Yearly Archives: 2025

12 March 1967

McDonnell F-4D Phantom II 66-7554. (Boeing)
McDonnell F-4D-30-MC Phantom II 66-7533, the 2,000th Phantom. (Boeing)

12 March 1967: McDonnell Aircraft Corporation, St. Louis, Missouri, delivered the 2,000th F-4 Phantom II to the United States Air Force. F-4D-30-MC 66-7533, c/n 2062, was assigned to the 40th Tactical Fighter Squadron, 33rd Tactical Fighter Wing, at Eglin Air Force Base, Florida.

On 26 May 1967, the personnel and equipment of the 40th TFS were transferred to the 8th Fighter Wing based in Thailand. The aircraft were deployed across the Pacific Ocean, 26–28 May, with flights to Hickam Air Force Base, Honolulu, Hawaii; Anderson Air Force Base, Guam; and Ubon-Rachitani Royal Thai Air Force Base, Thailand. On 25 July 1967, an additional twenty F-4Ds arrived at Ubon RTAFB, having been transferred from the 4th TFS. 66-7533 was included in this later group of Phantoms.¹

On 19 September 1967, the 2,000th Phantom II was being flown by Major Lloyd Warren Boothby and 1st Lieutenant George H. McKinney, Jr., of the 435th Tactical Fighter Squadron. Following a Rolling Thunder attack on railroad sidings at Trung Quang, about 10 miles (16.1 kilometers) north of Phúc Yên, 66-7533 was hit in the right wing by a 57 mm anti-aircraft cannon shell. The airplane was badly damaged but “Boots” Boothby fought to keep it under control for as long as possible. Finally, he and McKinney were forced to eject, having come within about 35 miles (56.3 kilometers) of their base.

At the time of its loss, 66-7533 had accumulated 155 flight hours on its airframe (TTAF).

Distinguished Flying Cross

For their airmanship in trying to save their airplane, Major Boothby and Lieutenant McKinney were each awarded the Distinguished Flying Cross, which was presented to them by President Lyndon B. Johnson, 23 December 1967, in a pre-dawn ceremony at Korat Royal Thai Air Force Base.

Lieutenant McKinney is quoted in USAF F-4 Phantom II MiG Killer 1965–1968:

“In the hail of AAA over the target seven miles north of Hanoi on that day was a ‘Golden BB’ which opened a three-foot hole in the Phantom II’s right wing, froze the right spoiler full up, immediately drained two of the three hydraulic systems and generally turned the day to crap! I mumbled an egress heading (and a few dozen prayers) while ‘Boots’ used every increment of incredible aviation instincts, honed by countless hours at the edge of the envelope, to keep the F-4 airborne and headed away from the ‘Hanoi Hilton.’ Doing so required full manual depression of the left rudder pedal, and holding the stick within one inch of the left limit of travel.

“Despite the physical exertion, coupled with the precise touch necessary to remain airborne as the Black River receded behind the crippled Phantom II and rescue became at least a possibility, ‘Boots” managed to announce to the world on ‘Guard’ channel that they had so many warning lights lit up that it ‘looks like we’ve won a free game at the arcade.’ “

USAF F-4 Phantom II MiG Killer 1965–1968, by Peter E. Davies, Osprey Publishing, 2004, at Page 75.

[A number of sources state that Lt. McKinney did not survive the ejection, but this is incorrect. Both pilots were rescued by helicopter. McKinney went on to earn credit for 2.5 kills as a Weapons System Officer, and returned for another combat tour as an F-4 aircraft commander.]

Boothby
Lieutenant Colonel Lloyd Warren Boothby, United States Air Force

WASHINGTON (AFPN) — I’d hate to see an epitaph on a fighter pilot’s tombstone that says, “I told you I needed training”. . . How do you train for the most dangerous game in the world by being as safe as possible? When you don’t let a guy train because it’s dangerous, you’re saying, “Go fight those lions with your bare hands in that arena, because we can’t teach you to learn how to use a spear. If we do, you might cut your finger while you’re learning.” And that’s just about the same as murder. —Lt. Col. Lloyd “Boots” Boothby, April 17, 1931, to Nov. 26, 2006

That quote may seem a little extreme, but Colonel Boothby was referring to the Air Force’s urgent need to improve fighter tactics training, balanced against safety, but not at the expense of effectiveness.

