 Vulcan six-barreled revolving cannon with 725 rounds of 20 mm ammunition. An AIM-9B Sidewinder heat-seeking air-to-air missile could be carried on each wing tip, or a jettisonable fuel tank with a capacity of 141.5 gallons (535.6 liters).
Lockheed built 153 of the F-104A Starfighter initial production version. A total of 2,578 F-104s of all variants were produced by Lockheed and its licensees, Canadair, Fiat, Fokker, MBB, Messerschmitt, Mitsubishi and SABCA. By 1969, the F-104A had been retired from service. The last Starfighter, an Aeritalia-built F-104S ASA/M of the Aeronautica Militare Italiana, was retired in October 2004.
Lockheed JF-104A Starfighter 55-2956 at NOTS China Lake. (U.S. Navy)
This Starfighter, 55-2956, was converted to a JF-104A with specialized instrumentation. It was transferred to the U.S. Navy to test AIM-9 Sidewinder missiles at Naval Ordnance Test Station (NOTS) China Lake, approximately 55 miles (88 kilometers) north-northeast of Edwards Air Force Base in the high desert of Southern California. 55-2956 was damaged beyond repair when it lost power on takeoff and ran off the runway at Armitage Field, 15 June 1959.
While on loan to the U.S. Navy for testing the AIM-9 Sidewinder missile, Lockheed JF-104A Starfighter 55-2956, with Commander Herk Camp in the cockpit, crashed on takeoff at Armitage Field, NOTS China Lake. (U.S. Navy)
Lockheed C-69 Constellation. (Lockheed Martin Aeronautics Company)
17 April 1944: The first production Lockheed C-69 Constellation, 43-10310, was delivered to the Air Transport Command at National Airport, Arlington, Virginia. The new transport carried the markings of Transcontinental and Western Airlines (T.W.A.), and was flown by that company’s owner, Howard Robard Hughes, Jr., and T.W.A.’s president, William John (“Jack”) Frye.
Lockheed C-69 Constellation 43-10310 ready to depart Lockheed Air Terminal, 17 April 1944. (Image scanned from Queen of the Skies, by Claude G. Luisada. Schiffer Publishing Ltd., Atglen, Pennsylvania, 2014. Chapter 5, Page 76, Fig. 5–1.)
The C-69 departed Lockheed Air Terminal, Burbank, California, at 3:56:45 a.m., Pacific War Time. The other crew members were Edward T. Bolton, Navigator; R. L. Proctor, Flight Engineer; and Charles L. Glover, Radio Operator. Also on board were 12 passengers representing the Air Corps, T.W.A. and Lockheed.¹
The Dayton Herald reported:
Constellation Sets Record; To Be in Dayton Thursday
(BULLETIN)
WASHINGTON, April 17.—(UP)—The giant transport Constellation landed at Washington National Airport at 1:59 p.m. EWT today, setting a new trans-continental airplane speed record.
The huge four-motor transport made the crossing from Burbank, Calif., in approximately 7 hours and three minutes on the basis of unofficial timing. Howard Hughes, who set the previous record, piloted the plane here for delivery to the Army.
The Constellation, Transcontinental and Western Airline’s (TWA) super transport, which left Burbank, Calif., today for delivery to the air transport command at Washington, will fly to Wright Field Thursday afternoon, Material Command officials said here.
Considered the largest land-based cargo plane in the country, the “Constellation” took off from Lockheed Air Terminal at 5:56 a.m., (Dayton time) today with veteran pilot Howard Hughes and Jack Frye, TWA president, co-designers of the plane, as pilot and co-pilot, respectively. It passed over Butler Mo., 50 miles south of Kansas City, at 10:20 a.m. (Dayton time).
Materiel Command officials said the plane was expected to make the trip in nine hours. They estimated she could fly from Los Angeles, Calif., to Honolulu in 12 hours.
Also aboard were Lt. Col. Clarence Shoop, resident Material Command inspector at the Lockheed Burbank plant, 17 Lockheed and TWA technical experts and a civilian air expert.
