1 July 1933: 12:36 p.m., the Douglas DC-1 took off from Clover Field, Santa Monica, California, on its first flight. In the cockpit were Carl Anson Cover and Fred Herman.

The duration of the flight was just twelve12 minutes. during the flight both engines lost power several times. It was later determined that the engines’ carburetors had been installed backwards. This caused their floats to close when the airplane was in a climb.

The Douglas DC-1 was a prototype commercial transport, built by the Douglas Aircraft Company, Santa Monica, California. It was a twin-engine, all-metal, low-wing monoplane with conventional landing gear. It had a flight crew of two pilots, and provisions for 12 passengers.

The new airplane had been requested by Transcontinental and Western Air, Inc. It would be required to take off on a single engine from Winslow, Arizona—at 4,941 feet (1,506 meters) above Sea Level, the highest airfield in the T.W.A. route—and to climb to an altitude of 10,000 feet (3,048 meters), again on only one engine. It was required to carry more passengers than the Boeing Model 247, and to have a landing speed of 55 miles per hour (89 kilometers per hour).

The DC-1 was 60 feet, 0 inches (11.288 meters) long, with a wing span of 85 feet, 0 inches (25.908 meters), and height of 16 feet, 0 inches (4.877 meters). Its empty weight was 11,780 pounds (5,343 kilograms), and gross weight, 17,500 pounds (7,938 kilograms).

The DC-1 was powered by two supercharged, air-cooled, Wright Cyclone SGR-1820-F3 nine-cylinder radial engines, These engines had a compression ratio of 6.4:1 and required 87-octane gasoline. They were rated at 700 horsepower at 1,950 r.p.m. They turned three-bladed variable-pitch propellers throug a 16:11 gear reduction. The -F3 was 3 feet, 11-3/16 inches (1.199 meters) long, 4 feet, 5¾ inches (1.365 meters) in diameter, and weighed 1,047 pounds (475 kilograms).

The DC-1 had a cruise speed of 190 miles per hour (306 kilometers per hour) and maximum speed of 210 miles per hour (338 kilometers per hour). Its range was 1,000 miles (1,609 kilometers), and the service ceiling was 23,000 feet (7,010 meters).

Only one DC-1 was built. It was rolled out of its hangar 22 June 1933. Registered X223Y, it made its first flight, 1 July 1933, at Clover Field, Santa Monica, California, with test pilots Carl Cover and Fred Herman in the cockpit.

NC223Y was retired from passenger service in 1936. T.W.A. loaned it to the U.S. government for  high altitude research. In May 1938 NC223Y was sold to The Right Honourable Vicount Forbes at Croydon, 27 May 1938, and registered G-AFIF, 25 June 1938. It was re-sold to France, in September 1938. The DC-1 was again sold, this time to Spanish Republican government, and operated by Lineas Aéreas Postales Espanolas, also known as LAPE. The airplane made a forced landing at Malaga, Spain, in December 1940. It was damaged beyond repair.

© 2023 Bryan R. Swopes

30 June 1975: The last operational Douglas C-47 Skytrain transport in service with the United States Air Force, 43-49507, was retired and flown to the National Museum of the United States Air Force at Wright-Patterson Air Force Base, Ohio.

A C-47D, it is on display in the World War II Gallery, painted and marked as C-47A-80-DL 43-15213 of the 91st Troop Carrier Squadron, 439th Troop Carrier Group, during World War II. At the time it was withdrawn from service, 43-49507 had flown a total of 20,831 hours.

43-49507 (Douglas serial number 26768) was built at Oklahoma City as a C-47B-15-DK Skytrain. The C-47B differed from the C-47A in that it was powered by Pratt & Whitney Twin Wasp S3C4-G (R-1830-90) engines. These engines were equipped with two-speed superchargers for improved high-altitude performance. Following World War II, the second speed (“high blower”) was either disabled or removed. Following this modification, the airplane was redesignated C-47D.

The Douglas C-47 Skytrain is a military transport variant of the Douglas Aircraft Company DC-3 commercial airliner. It is an all-metal, twin-engine, low-wing monoplane with retractable landing gear. It was operated by a minimum flight crew of two pilots, navigator, radio operator and mechanic/load master. The airplane’s control surfaces are covered with doped-fabric. The primary differences between the civil DC-3 and military C-47 was the addition of a cargo door on the left side of the fuselage, a strengthened cargo floor, a navigator’s astrodome and provisions for glider towing.

