All posts by Bryan Swopes

About Bryan Swopes

Bryan R. Swopes grew up in Southern California in the 1950s–60s, near the center of America's aerospace industry. He has had a life-long interest in aviation and space flight. Bryan is a retired commercial helicopter pilot and flight instructor.

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

15 October 1957

Clipper America at McMurdo Sound, 1957. (southpolestation.com)

15 October 1957: A Pan American World Airways Boeing Model 377 Stratocruiser, Clipper America, flies from Christchurch, New Zealand, to the United States Navy’s Antarctic research station on Ross Island in McMurdo Sound.

The flight was to test the feasibility of conducting commercial flights to support the U.S. Navy’s operations in the Antarctic. It originated with a load of passengers from NAS Quonset Point, Rhode Island, and flew to San Francisco, California, then on to Honolulu in the Hawaiian Islands. There, command of the aircraft was assumed by Pan Am’s Seattle Sector Chief Pilot, Captain Ralph Walter Savory, who was considered an expert in Arctic flying.

The Boeing Stratocruiser departed Honolulu and flew to Canton Island (named for a whaling ship that went aground there in 1854). Canton was a frequent waypoint for Pan Am’s transpacific flights. Clipper America remained there overnight, and continued to Fiji the next day. After another overnight stay, the airliner headed to Christchurch on the south island of New Zealand.

Airliner Lands in Antarctica

     MCMURDO SOUND, Antarctica, Oct. 15 (UP) — The Pan American Clipper America landed today at McMurdo Sound, completing the first commercial aircraft flight to Antarctica

     Capt. Ralph Savory, veteran of 23 years of arctic flying, lifted the 73-ton Pan American stratoclipper from the Christchurch runway at 10:25 a.m. and set course for McMurdo Sound.

     PASSENGERS on the 2,400-mile history-making flight included U.S. Ambassador to New Zealand Francis H. Russell; New Zealand Labor Minister J. K. McAlpine, and 36 U.S. Navy officers and men assigned to Geophysical Year scientific stations.

     The crew had two pretty stewardesses, reputedly the first women ever to reach such a southernly point on the “white continent” as the Ross Island Navy Station on McMurdo Sound.

     They were dark-haired Patricia Hepinstall, 25, former model for I. Magnin, San Francisco, and a native of 3752 Garnet St., Houston, Tex., and blonde Ruth Kelly, 28, former school teacher from Holyoke, Colo., who resembles Princess Grace.

     BOTH ARE BASED in San Francisco and are probably the most thrilled members of the plane’s complement. They were to ride in an American versus New Zealand dog sled race and judge a beard-growing contest among the men at McMurdo.

     Seabees and other Navy specialists had a last fling with card games and steaks 21,000 feet in the sky. In a few more hours they would spread to seven scientific stations for 18-month tours of duty on the blizzard-beaten continent.

     TRAVELING as a passenger was Navy Capt. William F. (Trigger) Hawkes, air officer for Rear Adm. George Dufek, commander of “Operation Deepfreeze.” Hawkes is considered to have more Antarctic flying experience than any other pilot.

The Honolulu Advertiser, 101st year, No. 34,083, Tuesday, 15 October 1957, Page 2, Columns 3–5

“Shown just after climbing down from their nice, warm Clipper at McMurdo Sound is the crew that was on Pan Am’s Antarctic flight. Kneeling are 2nd Officer Earl Lemon, Stewardess Pat Hepinstall, Flight Engineer George Coppin, and 2nd Officer Bob Finley. Standing are Captain Don McLennan, Purser John Bell, Sterwardess Ruth Kelly, Flight Engineer Al Loeffler, 1st Officer Roy Moungovan, and the Aircraft Commander, Captain Ralph Savory.” (Pam Am Museum Foundation)

Following this flight to the Antarctic, Captain Savory was asked for his opinion as to the route’s viability. Because there was no alternate airport should landing at McMurdo not be possible (because of weather, or some other factor), Savory said that it was too dangerous for commercial operations. No further flights were made.

