17 October 1922

A Vought VE-7SF takes off from USS Langley (CV-1). (National Naval Aviation Museum)
A Vought VE-7 takes off from USS Langley (CV-1). (National Naval Aviation Museum)

17 October 1922: Lieutenant Commander Virgil Childers (“Squash”) Griffin, Jr., United States Navy, made the first takeoff from an aircraft carrier of the U. S. Navy when he flew a Chance Vought Corporation VE-7 fighter from the deck of USS Langley (CV-1) while the ship was anchored in the York River along the west side of Chesapeake Bay, Virginia.

A Vought VE-7 taking off from USS Langley, 1922. The second airplane is an Aeromarine. (U.S. Navy)
A Vought VE-7 taking off from USS Langley, 1922. The second airplane is an Aeromarine 39 trainer. (U.S. Navy)

USS Langley was the United States Navy’s first aircraft carrier. The ship was named in honor of an American scientist, Samuel Pierpont Langley. It was a former collier, USS Jupiter (AC-3), which had been converted at the Norfolk Navy Yard, 1921–1922. As an aircraft carrier, Langley had a complement of 468 men, including the air wing. The ship was 542 feet, 2.5 inches (165.27 meters) in length, overall, with a beam of 65 feet, 6 inches (19.96 meters) and draft of 22 feet, 1 inch (6.73 meters). The aircraft carrier had a full load displacement of 15,150 long tons (15,393 Metric tons).

Langley was powered by a General Electric turbo-electric drive, with a total of 6,500 shaft horsepower. She could make 15.5 knots (17.8 miles per hour; 28.7 kilometers per hour). The aircraft carrier had a maximum range of 4,000 miles (6,437 kilometers).

USS Langley (CV-1) with Vought VE-7SF fighters on the flight deck, at anchor off Culebra Island, Puerto Rico, 18 March 1926. In the background are a USS Tennessee-class and two USS New Mexico-class battleships. (U.S. Navy)

In addition to her air group of up to 36 airplanes, Langley was defended by four 5-inch/51-caliber guns (127 mm × 6.477 meters). This gun could fire a 50-pound (22.7 kilogram) shell a distance of 15,850 yards (14, 493 meters) when elevated to 20°. Its maximum rate of fire was 9 rounds per minute.

As the more modern aircraft carriers Lexington and Saratoga came in to service, Langley was once again converted, this time to a sea plane tender, and reclassified as AV-3, 21 April 1937.

USS Langley was badly damaged by Japanese dive bombers during the Battle of the Java Sea, 27 February 1942, having been struck by five bombs. The ship was scuttled approximately 75 miles south of Tjilatjap, Java, to prevent capture, when her escorting destroyers fired two torpedoes into her.

USS Langley (CV-1), 1922. (U.S. Navy)
USS Langley (CV-1), 1922. (U.S. Navy)

The Chance Vought VE-7 was originally ordered as a two-place trainer, but its performance and handling qualities were so good that it was widely used as a fighter. The VE-7SF was a single-place, single-engine biplane built for the U.S. Navy.

The VE-7 was 22 feet 5-3/8 inches (6.842 meters) long, with a wingspan of 34 feet, 4 inches (10.465 meters), and height of 8 feet 7½ inches (2.629 meters). The two-bay wings were separated by a vertical gap of 4 feet, 8 inches (1.422 meters) and the leading edge of the  lower wing was staggered 11 inches (27.9 centimeters) behind that of the upper wing. Both wings had 1.25° dihedral. The upper wing had +1.75° incidence, lower wing had +2.25°. The VE-7 had weighed 1,392 pounds (631 kilograms) empty and had gross weight of 1,937 pounds (879 kilograms)

Vought VE-7SF 2-F-16. (Chance Vought)
Vought VE-7SF 2-F-16. (Chance Vought)

The VE-7 was powered by a water-cooled, normally-aspirated, 716.69-cubic-inch-displacement (11.744 liters) Wright-Hispano E3 Alert single-overhead-camshaft (SOHC) 60° V-8 engine, rated at 215 horsepower at 2,000 r.p.m. The engine drove a two-bladed fixed-pitch wooden propeller with a diameter of 8’8″ (2.642 meters). The Wright E3 weighed 465 pounds (211 kilograms).

The VE-7 had a maximum speed of 106  miles per hour (171 kilometers per hour) and service ceiling of 15,000 feet (4,572 meters). Its maximum range was 290 miles (467 kilometers).

The fighter was armed with two Vickers .30-caliber (7.62 mm) machine guns, synchronized to fire forward through the propeller arc.