The DC-3 made its first flight 17 December 1935, while the C-47 flew for the first time six years later, 23 December 1941.

The C-47 is 64 feet, 5½ inches (19.647 meters) long with a wingspan of 95 feet (28.956 meters) and height of 17 feet (5.182 meters). The total wing area is 988.9 square feet (91.872 square meters). The angle of incidence is 2°. The wing center section is straight, but outboard of the engine nacelles there is 5º dihedral. The wings’ leading edges are swept aft 15.5°. The trailing edges have no sweep.  Empty weight of the C-47D is 17,865 pounds (8,103 kilograms) and the maximum takeoff weight is 33,000 pounds (14,969 kilograms).

The C-47A was powered by two 1,829.4-cubic-inch-displacement (29.978 liter) air-cooled, supercharged R-1830-92 (Pratt & Whitney Twin Wasp S1C3-G) two-row 14-cylinder radial engines with a compression ratio of 6.7:1. These were rated at 1,060 horsepower at 2,550 r.pm., up to 7,500 feet (2,286 meters), maximum continuous power, and 1,200 horsepower at 2,700 r.p.m. at Sea Level for takeoff. Each engine drives a three-bladed Hamilton Standard Hydromatic constant-speed full-feathering propeller with a diameter of 11 feet, 6 inches (3.505 meters) through a 16:9 gear reduction. The R-1830-92 is 48.19 inches (1.224 meters) long, 61.67 inches (1.566 meters) in diameter, and weighs 1,465 pounds (665 kilograms).

The specifications of the  Pratt & Whitney Twin Wasp S3C4-G (R-1830-90) installed on the C-47B and C-47D were nearly the same as the -92 engine of the C-47A. Displacement and compression ratio were identical. The engines’ diameters were the same, though the -90 was very slightly longer than the -92—1.85–2.74 inches (4.699–6.960 centimeters), depending on specific variant. Also, the -90 was heavier than the -92 by 25–30 pounds (11.34–13.61 kilograms), again, depending on the specific variant. The R-1830-90 could maintain 1,000 horsepower at 2,550 r.p.m. at 12,500 feet (3,810 meters), and 1,000 horsepower at 2,700 r.p.m. at 14,000 feet (4,267 meters), a significant increase over the -92.

The C-47D has a cruising speed of 161 knots (185 miles per hour/298 kilometers per hour) at 10,000 feet (3,048 meters), and maximum speed of 202 knots (232 miles per hour/374 kilometers per hour) at 3,500 feet (1,067 meters). Its service ceiling was 22,150 feet (6,751 meters). The Skytrain had a maximum range of 1,026 nautical miles (1,181 miles/1,900 kilometers) with full cargo.

The C-47 could carry 9,485 pounds (4,302 kilograms) of cargo, or 27 fully-equipped paratroopers. Alternatively, 24 patients on stretchers could be carried, along with two attendants.

On D-Day, The Sixth of June, 1944, a formation of C-47 Skytrains, nine airplanes abreast, 100 feet (30 meters) from wing tip to wing tip, 1,000 feet (305 meters) in trail, stretching for over 300 miles (483 kilometers), airdropped 13,348 paratroopers of the 82nd and 101st Airborne Divisions, United States Army, and another 7,900 men of the British Army 6th Airborne Division and the 1st Canadian Parachute Battalion, behind the beaches at Normandy, France.

During the Vietnam War, 53 C-47s were converted from their transport role to AC-47 Spooky gunships. These were armed with three fixed, electrically-powered General Electric  GAU-2/A .30-caliber (7.62 NATO) Gatling guns firing out the left side of the fuselage. These aircraft were highly effective at providing close air support. The three Miniguns could fire a total of 12,000 rounds per minute.

Douglas Aircraft Company built 10,174 C-47 Skytrains at its factories in Santa Monica and Long Beach, California, and at Oklahoma City, Oklahoma.

© 2018, Bryan R. Swopes

30 June 1956: At approximately 10:32 a.m., two airliners, United Airlines’ Douglas DC-7 serial number 44288, Mainliner Vancouver, Civil Aeronautics Administration registration N6324C, and Trans World Airlines’ Lockheed L-1049-54-80 Super Constellation serial number 4016, Star of the Seine, N6902C, were over the Grand Canyon at 21,000 feet (6,400 meters).