The ship originally was designed to carry 57 passengers, TWA officials said. The airline company commissioned Lockheed to build the plane two years ago.
Hughes described the trip as a “routine delivery mission” and would not say whether he would attempt to break any speed records or whether the flight would be non-stop.
“It all depends on the performance of the Connie,” he said.
The 40-ton ship, which has a cruising speed of 300 miles an hour, took off with enough gasoline for a non-stop trip. Cargo and airline planes in general use now cruise at around 180 miles an hour. Her takeoff was clocked by Larry Therkelsen, National Aeronautical Association timekeeper and official timer of the national air races before the war.
The Constellation is powered by four, 2,000-horsepower Wright air-cooled, radial engines, with 18 cylinders each, the Materiel Command said. It has three-bladed Hamilton Standard propellers and is equipped with a pressurized cabin for stratosphere flights. Its service ceiling is from 20,000 to 35,000 feet.
—The Dayton Herald, Vol. 65, No. 91, Monday, 17 April 1944, Page 1, Columns 5 and 6
Lockheed C-69-LO Constellation 43-10310, c/n 049-1962, was the first production airplane. It had been flown to Las Vegas, Nevada, on the previous day, where T.W.A. personnel applied the company’s livery to the Army Air Corps-owned airplane. Flown by Lieutenant Colonel C. A. Shoup, it then returned to Burbank to prepare for the transcontinental flight.
Lockheed C-69-LO Constellation 43-10310, the first production airplane. (Lockheed Martin Aeronautics Company)
The plan called for Howard Hughes to fly as pilot-in-command for the first half of the flight, with Captain Frye in the right seat. They would switch positions at the half-way point. Both men were experienced four-engine pilots but the Constellation was new to them. In the previous week, they had each made two training flights in the C-69, with Hughes flying 2.9 hours and Frye, 3.4.
Lockheed C-69 Constellation 43-10310 (c/n 1962), the first production airplane. (Lockheed Martin Aeronautics Company via Burbank in focus pub00013)
Initially, the transport followed T.W.A.’s normal transcontinental route. It had climbed to 15,000 feet (4,572 meters) by the time it reached Kingman, Arizona. The night sky was “CAVU”—ceiling and visibility unrestricted—and there was a bright last-quarter moon shining. Passing north of Winslow, Arizona, the C-69 left the T.W.A. route and turned north to pick up a Great Circle course.
Flying over northern New Mexico, they encountered turbulence and thunderclouds. Hughes climbed to 17,500 feet (5,334 meters) to remain clear of the clouds. Light ice began forming on the airplane as they crossed over Kansas. They climbed into colder, drier air at 18,500 feet (5,639 meters).
Lockheed C-69 Constellation 43-10310 (c/n 1962). (Lockheed Martin Aeronautics Company via Burbank in focus pub00019)
Over the eastern part of the state, Jack Frye took over as pilot command and he and Hughes switched places in the cockpit. The C-69 crossed over Butler, Missouri, 50 miles (80 kilometers) south of Kansas City, at 10:20 a.m., Central War Time (8:20 a.m., P.W.T.).
—ST. LOUIS STAR-TIMES, Vol. 58—No. 168, Monday Evening, 17 April 1944, Page 1, Columns 5 and 6
The Constellation crossed overhead Cincinnati, Ohio, at 11:48 a.m., C.W.T. Stormy weather delayed their descent until after crossing the Ohio River.
The Constellation flew overhead National Airport at 1:54 p.m., Eastern War Time (10:54 a.m., P.W.T.). They circled overhead while traffic cleared the runway, then landed four minutes later.
The Lockheed C-69 Constellation, 43-10310, flown by Howard Hughes and Jack Frye, lands at National Airport, Arlington, Virginia, at 1:58 p.m., E.W.T., 17 April 1944. Image edited. (Original image: UNLV Digital Collection whh 001297).