Colonel Boothby, who passed away Nov. 26, was an experienced combat pilot and an academic instructor in the 57th Fighter Weapons Wing in the early 1970s. He looked at the Air Force’s declining kill ratio from Korea to Vietnam which was 2.4 to 1 in Vietnam compared to 8 to 1 in the Korean War. He led the effort to fix it. This involved several key steps, starting with a thorough analysis of the engagements over Vietnam.

Colonel Boothby led a series of studies at the Tactical Fighter Weapons Center, which were part of Project Red Baron, examining each of the war’s air-to-air battles. While the subsequent reports noted many accomplishments and even more lessons learned, they highlighted several significant trends. The colonel’s team discovered that pilots of multi-role fighters tended to have such a diverse range of missions that they seldom had a chance to master air combat tactics. They also noted pilots who were shot down rarely saw the enemy aircraft or even knew they were being engaged.

Additionally, few U.S. pilots, before flying into combat, had any experience against the equipment, tactics or capabilities of the enemy’s smaller, highly maneuverable fighters.

In short, the Red Baron Reports called for “realistic training (that) can only be gained through study of, and actual engagements with, possessed enemy aircraft or realistic substitutes.”

Based on this report and Colonel Boothby’s persuasiveness to get himself and Capt. Roger Wells access to an intelligence organization’s restricted collection of Soviet equipment, training manuals and technical data, they developed the dissimilar air combat training, or DACT, program to meet the Tactical Air Command’s initiative of “Readiness through Realism.”

Under the DACT program, Air Force officials had some T-38s painted with Soviet-style paint schemes and flew them based on adopted Soviet tactics.

Northrop F-5E Tiger II 74-01561 of the 64th Fighter Weapons Squadron, 57th Fighter Weapons Wing, in October 1976. (U.S. Air Force)

Because of his combat experience, academic instructor background, and involvement in Project Red Baron and in developing the DACT program, Colonel Boothby served as the first aggressor squadron’s commander when the 64th Fighter Weapons Squadron activated Oct. 15, 1972.

As an instructor, Colonel Boothby proved himself an effective teacher who relished the attention of his captive audience. Ever-animated and quick with a joke or “fighter” story to make a point, he told the pilots he was instructing what they needed to know to succeed. These qualities ensured his students’ attention remained spellbound and eager.

One former student recalled one of the colonel’s more popular attention steps. In typical fighter pilot stance, using his hands to represent a dogfight, he would spray lighter fluid from his mouth across his right hand (palming a lighter at the time) and literally flame the left hand and wristwatch bogie. He generally walked away with a few singed hairs on his hand, but his students received a magnificent visual demonstration of the seriousness of air combat.

Such object lessons ensured this charismatic instructor’s students learned and retained the knowledge they might need to save their lives one day.

Upon learning of Colonel Boothby’s death recently, Air Force Chief of Staff Gen. T. Michael Moseley noted:

“He. . . had an impact on how we do business and how we think about this air combat work. Folks out there like [Colonel Richard] Moody Suter and Boots Boothby have left a true legacy. I know one Texas public school-educated, land grant college graduate, F-15 weapons officer, Fighter Weapons Instructor Course instructor and ex-57th Wing commander who has certainly benefited from folks like this.”

—Ellery Wallwork, Air Force History Office, 5 December 2006

Fred Straile (at far right) with the 2,000th Phantom, F-4D 66-7533. (Fred C. Straile Collection)

Colonel Lloyd Warren Boothby passed away 26 November 2006, and Lieutenant Colonel George H. McKinney, Jr., 28 May, 2019.

¹ Mr. F.C. Straile informed me that he crewed McDonnell F-4D Phantom II 66-7533 with the 4th Tactical Fighter Squadron at Eglin Air Force Base, Florida, and transferred along with it to the 435th TFS at Ubon RTAFB. Thanks, Mr. Straile!

© 2017, Bryan R. Swopes

12 March 1955

Jean Boulet (1920–2011)
Chief Test Pilot Jean Boulet (1920–2011)

12 March 1955:  Société nationale des constructions aéronautiques du Sud-Est (SNCASE) Chief Test Pilot Jean Boulet and Flight Test Engineer Henri Petit made the first flight of the SE.3130 Alouette II prototype, F-WHHE, at Buc Airfield, near Paris, France.

Powered by a Societé Anonyme Turboméca Artouste II B1 turboshaft engine, the Alouette II was the first gas turbine powered helicopter to enter series production. SNCASE would become Aérospatiale, later, Eurocopter, and is now Airbus Helicopters.