Both airliners had departed Los Angeles International Airport shortly after 9:00 a.m. TWA Flight 2 was headed for Kansas City Municipal Airport with 64 passengers and 6 crew members. United Flight 718 was enroute to Chicago Midway Airport with 53 passengers and 5 crew members.

The airplanes were over the United States desert southwest, which, at that time, was outside of radar-controlled airspace. They were flying around towering cumulus clouds to comply with regulations that they “remain clear of clouds.”

The airplanes collided at about a 25° angle. The accident report describes the impact:

First contact involved the center fin leading edge of the Constellation and the left aileron tip of the DC-7. The lower surface of the DC-7 left wing struck the upper aft fuselage of the L-1049 with disintegrating force. The collision ripped open the fuselage of the Constellation from just forward of its tail to near the main cabin door. The empennage of the L-1049 separated almost immediately. The plane pitched down and fell to the ground. Most of the left outer wing of the DC-7 had separated and aileron control was restricted. . . .

The Constellation struck the ground near Temple Butte at an estimated 475 miles per hour (765 kilometers per hour). The DC-7’s left wing was so badly damaged that it went into an uncontrolled left spin and crashed at Chuar Butte. All 128 persons on the two airliners were killed.

This, as well as other accidents, resulted in significant changes in the United States air traffic control system.

© 2018, Bryan R. Swopes

27 June 1941: The experimental Douglas XB-19 long range heavy bomber took off on its first flight from Clover Field, Santa Monica, California. The four-engine airplane, which had originally been designated XBLR-2, serial number 38-471, was under the command of Major Stanley Milward Ulmstead, U.S. Army Air Corps, with 7 additional crewmembers. (Ulmstead had previously made the first flight of the Boeing XB-15.)

Major Ulmstead flew the XB-19 from Santa Monica to March Field in Riverside County. The duration of the flight was 55 minutes.

The Douglas XB-19 was a gigantic airplane for its time. The airplane was 132 feet, 1-7/8 inches (40.281225 meters) long with a wingspan of 212 feet, 0 inches (64.618 meters) and overall height of 41 feet, 4½ inches (12.611 meters). Its empty weight was 86,000 pounds (39,009 kilograms), and the gross weight, 140,000 pounds (63,503 kilograms). The maximum takeoff weight was 162,000 pounds (73,482 kilograms).

The wings had a chord of 33 feet, 0 inches (10.058 meters) at the root, and a maximum thickness of 8 feet (2.44 meters). The total area was 4,285 square feet (398.09 square meters). Their angle of incidence was 6°, and they had 6° dihedral. The wings were swept aft 10° 13′ at 25% chord.

The XB-19 was powered by four air-cooled, supercharged, direct-fuel-injected 3,347.662-cubic-inch-displacement (54.858 liter) Wright Aeronautical Division R3350-5 Duplex-Cyclone (GR3350A77) twin-row 18-cylinder radial engines. These had a compression ratio of 6.85:1 and required 100-octane gasoline. They had a normal power rating of 1,620 horsepower at 2,300 r.p.m., and a maximum 2,000 horsepower at 2,400 r.p.m. The R3350-5 was 4 feet, 7.12 inches (1.400 meters) in diameter, 5 feet, 11.5 inches (1.816 meters) long, and weighed 2,450 pounds (1,111 kilograms). The engines turned three-bladed propellers with a diameter of 18 feet, 2 inches (5.537 meters) through a 16:7 gear reduction.

The XB-19 had a cruise speed of 135 miles per hour (217 kilometers per hour) and a maximum speed of 224 miles per hour (360 kilometers per hour) at 15,700 feet (4,785 meters). The service ceiling was 39,000 feet (11,887 meters) and the maximum range was 7,750 miles (12,472 kilometers).

Defensive armament consisted of two 37 mm cannon, five .50-caliber machine guns, and six .30-caliber machine guns.

The XB-19 was converted to a transport and re-engined with experimental liquid-cooled, turbosupercharged Allison V-3420-11 24-cylinder “double-vee” engines. It was redesignated XB-19A. The airplane was scrapped at Davis-Monthan Air Force Base, Tucson, Arizona, in July 1949.

© 2020, Bryan R. Swopes

17 June 1986: After being returned to flyable condition, B-47E-25-DT Stratojet serial number 52-166, made the very last flight of a B-47 when it was flown by Major General John D. (“J.D.”) Moore and Lieutenant Colonel Dale E. Wolfe, U.S. Air Force, from the Naval Air Weapons Station China Lake in the high desert of Southern California, to Castle Air Force Base in California’s San Joaquin Valley, to be placed on static display.