The C-69’s log book showed the Burbank to overhead National Airport flight as having taken 6 hours, 56 minutes, 15 seconds.² The Aircraft Yearbook for 1945 gives the record time as “6 hours, 57 minutes and 51 seconds.” ³
Because of wartime security concerns, the Air Corps would not allow Lockheed or TWA to release specific information about the flight, other than to say that it had broken the existing transcontinental speed record. The Great Circle distance from Lockheed Air Terminal to Washington National is 2,000 nautical miles (2,302 statute miles/3,705 kilometers). Assuming that the route was flown without any deviations, the average speed of the C-69 would have been 288 knots (331 miles per hour/533 kilometers per hour).
Lockheed C-69 Constellation 43-10310 taxis to parking at National Airport, 17 April 1944. (UNLV Digital Collections whh001301)Lockheed C-69 Constellation 43-10310 taxis to parking at National Airport, 17 April 1944. (UNLV Digital Collections whh001302)Lockheed C-69 Constellation 43-10310, wheels stop. National Airport, 17 April 1944. (LIFE Magazine)
At the time, the only airplanes which were larger than the C-69 were the prototype Douglas B-19 long range bomber and the Martin Mars flying boat. A large crowd watched the arrival of the new airplane. Dignitaries meeting the flight were General Henry H. (“Hap”) Arnold, Chief the U.S. Army Air Forces, and Secretary of Commerce Jesse H. Jones, with Oswald Ryan and Josh Lee of the Civil Aeronautics Board.
Secretary of Commerce Jesse Holman Jones, Howard Hughes and Jack Frye. “She performed perfectly marvelously,” said Frye. “She handled like a pursuit ship and flies like a dream.” (UNLV Digital Collections whh001313)Flight crew and passengers of transcontinental flight. Howard Hughes is 8th from left. (UNLV Digital Collection whh01324)Lockheed C-69 Constellation 43-10310 at National Airport, Arlington, Virginia, 17 April 1944. (UNLV Digital Collections whh001317)
After the arrival ceremonies, the new Lockheed C-69 Constellation was handed over to the Air Corps Air Transport Command and taken to Wright Field, Dayton, Ohio, to begin its military flight tests.
Lockheed C-69 Constellation 43-10310 after rollout at Lockheed Burbank, August 1943. (Lockheed Martin Aeronautics Company)
As stated above, 43-10310, c/n 1962, was the first production C-69 Constellation, following the XC-69 prototype, 43-10309, c/n 1961. It had been designed and built by the Lockheed Aircraft Corporation at Burbank, California, for Transcontinental and Western Airlines. The C-69 made its first flight in August 1943, and remained with Lockheed for manufacturer’s tests.
The Constellation was operated by a flight crew of five: two pilots, a navigator, flight engineer and radio operator. It could carry up to 81 passengers. The airplane was 95 feet, 1 3⁄16 inches (28.986 meters) long with a wingspan of 123 feet, 0 inches (37.490 meters), and overall height of 23 feet, 7⅞ inches (7.210 meters). It had an empty weight of 49,392 pounds (22,403.8 kilograms) and maximum takeoff weight of 86,250 pounds (39,122.3 kilograms).
Lockheed C-69 Constellation. (Lockheed Martin Aeronautics Company)
The C-69 was powered by four air-cooled, supercharged, 3,347.662-cubic-inch-displacement (54.858 liter), Wright Aeronautical Division R3500–35 (Cyclone 18 711C18BA2) engines. Also known as the Duplex Cyclone, these were a two-row, 18-cylinder radial engines with a compression ratio of 6.85:1, which required 100/130-octane aviation gasoline. They were rated at 2,000 horsepower at 2,400 r.p.m., and 2,200 horsepower at 2,800 r.p.m. for takeoff (five minute limit), The 745C18BA2 was 6 feet, 4.26 inches (1.937 meters) long, 4 feet, 7.78 inches (1.417 meters) in diameter and weighed 2,707 pounds (1,228 kilograms). The engines drove 15 foot, 2 inch (4.623 meter) diameter, three-bladed Hamilton Standard Hydromatic 43E60 constant-speed propellers through a 0.4375:1 gear reduction. Wright produced 58 of these engines between August 1942 and October 1944.