Chance Vought VE-7, 2-F-16, assigned to Fighter Squadron 2 (VF-2) (Chance Vought)
Chance Vought VE-7SF, 2-F-16, assigned to Fighter Squadron 2 (VF-2) (Chance Vought)

Rear Admiral Jackson R. Tate, U.S. Navy (Retired) described the first takeoff:

“We were operating just north of the Tongue of the Shoe, seaward of the main channel from Norfolk, Va. A trough about 6 feet long, set up on sawhorses was rigged at the aft end of the flight deck. When the tail skid of the VE-7 used in the test was placed in the trough, she was in the flight attitude.

“We had no brakes, so the plane was held down on the deck by a wire with a bomb release at the end. This was attached to a ring in the landing gear. ‘Squash’ Griffin climbed in, turned up the Hispano Suiza engine to its full 180 hp and gave the “go” signal. The bomb release was snapped and the Vought rolled down the deck. Almost before it reached the deck-center elevator it was airborne. Thus, the first takeoff from a U.S. carrier.”

United States Navy aircraft carrier USS. George H.W. Bush (CVN-77) (Mass Coomunications Specialist 3rd Class Tony Curtiss, U.S. Navy)
United States Navy nuclear-powered aircraft carrier USS George H. W. Bush (CVN-77). (Mass Communications Specialist 3rd Class Tony Curtis, U.S. Navy)

Virgil Childers Griffin, Jr., was born at Montgomery, Alabama, 18 April 1891. He was the first of three children of Virgil Childers Griffin, secretary of the Railroad Commission of Alabama, and Mary Lee Besson Griffin.

Midshipman Virgil C. Griffin, Jr., U.S.N.A.

Griffin was admitted as a midshipman at the United States Naval Academy, Annapolis, Maryland, 25 June 1908, a member of the Class of 1912. Four years later he graduated. Virgil C. Griffin, Jr., was commissioned an ensign, United States Navy, 8 June 1912, with a date of precedence 28 April 1908.

On 14 July 1912, Ensign Griffin was assigned to the 16,000 ton battleship, USS South Carolina (BB-26). Griffin was promoted to lieutenant (junior grade), 8 June 1915. He remained aboard South Carolina until June 1916.

Lieutenant (j.g.) Griffin applied for flight trainning, and on completion, was designated Naval Aviator # 41.

The United States entered World War I in April 1917. On 8 June 1917, Lieutenant (j.g.) Griffin was one of one hundred Naval Aviators who “arrived safely in France for any duty that may present itself. . . They are the first of the American fighting forces to reach France.” On 8 June 1918, Griffin was promoted to lieutenant (permanent rank). He was in command of the U.S. Navy sea plane base at Saint-Trojan, in southwestern France. Griffin was promoted to the rank of lieutenant commander (temporary), 21 September 1918 (Constructive date of precedence 28 February 1907).

Lieutenant Commander Griffin returned to the United States in 1919. He was assigned to the Department of the Navy, Washington, D.C., first to the Naval Operations Aviation Divivision, and in 1920, Naval Operations Inspection Division. Later in 1920, Griffin was assigned to the Atlantic Fleet Ship Plane Division, Mitchel Field, Mineola, New York.

On 8 December 1920, Lieutenant Commander Griffin married 25-year-old Alabama native Miss Elize Whiting Hall, at Mobile, Alabama.

In 1923, Lieutenant Commander Griffin returned to sea duty aboard USS Langley. he was next stationed at NAS Pensacola, Florida, 1924–1925. He served aboard USS Lexington (CV-2), 1926–1927. In 1929, Griffin returned to Langley, before being assigned Scoutig Squadron TWO (VS-2B) aboard USS Saratoga, flying the Vought O2U-2 Corsair.

On 29 December 1931, Griffin was promoted to commander. He was stationed at NAS Pearl Harbor, Territory of Hawaii, in 1932.

Commander Griffin once again returned to Langley, as the aircraft carrier’s executive officer, 1933–1934.

In 1937, Commander Griffin was commanding officer, NAS Anacostia, Washington D.C. He had additional duties in the Navy’s Bureau of Aeronautics.

In 1938 and 1939, Commander Griffin was chief of staff and aide to the Commander, Carrier Division TWO (ComCarDiv 2), aboard USS Yorktown.

Consolidated PBY-3 of Patrol Wing FIVE, circa 1939. (U.S. Navy)

Later in 1939, Commander Griffin was assigned as commanding officer Patrol Wing FIVE. The wing included patrol squadrons VP-51, VP-52, VP-53 VP-54, and the airplane tenders USS Gannet (AVP-8), USS Thrush (AVP-3), USS Owl (AM-2) and USS Patoka (AV-6).