52-166 had been built by the Douglas Aircraft Company at Air Force Plant No. 3, Tulsa, Oklahoma, in 1952. 52-166 had not been flown in twenty years, having sat in the Mojave Desert serving as a radar target. General Moore and Colonel Wolf were experienced B-47 pilots, though they hadn’t flown one in the same twenty years. Because the B-47 it had not been through a complete overhaul prior to the ferry flight, it was decided to leave the landing gear extended to avoid any potential problems.

During the 43 minute trip, the aircraft had several systems fail, including airspeed sensors, intercom, and partial aileron control. On approach to Castle Air Force Base, a 16 foot (4.9 meters) approach parachute was deployed. This created enough aerodynamic drag to slow the airplane while the early turbojet engines were kept operating at high power settings. These engines took a long time to accelerate from idle, making a go-around a very tricky maneuver. Releasing the chute allowed the airplane to climb out as the engines were already operating at high r.p.m.

Designed by Boeing, the Stratojet was a high-subsonic speed strategic bomber and reconnaissance aircraft, in service from 1951 until 1977. The B-47 could fly higher and faster than jet fighters of the time, and it was also highly maneuverable. B-47E (Boeing Model 450-157-35) was flown by a two pilots in a tandem cockpit. A navigator/bombardier was at a station in the nose.

The B-47E Stratojet differed from the earlier B-47B primarily with upgraded engines and strengthened landing gear to handle an increase in maximum weight. The B-47E Stratojet is 107.1 feet (32.644 meters) long with a wingspan of 116.0 feet (35.357 meters), and an overall height of  28.0 feet (8.534 meters). The wings are shoulder-mounted and have a total area of 1,428 square feet (132.67 square meters). The wings’ leading edges are swept aft to 36° 37′. The angle of incidence is 2° 45′ and there is 0° dihedral (the wings were very flexible). The B-47E in standard configuration had an empty weight of 78,620 pounds (35,661 kilograms) and maximum takeoff weight of 200,000 pounds (90,718 kilograms).

The B-47E was powered by six General Electric J47-GE-25 turbojet engines in four nacelles mounted on pylons below the wings. This engine has a 12-stage axial-flow compressor, eight combustion chambers, and single-stage turbine. The -25 has a continuous power rating of 5,320 pounds of thrust (23.665 kilonewtons) at 7,630 r.p.m., at Sea Level; Military Power, 5,670 pounds (25.221 kilonewtons) at 7,800 r.p.m. (30 minute limit); and Maximum Power, 7,200 pounds (32.027 kilonewtons) at 7,950 r.p.m. with water/alcohol injection (5 minute limit). The J47-GE-25 has a maximum diameter of 3 feet, 1 inch (0.940 meters) and length of 12 feet, 0 inches (3.658 meters) and weighs 2,653 pounds (1,203 kilograms)

The B-47E had a maximum speed of 497 knots (572 miles per hour/920 kilometers per hour) at 20,000 feet (6,096 meters), and 485 knots (558 miles per hour/898 kilometers per hour) at 38,600 feet (11,765 meters).

The service ceiling was 31,500 feet (9,601 meters) and combat ceiling 40,800 feet (12,436 meters).

The combat radius of the B-47E was 1,780 nautical miles 2,048 miles (3,297 kilometers with a 10,000 pound (4,536 kilograms) bomb load. Ferry range with 14,720 gallons (55,721 liters) of fuel was 4,095 nautical miles (4,712 miles/7,584 kilometers).

For defense the B-47E was armed with two M24A1 20 mm autocannons with 350 rounds of ammunition per gun. The remotely-operated tail turret was controlled by the co-pilot.

The maximum bomb load of the B-47E was 12,000 pounds (5,443 kilograms). The B-47 could carry up to six 2,000 pound (907 kilogram) bombs, or one 10,670 pound (4,840 kilograms) “Special Store”: a B-41 three-stage radiation-implosion thermonuclear bomb with a yield of 25 megatons).

A total of 2,032 B-47s were built by a consortium of aircraft manufacturers: Boeing Airplane Company, Wichita, Kansas; Douglas Aircraft Company, Tulsa, Oklahoma; Lockheed Aircraft Company, Marietta, Georgia.