Pan American World Airways Boeing Model 377 Stratocruiser, N1022V, Clipper America. (Boeing)

Pan American’s Clipper America was a Boeing Model 377-10-26 Stratocruiser, N1030V, serial number 15930. The airliner was delivered to Pan American on 30 March 1949 and named Clipper Southern Cross. Later the name was changed to Clipper Reindeer, and finally, Clipper America. (Nearly all of Pan Am’s Stratocruisers were named Clipper America at some time during their service with the airline.)

Marie Machris Westbrook. (Los Angeles Times)

On 27 July 1952, N1030V was operating as Flight 201 from Rio de Janeiro when a passenger cabin door opened at 12,000 feet (3,658 meters). A passenger, Mrs. Marie Elizabeth Machris Westbrook, was sucked out of her seat and fell to the Atlantic, below. The airliner safely returned to Rio. “Pan American officials were unable to explain how the door could have opened accidentally.” ¹ ²

N1030V was removed from service with Pan Am in 1961, and on 2 February 1962, delivered to Israeli Aircraft Industries, registered 4X-AOH. The airliner was converted to a military transport. In November 1962, it was placed in service with the Israeli Air Force, re-registered 4X-FOH, and finally, 4X-FPV.

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).

Pan American World Airways’ Boeing 377-10-26 Stratocruiser N1030V, circa 1952. The airliner is carrying the name Clipper Southern Cross. (R.A. Scholefield Collection)

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.

Captain Ralph Walter Savory, Pan American World Airways Master Pilot. (University of Alaska Fairbanks UAF-2008-31-16b)

Captain Ralph Walter Savory, Pan American World Airways Master Pilot, was born 14 October 1909, in Bennett Valley, Sonoma County, California. He was the second child of Walter Adrian Savory, a farmer, and Lillian Frances Philips Savory.

Ralph Savory attended Santa Rosa High School, where he was president of the aeronautics club. He graduated in 1928, then studied at Santa Rosa Junior College. He moved to San Francisco and worked as a mechanic to pay for flight lessons at “Speed” Johnson’s Flying School at San Mateo. He earned his private pilot certificate, No. 8105, in August 1929.

Ralph W. Savory’s Pilot’s Identification Card, issued by the Department of Commerce, 1 September 1929. (University of Alaska Fairbanks UAF-2009-31-7d)

Ralph W. Savory married Ms. Ida Scott (née Ida Elfreda Koffer) at Berkeley, California, 31 March 1934. The marriage was officiated by L.L. Cross Miu. They would have one child, Diane.

Savory and a friend bought a Curtiss Thrush. In 1933, Savory was issued a commercial pilot certificate. In 1935, he had the Thrush shipped to Alaska where he began flying in the remote parts of the territory (“bush flying”).

Ralph Savory’s Curtiss Thrush, 1935 (University of Alaska Fairbanks UAF-2009-31-1)

After a year gaining experience, Savory was hired as a pilot for Star Air Service (a predecessor of Alaska Airlines). He flew for Star for just under two years and then went to work for Pacific Alaska Airways in late 1938. This company was taken over by Pan American Airways.

During World War II, Pan American operated transport flights for the U.S. military. Flight crews were commissioned as reserve officers. Ralph Savory was commissioned a lieutenant, United States Naval Reserve, 22 July 1943, with date of precedence retroactive to 26 April 1943.

Following the war, Savory helped expand Pan Am’s operations in the Pacific Northwest and Alaska. He was designated as a Master Pilot and made sector chief pilot at Seattle.

In 1958 Captain Savory was one of the first of Pan Am’s pilots to be trained in the new turbojet-powered Boeing 707 airliner. As one of the world’s most experienced commercial pilots, Captain Savory retired in 1969.

Captain and Mrs. Savory in the cockpit of a Pan American World Airways Boeing 707-320, just prior to his final flight from London, England, to Seattle, Washington, U.S.A., 13 October 1969. He reached the mandatory retirement age effective at midnight on that date. (University of Alaska Fairbanks UAF-1993-28-1)

Mrs. Savory died in 1992. Two years later, Savory married Ms. Gladys T. Crum (née Gladys Theawilla Worden). She also died, in 2000.