Griffin was promoted to the rank captain, 1 November 1939. On 1 May 1940, Captain Griffin was placed in command of NAS Isle Grande, San Juan, Puerto Rico.

Captain Virgil C. Griffin, Jr., U.S. Navy, with Mrs. Ernest Hemingway (née Martha Ellis Gelhorn), circa 1942. (National Museum of the United States Navy) 80-G-13028a

Captain Virgil Childers Griffin, Jr., retired from the United States Navy, 1 January 1947. He died at San Diego, California, 27 March 1957, at the age of 66 years. He was buried at the Fort Rosecrans National Cemetery.

© 2018, Bryan R. Swopes

17 October 1913

Zeppelin L2 LZ 18 (© Ullstein Bild)
Zeppelin L2 (LZ 18). The smoke is coming from the forward engine car. (© Ullstein Bild)

17 October 1913: On the morning of a scheduled test flight at Flugplatz Johannisthal-Adlershof, an airfield south east of Berlin, Germany, Marine-Luftschiffes L2, the second rigid airship built for the Kaiserliche Marine (Imperial German Navy) by Luftschiffbau Zeppelin at Friedrichshafen, was delayed by problems with the engines. The morning sun heated the hydrogen contained in the airship’s gas bags, causing the gas to expand and increasing the airship’s buoyancy.

L2 New York Times 18 October 1913
L2 at altitude. This photograph was published in the New York Times, 18 October 1913. (George Grantham Bain Collection, Library of Congress)

Once released, L2 rapidly rose to approximately 2,000 feet (610 meters). The hydrogen expanded even more due to the decreasing atmospheric pressure. To prevent the gas bags from rupturing, the crew vented hydrogen through relief valves located along the bottom of the hull.

L2 leaves a trail of smoke as it crashes to the ground, 17 October 1913. (Zeppelin-Luftschiffe.com)

In this early design, the builders had placed the relief valves too close to the engine cars. Hydrogen was sucked into the engines’ intakes and detonated. L2 caught fire and a series of explosions took place as it fell to the ground.

All 28 persons on board were either killed immediately, or died of their injuries shortly thereafter.

At the time of the accident, L2 had made ten flights, for a total of 34 hours, 16 minutes.

The flight crew of Marine-Luftschiffes L2 (via LZDEAM.NET)
The flight crew of Marine-Luftschiffes L2

A contemporary news article described the accident:

AIRSHIP AND BALLOON NEWS.

The Wreck of the Zeppelin.

ELSEWHERE in this issue we comment upon the terrible catastrophe which befell the German Navy’s new Zeppelin L2, on Friday last week, just outside the Johannisthal aerodrome, near Berlin. From the following official account it appears that the airship was making a trial voyage:—

“She started this morning for a high flight, with twenty-eight persons on board. After three minutes she had attained a height of two hundred metres (over 600 feet) when flames burst forth between the fore engine-car and the envelope. In two or three seconds the whole ship was on fire and an explosion occurred. At the same time the airship fell slowly head downwards, until she was forty metres (130 feet) from the earth. Here a second explosion took place, presumably of benzine. When the vessel struck the earth a third explosion occurred, and the framework collapsed. A company of pioneers and guide-rope men hastened to the scene, and doctors were immediately in attendance. Two of the crew were picked up outside the ship still alive, but they died shortly afterwards. Lieut. Bleuel, who was severely injured, was taken to hospital. The remaining 25 of the crew had been killed during the fall of the airship or by the impact with the earth. The cause of the disaster appears to have been, so far as is at present known, an outbreak of fire in or over the fore engine-car.”

The commanding officer was Lieut. Freyer, and he was assisted by Lieuts. A. Trenck, Hansmann, and Busch, with thirteen warrant and petty officers. There were also on board as representing the German Navy, Commander Behnisch, Naval Construtors Neumann, and Pretzker, and three secretaries, named Lehmann, Priess, and Eisele. The Zeppelin Co. were represented by Capt. Glund and three mechanics, and Lieut. Baron von Bleuel was a passenger. The last mentioned was the only one rescued alive, and he died from his injuries a few hours later.

One of the first messages of sympathy was addressed by President Poincare’ to the German Emperor.

Extraordinary scenes, showing the way in which the calamity was regarded in Germany, were witnessed at the funeral service of 23 of the victims, held on Tuesday at the Garrison Church. Upon each of the coffins Prince Adalbert placed a wreath from the German Emperor and Empress, who with the Crown Prince and princess, and Princes Eitel Friedrich, Adalbert, August Wilhelm,  Oscar and Joachim attended in person, while the Government was represented by the Chancellor, Admiral Tirpitz, the Chief of the General Staff, Field Marshall von Moltke, and many other officers. Count Zeppelin was also present.

