15 April 1952: At 11:08 a.m., Boeing’s Chief of Flight Test, Alvin M. “Tex” Johnston, and Lieutenant Colonel Guy M. Townsend, U.S. Air Force, ran all eight turbojet engines to full power and released the brakes on the YB-52 Stratofortress prototype, 49-231.

With an awesome eight-engine roar, the YB-52 sprang forward, accelerating rapidly, wings curving upward as they accepted the 235,000-pound initial flight gross weight. At V₂ (takeoff speed) the airplane lifted off the runway, because of the 6-degree angle of incidence of the wing, and at 11:08 a.m. we were airborne. The initial flight of the YB-52 had begun.

—Tex Johnston: Jet-Age Test Pilot, by A.M. “Tex” Johnston with Charles Barton, Smithsonian Books, Washington, D.C., 1992, Chapter 13 at Pages 397–398.

The YB-52 remained over the Seattle area for approximately 40 minutes while Johnson and Townsend ran through a series of systems checks. When completed, they climbed to 25,000 feet (7,620 meters) and flew the new bomber to Larson Air Force Base at Moses Lake, Washington, where they stayed airborne for continued testing. The Stratofortress finally touched down after 3 hours, 8 minutes—the longest first flight in Boeing’s history up to that time. Johnston radioed that the airplane performed exactly as the engineers had predicted.

The YB-52 had actually been ordered as the second of two XB-52s, but modifications and additional equipment installed during building resulted in enough differences to warrant a designation change. The first XB-52, 49-230, should have been the first to fly, but it was damaged during ground testing.

The Boeing XB-52 and YB-52 were prototypes for a very long range strategic bomber. Both were built with a tandem cockpit for the pilot and co-pilot, similar to the earlier B-47 Stratojet. The wings were swept and mounted high on the fuselage (“shoulder-mounted”). The eight turbojet engines were in in two-engine nacelles mounted on pylons, below and forward of the wings. This had the effect of preventing the airplane’s center of gravity from being too far aft, and also provided cleaner air flow across the wings. The B-52’s landing gear has four main struts with two wheels, each. They can turn to allow the airplane to face directly into the wind while the landing gear remain aligned with the runway for takeoff and landing. With the landing gear under the fuselage, the wings could be constructed with greater flexibility.

The YB-52 was 152 feet, 8 inches (46.533 meters) long with a wingspan of 185 feet, 0 inches (56.388 meters). The prototype’s overall height was 48 feet, 3.6 inches (14.722 meters). The vertical fin could be folded over to the right so that the B-52 could fit into a hangar. The total wing area was 4,000 square feet (371.6 square meters). The wings’ leading edges were swept aft to 36° 54′. Their angle of incidence was 6° and there was 2° 30′ dihedral. The YB-52 had an empty weight of 155,200 pounds (70,398 kilograms) and gross weight of 405,000 pounds (183,705 kilograms).

The YB-52 was powered by eight Pratt & Whitney Turbo Wasp YJ57-P-3 turbojet engines. The J57 was a two-spool, axial-flow turbojet developed from an experimental turboprop engine. It had 16-stage compressor section (9 low- and 7-high-pressure stages), 8 combustors and a 3-stage turbine section (1 high- and 2 low-pressure stages). The YJ57-P-3s had a continuous power rating of 8,700 pounds of thrust (38.70 kilonewtons). The YJ57-P-3 was 183.5 inches (4.661 meters) long, 41.0 inches (1.041 meters) in diameter and weighed 4,390 pounds (1,991 kilograms).

The YB-52 had a cruise speed of 519 miles per hour (835 kilometers per hour) and maximum speed of 611 miles per hour (983 kilometers per hour) at 20,000 feet (6,096 meters). Its range was 7,015 miles (11,290 kilometers).

The two prototypes were unarmed.

The B-52 was produced by Boeing at its plants in Seattle and Wichita from 1952 to 1962, with a total of 744 Stratofortresses built. The last version, the B-52H, entered service with the Strategic Air Command in 1960. The final B-52, B-52H-175-BW Stratofortress 61-0040, was rolled out at Wichita, Kansas, 26 October 1962. This airplane remains in service with the United States Air Force. The newest B-52 in service, 61-0040 is 62 years old and has flown more than 21,000 hours.

All previous versions, B-52A through B-52G, have long been retired to The Boneyard and scrapped. Of the 102 Boeing B-52H Stratofortress bombers, 76 are still in the active inventory. One, 61-007, known as Ghost Rider, was recently taken from Davis-Monthan and after an extensive restoration and update, returned to service.

The YB-52 prototype was retired to the National Museum of the United States Air Force in the late 1950s. By the mid-60s it was determined to be excess and was scrapped.

© 2019, Bryan R. Swopes

8 April 1945: Wee Willie, a Flying Fortress heavy bomber, left its base at Air Force Station 121 (RAF Bassingbourne, Cambridgeshire, England), on its 129th combat mission over western Europe. The aircraft commander was 1st Lieutenant Robert E. Fuller, U.S. Army Air Forces.