SNCASE SE.3130 Alouette II No. 01 prototype, F-WHHF, with test pilot Jean Boulet and Henri Petit, 12 March 1955. (Eurocopter)
SNCASE SE.3130 Alouette II No. 01 prototype, F-WHHE, with test pilot Jean Boulet and Henri Petit, 12 March 1955. (Airbus Helicopters)

The Alouette II is a 5-place light helicopter operated by a single pilot. The fuselage is 31 feet, 8.5 inches (9.665 meters) long. The landing skids have a width of 6 feet, 10 inches (2.083 meters). With rotors turning, the overall length of the Alouette II is 39 feet, 6.5 inches (12.052 meters). Its height is 9 feet, 0.25 inches (2.750 meters) to the top of the main rotor mast. (Optional wide-track skids, or installation of an Alouette III three-blade tail rotor will change dimensions slightly.)

The three-bladed fully-articulated main rotor has a diameter of 33 feet, 5.5 inches (10.198 meters). It turns clockwise, as seen from above. (The advancing blade is on the left side of the helicopter.) Normal main rotor speed, NR, is 350–360 r.p.m. In autorotation, the allowable range is 280–420 r.p.m. The two-blade anti-torque rotor is 5 feet, 11.5 inches (1.816 meters) in diameter and turns clockwise, as seen from the helicopter’s left side. (The advancing blade is below the axis of rotation.) The tail rotor turns at 2,020 r.p.m.

The SE.3130 has an empty weight of 1,934 pounds (877 kilograms), depending on installed equipment, and minimum operating weight of 2,050 pounds (930 kilograms). The maximum permissible weight is 3,300 pounds (1,497 kilograms).

SNCASE SE.3130 No. 01, F-WHHE. (Airbus Helicopters)

The prototype was powered by one Turboméca Artouste II B1 turboshaft engine. The Artouste II B1 is a single-shaft turboshaft engine with a single-stage centrifugal flow compressor section and a three-stage axial-flow turbine. The turbine drives both the compressor and an output drive shaft through reduction gearbox. As installed in the Alouette II, the engine was certified for operation at 33,000–34,000 r.p.m (N1), with transient overspeeds to 35,000 r.p.m. It is capable of producing 400 shaft horsepower, but was derated to 360 shaft horsepower at 5,780 r.p.m. (N2) for installation in the Alouette II.

SE.3130 Alouette II three-view illustration with dimensions. (SNCASE)

The helicopter has an economical cruise speed of 92 knots (106 miles per hour/170 kilometers per hour) at 33,000 r.p.m., and a maximum speed (VNE) of 105 knots (121 miles per hour/194 kilometers per hour) at Sea Level, which decreases with altitude. Sideward or rearward flight (or operation in tailwinds or crosswinds) is limited to 18 knots (20 miles per hour/33 kilometers per hour).

The Allouette II is limited to a maximum operating altitude of 14,800 feet (4,511 meters). At 1,350 kilograms (2,976 pounds) the Alouette II has a hover ceiling in ground effect, HIGE, of 3,400 meters (11,155 feet) and hover ceiling out of ground effect of 1,900 meters (6,234 feet). At 1,500 kilograms the Alouette II’s HIGE is 2,000 meters (6,560 feet) and HOGE is 600 meters (1,968 feet).

The SE.3130 Alouette was in production from 1956 until 1975. It was marketed in the United States by the Republic Aviation Corporation’s Helicopter Division. More than 1,300 of these helicopters were built.

Jean Boulet hovers the prototype SE.3130 Alouette II, F-WHHF, 12 March 1955. (Eurocopter)
Jean Boulet hovers the prototype SNCASE SE.3130 No. 01, F-WHHE. (Airbus Helicopters)

Jean Ernest Boulet was born 16 November 1920, in Brunoy, southeast of Paris, France. He was the son of Charles-Aimé Boulet, an electrical engineer, and Marie-Renée Berruel Boulet.

He graduated from Ecole Polytechnique in 1940 and the Ecole Nationale Supérieure de l’aéronautique In 1942. (One of his classmates was André Edouard Turcat, who would also become one of France’s greatest test pilots.)

Following his graduation, Boulet joined the Armée de l’Air (French Air Force)and was commissioned a sous-lieutenant. He took his first flight lesson in October. After the surrender of France in the Nazi invaders, Boulet’s military career slowed. He applied to l’Ecole Nationale Supérieure de l’Aéronautique in Toulouse for post-graduate aeronautical engineering. He completed a master’s degree in 1943.