FLIGHT, First Aero Weekly in the World. No. 252. (No. 43, Vol. V.), 25 October 1913 at Page 1179

Wreckage of the L2 at Flugplatz Johannisthal-Adlershof, Germany, 17 October 1913. (Photo Gebr. Haeckel, Berlin # 3227/2)
Wreckage of the L2 at Flugplatz Johannisthal-Adlershof, Germany, 17 October 1913. (Gebrüder Haeckel, Berlin  3227/2)

The Marine-Luftschiffes L2 had been designated LZ 18 by the builders. Both identifications are commonly used (sometimes, L.II). Technical data for L2 is limited and contradictory. One source describes it as having a length of 158 meters (518 feet, 4½ inches), with a diameter of 16.6 meters (54 feet, 5½ inches). Another states 492 feet.

Eighteen hydrogen-filled gas bags were placed inside the rigid framework and covered with an aerodynamic envelope. The airship had a volume of 27,000 cubic meters (953,496 cubic feet), and a lift capacity of 11.1 tons (24,471 pounds).

Four water-cooled, normally-aspirated, 22.921 liter (1,398.725 cubic inches) Maybach C-X six-cylinder inline engines were carried in two cars beneath the hull. They produced 207 horsepower at 1,250 r.p.m., burning bensin (gasoline). Each engine drove a four-blade propeller through a drive shaft and gear arrangement. These engines weighed 414 kilograms (913 pounds), each.

L2 had a maximum speed of approximately 60 miles per hour (97 kilometers per hour). At reduced speed, L2 had a 70 hour radius of action.

The Kaiser and Imperial princes lead the funeral procession.
The Imperial Princes lead the funeral procession. Left to right, Prince Oskar, Prince August Wilhelm, Prince Adalbert, Crown Prince Wilhelm, Prince Eitel Friederich, Prince Joachim.

© 2016, Bryan R. Swopes

16 October 1963

Convair B-58A-20-CF Hustler 61-2059, Greased Lightning. (U.S. Air Force)
Major Sidney Kubesch with his wife, Joanna Alice Cole Kubesch, 16 October 1963. (Kokomo Tribune)
Major Sidney J. Kubesch, U.S. Air Force, with his wife, Joanna Alice Cole Kubesch, at RAF Greenham Common, 16 October 1963. (Kokomo Tribune)

16 October 1963: Operation Greased Lightning. Major Sidney J. Kubesch, Major John Barrett and Captain Gerard Williamson flew from Tokyo, Japan, to London, England, non-stop, in 8 hours, 35 minutes, 20.4 seconds. Their airplane was a Convair B-58A-20-CF Hustler, serial number 61-2059, named Greased Lightning. It was assigned to the 305th Bombardment Wing, 19th Air Division, at Bunker Hill Air Force Base, Indiana.

Five inflight refuelings were required to complete the flight. The bomber had to slow from its supersonic cruise to rendezvous with the tankers. The B-58’s average speed was 692.71 miles per hour (1,114.81 kilometers per hour). The time from Tokyo to Anchorage, Alaska was 3 hours, 9 minutes, 42 seconds at an average speed of 1,093.4 miles per hour (1,759.7 kilometers per hour); and Anchorage to London, 5 hours, 24 minutes, 54 seconds at 826.9 miles per hour (1.330.8 kilometers per hour).

Greased Lightning‘s speed record still stands.

Screen Shot 2015-10-15 at 08.56.36 The three crewmen were awarded the Distinguished Flying Cross.

Major Sidney Kubesch, Aircraft Commander, John Barrett, Navigator and Gerard Williamson. (Kokomo Tribune)
Major Sidney J. Kubesch, Aircraft Commander, Major John Barrett, Navigator and Captain Gerard Williamson. (Kokomo Tribune)

The B-58 Hustler was a high-altitude Mach 2 strategic bomber which served with the United States Air Force from 1960 to 1970. It was crewed by a pilot, navigator/bombardier and a defensive systems operator located in individual cockpits. The aircraft is a delta-winged configuration similar to the Convair F-102A Delta Dagger and F-106 Delta Dart supersonic interceptors.

The Hustler is 96 feet, 10 inches (29.515 meters) long, with a wing span of 56 feet, 10 inches (17.323 meters) and an overall height of 31 feet 5 inches (9.576 meters). The wing’s leading edge is swept back at a 60° angle and the fuselage incorporates the “area rule” which resulted in a “wasp waist” or “Coke bottle” shape for a significant reduction in aerodynamic drag. The airplane’s only control surfaces are two “elevons” and a rudder, and there are no flaps.

