Tag Archives: Pratt & Whitney Wasp SE

8 November 1935

Sir Charles Edward Kingsford Smith, MC, AFC (National Archives of Australia, A1200, L93634)
Sir Charles Edward Kingsford Smith, M.C., A.F.C. (National Archives of Australia, A1200, L93634)

On 8 November 1935: Sir Charles Edward Kingsford Smith, MC, AFC, and co-pilot John Thompson Pethybridge disappeared while flying Lady Southern Cross, a Lockheed Altair 8D Special, across the Andaman Sea from Allahabad, Indian Empire, to Singapore, Straits Settlements, a distance of approximately 2,200 miles (3,540 kilometers). The aviators were attempting to break a speed record for flight from England to Australia.

On 1 May 1937, about eighteen months after the disappearance, two Burmese fisherman found a landing gear assembly floating in the Andaman Sea near Kokunye Kyun (Aye Island), off the west coast of Burma. Lockheed was able to confirm that it was from Lady Southern Cross. The unit is the collection of the Powerhouse Museum, Sydney, Australia.

Landing gear assembly of Kingsford Smith’s Lady Southern Cross is in the collection of the Powerhouse Museum venue of the Museum of Applies Arts and Sciences. (MAAS Collection 94/64/1)

In 2009, searchers claimed to have located the wreck of the airplane near the island, but this has not been confirmed.

Lockheed 8-D Altair VH-USB, Lady Southern Cross, at Burbank, California, September 1935. (Unattributed)
Lockheed Altair 8D Special VH-USB, Lady Southern Cross, at Burbank, California, September 1935. The Altair is “. . . painted consolidated blue with silver wing and silver striping. . . .” (David Horn Collection No. 9099)

Kingsford Smith was a former Royal Air Force pilot and flight instructor. He had been a barnstormer, airline pilot, and gained world-wide fame for his trans-Pacific flights. From 31 May to 9 June 1928 he and Charles Ulm, Harry Lyon and James Warner had flown Southern Cross, a Fokker F.VIIB/3m, from Oakland, California to Brisbane, with stops at Hawaii and Fiji. In 1934, with Lady Southern Cross, he and Patrick Gordon Taylor flew from Australia to Hawaii and on to Oakland, California, arriving 4 November.

Charles Kingsford Smith’s Lady Southern Cross at Lockheed, Burbank, California. Note the navigator’s sighting lines on the elevators. (Code One Magazine/Lockheed Martin)

After the transpacific flight, Lady Southern Cross spent the next 11 months at Lockheed being repaired and overhauled. Kingsford Smith then flew it across the United States and had it transported to England aboard a ship.

Lady Southern Cross was a Lockheed Altair 8D Special, a single-engine monoplane with the fuselage, wings and tail surfaces built of spruce. The Altair had been modified from a 1930 Lockheed Sirius 8A Special, NR118W, c/n 152, which was an airplane with fixed landing gear. Lockheed designed a new wing which included retractable landing gear, operated by a hand crank from the cockpit. The Sirius and Altair were single-place utility transports. Kingsford Smith’s Altair was further modified with two cockpits in tandem. Lady Southern Cross was painted Consolidated Blue (a dark blue color) with silver accents.

Sir Charles Edward Kingsford Smith, MC, AFC, with the Lady Southern Cross at Croydon, 17 October 1935. The airplane's registration has been changed to G-ADUS.
Air Commodore Sir Charles Edward Kingsford Smith, Kt, MC, AFC, with the Lady Southern Cross at Croydon, 17 October 1935. The airplane’s registration has been changed to G-ADUS. (PHOTOSHOT)

Lady Southern Cross, designated a Lockheed Altair 8D Special, had a length of 27 feet, 10 inches (8.484 meters) with a wingspan of 42 feet, 9¼ inches (13.037 meters) and height of 9 feet, 3 inches (2.819 meters). The modified airplane had an empty weight of 3,675 pounds (1,667 kilograms) and a maximum gross weight of 6,700 pounds (3,039 kilograms).

The airplane’s standard Pratt & Whitney Wasp C1 engine was replaced at Kingsford Smith’s request with a more-powerful Pratt & Whitney Wasp SE, serial number 5222. The Wasp SE was an air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) single-row 9-cylinder radial engine with a compression ratio of 6:1. It was rated at 500 horsepower at 2,200 r.p.m., at an altitude of 11,000 feet (3,353 meters). The SE was a direct-drive, right-hand tractor engine which turned a two-bladed Hamilton Standard controllable-pitch metal propeller with a diameter of 9 feet, 0 inches (2.743 meters). The Wasp SE was 3 feet, 6.59 inches (1.082 meters) long, 4 feet, 3.44 inches (1.307 meters) in diameter and weighed 750 pounds (340.2 kilograms).