Captain Ralph Walter Savory died at Spring Lake Village, Santa Rosa, California, 18 January 2010, at the age of 99 years.

¹ The Pittsburgh Press, Vol. 69, No. 35, Monday, 28 July 1952, Page 2, Columns 2 and 3

² For additional information about this incident, see Aviation Safety Network at  https://aviation-safety.net/database/record.php?id=19520727-1

© 2020, Bryan R. Swopes

15 October 1955

Lieutenant Gordon L. Gray, Jr., United States Navy, with record-setting Douglas YA4D-1 Skyhawk, Bu. No. 137820, at Edwards Air Force Base, 15 October 1955. (Navy Pilot Overseas)
Lieutenant Gordon L. Gray, Jr., United States Navy, with record-setting Douglas YA4D-1 Skyhawk, Bu. No. 137820, at Edwards Air Force Base, 15 October 1955. (Navy Pilot Overseas)

15 October 1955: At Edwards Air Force Base, California, Lieutenant Gordon L. (“Gordo”) Gray, Jr., United States Navy, set a Fédération Aéronautique Internationale (FAI) World Record For Speed Over a Closed Circuit of 500 Kilometers when he flew a pre-production Douglas Aircraft Company YA4D-1 Skyhawk light attack bomber, Bureau of Aeronautics serial number (Bu. No.) 137820, to an average speed of 1,118.7 kilometers per hour (695.128 miles per hour).¹

Douglas Aircraft Company YA4D-1 Skyhawk, Bu. No. 137820. (Navy Pilot Overseas)
Douglas Aircraft Company YA4D-1 Skyhawk, Bu. No. 137820. (Navy Pilot Overseas)

The Douglas A4D-1 Skyhawk is a single-place, single-engine, delta-winged light attack bomber designed for operation from aircraft carriers. It is 39 feet, 4 inches (11.989 meters) long with a wingspan of 27 feet, 6 inches (8.382 meters) and overall height of 15 feet (4.572 meters). Its empty weight is 8,400 pounds (3,810.2 kilograms). It was powered by a Curtiss-Wright J65-W-2, a licensed-production version of the Armstrong Siddeley Sapphire axial flow turbojet engine, which had a 13-stage compressor and 2-stage turbine. It produced 7,200 pounds of thrust (32.03 kilonewtons).

The A4D was in production from 1956 to 1979. 2,960 one- and two-place aircraft were built. The Skyhawk remained in service with the United States Navy until 2003.

Lieutenant Gordon L. Gray, Jr., U.S. Navy (thrid from left) with the Douglas Aircraft Company A4D team at Edwards AFB, California, 15 October 1955. (Navy Pilot Overseas)
Lieutenant Gordon L. Gray, Jr., U.S. Navy (third from left) with the Douglas Aircraft Company YA4D-1 Skyhawk team at Edwards AFB, California, 15 October 1955. (Navy Pilot Overseas)

¹ FAI Record File Number 8859

© 2017, Bryan R. Swopes

15 October 1952

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

15 October 1952: At Edwards Air Force Base, California, Douglas Aircraft Company test pilot William Barton (“Bill”) Bridgeman, while conducting high speed taxi tests, took a short flight in the new Douglas X-3. The experimental airplane flew about one mile (1.6 kilometers) over the dry lake bed before touching down. The official first flight would come five days later on 20 October.

In his biography, The Lonely Sky, Bill Bridgeman discussed his concerns about taking on the new project:

Then one morning Johnny called me to his office. "Bill, we would like you to take a look at the X-3. Maybe you would like to test her. She's in the final stages over in Hangar Three. Go over and take a look at the mock-up. See what you think. . ." On the ground floor in front of a door marked KEEP OUT. SECRET PROJECT MX656. . . . — The Lonely Sky, by William Bridgeman and Jacqueline Hazard, Cassell and Company Limited, London, 1956, Chapter XXIII at Page 276.
Mock-up of the Douglas X-3 (U.S. Air Force)
William B. Bridgeman with the Douglas X-3.
William B. Bridgeman with the Douglas X-3.