The B-58A was powered by four General Electric J79-GE-5 axial-flow afterburning turbojet engines, suspended under the wings from pylons. This was a single-shaft engine with a 17-stage compressor and 3-stage turbine, rated at 10,300 pounds of thrust (45.82 kilonewtons), and 15,600 pounds (69.39 kilonewtons) with afterburner. The J79-GE-5 was 16 feet, 10.2 inches (5.136 meters) long and 3 feet, 2.0 inches (0.965 meters) in diameter.

The bomber had a cruise speed of 610 miles per hour (981.7 kilometers per hour) and a maximum speed of 1,325 miles per hour (2,132.4 kilometers per hour). The service ceiling is 64,800 feet (19,751 meters). Unrefueled range is 4,400 miles (7,081 kilometers). Maximum weight is 168,000 pounds (76,203.5 kilograms).

The B-58 weapons load was a combination of a W-39 warhead, and/or Mk.43 or B61 nuclear bombs. The W-39 warhead, the same used with the Redstone IRBM or Snark cruise missile, was carried in a jettisonable centerline pod, which also carried fuel for the aircraft. The smaller bombs were carried on underwing hardpoints. For defense, there was a General Electric M61 Vulcan 20×102 mm six-barreled rotary cannon mounted in the tail, with 1,200 rounds of linked ammunition, controlled by the Defensive Systems Officer.

Convair B-58A-20 CF 61-2059 is in the collection of the Strategic Air and Space Museum, Ashland, Nebraska.

Convair B-58A-20-CF 61-2059, “Greased Lightning,” at the Strategic Air and Space Museum, Ashland, Nebraska. (SASM)

© 2017, Bryan R. Swopes

16 October 1956

Boeing 377 Stratocruiser N90943, Pan American World Airways' Sovereign of the Skies, seen over San Francisco, circa 1947. (University of Washington Libraries Digital Collections, TRA0138)
Boeing 377 Stratocruiser N90943, Pan American World Airways’ Sovereign of the Skies, seen over San Francisco, circa 1947. (University of Washington Libraries Digital Collections, TRA0138)

16 October 1956: Pan American World Airways’ Flight 6 was a scheduled around-the-world passenger flight. The final leg, Honolulu to San Francisco, was flown by a Boeing Model 377 Stratocruiser with civil registration N90943, and named Sovereign of the Skies.

The airplane had a flight crew of 7 and carried 24 passengers. The aircraft commander was Captain Richard N. Ogg, a veteran pilot with more than 13,000 flight hours accumulated over twenty years. First Officer George L. Haaker, Flight Engineer Frank Garcia, Jr., and Navigator Richard L. Brown completed the flight crew. The cabin crew were Purser Patricia Reynolds, who had been with Pan Am for over ten years, and Stewardesses Katherine S. Araki and Mary Ellen Daniel.

The flight from Honolulu to San Francisco was estimated to take 8 hours, 54 minutes. Captain Ogg had the airplane fueled for a total flight time of 12 hours, 18 minutes.

Pan American World Airlines’ Boeing 377 Stratocruiser, Clipper America. This airplane is similar to Sovereign of the Skies. (Boeing)

Flight 6 departed Honolulu at 8:24 p.m., Hawaii Standard Time, 15 October (06:24, 16 October, GMT), and climbed to 13,000 feet (3,962 meters) on course.

4 hours, 38 minutes after takeoff, Flight 6 requested a pre-planned climb to 21,000 feet (6,400 meters), at a point about half-way—in terms of flight time—between the departure point and destination, what is dramatically called “The Point of No Return” in suspense movies. (Actually, this is called the Equal Time Point: Taking into consideration forecast winds, the time to fly back to the departing point is the same as the time to continue toward the destination.)

On leveling at the new cruise altitude at 1:19 a.m. (HST), First Officer Haaker reduced engine power. The propeller for the Number 1 engine, the outside engine on the left wing, suffered a prop governor failure and began to overspeed, with engine r.p.m. actually exceeding the limits of its tachometer. This created a very dangerous condition: If the propeller turned fast enough, it could be torn apart by centrifugal force. (See This Day In Aviation, 22 March 1956, for an example.)

The crew was unable to feather the propeller, which would cause its four blades to turn parallel to the slip stream, and increasing the load on the engine while reducing aerodynamic drag. The engine and propeller continued to turn at dangerously high speed so Captain Ogg decided to force the engine to stop by cutting off its lubricating oil supply. This caused the engine to seize but the propeller continued to “windmill.”