An Altair 8D  had a cruising speed of 175 miles per hour (282 kilometers per hour) and a maximum speed of 207 miles per hour (333 kilometers per hour) at 7,000 feet (2,134 meters). Contemporary news reports stated that Kingsford Smith had reached speeds of 230 miles per hour (370 kilometers per hour) while testing VH-USB.

Sir Charles Edward Kingsford Smith, MC, AFC, At Lympne Airport, Kent, England, 6 November 1935. This may be the last photograph ever taken of "Smithy". (International News Photos)
Air Commodore Sir Charles Edward Kingsford Smith, Kt, MC, AFC, at Lympne Airport, Kent, England, 6 November 1935. This may be the last photograph ever taken of “Smithy.” (International News Photos)

© 2017, Bryan R. Swopes

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8 March 1936

Boeing P-26 32-414 at Barksdale Field, 23 January 1934. (U.S. Air Force)

8 March 1936: First Lieutenant Robert Kinnaird Giovannoli, United States Army Air Corps, a test pilot assigned to the Material Division at Wright Field, Ohio, was killed when the right wing of his Boeing P-26 pursuit, serial number 32-414, came off in flight over Logan Field, near Baltimore, Maryland.

The Cincinnati Enquirer reported:

DAYTON HERO

Air Crash Victim.

Robert Giovannoli Dies At Baltimore Field

When Wing Of Plane Falls Off—Lexington, Ky., Man An Army Lieutenant.

     Baltimore, March 8—(AP)—Lieutenant Robert K. Giovannoli, 31 years old of Lexington, Ky., hero of the spectacular bombing plane crash during army tests at Dayton, Ohio, last October, was killed today in the crack-up of his army plane at Logan Field, here.

     Giovannoli’s single-seated pursuit plane lost its right wing coming out of a glide and hurtled down in a crazy spin from an altitude of less than 500 feet [ meters]. It rolled over after hitting the landing field and was demolished.

     Lieutenant Giovannoli received a medal for his heroism in rescuing two men from the flaming wreckage of the Boeing “flying fortress” after it crashed in the army bomber tests at Wright Field, Dayton.

     The Wright Field hero was taking off for the Middletown, Penn., air station when his plane plunged him to death at Logan Field.

QUIZ TO BE BEGUN.

     The flier had arrived here yesterday.

     Lieutenant Colonel H.C.K. Nuhlenberg, air officer of the Third Corps Area and in command of Logan Field, said an Army Board of Inquiry would be summoned promptly to investigate the fatal crash.

     Nuhlenberg, who had just landed at the field himself, said Giovannoli had gotten his craft under way and turned back to fly over the field at a low altitude.

     The wing of Giovannoli’s plane wrenched off, Nuhlenberg said, just as the craft was coming out of the glide and starting a zoom to regain altitude.

The Cincinnati Enquirer, Vol. XCV, No. 334, Monday, 9 March 1936,  at Page 7, Column 1

Lt. Robert K. Giovannoli

Lieutenant Giovannoli had been awarded the Soldier’s Medal and the Cheney Award for his heroic rescue of two men from the burning wreck of the Boeing Model 299, which had crashed on takeoff at Wright Field, 30 October 1935. His citation reads:

The President of the United States of America, authorized by Act of Congress, July 2, 1926, takes pleasure in presenting the Soldier’s Medal to First Lieutenant Robert K. Giovannoli, United States Army Air Corps, for heroism, not involving actual conflict with an enemy, displayed at Wright Field, Dayton, Ohio, 30 October 1935. When a Boeing experimental bomber crashed and burst into flames, Lieutenant Giovannoli, who was an onlooker, forced his way upon the fuselage and into the front cockpit of the burning plane and extricated one of the passengers. Then upon learning that the pilot was still in the cockpit, Lieutenant Giovannoli, realizing that his own life was in constant peril from fire, smoke, and fuel explosions, rushed back into the flames and after repeated and determined efforts, being badly burned in the attempt, succeeded in extricating the pilot from an entrapped position and assisted him to a place of safety.

General Orders: War Department, General Orders No. 4 (1936)

The wreck of the Boeing Model 299, NX13372, burns after the fatal crash at Wright Field, 30 October 1935. (U.S. Air Force)

Robert Kinnaird Giovannoli was born at Washington, D.C., 13 March 1904, the second of two sons of Harry Giovannoli, a newspaper editor, and Carrie Kinnaird Giovanolli. His mother died when he was six years old.