Wee Willie was a B-17G-15-BO, serial number 42-31333, built by the Boeing Airplane Company’s Plant 2, Seattle, Washington. It was delivered to the United States Army Air Forces at Cheyenne, Wyoming on 22 October 1943, and arrived at Bassingbourne 20 December 1943. It was assigned to the 322nd Bombardment Squadron (Heavy), 91st Bombardment Group (Heavy), 1st Air Division, 8th Air Force. The identification letters LG W were painted on both sides of its fuselage, and a white triangle with a black letter A on the top of its right wing and both sides of its vertical fin.

On 8 April 1945, the 322nd Bombardment Squadron was part of an attack against the locomotive repair facilities at the railroad marshaling yards in Stendal, Saxony-Anhalt Germany. The squadron was bombing through clouds using H2S ground search radar to identify the target area. Antiaircraft gunfire (flak) was moderate, causing major damage to four B-17s and minor damage to thirteen others. Two bombers from the 91st Bomb Group were lost, including Wee Willie.

The Missing Air Crew Report, MACR 13881, included a statement  from a witness:

We were flying over the target at 20,500 feet [6,248 meters] altitude when I observed aircraft B-17G, 42-31333 to receive a direct flak hit approximately between the bomb bay and #2 engine. The aircraft immediately started into a vertical dive. The fuselage was on fire and when it had dropped approximately 5,000 feet [1,524 meters] the left wing fell off. It continued down and when the fuselage was about 3,000 feet [914.4 meters] from the ground it exploded and then exploded again when it hit the ground. I saw no crew member leave the aircraft or parachutes open.

The pilot, Lieutenant Fuller, did escape from the doomed bomber. He was captured and spent the remainder of the war as a Prisoner of War. The other eight crew members, however were killed.

1st Lieutenant Robert E. Fuller, O-774609, California. Aircraft Commander/Pilot—Prisoner of War

2nd Lieutenant Woodrow A. Lien, O-778858, Montana. Co-pilot—Killed in Action

Technical Sergeant Francis J. McCarthy, 14148856, Tennessee. Navigator—Killed in Action

Staff Sergeant Richard D. Proudfit, 14166848, Mississippi. Togglier—Killed in Action

Staff Sergeant Wylie McNatt, Jr., 38365470, Texas. Flight Engineer/Top Turret Gunner—Killed in Action

Staff Sergeant William H. Cassiday, 32346219, New York. Ball Turret Gunner—Killed in Action

Staff Sergeant Ralph J. Leffelman, 19112019, Washington. Radio Operator/Top Gunner—Killed in Action

Staff Sergeant James D. Houtchens, 37483248, Nebraska. Waist Gunner—Killed in Action

Sergeant Le Moyne Miller, 33920597, Pennsylvania. Tail Gunner—Killed in Action

Wee Willie was the oldest B-17G still in service with the 91st Bomb Group, and the next to last B-17 lost to enemy action by the group before cessation of hostilities. The War in Europe came to an end with the unconditional surrender of Germany just 30 days later, 7 May 1945.

© 2019, Bryan R. Swopes

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 [152 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

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)

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.

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 sent to observe naval aircraft operations aboard USS Ranger (CV-4) in the Pacific Ocean. He 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 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 3 feet, 3.44 inches (1.307 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, the P-26 was 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.

© 2019, Bryan R. Swopes

26 February–2 March 1949: A Boeing B-50A Superfortress, Air Force serial number 46-010, named Lucky Lady II, flew from Carswell Air Force Base, Fort Worth, Texas, and with inflight refueling, circumnavigated the Earth non-stop, landing back at Carswell after 94 hours, 1 minute. The bomber had traveled 23,452 miles (37,742 kilometers).

Lucky Lady II was the backup aircraft for this flight, but became primary when the first B-50, Global Queen, had to abort with engine problems. It was a standard production B-50A-5-BO (originally designated B-29D) with the exception of an additional fuel tank mounted in its bomb bay.

The aircraft commander was Captain James G. Gallagher, with 1st Lieutenant  Arthur M. Neal as second pilot. Captain James H. Morris was the copilot. In addition to the three pilots, the flight was double-crewed, with each man being relieved at 4-to-6 hour intervals. The navigators were  Captain Glenn E. Hacker and 1st Lieutenant Earl L. Rigor, and the radar operators were 1st Lieutenant Ronald B. Bonner and 1st Lieutenant William F. Caffrey. Captain David B. Parmalee was project officer for this flight and flew as chief flight engineer, with flight engineers Technical Sergeant Virgil L. Young and Staff Sergeant Robert G. Davis. Technical Sergeant Burgess C. Cantrell and Staff Sergeant Robert R. McLeroy were the radio operators. Gunners were Technical Sergeant Melvin G. Davis and Staff Sergeant Donald G. Traugh Jr.

Four inflight refuelings were required using the looped hose method. Two KB-29M tankers of the 43d Air Refueling Squadron were placed at air bases along the Lucky Lady II‘s route, at the Azores, Saudi Arabia, the Philippine Islands and Hawaiian Islands. The KB-29 flew above the B-50 and lowered a cable and drogue. This was captured by equipment on the bomber and then reeled in, bringing along with it a refueling hose. The hose was attached to the B-50’s refueling manifold and then fuel was transferred from the tanker to the bomber’s tanks by gravity flow.