The drag caused by the propeller slowed the airplane considerably and the three remaining engines had to run at high power for the Boeing 377 to maintain its altitude. The Number 4 engine (the outer engine on the right wing) was developing only partial power at full throttle. At 2:45 a.m., it began to backfire and had to be shut down.

The airplane began to descend toward the ocean’s surface.

With the drag of the windmilling Number 1 propeller and only two engines running, Sovereign of the Skies could fly at just 140 knots (161 miles per hour/259 kilometers per hour), not fast enough to reach San Francisco or to return to Honolulu before running out of fuel. The navigator estimated that they would run out of fuel 250 miles (402 kilometers) from land.

The United States Coast Guard kept a high endurance cutter on station between Hawaii and California, at a point known as Ocean Station November. This ship provided assistance with weather information, radio communications and was available to assist should an emergency arise aboard trans-Pacific airplanes.

USCGC Pontchartrain (WHEC 70) circa 1958. (U.S. Coast Guard)
USCGC Pontchartrain (WHEC 70) circa 1958. (U.S. Coast Guard)

On 16 October 1956, this cutter was USCGC Pontchartrain (WHEC 70), under the command of Commander William K. Earle, USCG. Pontchartrain was a 255-foot (77.7 meter) Lake-class patrol gunboat built by the U.S. Coast Guard ship yard at Curtiss Bay, Maryland, and commissioned 28 July 1945. The ship was redesignated as a high endurance cutter in 1948. Pontchartrain had a complement of 143 men.

The ship was 254 feet (77.42 meters) long, overall, with a beam of 43 feet, 1 inch (13.13 meters) and draft of 17 feet, 3 inches (5.25 meters). Its full load displacement was 1,978 tons (1,794 Metric tons). It was powered by a Westinghouse turbo-electric drive of 4,000 shaft horsepower and was capable on making 17.5 knots (20.41 miles per hour, or 32.41 kilometers per hour). Its maximum range was 10,376 miles (19,216 kilometers).

Pontchartrain was armed with a single 5-inch/38-caliber naval gun forward. It carried Hedgehog anti-submarine mortars and Mk 23 acoustic-homing antisubmarine torpedoes.

Captain Ogg notified Ponchartrain that he intended to ditch the airliner near the ship. The Coast Guard provided Captain Ogg with wind and wave information—five-foot (1.5 meter) swells, wind at eight knots (4 meters per second) from the northwest—and advised the best heading for ditching. The ship laid a trail of foam to mark this course.

Pan American World Airways Flight 6, a Boeing 377 Stratocruiser, ditches in the North Pacific Ocean near USCGC Pontchartrain (WHEC 70), 6:15 am., 16 October 1956. (U.S. Coast Guard)
Pan American World Airways Flight 6, a Boeing 377 Stratocruiser, ditches in the North Pacific Ocean near USCGC Pontchartrain (WHEC 70), 6:15 am., 16 October 1956. (U.S. Coast Guard)

At 6:15 a.m., at approximately 90 knots airspeed (104 miles per hour/167 kilometers per hour), the Boeing 377 landed on the water. A wing hit a swell, spinning the airplane to the left. The tail broke off and the airplane began to settle.

Pan American World Airways’ Boeing 377 Stratocruiser, Sovereign of the Skies, with its fuselage broken after ditching in the North Pacific Ocean, 16 October 1956. (Pan Am Historical Foundation/The New York Times)

Injuries were minor and all passengers and crew evacuated the airliner. They were immediately picked up by Pontchartrain.

Captain Ogg and Purser Reynolds were the last to leave the airplane.

Twenty minutes after touching down, at 6:35 a.m., Sovereign of the Skies sank beneath the ocean’s surface.

Sovereign of the Seas sinks into the Pacific Ocean, 16 October 1956. (U.S. Coast Guard)
Sovereign of the Skies sinks into the Pacific Ocean, 16 October 1956. (U.S. Coast Guard)

Pan American’s Sovereign of the Skies was a Boeing Model 377-10-29, construction number 15959, originally operated by American Overseas Airlines as Flagship Holland, and later, Flagship Europe. Pan Am acquired the airliner during a merger. On 16 October 1956, the airplane had accumulated 19,820:51 total time on the airframe (TTAF) since it was built.

The Boeing 377 was a large, four-engine civil transport which had been developed, along with the military C-97 Stratofreighter, from the World War II B-29 Superfortress long-range heavy bomber. It utilized the wings and engines of the improved B-50 Superfortress. The airplane was operated by a flight crew of four. It was a double-deck aircraft, with the flight deck, passenger cabin and galley on the upper deck and a lounge and cargo compartments on the lower. The airliner was pressurized, and could maintain Sea Level atmospheric pressure while flying at 15,500 feet (4,724 meters). The Model 377 could be configured to carry up to 100 passengers, or 28 in sleeping births.