During this time, Boulet joined two brothers with La Resistance savoyarde, fighting against the German invaders as well as French collaborators.

In 1943, Jean Boulet married Mlle Josette Rouquet. They had two sons, Jean-Pierre and Olivier.

In February 1945, Sous-lieutenant Boulet was sent to the United States for training as a pilot. After basic and advanced flight training, Boulet began training as a fighter pilot, completing the course in a Republic P-47D Thunderbolt. He was then sent back to France along with the other successful students.

On 1 February 1947 Jean Boulet joined Société nationale des constructions aéronautiques du Sud-Est (SNCASE) as an engineer and test pilot. He returned to the United States to transition to helicopters. Initially, Boulet and another SNCASE pilot were sent to Helicopter Air Transport at Camden Central Airport,  Camden, New Jersey, for transition training in the Sikorsky S-51. An over-enthusiastic instructor attempted to demonstrate the Sikorsky to Boulet, but lost control and crashed. Fortunately, neither pilot was injured. Boulet decided to go to Bell Aircraft at Niagara Falls, New York, where he trained on the Bell Model 47. He was awarded a helicopter pilot certificate by the U.S. Federal Aviation Administration, 23 February 1948.

Test pilot Jean Boulet (center), with Mme. Boulet and the world-record-setting Alouette II.

As a test pilot Boulet made the first flight in every helicopter produced by SNCASE, which would become Sud-Aviation and later, Aérospatiale (then, Eurocopter, and now, Airbus Helicopters).

While flying a SE 530 Mistral fighter, 23 January 1953, Boulet entered an unrecoverable spin and became the first French pilot to escape from an aircraft by ejection seat during an actual emergency. He was awarded the Médaille de l’Aéronautique.

Jean Boulet was appointed Chevalier de la légion d’honneur in 1956, and in 1973, promoted to Officier de la Légion d’honneur.

Jean Boulet had more than 9,000 flight hours, with over 8,000 hours in helicopters. He set 24 Fédération Aéronautique Internationale world records for speed, distance and altitude. Four of these are current.

Jean Boulet wrote L’Histoire de l’Helicoptere: Racontée par ses Pionniers 1907–1956, published in 1982 by Éditions France-Empire, 13, Rue Le Sueuer, 75116 Paris.

Jean Ernest Boulet died at Aix-en-Provence, in southern France, 15 February 2011, at the age of 90 years.

© 2019, Bryan R. Swopes

11 March 1959

Sikorsky XHSS-2 Sea King, Bu. No. 147137, made its first flight at Stratford, CT. (U.S. Navy)
Sikorsky XHSS-2 Sea King, Bu. No. 147137, made its first flight at Stratford, CT. (Sikorsky, a Lockheed Martin Company)

11 March 1959: At Stratford, Connecticut, the prototype Sikorsky XHSS-2 Sea King, U.S. Navy Bureau of Aeronautics serial number (Bu. No.) 147137, company serial number 61001, makes its first flight. Sikorsky’s Assistant Chief Test Pilot Robert Stewart Decker is at the controls.

The Sikorsky SH-3A Sea King was the first of the S-61 series of military and civil helicopters, designated as HSS-2 until 1962. It is a large twin-engine helicopter with a single main rotor/tail rotor configuration. The fuselage is designed to allow landing on water. The helicopter was originally used as an anti-submarine helicopter.

HSS-2 mockup, October 1957. (Sikorsky Historical Archives)

The HSS-2 is 72 feet, 6 inches (22.098 meters) long and 16 feet, 10 inches (5.131 meters) high with all rotors turning. The helicopter’s width, across the sponsons, is 16 feet. The main rotors and tail can be folded for more compact storage aboard aircraft carriers, shortening the aircraft to 46 feet, 6 inches (14.173 meters). The empty weight of the HSS-2 is 10,814 pounds (4,905 kilograms). The overload gross weight is 19,000 pounds (8,618 kilograms).

The main rotor has five blades and a diameter of 62 feet, 0 inches (18.898 meters). Each blade has a chord of 1 foot, 6¼ inches (0.464 meters). The rotor blade airfoil was the NACA 0012, which was common for helicopters of that time. The total blade area is 222.5 square feet (20.671 square meters), and the disc area is 3,019 square feet (280.474 square meters). The tail rotor also has five blades and a diameter of 10 feet, 4 inches (3.150 meters). They each have a chord of 7–11/32 inches (0.187 meters). At 100% NR, the main rotor turns 203 r.p.m. and the tail rotor, 1,244 r.p.m.