The C-69 had a cruise speed of 313 miles per hour (504 kilometers per hour) and a range of 3,995 miles (6,429 kilometers). Its service ceiling was 25,300 feet (7,711 meters).
During the War, Lockheed Constellations were operated for the War Department by T.W.A. and Pan American Airways.
On 31 March 1947, War Assets Administration sold 43-10310 for spare parts. It was salvaged to repair other C-69 and L-049 airplanes.
In 1952, Lockheed rebuilt -310 for Inter-National Airways, Inc., which leased it to Flying Tiger Line. It was assigned civil registration NC38936.
NC38936 was destroyed by fire after landing accident during training/certification flight at Burbank, 22 January 1953.
Lockheed Martin C-69-1-LO Constellation 43-10314. (Lockheed Martin)
The Los Angeles Times reported:
Fire Destroys Huge Plane on L.A. Test Hop
A rebuilt, four-engine Constellation was destroyed by fire last night seconds after it landed at Lockheed Air Terminal. Ten persons aboard the aircraft escaped without injury.
The huge craft, owned by Inter-Continental Airways, Inc., had made its second test landing for two Civil Aeronautics Authority inspectors when the main landing-gear section burst into flames which quickly spread to the fuselage and other parts of the ship, according to airport tower observers.
The plane’s landing gear apparently failed to function properly as the ship touched down and caused the plane to skid on its belly with the propellers scraping the runway, according to the observers.
Changes in Plane
The Constellation was the second in the C-69 series built by Lockheed Aircraft and during the last two years had undergone changes in construction prior to being chartered by Flying Tiger Lines from the Inter-Continental Airways, according to William Sosnow, purchasing agent for the latter company.
Burbank and Lockheed Fire Departments fought the fire and kept the flames from spreading to nearby hangars and other aircraft. Fire officials said the plane, valued at $1,000,000, was a total loss.
Final Checkout
Sosnow said the plane had received CAA partial approval Wednesday and that last night’s pilot training flight was to complete the inspection routine. It was to have flown to Oakland today for its first pay passengers, he said.
Aboard the plane, Lockheed officials said, were CAA Inspectors M.H. Griffith and Sam Chandler, Senior Pilot C.G. Fredericks, Pilots Lawrence Raab, Sheldon Eichel, August Martin and Leo Gardner; Flight Engineers Frank Lutomski and Robert R. Jackson and Radioman Morris H. Sherry.
All the crewmen were employed by Inter-Continental.
—Los Angeles Times, Vol. LXXI, Friday Morning, 23 January 1953, Part 1, Page 1, Column 3
The Bureau of Aircraft Accidents Archives, (BAAA, or B3A) data base states:
“The crew was engaged in a local test flight. On final approach, during the last segment, the crew inadvertently raised the gears. The four engine aircraft belly landed and slid for dozen yards before coming to rest in flames. While all five crew members were unhurt, the aircraft was lost.”
¹ LCOL Clarence A. Shoop USAAC. TWA: Lawrence J. Chiappino, Test Pilot; Leo Baron, Robert L. Loomis, pilot; Ed J. Minser, Chief Meteorologist; Orville R. Olson, chief clerk, Kansas City traffic department; Lee Spruill, Richard De Campo, Flight Engineer. Lockheed: Rudy L. Thoren, Chief Flight Test Engineer; Richard Stanton; Thomas Watkins. S.J. Solomon, Chairman, Airlines Committee for Aviation Policy
² TDiA checked with the National Aeronautic Association, which does not have any information about this flight.
³ The AIRCRAFT YEAR BOOK For 1945, Howard Mingos, Editor. Aeronautical Chamber of Commerce of America, Inc., Lanciar Publishers, Inc., New York. Chapter IV, Page 123.