Each refueling occurred during daylight, but weather made several transfers difficult. One of the two tankers from Clark Field in The Philippines, 45-21705, crashed in bad weather when returning to base, killing the entire 9-man crew.

On their arrival at Carswell, the crew of Lucky Lady II was met by Secretary of the Air Force W. Stuart Symington, Jr., General Hoyt S. Vandenberg, Chief of Staff of the Air Force, General Roger M. Ramey, commanding 8th Air Force, and Lieutenant General Curtis E. LeMay, Strategic Air Command. Each member of the crew was awarded the Distinguished Flying Cross. They also were awarded the Mackay Trophy for the most meritorious flight of the year.

At 11:25 a.m., 13 August 1950, B-50A 46-010, under the command of  Captain Warren E. Griffin, was on a maintenance test flight and returning to its base, Davis-Monthan AFB, Tucson, Arizona  when all four engines failed. Unable to reach the runways, Captain Griffin landed in the desert approximately two miles southeast. Though the landing gear were down, the bomber was severely damaged with all four propellers bent, the belly dented and its tail breaking off. The 11-man crew were uninjured except for the bombardier, 1st Lieutenant Theodore Hastings, who was scratched by cactus which entered the cockpit through the broken Plexiglas nose.

The Superfortress was damaged beyond economical repair and was stricken from the Air Force inventory (“written off”). The unrestored fuselage of Lucky Lady II is at the Planes of Fame Air Museum, Chino, California.

© 2016, Bryan R. Swopes

8 February 1949: One of the two Boeing XB-47 Stratojet prototypes made a record-breaking transcontinental flight from Moses Lake Air Force Base, Washington, to Andrews Air Force Base, Maryland, in 3 hours, 46 minutes. The XB-47 departed Moses Lake at 10:22 a.m., Eastern Standard Time (15:22 UTC), and crossed over the Andrews Field control tower at 13,000 feet (3,962 meters) at 2:08 p.m. (19:08 UTC). Majors Russell Ellsworth (“Russ”) Schleeh and Joseph Woodrow Howell beat the official U.S. national record set two years earlier by Colonel William Haldane Councill in a specially-prepared Lockheed P-80A Shooting Star.¹

Major Schleeh was the Deputy Chief of Bomber Operations in the Flight Test Division of the Air Material Command, Wright-Patterson Air Force Base, Dayton, Ohio.

The Los Angeles Times reported:

Jet Bomber Spans Nation in 3 Hours 46 Minutes

New Plane Averages 607.2 m.p.h. to Make Fastest Coast-to-Coast Journey on Record

     Washington, Feb. 8 (AP)—An arrow-shaped XB-47 jet bomber streaked through the stratosphere at an average speed of 607.2 miles an hour today in the fastest transcontinental flight ever made.

     The bomber, rated as “light” despite its 125,000 pounds, flew 2289 miles from Moses Lake (Wash.) Air Base to Andrews Field, Md., a few miles south of the capital, in 3h. 46m.

     The pace was 27 minutes shorter in time and 23 miles faster in average speed than the official record of 4h. 13m. at 584 m.p.h. established by Col. William H. Council [sic] in an F-80 Shooting Star two years ago.

     No Official Claim

     However, the Air Force will claim no record. The flight was not timed officially and it did not fly the recognized contest course. The recognized course—the one Col. Council flew—is Los Angeles to new York, 2464 miles.

     The XB-47 is a six-engine, swept wing bomber built by Boeing Airplane Co. at Seattle, known as the Stratojet, it is the Air Force’s first bomber designed for speeds in excess of 600 miles an hour.

     The XB-47 is the plane to which Air Force Secretary Symington referred last fall when he mentioned a jet bomber running away from jet fighters. Ten XB-47s are to be built at Boeing’s Wichita (Kan.) plant, where about half of all the B-29s were built during the war.

     Maj. Russell E. Schleeh, pilot, and Maj. Joseph W. Howell, co-pilot, both said the flight was strictly routine. They were comfortable in a new type flying suit being tested by the Materiel Command, used oxygen all the way, and navigated by radio compass on a great circle course which took them 20 miles south of Chicago.

     The first  part of the flight was at 32,000 feet. Later they moved up to 37,000 feet. The pressurized cabin was maintained at 23,000 feet. During one hour they covered 648 miles.

     In addition to six J-35 turbo-jet engines built by General Electric Co. at Lynn, Mass., which gave a total of 24,000 pounds of thrust, the Stratojet can use 18 rockets each capable of delivering 1000 pounds of thrust for a few seconds. The rockets were not carried today.

     The XB-47 carries a parachute in its tail to help it stop quickly.

—Los Angeles Times, Vol. LXVIII, 9 February 1949, Page 1, Columns 6 and 7, and Page 3, Columns 1–8

Designed as a strategic bomber, the B-47 could fly higher and faster than jet fighters of the time, and it was also highly maneuverable. The XB-47 (Boeing Model 450) was flown by a two-man crew in a tandem cockpit. It was 107 feet, 6 inches (32.766 meters) long with a wingspan of 116 feet (35.357 meters). The top of the vertical fin was 27 feet, 8 inches (8.433 meters) high. The wings were shoulder-mounted with the leading edges swept at 35°.