The first Sea King, prototype XHSS-2 Bu. No. 147137, demonstrates its capability of landing on water. (Sikorsky, a Lockheed Martin Company)

The HSS-2 was powered by two General Electric T58-GE-6 turboshaft engines, which had a Normal Power rating of 900 horsepower, and Military Power rating of 1,050 horsepower; both ratings at 19,555 r.p.m. at Sea Level. The main transmission was rated for 2,000 horsepower, maximum. (Later models were built with more powerful T58-GE-8 engines. Early aircraft were retrofitted.)

The HSS-2 has a cruise speed of 125 knots (144 miles per hour/232 kilometers per hour) at Sea Level, and a maximum speed of 133 knots (153 miles per hour/246 kilometers per hour) at Sea Level. The service ceiling is 12,100 feet (3,688 meters). The hover ceiling at normal gross weight is 5,200 feet (1,585 meters), out of ground effect (HOGE), and 7,250 feet (2,210 meters), in ground effect (HIGE). The HSS-2 had a combat endurance of 4 hours and a maximum range of 500 nautical miles (575 statute miles/926 kilometers).

The Sea King was primarily an anti-submarine aircraft. It could be armed with up to four MK 43 or MK 44 torpedoes and one MK 101 nuclear-armed depth bomb. Other weapons loads included four MK 14 depth charges and four MK 54 air depth bombs.

In 1962, the HSS-2 was redesignated SH-3A Sea King. Many early production aircraft have remained in service and have been upgraded through SH-3D, SH-3G, etc. In addition to the original ASW role, the Sea Kings have been widely used for Combat Search and Rescue operations. Marine One, the call sign for the helicopters assigned to the President of the United States, are VH-3D Sea Kings.

Sikorsky produced the last S-61 helicopter in 1980, having built 794. Production has been licensed to manufacturers in England, Italy, Canada and Japan. They have produced an additional 679 Sea Kings.

A U.S. Navy Sikorsky SH-3A Sea King (S-61), Bu. No. 149867, near Oahu, Hawaiian Islands, 5 April 1976. (PH2 (AC) Westhusing, U.S. Navy)

© 2019, Bryan R. Swopes

11 March 1957

The Boeing 367-80, prototype of the Model 707 airliner, being brepared for taakeoff on teh morning of 11 March 1957, Boeing Field, Seattle, Washington. (Leonard Mccombe/LIFE Magazine)
The Boeing 367-80, N70700, prototype for the Model 707 airliner and KC-135 air tanker, being prepared for takeoff on the morning of 11 March 1957, Boeing Field, Seattle, Washington. (Leonard Mccombe/LIFE Magazine)
Pre-flight inspection at Boeing Field, Seattle, Washington. In the background are newly-built Boeing B-52 Stratofortress bombers. (Leonard Mccombe/LIFE Magazine)
Pre-flight inspection at Boeing Field, Seattle, Washington. In the background are newly-built Boeing B-52 Stratofortress bombers. (Leonard Mccombe/LIFE Magazine)
Tex Johnston checks that the ramp is clear for engine start. Ready to start number one. (Leonard Mccombe/LIFE Magazine)
Tex Johnston checks that the ramp is clear for engine start. Ready to start number one. (Leonard Mccombe/LIFE Magazine)

11 March 1957: The Boeing jet airliner prototype, the Model 367-80, N70700, made a transcontinental demonstration flight from Seattle’s Boeing Field (BFI) to Friendship National Airport (BWI), Baltimore, Maryland. The aircraft commander was Boeing’s Chief of Flight Test, Alvin Melvin (“Tex”) Johnston. Test pilots James Russell (“Jim”) Gannett and Samuel Lewis (“Lew”) Wallick, Jr., completed the flight crew. The flight covered 2,350 miles (3,782 kilometers) and took 3 hours, 48 minutes.