The Stratojet is one of the most influential aircraft designs of all time and its legacy can be seen in almost every jet airliner built since the 1950s: the swept wing with engines suspended below and ahead on pylons. The B-47 served the United States Air Force from 1951 to 1977. From the first flight of the Boeing XB-47 Stratojet prototype, 17 December 1947, to the final flight of B-47E 52-166, was 38 years, 6 months, 1 day.

© 2018, Bryan R. Swopes

30 May 1958: Douglas Aircraft Company Flight Operations Manager and engineering test pilot Arnold G. Heimerdinger, with co-pilot William M. Magruder and systems engineer Paul H. Patten, were scheduled to take off from Long Beach Airport (LGB) on the coast of southern California, at 10:00 a.m., to make the first flight of the new Douglas DC-8 jet airliner, c/n 45252, FAA registration N8008D.

Crowds of spectators, estimated as many as 50,000 people, were surrounding the airport. For this first test flight, the Federal Aviation Administration required a minimum of five miles visibility. Typical Southern California coastal low clouds and fog caused a ten minute delay.

Taking off at 10:10 a.m., N8008D climbed out to the south over the Pacific Ocean. Escorted by a company-owned Douglas DC-7 engineering and photo plane and a Lockheed T-33A Shooting Star chase, the DC-8 climbed to 11,000 feet (3,353 meters) and went through a series of pre-planned flight maneuvers and systems checks. Heimerdinger took the airliner north to Edwards Air Force Base in the high desert of southern California, where the full flight test program would be carried out. The total duration of the first flight was 2 hours, 10 minutes.

In an article written the following year, Heimerdinger said that the DC-8 was easy to fly and never presented any difficulties during the test program.

The Douglas DC-8 Jetliner is a commercial airliner, a contemporary of the Boeing 707 and Convair 880. It was operated by a flight crew of three and could carry up to 177 passengers. It was powered by four turbojet engines mounted on pylons suspended below the wings. The wings’ leading edges were swept to 30° as were the vertical fin and horizontal tailplane. The airplane is 150 feet, 6 inches (45.872 meters) long with a wingspan of 142 feet, 5 inches (43.409 meters) and overall height of 42 feet, 4 inches (12.903 meters). N8008D was a Series 10 version. It had an empty weight of 119,767 pounds (54,325 kilograms) and maximum takeoff weight of 273,000 pounds (123,831 kilograms).

N8008D was originally powered by four Pratt & Whitney JT3C-6 turbojet engines, the same engines which powered its Boeing rival. It is a two-spool, axial-flow turbojet engine with a 16-stage compressor and 2-stage turbine. The JT3C-6 was rated at 11,200 pounds of thrust (49.82 kilonewtons), and 13,500 pounds (60.05 kilonewtons) with water/methanol injection). The JT3C is 11 feet, 6.6 inches (3.520 meters) long, 3 feet, 2.9 inches (0.988 meters) in diameter, and weighs 4,235 pounds (1,921 kilograms). The engines were later upgraded to JT3D-1 turbofan engines which produced 17,000 pounds of thrust.

The DC-8-10 series had a cruising speed of 0.82 Mach (542 miles per hour/872 kilometers per hour) at 35,000 feet (10,668 meters). Its maximum range was 5,092 miles (8,195 kilometers).

On 21 August 1961, a Douglas DC-8-43, N9604Z, c/n 45623, Line Number 130, flown by Chief Test Pilot William Magruder, Paul Patten, Joseph Tomich and Richard Edwards, climbed to 50,090 feet (15,267 meters) near Edwards Air Force Base. Magruder put the DC-8 into a dive, and the airplane reached Mach 1.012 (668 miles per hour/1,075 kilometers per hour) while descending through 41,088 feet (12,524 meters). The airliner maintained this supersonic speed for 16 seconds.

This was the first time that a civil airliner had “broken the Sound Barrier.” An Air Force F-100 Super Sabre and F-104 Starfighter were chase planes for this flight. Reportedly, the F-104 was flown by the legendary test pilot, Colonel Chuck Yeager.

N9604Z was powered by four Rolls-Royce Conway RCo.12 Mk 509 two-shaft axial-flow turbofan engines, rated at 17,500 pounds of thrust (77.844 kilonewtons) at 9,990 r.p.m. The 509 is 11 feet, 3.9 inches (3.452 meters) long, 3 feet, 6.2 inches (1.072 meters) in diameter, and weighs 4,542 pounds (2,060 kilograms).