The first prototype, 46-065, was powered by six General Electric J35-GE-7 axial flow turbojet engines in four pods mounted on pylons below the wings. The J35 was a single-spool, axial-flow turbojet engine with an 11-stage compressor and single-stage turbine. The J35-GE-7 was rated at 3,750 pounds of thrust (16.68 kilonewtons) at 7,700 r.p.m. (static thrust, Sea Level). The engine was 14 feet, 0.0 inches (4.267 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,400 pounds (1,089 kilograms). (The second prototype, 46-066, was completed with J47 engines. 46-065 was later retrofitted with these engines.)

The XB-47 prototype had a maximum speed of 502 knots (578 miles per hour/930 kilometers per hour/0.80 Mach) at 15,000 feet (4,572 meters). The combat speed was 462 knots (532 miles per hour/856 kilometers per hour/0.70 Mach) at 35,000 feet (10,668 meters). The prototype’s empty weight was 74,623 pounds (33,848 kilograms), while its maximum takeoff weight was 162,500 pounds (73,709 kilograms). It required a ground run of 11,900 feet (3,627 meters), or 4,800 feet (1,463 meters) with JATO assist. The bomber could climb at a rate of 3,650 feet per minute (18.5 meters per second) at Sea Level, at combat weight and maximum power. The service ceiling was 37,500 feet (11,430 meters). The XB-47 carried 9,957 gallons (37,691 liters) of fuel. The combat radius was 1,175 nautical miles (1,352 statute miles/2,176 kilometers) with a 10,000 pound (4,536 kilogram) bomb load.

Planned armament (though the XB-47s were delivered without it) consisted of two .50-caliber machine guns in a tail turret, with 1,200 rounds of ammunition, and 10,000 pounds (4,536 kilograms) of bombs.

The Stratojet was 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 on pylons, , mounted forward of the leading edge.

2,032 B-47s were built by Boeing Wichita, Douglas Tulsa and Lockheed Marietta. They served the United States Air Force from 1951 to 1977.

The very last B-47 flight took place 18 June 1986 when B-47E-25-DT, serial number 52-166, was flown from the Naval Air Weapons Center China Lake to Castle Air Force Base to be placed on static display.

XB-47 45-065 stalled while landing at Larson Air Force Base, near Moses Lake, Washington, 18 August 1951. The crew of three escaped uninjured. The airplane was damaged beyond repair. The second prototype, XB-47 46-066, is in the collection of the Air Force Flight Test Museum, Edwards Air Force Base, California.

¹ See This Day in Aviation for 26 January 1946 at: https://www.thisdayinaviation.com/26-january-1946/

© 2023, Bryan R. Swopes

8 February 1933: Boeing test pilot Leslie R. (“Les”) Tower and United Air Lines Captain Louis C. Goldsmith made the first flight of the Boeing Model 247, NX13300, a twin-engine airline transport, at Boeing Field, Seattle, Washington. The first flight lasted 40 minutes and Tower was quite pleased with the airplane. He took it up a second time later in the day.

The 247 is considered to be the first modern airliner because of its all-metal semi-monocoque construction, cantilevered wing and retractable landing gear. It was 50 miles per hour (80.5 kilometers per hour) faster than its contemporaries, and could climb on one engine with a full load.

The airplane was built at Boeing’s Oxbow factory on the Duwamish River, then barged to Boeing Field where it was assembled and tested. The 247 was originally named “Skymaster,” but this was soon dropped.

Two months after the first flight, the first production 247, NC13301, was placed in service with United Air Lines. It was the first of ten 247s bought by United.

The Model 247 was operated by a pilot, co-pilot and a flight attendant and carried up to ten passengers. The airplane was 51 feet, 5 inches (15.672 meters) long, with a wingspan of 74 feet, 1 inch (22.581 meters) and overall height of 12 feet, 5 inches (3.785 meters). The empty weight was 8,921 pounds (4,046.5 kilograms) with a maximum takeoff weight of 16,805 pounds (7,622.6 kilograms).

The Duralamin skin panels were anodized, rather than painted, for corrosion protection. This saved weight, and resulted in the 247’s characteristic gray-green color.

The airliner was powered by two air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liters) Pratt & Whitney Wasp S1H1-G nine-cylinder radial engines with a compression ratio of 6.03:1. The S1H1-G had a Normal power rating of 550 horsepower at 2,200 r.p.m., to 8,000 feet (2,438 meters), and 600 horsepower at 2,250 r.p.m. for Takeoff. They drove three-bladed Hamilton Standard constant-speed propellers through a 3:2 gear reduction. The Wasp S1H1-G was 3 feet, 11.80 inches (1.214 meters) long, 4 feet, 3.61 inches (1.311 meters) in diameter, and weighed 930 pounds (422 kilograms).