Robert Giovannoli, 1925. (The Kentuckian)

Giovannoli graduated from Lexington High School at Lexington, Kentucky, in 1920 and then attended the University of Kentucky, where, in 1925, he earned a Bachelor of Science degree in Mechanical Engineering (B.S.M.E.). He was a member of the Phi Delta Theta (ΦΔΘ) and Tau Beta Phi (ΤΒΦ) fraternities, treasurer of the sophomore class, and president of the American Institute of Electrical Engineers. He was employed by the General Electric Company at Schenectady, New York.

Giovannoli enlisted in the United States Army in 1927. After completing the Air Corps Primary Flying School at Brooks Field, and the Advanced Flying School at Kelly Field, both in San Antonio, Texas, he was commissioned as a second lieutenant in the Air Corps Reserve, 20 October 1928. Lieutenant Giovannoli was called to active duty 8 May 1930. In 1933, he was assigned to a one year Engineering School at Wright Field. He then was assigned to observe naval aircraft operations aboard USS Ranger (CV-4) in the Pacific Ocean, and had returned just a few days prior to the accident.

At the time of his death, Lieutenant Giovannoli had not yet been presented his medals.

First Lieutenant Robert Kinnaird Giovannoli was buried at the Bellevue Cemetery, Danville, Kentucky. In 1985, the Robert Kinnaird Giovannoli Scholarship was established to provide scholarships for students in mechanical engineering at the University of Kentucky College of Engineering.

The P-26, Air Corps serial number 32-414, was the last of three prototype XP-936 pursuits built by Boeing in 1932. Boeing’s chief test pilot, Leslie R. Tower, conducted the first flight of the type on 20 March 1932. Leslie Tower was one of the two men that Lieutenant Giovannoli had pulled from the burning Boeing 299.

The first of three Boeing Model 248 prototypes, XP-26 32-412. (Boeing)

The Boeing P-26 was a single-seat, single-engine monoplane. It was the first all-metal U.S. Army pursuit, but retained an open cockpit, fixed landing gear and its wings were braced with wire. The airplane was 23 feet, 7 inches (7.188 meters) long with a wingspan of 28 feet (8.534 meters). The empty weight of the prototype was 2,119 pounds (961.2 kilograms) and gross weight was 2,789 pounds (1,265.1 kilograms).

The Y1P-26 was powered by an air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney R-1340-21 (Wasp S2E), a single-row, nine-cylinder radial engine. The P-26A and P-26C were powered the Pratt & Whitney R-1340-27 (Wasp SE), while the P-26B used a more powerful, fuel-injected R-1340-33 (Wasp D2). Each of these engines were direct drive and had a compression ratio of 6:1. The engine was surrounded by a Townend Ring which reduced aerodynamic drag and improved engine cooling.

The R-1340-21 had a Normal Power rating of 600 horsepower at 2,200 r.p.m. at 6,000 feet (1,829 meters); 500 horsepower at 2,200 r.p.m. at 11,000 feet (3,353 meters); and 500 horsepower at 2,000 r.p.m. for takeoff. It required 87-octane gasoline. The –21 had a diameter of 51.44 inches ( meters) and weighed 715 pounds (324 kilograms).

The R-1340-27 had a Normal Power and Takeoff power rating of 570 horsepower at 2,200 r.p.m., to 7,500 feet (1,524 meters), using 92-octane gasoline. The –27 was 3 feet, 7.25 inches (1.099 meters) long, 4 feet, 3.50 inches (1.308 meters) in diameter and also weighed 715 pounds (324 kilograms).

The R-1340-33 was rated at 575 horsepower at 2,200 r.p.m. to 10,000 feet (3,048 meters), and 600 horsepower at 2,120 r.p.m. for Takeoff, with 87-octane gasoline. It was 3 feet, 10.75 inches (1.187 meters) long, with the same diameter as the –27. It weighed 792 pounds (359 kilograms).

The engines drove a two-bladed, Hamilton Standard adjustable-pitch propeller.

The pursuit had a maximum speed of 227 miles per hour (365 kilometers per hour) at 10,000 feet (3,048 meters), and a service ceiling of 28,900 feet (8,809 meters).

As a pursuit, it would be armed with two air-cooled Browning M1919 .30-caliber machine guns, synchronized to fire forward through the propeller arc.

Boeing built 136 production P-26s for the Air Corp and another 12 for export. Nine P-26s remained in service with the Air Corps at the beginning of World War II.

A Boeing P-26 at Wright Field, Ohio. (U.S. Air Force)
A Boeing P-26 at Wright Field, Ohio. (U.S. Air Force)

© 2018, Bryan R. Swopes

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