N9604Z was delivered to Canadian Pacific Airlines, 15 November 1961, registered CF-CPG, and named Empress of Montreal. It later flew under CP Air as Empress of Buenos Aires. It was scrapped at Opa Locka Municipal Airport, north of Miami, Florida, in May 1981.

In 1960, N8008D was converted to the DC-8-51 configuration. With a change to the more powerful JT3D-1 turbofan engines, the airliners maximum takeoff weight was increased to 276,000 pounds (125,191 kilograms).

After the flight test and commercial certification program was completed, on 21 June 1961, Douglas leased N8008D to National Airlines, based at Miami, Florida. One year later, 20 June 1961, it was sold to Trans International Airlines. TIA leased the DC-8 to Lufthansa, 11 May 1965, and to Canadian Pacific, 1 October 1966. It was re-registered CF-CPN and named Empress of Santiago.

TIA sold the DC-8 to Delta Airlines, Atlanta, Georgia, 1 October 1967. It reverted to its FAA-assigned registration, N8008D. Delta gave it fleet number 800.

In March 1979, Delta sold N8008D to F.B. Myers and Associates. On 1 April, F.B. Myers leased the it to Aerovias de México, S.A. de C.V. (Aeroméxico). The DC-8 was assigned Mexican registration XA-DOE and named Quintana Roo.

The first Douglas DC-8 was placed in storage at Marana-Pinal Airpark, north of Tucson, Arizona, 7 January 1982. In May 1989, it was sold to Agro Air, a Caribbean regional cargo airline. It remained at Marana and was used as a source of parts. In 2001, c/n 45252 it was scrapped.

Between 1959 and 1972, Douglas produced 556 DC-8s in passenger and freighter configurations.

Arnold George Heimerdinger was born in Manchester Township, Michigan, 7 December 1910. His parents were Charles and Minnie L. Uphaus Heimerdinger. He studied electrical engineering at the University of Michigan. Heimerdinger married Miss Mary Aileen Eggert 19 August 1935.

A.G. Heimerdinger was commissioned as an ensign in the United States Navy, 27 November 1942 and served as a Naval Aviator until he was released from active duty, 14 October 1945.

Heimerdinger worked as an engineering test pilot for the Federal Aviation Administration, and he flew certification tests of the Boeing 377 Stratocruiser, Convair 240 and 340 Metroliner, and the Lockheed L-640 and L-1049 Constellation.

He joined the Douglas Aircraft Company at Santa Monica, California, in 1952 and remained with the company until he retired in 1974. He was the project test pilot for the Douglas DC-6B and the DC-7. Transferring to Douglas’ Long Beach Division, a few miles southeast, he was project test pilot for the DC-8 and DC-9 jet airliners.

Arnold G. “Heimie” Heimerdinger died at Santa Monica, California, 17 July 1975.

© 2018, Bryan R. Swopes

3 May 1952: A ski-equipped United States Air Force Douglas C-47A Skytrain, piloted by Lieutenant Colonels William P. Benedict and Joseph O. Fletcher, USAF, was the first airplane to land at the North Pole.¹ The navigator was 1st Lieutenant Herbert Thompson. Staff Sergeant Harold Turner was the flight engineer and Airman 1st Class Robert L. Wishard, the radio operator.

Also on board was Arctic research scientist Dr. Albert P. Crary and his assistant, Robert Cotell. Additional personnel were Fritza Ahl, Master Sergeant Edison T. Blair and Airman 2nd Class David R. Dobson.

Colonel Fletcher was commanding officer of the 58th Strategic Reconnaissance Squadron, Eielson Air Force Base, Fairbanks, Alaska. He was responsible for establishing Drift Ice Stations within the polar ice cap for remote weather observation bases. Ice Island T-3 was renamed Fletcher’s Ice Island in his honor. He became a world authority on Arctic weather and climate. Various geographic features, such as the Fletcher Abyssal Plain in the Arctic Ocean, and the Fletcher Ice Rise in the Antarctic are also named for him.

The airplane flown on this expedition was Douglas C-47A-90-DL Skytrain 43-15665.

The Douglas C-47 in the photograph below is similar to the Skytrain that Benedict and Fletcher landed at the North Pole, however it is a screen image from the RKO/Winchester Pictures Corporation motion picture, “The Thing from Another World,” which was released just one year earlier, 29 April 1951. Howard Hawks’ classic science fiction film involves an Air Force C-47 Skytrain crew that flies in support of a remote Arctic research station.