The Boeing 247 had a maximum speed of 200 miles per hour (321.9 kilometers per hour) with a cruising speed of 188 miles per hour (302.6 kilometers per hour. It had a range of 745 miles (1,199 kilometers) and a service ceiling of 25,400 feet (7,742 meters).

75 Model 247s were built. 60 were bought by Boeing Air Transport.

[Note: the windshield was canted forward to prevent instrument panel lighting from reflecting into the cockpit at night. Unfortunately, ground lighting was reflected instead. This was soon changed to a rearward slant and resulted in a slight increase in speed.]

© 2019, Bryan R. Swopes

24 January 1963: A Boeing B-52C-40-BO Stratofortress, 53-0406, call sign “Frosh 10,” of the 99th Bombardment Wing, Heavy, was conducting a low-altitude training flight using terrain-following radar. Eight crewmen were aboard. Flying at or below 500 feet (152 meters) above ground level (AGL) and at 280 knots (322 miles per hour, 519 kilometers per hour) the bomber encountered wind gusts of up to 40 knots (21 meters per second).

As the turbulence became severe, the aircraft commander, Lieutenant Colonel Dante E. Bulli, began a climb to avoid it. At approximately 2:52 p.m., EST, however, the vertical fin attachment failed and the B-52 began rolling to the right and pitching down. Colonel Bulli, unable to control the airplane, ordered the crew to abandon the bomber.

B-52C 53-0406 crashed into the west side of Elephant Mountain, a 3,774 foot (1,150 meters) forest-covered mountain, 6 miles (10 kilometers) from Greenville, Maine. Only three men, Colonel Bulli, co-pilot Major Robert J. Morrison and navigator Captain Gerald J. Adler, were able to get out of the B-52, but Major Morrison died when he hit a tree. Lieutenant Colonel Joe R. Simpson, Jr., Major William W. Gabriel, Major Robert J. Hill, Jr., Captain Herbert L. Hansen, Captain Charles G. Leuchter and Technical Sergeant Michael F. O’Keefe were also killed.

Large sections of Frosh 10 are still on Elephant Mountain. The crash site is a popular hiking destination.

The Boeing B-52 Stratofortress had been designed as a very high altitude penetration bomber, but changes in Soviet defensive systems led to a change to very low altitude flight as a means of evading radar. This was subjecting the airframes to unexpected stresses. Several crashes resulted from structural failures during turbulence.

Less than one year later, Boeing was conducting flight tests of the B-52 in turbulence, using a highly-instrumented B-52H. That airplane also lost its vertical fin when it encountered severe turbulence in Colorado. The Boeing test pilots aboard were able to save the bomber and landed it six hours later.

Dante E. Bulli was born at Cherry, Illinois, 17 July 1922, the second child of Italian immigrants Giovanni Bulli, a salesman, and Anna Gareto Bulli.  He attended Hall High School before working on the aircraft assembly lines of the Lockheed Aircraft Company in California.

Bulli enlisted as an aviation cadet in the U.S. Army Air Corps in 1942. He was commissioned as a second lieutenant, Army of the United States, 5 December 1943, and promoted to first lieutenant, 5 December 1946.

In 1947 Lieutenant Bulli married Miss Evelyn Lewis, also from Cherry, Illinois.

“Dan” Bulli was a combat veteran of World War II, the Korean War and the Vietnam War. He flew B-24 Liberators, the B-29 Superfortress and B-52 Stratofortress. He retired from the Air Force in 1974.

Colonel Dante E. Bulli died at Omaha, Nebraska, 30 December 2016, at the age of 94 years.

© 2018, Bryan R. Swopes

12 January 1937: Western Air Express Flight 7, a Boeing 247D airliner, NC13315, had originated at Salt Lake City, Utah, and after a stop at Las Vegas, Nevada, continued on toward Union Air Terminal, Burbank, California. Aboard were a crew of three and ten passengers.

In fog and falling snow, Captain William Walker Lewis and co-pilot Clifford P. Owens crossed over Saugus, California,

“. . . at 5,200 feet [1,585 meters], aircraft was already 300 feet [91 meters] too low. . . Pilot tried to contact Burbank without any success. Due to low visibility caused by fog, pilot did not realize he was flying at an insufficient altitude. In a descent rate of 525 feet per minute [2.667 meters per second], aircraft hit Pinetos Peak.”

— Bureau of Air Commerce report.

According to statements after the accident, Captain Lewis suddenly saw a ridge immediately ahead, and unable to avoid it, cut his engines and raised the nose in an attempt to reduce the impact. The accident occurred at 11:07 a.m., Pacific Time.

The crash was heard by patients at the Olive View Sanitorium and ranchers on the north side of the mountains. Two hours later, passenger Arthur S. Robinson arrived at the hospital and said, “Get help up there for the twelve others. It was a forced landing—they’re all injured but I believe they’re all alive.”

One passenger, James A. Braden, president of the Braden-Sutphin Ink Co., of Cleveland, Ohio, was killed immediately. The co-pilot, Owens, and three more of the passengers died of injuries within the next several days.