Cruising at 0.86 Mach. (Leonard Mccombe/LIFE Magazine)
Cruising at 0.86 Mach. The four Pratt & Whitney JT3C turbojet engines are turning 100% r.p.m. (Leonard Mccombe/LIFE Magazine)
The flight deck of the Boeing 367-80 during the transcontinental demonstration flight, 11 March 1957. (Leonard Mccombe, LIFE magazine)
The flight deck of the Boeing 367-80 during the transcontinental demonstration flight, 11 March 1957. The flight attendants are (left) Miss Shirlee Mae Adams of American Airlines, and Miss Jo Ann Reeber, Trans World Airways.(Leonard Mccombe/LIFE magazine)
Reporters balance a pen and a coin in the Dash 80's vibration-free cabin. (Leonard Mccombe/LIFE Magazine)
Reporters balance a pen and a coin in the Dash 80’s vibration-free cabin. (Leonard Mccombe/LIFE Magazine)
A news reporter types his story during the transcontinental flight. (Leonatd Mccombe/LIFE Magazine)
A news reporter types his story during the transcontinental flight. (Leonard Mccombe/LIFE Magazine)
Boeing test pilot S.L. "Lew" Wallick updates the chart with the Dash 80's present position. (Leonard Mccombe/LIFE Magazine)
Boeing test pilot Samuel Lewis (“Lew”) Wallick, Jr., updates the chart with the Dash 80’s present position. (Leonard Mccombe/LIFE Magazine)
Flight attendants from Pan American World Airways, American Airlines and Trans World Airlines made up the cabin crew. (Leonard Mccombe/LIFE Magazine)
Flight attendants from three customer airlines made up the cabin crew of the Boeing 367-80. Left to right, they are: Miss Shirlee Mae Adams, American Airlines; Miss Jackee Gibson, Braniff International Airways; and Miss Jo Ann Reeber, Trans World Airways. (Leonard Mccombe/LIFE Magazine)

Jet Airliner Crosses U.S. At Record Clip

Seattle-To-Baltimore Flight Made In 3 Hours, 48 Minutes

WASHINGTON, March 12 (AP) A Boeing 707 jet passenger plane set a new transcontinental speed record for commercial aircraft yesterday, flying the 2,325 miles from Seattle to Baltimore in 3 hours and 48 minutes.

At one point it attained a speed of 698 miles an hour.

A.M. (Tex) Johnston, Boeing chief of flight tests, said he would fly back to Seattle tomorrow with stops at Chicago’s O’Hare Airport and at Denver. He planned a series of local flights for congressmen, Pentagon officials and experts.

The big plane averaged 612 miles an hour for its Puget Sound-to-Chesapeake Bay flight, and sliced 10 minutes off the unofficial transport plane record it set between Seattle and Washington, D.C., in 1955.

There were 52 persons aboard, all but 20 of them newsmen.

‘Jet Stream’ Helps

The 707 left Boeing Field at 10:06 a.m., EST. East of Spokane at 31,000 feet, it hit the “jet stream,” a vast windstream with speeds of up to 125 miles an hour.

These winds enabled the plane to attain supersonic speeds in relation to the ground over northwestern Montana and northern Idaho. However, the plane was actually in subsonic flight and did not break the “sound barrier.”

While in the jet stream, the plane’s peak air speed was 596 miles an hour, but at one point the stream boosted this by 102 miles an hour, for a top speed of 698 in relation to the ground.

Fighter Holds Record

The official transcontinental speed record was set by a one-place F-84F jet fighter two years ago—652½ mph for the 2,446 miles from Los Angeles to New York City. [LCOL Robert R. Scott, USAF, 9 March 1955—TDiA]

The fastest unofficial transcontinental crossing listed by the Defense Department: 715 mph for the 2,700 miles from Riverside, Calif., to Boston last Jan. 25, by a Boeing B-47 bomber.

The 707 is to be delivered to its first airline buyers—Pan American and American—late next year and early in 1959.

The plane’s cost varies from 4½ to 5½ million dollars, depending on size and range, Various models will carry from 120 to 162 passengers.