The Douglas C-47A Skytrain is an all-metal twin-engine, low wing monoplane transport with retractable landing gear. It was operated by a minimum flight crew of two pilots, a navigator and a radio operator. The wing is fully cantilevered and the fuselage is of semi-monocoque construction. Control surfaces are fabric-covered.

The C-47 is 64 feet, 5½ inches (19.647 meters) long with a wingspan of 95 feet (28.956 meters) and height of 17 feet (5.182 meters). Empty weight of the C-47A is 17,257 pounds (7,828 kilograms) and the maximum takeoff weight is 29,300 pounds (13,290 kilograms).²

The C-47A is powered by two 1,829.4-cubic-inch-displacement (29.978 liter) air-cooled, supercharged R-1830-92 (Pratt & Whitney Twin Wasp S1C3-G) two-row 14-cylinder radial engines. These were rated at 1,200 horsepower at 2,700 r.p.m. at Sea Level for takeoff. The maximum continuous rating for normal operation was 1,060 horsepower at 2,550 r.pm., up to 7,500 feet (2,286 meters). Each engine drives a three-bladed Hamilton Standard Hydromatic constant-speed full-feathering propeller with a diameter of 11 feet, 6 inches (3.505 meters) through a 16:9 gear reduction. The R-1830-92 is 48.19 inches (1.224 meters) long, 61.67 inches (1.566 meters) in diameter, and weighs 1,465 pounds (665 kilograms).

The C-47 has a cruising speed of 185 miles per hour (298 kilometers per hour) at 10,000 feet (3,048 meters) and service ceiling of 24,100 feet (7,346 meters).

The C-47-DL could carry 6,000 pounds (2,722 kilograms) of cargo, or 28 fully-equipped paratroopers. Alternatively, 14 patients on stretchers could be carried, along with three attendants.

43-15665 crashed on Fletcher’s Ice island 3 November 1952. It has since sunk to the floor of the Arctic Ocean.

¹ At least one source states that a Soviet expedition aboard three Lisunov Li-2 transports (a license-built Douglas DC-3) landed near the North Pole on 23 April 1948.

² Data from AAF Manual 51-129-2, Pilot Training Manual for the C-47 Skytrain

© 2019, Bryan R. Swopes

2 May 1925: At Santa Monica, California, the Douglas Aircraft Company C-1, A.S. 25-425, made its first flight. The new aircraft was requested by the U.S. Army Air Service to fill the role of a cargo transport. The single-engine, two-bay biplane had a crew of two in an open cockpit and could carry 6–8 passengers in an enclosed compartment, or 2,500 pounds (1,134 kilograms) of cargo. A trapdoor in the floor allowed heavy cargo to be lifted directly into the airplane.

The Douglas C-1 was 35 feet, 4 inches (10.770 meters) long with a wingspan of 56 feet, 7 inches (17.247 meters) and height of 14 feet (4.267 meters). The transport’s empty weight was 3,836 pounds (1,740 kilograms) and its loaded weight was 6,443 pounds (2,922 kilograms).

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

The Liberty L12 aircraft engine was designed by Jesse G. Vincent of the Packard Motor Car Company and Elbert J. Hall of the Hall-Scott Motor Company. This engine was produced by Ford Motor Company, as well as the Buick and Cadillac Divisions of General Motors, The Lincoln Motor Company (which was formed by Henry Leland, the former manager of Cadillac, specifically to manufacture these aircraft engines), Marmon Motor Car Company and Packard. Hall-Scott was too small to produce engines in the numbers required.

The C-1 had a maximum speed of 116 miles per hour (187 kilometers per hour), though its cruising speed was 85 miles per hour (137 kilometers per hour). The service ceiling was 14,850 feet (4,526 meters) and its range was 385 miles (620 kilometers)

In addition to a passenger and cargo transport, the Douglas C-1 was used experimentally as a medical evacuation aircraft and as an aerial refueling tanker. Nine C-1 and C-1A transports were built, and seventeen slightly larger C-1Cs.

The C-1 was the first U.S. Air Force airplane to use the designation “C-” to indicate a cargo transport. That designator is still in use today.

© 2018, Bryan R. Swopes

1 May 1940: The first Douglas Aircraft Company SBD-1 Dauntless dive bomber, Bu. No. 1596 (s/n 549), made its first flight at El Segundo, California. The airplane was delivered to the U.S. Navy 6 September 1940. Assigned to Marine Scout Bomber Squadron 234 (VMSB-234) at MCAS Ewa, 7 miles (11 kilometers) west of Pearl Harbor, Oahu,Territory of Hawaii, it ditched in the ocean and was lost, 8 August 1942.