One of those who died was famed adventurer and film maker Martin Johnson. His wife, Osa Johnson, was also aboard Flight 7 and was seriously injured. Another survivor, Robert T. Anderson, would later own Pea Soup Anderson, a famous restaurant in Buellton, California.

The Boeing Model 247 is considered to be the first modern airliner because of its all-metal, semi-monocoque construction, cantilevered wing and retractable landing gear. It was 50 miles per hour (80 kilometers per hour) faster than its contemporaries, and could climb on one engine with a full load.

The Model 247 was operated by a pilot, co-pilot and a flight attendant and carried up to ten passengers. The airplane was 51 feet, 5 inches (15.672 meters) long, with a wingspan of 74 feet, 1 inch (22.581 meters) and overall height of 12 feet, 5 inches (3.785 meters). The empty weight was 8,921 pounds (4,046.5 kilograms) with a maximum takeoff weight of 16,805 pounds (7,622.6 kilograms).

The Duralamin skin panels were anodized, rather than painted, for corrosion protection. This saved weight, and resulted in the 247’s characteristic gray-green color.

The airliner was powered by two air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liters) Pratt & Whitney Wasp S1H1-G nine-cylinder radial engines with a compression ratio of 6.03:1. The S1H1-G had a Normal Power rating of 550 horsepower at 2,200 r.p.m., to 8,000 feet (2,438 meters), and 600 horsepower at 2,250 r.p.m. for Takeoff. They drove three-bladed Hamilton Standard constant-speed propellers through a 3:2 gear reduction, when installed on the 247D. The Wasp S1H1-G was 3 feet, 11.80 inches (1.214 meters) long, 4 feet, 3.61 inches (1.311 meters) in diameter, and weighed 930 pounds (422 kilograms).

The Boeing 247 had a maximum speed of 200 miles per hour (322 kilometers per hour) with a cruising speed of 188 miles per hour (303 kilometers per hour. It had a range of 745 miles (1,199 kilometers) and a service ceiling of 25,400 feet (7,742 meters).

75 Model 247s were built. 60 were operated by Boeing Air Transport.

[Note: the windshield was canted forward to prevent instrument panel lighting from reflecting into the cockpit at night. Unfortunately, ground lighting was reflected instead. This was soon changed to a rearward slant and resulted in a slight increase in speed.]

© 2019, Bryan R. Swopes

30 December 1964: The United States Air Force accepted the last of 732 Boeing KC-135 Stratotankers: KC-135A serial number 64-14840. The new tanker was assigned to the 380th Air Refueling Squadron at Plattsburgh Air Force Base, New York, 12 January 1965.

According to the most recent Air Force Fact Sheet, 414 KC-135R and -135RT tankers are still in service with the United States Air Force: 167 active duty Air Force, 67 Air Force Reserve, and 180 Air National Guard. It is estimated that the fleet is 33% through their design lifetime limits. (There are also 25 special variants of the C-135, such as the OC-135B Open Skies, RC-135S Cobra Ball, RC-135U Combat Sent, RC-135V Rivet Joint, and RC-135W Rivet Joint.)

Built as an aerial refueling tanker to support the U.S. Air Force fleet of B-52 Stratofortress strategic bombers, an initial order for 24 tankers was soon increased to 250. Eventually 732 KC-135As were built by Boeing, and an additional 81 of other versions.

With the company internal designation of Model 717, the KC-135 was developed from the Model 367-80 proof-of-concept prototype, the “Dash Eighty.” The Stratotanker is very similar in appearance to the Model 707 and 720 airliners but is structurally a different aircraft. It is also shorter than the 707 and has a smaller diameter fuselage.

The Stratotanker was originally operated by a flight crew of four: pilot, co-pilot, navigator and refueling boom operator. Upgrades over the decades have simplified operation and the crew has been reduced to two pilots and the boom operator.

The KC-135R is 136 feet, 3 inches (41.529 meters) long (156 feet/47.549 meters with fueling boom extended), with a wingspan of 130 feet, 10 inches (39.878 meters), and overall height of 41 feet, 8 inches (12.700 meters). Its maximum takeoff weight is 322,500 pounds (146,284 kilograms).

The Stratotanker can carry up to 200,000 pounds (90,718 kilograms) of fuel for inflight refueling. It can also be configured to carry 83,000 pounds (37,648 kilograms) of cargo, or 80 passengers.

The KC-135A was originally powered by four Pratt & Whitney J57-P-59W turbojet engines producing 13,750 pounds of thrust (61.163 kilonewtons) for takeoff, using water injection. The fleet has been re-engined with more efficient CFM International CFM56-2B1 (F108-CF-100) engines. Modified airplanes are designated KC-135R. The CFM56-2 is a two-spool, axial-flow, high-bypass turbofan with a single fan stage, 12-stage compressor section (3 low pressure and 9 high pressure stages), annular combustor, and a 5-stage turbine (1 high pressure and 4 low pressure stages). The engine is rated at 21,634 pounds of thrust (96.233 kilonewtons).

The tanker has a maximum speed of 350 knots (402 miles per hour/648 kilometers per hour) below 26,500 feet (8,077 meters), and 0.90 Mach when above that altitude. It has a range of 1,500 miles (2,424 kilometers) when carrying 150,000 pounds (68,039 kilograms) of transfer fuel. The service ceiling is 50,000 feet (15,200 meters).