Toledo Blade, Tuesday, 12 March 1957, Page 2 at Columns 2–4

Boeing's Chief of Flight Test, Alvin M. "Tex" Johnston updates a memeber of teh cabin crew on the progress of the flight. (Leonard Mccombe/LIFE Magazine)
Boeing’s Chief of Flight Test, Alvin M. “Tex” Johnston, updates a member of the cabin crew, Miss Jackie Gibson of Braniff International Airways, on the progress of the Dash 80’s transcontinental flight. (Leonard Mccombe/LIFE Magazine)
Boeing's Chief of Flight Test guides the Dash 80 to a touchdown on Runway 10, Friendship National Airport, (Leonard Mccombe/LIFE Magazine)
Boeing’s Chief of Flight Test Alvin M. “Tex” Johnston guides the Dash 80 to touchdown on Runway 10, Friendship National Airport, 2:02 p.m., Eastern Standard Time, 11 March 1957. (Leonard Mccombe/LIFE Magazine)
Tex Johnston with flight attendants from Boeing's customers: Pan American World Airways, American Airlines and Trans World Airways. (Leonard Mccombe/LIFE Magazine)
Tex Johnston with three flight attendants from Boeing’s customers: Miss Jackie Gibson, Braniff International Airways; Miss Shirlee Mae Adams, American Airlines; and Miss Jo Ann Reeber, Trans World Airways. (Leonard Mccombe/LIFE Magazine)
Boeing 367-80 N70700 parked at teh international terminal, Friendship National Airport, Baltimore, Maryland. (Leonard Mccombe/LIFE Magazine)
Boeing 367-80 N70700 parked at the international terminal, Friendship National Airport, Baltimore, Maryland. (Leonard Mccombe/LIFE Magazine)
N70700's route of flight, 0706–1102, 11 March 1957. (Leonard Mccombe/LIFE Magazine)
N70700’s route of flight, 0706–1102, 11 March 1957. (Leonard Mccombe/LIFE Magazine)

Boeing had risked $16,000,000 in a private venture to build the Dash 80 in order to demonstrate its capabilities to potential civilian and military customers, while rivals Douglas and Lockheed were marketing their own un-built jet airliners. Put into production as the U.S. Air Force KC-135A Stratotanker air refueling tanker and C-135 Stratolifter transport, a civil variant was also produced as the Boeing 707 Stratoliner, the first successful jet airliner. Though they look very similar, the 707 is structurally different than the KC-135 and has a wider fuselage.

The prototype Boeing Model 367-80 was operated by a pilot, co-pilot and flight engineer. The airplane’s wing was mounted low on the fuselage and the engine nacelles were mounted on pylons under the wing, as they were on Boeing’s B-47 Stratojet and B-52 Stratofortress. The wings and tail surfaces were swept to 35° at 25% chord, and had 7° dihedral. The Dash 80 was 127 feet 10 inches (38.964 meters) long with a wingspan of 129 feet, 8 inches (39.522 meters) and overall height of 38 feet (11.582 meters). The tail span is 39 feet, 8 inches (12.090 meters). The empty weight of the 367-80 was 75,630 pounds (34,505 kilograms) and the gross weight, 190,000 pounds (86,183 kilograms).

Cutaway scale model of the Boeing 367-80 showing interior arrangement. (Boeing)

N70700 was powered by four Pratt & Whitney Turbo Wasp JT3C engines. This engine is a civil variant of the military J57 series. It is a two-spool, axial-flow turbojet engine with a 16-stage compressor and 2-stage turbine. The JT3C-6 (used in the first production 707s) was rated at 11,200 pounds of thrust (49.82 kilonewtons), and 13,500 pounds (60.05 kilonewtons) with water/methanol injection). The JT3C is 11 feet, 6.6 inches (3.520 meters) long, 3 feet, 2.9 inches (0.988 meters) in diameter, and weighs 4,235 pounds (1,921 kilograms).

These gave the 367-80 a cruise speed of 550 miles per hour (885 kilometers per hour) and a maximum speed of 0.84 Mach (582 miles per hour, 937 kilometers per hour) at 25,000 feet (7,620 meters). The service ceiling was 43,000 feet (13,106 meters). Its range was 3,530 miles (5,681 kilometers).

Boeing continued to use the 367–80 for testing, finally retiring it 22 January 1970. At that time, its logbook showed 2,346 hours, 46 minutes of flight time (TTAF). It was flown to Davis-Monthan Air Force Base, Tucson, Arizona, and placed in storage. In 1990, Boeing returned it to flyable condition and flew it back it to Renton where a total restoration was completed. Many of those who had worked on the Dash 80, including Tex Johnston, were aboard.

The pioneering airplane was presented to the Smithsonian Institution and is on display at the National Air and Space Museum, Steven V. Udvar-Hazy Center. The Boeing 367-80 was designated an International Historic Mechanical Engineering Landmark by the American Society of Mechanical Engineers.