The Douglas SBD-1 Dauntless dive bomber was a single-engine, low-wing monoplane with retractable landing gear. It was developed from the Northrop BT-2. The flight crew consisted of a pilot and an aerial gunner. The SBD-1 was 32 feet, 2 inches (9.804 meters) long with a wingspan of 41 feet, 7 inches (12.675 meters) and height of 13 feet, 7 inches (4.140 meters). The wing area was 325 square feet (30.19 square meters). It had an empty weight of 5,903 pounds (2,678 kilograms) and maximum gross weight of 9,790 pounds (4,441 kilograms) with one 1,600 pound (726 kilogram) bomb.

Large, perforated split flaps were used to stabilize the airplane during steep dives.

The SBD-1 was powered by an air-cooled, supercharged R-1820-32 (Wright Aeronautical Corporation R-1820G133 Cyclone) nine-cylinder radial engine with a compression ratio of 6.45:1, requiring 100-octane gasoline. It drove a 3-bladed Hamilton Standard propeller with a diameter of 10 feet, 10 inches (3.302 meters) through a 16:11 gear reduction. The R-1820-32 had a normal power rating of 950 horsepower at 2,300 r.p.m. at Sea Level, and 1,000 horsepower at 2,350 r.p.m. for takeoff. The engine was 3 feet, 9.06 inches long (1.145 meters), 4 feet, 7.12 inches (1.400 meters) in diameter, and weighed 1,255 pounds (569 kilograms).

In scout configuration (no bombs) the SBD-1 had a maximum speed of 253 miles per hour (407 kilometers per hour at 16,000 feet (4,877 meters). It could reach 10,000 feet (3,048 meters) in 6.6 minutes, and 20,000 feet (6,096 meters) in 15.8 minutes. The service ceiling was 29,600 (9,022 meters). It had a fuel capacity of 180 gallons (681 liters). The airplane’s maximum range was 985 miles (1,585 kilometers) at 142 mph (229 kilometers per hour).

The SBD-1 was armed with two fixed .50-caliber machine guns synchronized to fire forward through the propeller, with 360 rounds of ammunition, and one .30-caliber machine gun on a flexible mount, with 600 rounds of ammunition. It could carry one 1,600 pound (726 kilogram) bomb or one 650 pound (295 kilogram) depth bomb under the fuselage. Two racks under the wings could each carry a 100 pound (45 kilogram) bomb, or a 325 pound (147 kilogram) depth bomb.

The airplane was also ordered by the U.S. Army Air Corps as the A-24 Banshee.

© 2023, Bryan R. Swopes

15 April 1970, 01:09:40 UTC: T plus 077:56:40.0: The Apollo 13 Saturn S-IVB-508 third stage impacted the surface of The Moon north of Mare Cognitum. (S. 2° 33′ 00″, W. 27° 52′ 48″). The S-IVB hit the lunar surface at a velocity of 2.58 kilometers per second (5,771 miles per hour). The impact energy was 4.63 x 10¹⁷ ergs (1.04 kiloton).

The impact was detected by seismometers placed on the Moon by Apollo 12 astronauts Pete Conrad and Alan Bean. This was part of the Apollo Lunar Surface Experiments Package, or ALSEP.

The Apollo 12 seismometer was located 135 kilometers (83.9 miles) from the Apollo 13 third stage impact. The signals were used to calibrate the instrument package, which was in service from 1969 to 1977.

The Saturn V third stage was designated Saturn S-IVB. It was built by Douglas Aircraft Company at Huntington Beach, California. The S-IVB was 58 feet, 7 inches (17.86 meters) tall with a diameter of 21 feet, 8 inches (6.604 meters). It had a dry weight of 23,000 pounds (10,000 kilograms) and fully fueled weighed 262,000 pounds (118,841 kilograms). The third stage had one Rocketdyne J-2 engine which used liquid hydrogen and liquid oxygen for propellant. Itproduced 232,250 pounds of thrust (1,033.10 kilonewtons). The S-IVB would place the Command and Service Module into Low Earth Orbit, then, when all was ready, the J-2 would be restarted for the Trans Lunar Injection.

© 2017, Bryan R. Swopes