The Stratocruiser was 110 feet, 4 inches (33.630 meters) long with a wingspan of 141 feet, 3 inches (43.053 meters) and overall height of 38 feet, 3 inches (11.659 meters). Empty weight was 83,500 pounds (37,875 kilograms) and the maximum takeoff weight was 148,000 pounds (67,132 kilograms). Sovereign of the Skies had a gross weight of 138,903 pounds (63,005 kilograms) when it took off from Honolulu.

Crew members of Pan American World Airways Flight 6 receive commendations for their service during the emergency of 16 October 1956. Left to right, Captain Richard N. Ogg; Navigator Richard L. Brown; Purser Patricia Reynolds; (unidentified); First Officer George L. Haaker; Flight Engineer Frank Garcia, Jr.. (Pan Am Historical Foundation/The New York Times)

The airliner was powered by four air-cooled, supercharged 4,362.49-cubic-inch-displacement (71.489 liter) Pratt & Whitney Wasp Major B6 four-row, 28-cylinder radial engines which had a Normal Power rating of 2,650 horsepower at 2,550 r.p.m., and 2,800 horsepower at 2,550 r.p.m. Maximum Continuous. It produced 3,250 horsepower at 2,700 r.p.m. for takeoff (3,500 horsepower with water injection). The engines drove four-bladed Hamilton-Standard Hydromatic, 24260 constant-speed propellers with a diameter of 17 feet, 0 inches (5.182 meters) through a 0.375:1 gear reduction. The Wasp Major B6 was 8 feet, 0.50 inches (2.451 meters) long, 4 feet, 7.00 inches (1.397 meters) in diameter, and weighed 3,584 pounds (1,626 kilograms).

The 377 had a cruise speed of 301 miles per hour (484 kilometers per hour) and a maximum speed of 375 miles per hour (604 kilometers per hour). During testing by Boeing, a 377 reached 409 miles per hour (658 kilometers per hour). Its service ceiling was 32,000 feet (9,754 meters) and the range was 4,200 miles (6,759 kilometers).

Boeing built 56 Model 377 Stratocruisers, with Pan American as the primary user, and another 888 military C-97 Stratofreighter and KC-97 Stratotankers.

A U.S. Coast Guard film of the incident can be seen at:

© 2018, Bryan R. Swopes

16 October 1910

Clément-Bayard No.2 at Issy-les-Moulineaux, 1910 (National Gallery of Canada)
Clément-Bayard No.2 at Issy-les-Moulineaux, 1910 (National Gallery of Canada)

16 October 1910: Maurice Clément-Bayard flew the dirigible, Clément-Bayard No. 2, from the Astra Clément-Bayard airship hangar at La Motte-Breuil, France, to Wormwood Scrubs, England, with six passengers. This was the first crossing of the English Channel by airship. The 244 mile (393 kilometer) distance was covered in less than six hours.

The Chronicle Annual Register reported,

The airship Clément-Bayard No. 2 travelled from near Paris to Wormwood Scrubbs between 6.55 a.m. and 1.25 p.m. Her average altitude was 200–300 metres, her average speed about 60 kil. hourly.

CHRONICLE OF EVENTS IN 1910, Part II, at Page 33

Gustave Adolphe Clément-Bayard
Gustave Adolphe Clément-Bayard

A contemporary newspaper article described the event:

LONDON, October 16.

The airship Clement Bayard II., carrying seven passengers, has made a remarkable journey from Compiegne, 52 miles to the north-east of Paris, to London, alighting at Shepherd’s Bush, five miles to the west of St. Paul’s Cathedral, in 6 hours, 11 minutes. The distance travelled was approximately 150 miles.

Later.

The Clement Bayard left Compiegne at 7.15 a.m. yesterday, the weather conditions being perfect at the time. Boulogne, about 75 miles distant, was reached three hours later, and then the trip across the Channel was made in three quarters of an hour.

French torpedo-boat destroyers were echelonned across the English Channel, and acted as guides to the airship as far as Folkestone, on the coast of Kent, and 71½ miles east south-east of London.

The Clement Bayard, however, outdistanced each torpedo-boat destroyer in turn. Tunbridge, 42 miles beyond Folkestone, was reached at a quarter past 12, and three-quarters of an hour later St. Paul’s Cathedral, 29½ miles from Tunbridge, was passed, the Clement Bayard on this part of the journey going faster than motor-cars following the airship. The remaining distance to Shepherd’s Bush was accomplished shortly afterwards.