(The Boeing Model 367-80 is on display at the Steven F. Udvar-Hazy center, Smithsonian Institution National Air and Space Museum. (Photo by Dane Penland, National Air and Space Museum, Smithsonian Institution)
The Boeing Model 367-80 is on display at the Steven F. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum. (Photo by Dane Penland, National Air and Space Museum, Smithsonian Institution)

Highly recommended: Tex Johnston, Jet-Age Test Pilot, by A.M. “Tex” Johnston with Charles Barton, Smithsonian Books, Washington, D.C., 1991

© 2019, Bryan R. Swopes

11 March 1918

1st Lieutenant Paul Frank Baer, Air Service, United States Army. (Campbell Studios, New York)

11 March 1918: 1st Lieutenant Paul Frank Baer, Air Service, United States Army, assigned to the103rd Aero Squadron,  American Expeditionary Forces, flying a SPAD S.VII C-1 chasseur, shot down an enemy Albatros D, near Cerney-les-Reims, France. For this and other actions, Lieutenant Baer was awarded the Distinguished Service Cross.

The President of the United States of America, authorized by Act of Congress, July 9, 1918, takes pleasure in presenting the Distinguished Service Cross to First Lieutenant (Air Service) Paul Frank Baer, United States Army Air Service, for extraordinary heroism in action while serving with 103d Aero Squadron, 3d Pursuit Group, U.S. Army Air Service, A.E.F., on 11 March 1918. First Lieutenant Baer attacked, alone, a group of seven enemy pursuit machines, destroying one, which fell near the French lines northeast of Reims, France. On 16 March 1918, he attacked two enemy two-seaters, one of which fell in flames in approximately the same region.

War Department, General Orders No. 128 (1919)

Lieutenant Baer was the first United States airman to receive the Distinguished Service Cross.

Lieutenant Baer is officially credited by the United States Air Force with 7.75 enemy airplanes shot down between 11 March and 22 May 1918, and he claimed an additional 7. (Credit for two airplanes was shared with four other pilots.) After shooting down his eighth enemy airplane on 22 May 1918, Baer and his SPAD S.XIII C.1 were also shot down. He was seriously injured and was captured by the enemy near Armentières and held as a Prisoner of War. At one point, Baer was able to escape for several days before being recaptured.

For his service in World War I, 1st Lieutenant Paul Frank Baer was awarded the United States’ Distinguished Service Cross with one oak leaf cluster (a second award). He was appointed Chevalier de la Légion d’honneur by Raymond Poincaré, the President of France. He was also awarded the Croix de Guerre with seven palms.

Biplan SPAD de chasse monoplace S.VII (rcgroups.com)

The Société Pour L’Aviation et ses Dérivés SPAD S.VII C.1 was a single-place, single-engine, two-bay biplane chasseur (fighter). The airplane was 19 feet, 11 inches (5.842 meters) long, with a wingspan of 25 feet, 7¾ inches (7.817 meters) and overall height of 7 feet, 2 inches (2.184 meters). It had a maximum gross weight of 1,632 pounds (740 kilograms).

Biplan SPAD de chasse monoplace S.VII (rcgroups.com)

The SPAD VII was initially powered by a water-cooled, normally-aspirated, 11.762 liter (717.769 cubic inches) Société Française Hispano-Suiza 8Aa, a single overhead camshaft (SOHC) 90° V-8 engine with a compression ratio of 4.7:1. The 8Aa produced 150 horsepower at 2,000 r.p.m. By early 1918, the S.VII’s engine was upgraded to the higher-compression 8Ab (5.3:1), rated at 180 horsepower at 2,100 r.p.m. These were right-hand tractor, direct-drive engines which turned a two-bladed fixed-pitch wooden propeller.

The SPAD VII had a maximum speed of 119 miles per hour (192 kilometers per hour). The 8Ab engine increased this to 129 miles per hour (208 kilometers per hour). The service ceiling was 17,500 feet (5,334 meters).

Biplan SPAD de chasse monoplace S.VII (rcgroups.com)

Armament consisted of a single air-cooled Vickers .303-caliber (7.7 × 56 millimeter) machine gun, synchronized to fire forward through the propeller arc.

The SPAD S.VII was produced by nine manufacturers in France and England. The exact number of airplanes built is unknown. Estimates range from 5,600 to 6,500.

The airplane in this photograph is a SPAD S.VII C.1, serial number A.S. 94099, built by Société Pour L’Aviation et ses Dérivés, and restored by the 1st Fighter Wing, Selfridge Air Force Base, Michigan. It is in the collection of the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.

SPAD VII C.1, serial number A.S. 94099, on display at the National Museum of the United States Air Force. (U.S. Air Force)

© 2023, Bryan R. Swopes