The newest Stratotanker in service with the United States Air Force, KC-135R 64-14840 is 59 years old. It is presently assigned to the 121st Air Refueling Wing, Ohio Air National Guard.

© 2018, Bryan R. Swopes

10 December 1941:¹ A single B-17C Flying Fortress heavy bomber, 40-2045, departed from Clark Field, on the island of Luzon, Commonwealth of the Philippines, alone and without escort, to search for an enemy aircraft carrier which had been reported near the coastal city of Aparri, at the northern end of the island. The aircraft was under the command of Captain Colin P. Kelly, Jr., Air Corps, United States Army, of the 14th Bombardment Squadron, 19th Bombardment Group.

Kelly’s Flying Fortress had not been fully fueled or armed because of an impending Japanese air raid. It carried only three 600-pound (272 kilogram) demolition bombs in its bomb bay.

While enroute to their assigned target area, Captain Kelly and his crew sighted a Japanese amphibious assault task force north of Aparri, including what they believed was a Fusō-class battleship. The crew was unable to locate the reported aircraft carrier and Kelly decided to return to attack the ships that they had seen earlier.

Kelly made two passes at 20,000 feet (6,096 meters) while the bombardier, Sergeant Meyer Levin, set up for a precise drop. On the third run, Sergeant Meyer released the three bombs in trail and bracketed the light cruiser IJN Natori. It and an escorting destroyer, IJN Harukaze, were damaged by near misses.

“. . . The battleship [actually, the light cruiser IJN Natori] was seen about 4 miles offshore and moving slowly parallel with the coastline. . . A quartering approach to the longitudinal axis of the ship was being flown. The three bombs were released in train as rapidly as the bombardier could get them away. The first bomb struck about 50 yards short, the next alongside, and the third squarely amidship. . . A great cloud of smoke arose from the point of impact. The forward length of the ship was about 10 degrees off center to portside. The battleship began weaving from side to side and headed toward shore. Large trails of oil followed in its wake. . . .”

— Narrative Report of Flight of Captain Colin P. Kelly, Air Corps, O-20811 (deceased) on Dec 10, 1947, by Eugene L. Eubank, Colonel, Air Corps, Commanding, Headquarters, 5th Bomber Command, Malang, Java, Feb 19, 1942

A group of Japanese Mitsubishi A6M2 Type 0 (“Zero”) fighters of the Tainan Kokutai, including the famed fighter ace Petty Officer First Class Saburō Sakai, attacked Kelly’s bomber as it returned to Clark Field, with the first pass killing Technical Sergeant William J. Delehanty and wounding Private First Class Robert E. Altman. The instrument panel was destroyed and oxygen tanks exploded. A second pass by the fighters set the bomber’s left wing on fire. This quickly spread to the fuselage. The two engines on the right wing failed.

Captain Kelly ordered his crew to bail out and though the fire had spread to the flight deck, Kelly remained at the bomber’s controls. Staff Sergeant James E. Halkyard, Private First Class Willard L. Money, and Private Altman were able to escape from the rear of the B-17. The navigator, Second Lieutenant Joe M. Bean, and the bombardier, Sergeant Levin, went out through the nose escape hatch. As co-pilot Lieutenant Donald Robins tried to open the cockpit’s upper escape hatch, the Flying Fortress exploded. Robins was thrown clear and was able to open his parachute.

Boeing B-17C 40-2045 crashed approximately three miles (4.8 kilometers) east of Clark Field. The bodies of Captain Kelly and Sergeant Delehanty were found at the crash site.

The wreckage was found along a rural road 2 miles west of Mount Aryat (Mount Aryat is about 5 miles east of Clark Field). The tail assembly was missing. Parts . . . were scattered over an area of 500 yards. The right wing with two engines still in place remained almost intact although it was burning when the search party arrived. The fuselage and left side of the plane were badly wrecked and burned. T/Sgt Delehanty’s body was lying about 50 yards north of the wreckage. Capt Kelly’s body . . . was found very near the wreckage with his parachute unopened. . . .

— Narrative Report of Flight of Captain Colin P. Kelly, Air Corps, O-20811 (deceased) on Dec 10, 1947, by Eugene L. Eubank, Colonel, Air Corps, Commanding, Headquarters, 5th Bomber Command, Malang, Java, Feb 19, 1942

Colin Purdie Kelly, Jr., was born in Madison County, Florida, 11 July 1915. He was the first of two children of Colin Purdie Kelly, a fresco artist, and Mary Eliza Mays (“Mamie”) Kelly. He had a younger sister, Emmala Mays Kelly. Kelly attended Madison High School, graduating in 1932.

Kelly was appointed to the United States Military Academy at West Point, New York. His stated intention was to become a bomber pilot.

According to his West Point yearbook, “C.P.” Kelly,

“. . . has not devoted all his effort to study and consequently not achieved high academic rank, but he has participated in sports and other activities and has found additional time to enjoy thoroughly West Point. He’s positive in his opinions; vigorous in his actions. All-around ability and a knack for making friends bespeak a bright future for him. . . .”