M. Clement Bayard was on board his airship, and the passengers also included Mr. William Harvey De Cros, the Unionist member for Hastings, who represented the British Parliamentary Aerial Committee.

The Clement Bayard I. was completed in April last, and was on the eve of making its departure for London, when the French Government exercised its right, and acquired the airship. In August M. Clement Bayard made several successful flights in the Clement Bayard II., the building of which was started immediately after the French Government acquired the Clement Bayard I. In September, 1909, the “Daily Mail” completed, at a cost of £5,000, a garage for an airship on land belonging to the War office. It was constructed to accommodate the Clement Bayard airship, which was to make the journey through the air from Paris to London. The British Government has the option of purchasing the vessel.

The Mercury, Vol. XCIV, No. 12,658., Tuesday, 18 October 1910, Page 5, Column 2

This photograph shows the airship arriving at Wormwood Scrubs, 16 October 1910.
This photograph shows the airship arriving at Wormwood Scrubs, 16 October 1910. (Central News)

Maurice Clément-Bayard was the son of the company’s founder, Gustave Adolphe Clément-Bayard, and would succeed him after his father’s death.

The airship had been built for the Armée de Terre (the French Army), but because of the very high price, ₣200,000, it was not accepted. It was then sold to the British War Office for ₤18,000, more than twice the price the builders had offered to the French government. The British newspaper, The Daily Mail, contributed the cost of building an airship hangar.

After arriving in England, Clément-Bayard No. 2 was deflated for transport to another location. The airship was damaged in transit and was never repaired.

Clément-Bayard No. 2 was  76.5 meters (251 feet) long, with a diameter of 13.2 meters (43 feet). The dirigible had a volume of 6,500 cubic meters (229,545 cubic feet). It was powered by two water-cooled, normally-aspirated, 1,590.75-cubic-inch-dispalcement (26.068 liters) Clément-Bayard four-cylinder overhead cam engines, which produced 120 horsepower, each. These turned two, two-bladed, fixed-pitch laminated wood propellers with a diameter of 6 meters (19 feet, 8 inches) at 350 r.p.m.

According to an article in American Machinist,

. . . This engine is a four-cylinder, vertical, water-cooled motor, of the latest Clement racing type. The cylinders are cast separately and are copper jacketed; have a bore of 7.48 inches and a stroke of  9.05 inches[1,590.75 cubic inches, 26.07 liters], giving a horsepower estimated at over 200. The valves are mechanically operated and placed in the cylinder head. A magneto is used for ignition. The weight is 1100 pounds [499 kilograms].

There will be two of these motors used in the new Clement-Bayard airship being constructed for the British government; each motor having a propeller of its own, although when desired, both motors can run one propeller, or one motor can run two propellers.

American Machinist, Volume 33, Part I, 7 April 1910, at Page 645

Two 120 ch Clément-Bayard 4-cylinder engines installed on dirigible No. 2. (The Old Motor)
Two 120 ch Clément-Bayard 4-cylinder engines installed on dirigible No. 2. (The Old Motor)

The airship was debated in the British Parliament, with a question asked by Mr. Herbert Pike-Pease, M.P. (later, 1st Baron Daryngton): May I ask the right hon. Gentleman if he thinks the action of the War Office in regard to this airship was justified? If the airship was fit for service, why was it not used, and if it was not fit for service, why was it purchased?

John Edward bernard Seely, photographed by Walter Stoneman, 1924. (The National Portrait Gallery, London)
John Edward Bernard Seely, photographed by Walter Stoneman, 1924. (The National Portrait Gallery, London)

Colonel John Edward Bernard Seely, D.S.O., (Later, 1st Baron Mottistone, C.B., C.M.G., D.S.O., T.D., P.C., J.O., D.L.), the Secretary of State for War, replied, I think part of the last two supplementary questions is answered in some of the replies I have just given. Of course, it is the fact that the envelope of this balloon leaked so badly that it would have been very costly to have inflated it. No doubt mistakes were made on both sides, by hon. Gentlemen on both sides of the House, as well as by my Department, but we have not made half as many mistakes in this matter as our neighbours.

Mr. Pike Pease then asked,Was not the leakage known to the War Office before the ship was purchased?

Colonel Seely answered,It was before my time. There was a strong Committee of this House engaged in those transactions, and I understand they thought the airship was serviceable, and I suppose we thought it was when it was taken over. Mistakes must be made in a new matter of this kind. We have not made very many mistakes of a large kind in the matter of airships. We have been signally successful.

Earlier in the debate, Colonel Seely stated that,The engines are still available and are at the aircraft factory.

The Parliamentary Debates, 30 April 1913, at Page 1161.

© 2018, Bryan R. Swopes