Then one morning Johnny called me to his office. “Bill, we would like you to take a look at the X-3. Maybe you would like to test her. She’s in the final stages over in Hangar Three. Go over and take a look at the mock-up. See what you think. . . ” On the ground floor in front of a door marked KEEP OUT. SECRET PROJECT MX656. . .

I climbed aboard. In order to get into the cockpit, the seat was mechanically lowered to the ground. There was a button to raise the elevator. It buzzed ominously as it very slowly lifted me into the nose. Visibility was extremely poor from her windows, they were faired-in exaggerations of the Skyrocket slits. It was impossible to see the ground. The thin, insecure looking wings were so far behind me that they were out of sight. It would take some weighing to decide whether or not I wanted to bet my life on the integrity of this ship. . .

I was afraid to take on this airplane. I was also afraid someone else would accept the challenge. And I was afraid that I would decide to accept it.

The Lonely Sky, William Bridgeman with Jacqueline Hazard, Cassell and Company Limited, London, 1956, Chapter XXIII at Page 276–278.

Douglas X-3 Stilleto

The Douglas X-3, serial number 49-2892, was built for the Air Force and the National Advisory Committee for Aeronautics (NACA) to explore flight in the Mach 1 to Mach 2 range. It was radically shaped, with a needle-sharp nose, very long thin fuselage and small straight wings. The X-3 was 66 feet, 9 inches (20.345 meters) long, with a wing span of just 22 feet, 8.25 inches (6.915 meters). The overall height was 12 feet, 6.3 inches (3.818 meters). The X-3 had an empty weight of 16,120 pounds (7,312 kilograms) and maximum takeoff weight of 23,840 pounds (10,814 kilograms).

It was to have been powered by two Westinghouse J46 engines, but when those were unsatisfactory, two Westinghouse XJ34-WE-17 engines were substituted. This was an axial flow turbojet with an 11-stage compressor and 2-stage turbine. It was rated at 3,370 pounds (14.99 kilonewtons) of thrust, and 4,900 pounds (21.80 kilonewtons) with afterburner. The XJ34-WE-17 was 14 feet, 9.0 inches (4.496 meters) long, 2 feet, 1.0 inch (0.635 meters) in diameter and weighed 1,698 pounds (770 kilograms).

The X-3 had a maximum speed of 706 miles per hour (1,136 kilometers per hour) and a service ceiling of 38,000 feet (11,582 meters).

Three-view drawing of the Douglas X-3. (NASA)
Three-view drawing of the Douglas X-3. (NASA)

The X-3 was very underpowered with the J34 engines, and could just reach Mach 1 in a shallow dive. The X-3′s highest speed, Mach 1.208, required a 30° dive. It was therefore never able to be used in flight testing the supersonic speed range for which it was designed.

The X-3 was prone to Inertial Roll Coupling, a newly discovered and very dangerous situation in which an aircraft goes out of control in all three axes. Because of its design characteristics—a very long, thin, fuselage, small wings and tail surfaces, and concentrated mass—the X-3 was very useful in exploring stability and control in the transonic range.

At one point, replacing the X-3’s turbojet engines with two Reaction Motors XLR-11 rocket engines was considered. Predictions were that a rocket-powered X-3 could reach Mach 4.2. However, with Mach 2 Lockheed F-104 becoming operational and North American Aviation’s X-15 hypersonic research rocketplane under construction, the idea was dropped. Technology had passed the X-3 by.

Two X-3 aircraft had been ordered from Douglas, but only one completed. In addition to Bill Bridgeman, the Douglas X-3 was flown by Air Force test pilots Major Chuck Yeager and Lieutenant Colonel Frank Everest, and NACA test pilot Joseph A. Walker.

After the flight test program came to an end in May 1956, the X-3 was turned over to the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.

The Douglas X-3 in flight, just a few feet above the dry lake bed at Edwards AFB, California. (Cropped from a LIFE Magazine image at Jet Pilot Overseas)
The Douglas X-3 in flight, just a few feet above the dry lake bed at Edwards AFB, California. (Cropped detail from a LIFE Magazine image at Jet Pilot Overseas)

© 2016, Bryan R. Swopes