—The Howitzer of 1937, United States Military Academy, West Point, New York, 1937, at Page 218.

Cadet Kelly participated in football, boxing, cross country and track, and sang with the Cadet Chapel choir. Colin Purdie Kelly, Jr., graduated from West Point and was commissioned a second lieutenant, Infantry, United States Army, on 12 June 1937.

On 1 August 1937, Lieutenant Kelly married Miss Marion Estelle Wick. The ceremony was held in the Cadet Chapel at West Point. They would have a son, Colin Purdie Kelly III, born at Riverside, California, 6 May 1940. In 1963, “Corky” Kelly would also graduate from the United States Military Academy.

2nd Lieutenant Kelly was assigned to flight training at Randolph Field, Texas. He graduated 13 January 1939, was awarded his pilot’s wings and was transferred from Infantry to the Air Corps. Kelly was then ordered to join the 19th Bombardment Group (Heavy) at March Field, near Riverside, California. He was promoted to first lieutenant 4 June 1940.

Lieutenant Kelly was assigned to the 11th Bombardment Group (Heavy) at Hickam Field, Oahu, Territory of Hawaii, in April 1941. At about this time, he was promoted to the temporary rank of captain. Kelly served as a squadron operations officer and B-17 check pilot. Nine B-17s of the 14th Bombardment Squadron of the 11th Group were sent to Clark Field in the Philippine Islands, to join the 19th Bombardment Group. Flying to Midway Island, Wake Island, Port Moresby, New Guinea, and Darwin, Australia, they traveled approximately 10,000 miles (16,093 kilometers), 5–12 September 1941. For his actions during this transoceanic flight, Captain Kelly was awarded the Distinguished Flying Cross.

During a reconnaissance mission to Formosa (Taiwan) on 5 December 1941, Captain Kelly observed a large number of Japanese ships steaming toward Luzon. His squadron was then relocated to Del Monte Field on the island of Mindanao.

General Douglas MacArthur later said, “It is my profound sorrow that Colin Kelly is not here. I do not know the dignity of Captain Kelly’s birth, but I do know the glory of his death. He died unquestioning, uncomplaining, with a faith in his heart and victory his end. God has taken him unto Himself, a gallant soldier who did his duty.”

Colin Purdie Kelly, Jr. was awarded the Distinguished Service Cross, posthumously. The medal was presented to Mrs. Colin P. Kelly, Jr., by Major General Barney McKinney Giles, U.S. Army Air Corps.

Following the war, Captain Kelly’s remains were returned to the United States, and interred at the Oak Ridge Cemetery, Madison, Florida.

Kelly’s B-17 was the first Flying Fortress in U.S. service to be lost in air combat in World War II.

The Boeing Model 299H, designated B-17C, was the second production variant ordered by the U.S. Army Air Corps. 38 were built by Boeing, however 20 of these were transferred to Great Britain’s Royal Air Force, designated Fortress B.I. They were initially assigned to No. 90 Squadron.²

The B-17C was 67 feet, 10.6 inches (20.691 meters long with a wingspan of 103 feet, 9⅜ inches (31.633 meters) and the overall height was 15 feet, 5 inches (4.699 meters). The B-17C had an empty weight of 29,021 pounds (13,164 kilograms), gross weight of 39,320 pounds (17,835 kilograms) and maximum takeoff weight of 49,650 pounds (22,521 kilograms).

It was powered by four air-cooled, supercharged, 1,823.129-cubic-inch-displacement (29.875 liter) Wright Aeronautical Division Cyclone 9 C666A (R-1820-65) nine-cylinder radial engines. These engines were rated at 1,000 horsepower at 2,300 r.p.m., and 1,200 horsepower at 2,500 r.p.m., for takeoff. They drove three-bladed Hamilton Standard Hydromatic constant-speed propellers through a 0.5625:1 gear reduction. The R-1820-65 was 3 feet, 11.59 inches (1.209 meters) long, 4 feet, 7.12 inches (1.400 meters) in diameter, and weighed 1,315 pounds (596 kilograms).

The maximum speed of the B-17C was 323 miles per hour (520 kilometers per hour) at 25,000 feet (7,620 meters). Its service ceiling was 37,000 feet (11,278 meters) and the maximum range was 3,400 miles (5,472 kilometers).

The B-17C could carry 4,800 pounds (2,177 kilograms) of bombs. Defensive armament consisted of one .30-caliber air-cooled machine gun and four .50-caliber machine guns.

According to one source, all eighteen B-17Cs in service with the Army Air Corps were returned to Boeing in January 1941 to be upgraded to the B-17D configuration.

¹ 10 December in the Commonwealth of the Philippines, which is west of the International Date Line. This would have been 9 December in the United States of America.

² A 1941 book, War Wings: Fighting Airplanes of the American and British Air Forces, by David C. Cooke, published by Robert M. McBride & Company, New York, refers to the B-17C in British service as the “Seattle,” which is in keeping with the R.A.F.’s system of naming bombers after cities.

© 2018, Bryan R. Swopes