Today in Aviation History

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October 20, 1920

At Villacoublay, France, Joseph Sadi-Lecointe flew his Nieuport-Delâge 29V to a Fédération Aéronautique Internationale (FAI) World Speed Record of 302.53 kilometers per hour (187.98 miles per hour) over a straight 1 kilometer course.¹

Sadi-Lecointe's Ni-D 29V was one of three racing variants of the highly successful single-engine, single-seat Ni-D 29C.1 biplane fighter, which was the fastest in the world at the time. The Ni-D 29V was 21 feet, 3.5 inches (6.489 meters) long, with a wing span of just 6.00 meters (19 feet, 8¼ inches), shortened from the 31 feet, 10 inch (9.703 meters) wingspan of the standard production chasseur.
This Day in Aviation - Page 3 of 306 - Important Dates in Aviation History

Joseph Sadi-Lecointe. (Fédération Aéronautique Internationale)

Joseph Sadi-Lecointe in the cockpit of his Nieuport-Delâge 29V racer, after winning the Gordon Bennett Trophy, at Orleans/Etampes, 28 September 1920. Under the terms of trophy, the nation whose team won the event three consecutive times took permanent possession. After Sadi-Lecointe's victory, the Gordon Bennett Trophy was in the permanent possession of the Aéro-Club de France.

 

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21 October 1959

McDonnell Aircraft Corporation test pilot Gerald ("Zeke") Huelsbeck was killed while test flying the first prototype YF4H-1 Phantom II, Bureau of Aeronautics serial number ("Bu. No.") 142259.

In October 1959 the Navy tried, a bit prematurely, for its first world record with the F4H. McDonnell test pilot Gerald "Zeke" Huelsbeck, flying near Edwards AFB, was testing various flight plans for a high-altitude zoom, looking for one to recommend to the Navy test pilot who would fly the record attempt. Huelsbeck was flying the very first F4H prototype when an engine access door blew loose, flames shot through the engine compartment, and the F4H crashed, killing Huelsbeck. (Over the next three years of the F4H-1 test program three aircraft were destroyed and three crew members died, all preparing for record flights.)
—Engineering the F-4 Phantom II: Parts Into Systems by Glenn E. Bugos, Naval Institute Press, Annapolis, Maryland, 1996, Chapter 5 at Page 101.

The flight control system of the YF4H-1 was damaged by the fire and went it out of control at high speed and into a spin. Zeke Huelsbeck did eject but was too low. His parachute did not open. The prototype crashed in an open area near Mt. Pinos in the Los Padres National Forest, Ventura County, California, about 70 miles (113 kilometers) southwest of Edwards.

McDonnell YF4H-1 Bu. No. 142259 was the first prototype Phantom II. It had first been flown by Robert C. Little at Lambert Field, St. Louis, Missouri, 27 May 1958. The Phantom II was designed as a supersonic, high-altitude fleet defense interceptor for the United States Navy. It was a two-place twin engine jet fighter armed with radar- and infrared-homing air-to-air missiles.
This Day in Aviation - Page 2 of 306 - Important Dates in Aviation History

Gerald Huelsbeck

McDonnell YF4H-1 Phantom II Bu. No. 142259 takes off at Edwards Air Force Base during preparations for Operation Top Flight. (McDonnell Aircraft Corporation)

Test Pilot Gerald Huelsbeck with a prototype McDonnell YF4H-1 Phantom II. Huelsbeck is wearing a Goodyear Mk. IV full-pressure suit. (McDonnell Aircraft Corporation)

Test Pilot Gerald Huelsbeck with a prototype McDonnell YF4H-1 Phantom II. Huelsbeck is wearing a Goodyear Mk. IV full-pressure suit. (McDonnell Aircraft Corporation)

 

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October 21, 1947

At Northrop Field, Hawthorne, California, Northrop Corporation Chief Test Pilot Max R. Stanley took off in the first YB-49, 42-102367, and flew it to Muroc Air Force Base for flight testing.

42-102367 had been converted from the second YB-35 pre-production test aircraft. The original Flying Wing's four Pratt & Whitney Wasp Major (R-4360-21) radial engines were replaced by turbojet engines and several aerodynamic improvements were made.

The YB-49 was a very unusual configuration for an aircraft of that time. There was no fuselage or tail control surfaces. The crew compartment, engines, fuel, landing gear and armament were contained within the wing. Air intakes for the turbojet engines were placed in the leading edge and the exhaust nozzles were at the trailing edge. Four small vertical fins for improved yaw stability were also at the trailing edge.

The YB-49 had a length of 53 feet, 1 inch (16.180 meters), wingspan of 172 feet (52.426 meters) and overall height of 15 feet, 2 inches (4.623 meters). It weighed 88,442 pounds (40,117 kilograms) empty and its Maximum Takeoff Weight (MTOW) was 193,938 pounds (87,969 kilograms).

The Wing defined the airplane. The leading edge was swept aft 26° 57′ 48″, and the trailing edge, 10° 15′ 22″. The wing's total area was 4,000 square feet (371.6 square meters). It had an aspect ratio of 7.4:1. At the root, the chord was 37 feet, 6 inches (11.430 meters), tapering to 9 feet, 4 inches (2.844 meters) at the tip. There was 0° angle of incidence at the root, -4° at the wing tips, and 0° 53′ dihedral.

The YB-49 was powered by eight General Electric-designed, Allison Engine Company-built J35-A-5 engines. (This same engine variant was used in the North American Aviation XP-86, replacing its original Chevrolet-built J35-C-3.) The engines were later upgraded to J35-A-15s. The J35 was a single-spool, axial-flow turbojet engine with an 11-stage compressor and single-stage turbine. The J35-A-15 had a Normal Power rating of 3,270 pounds of thrust (14.546 kilonewtons) at 7,400 r.p.m. The Military Power rating was 3,750 pounds (16.681 kilonewtons) at 7,700 r.p.m. 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).
During testing the YB-49 reached a maximum speed of 428 knots (493 miles per hour/793 kilometers per hour) at 20,800 feet (6,340 meters). Cruise speed was 365 knots (429 miles per hour/690 kilometers per hour). The airplane had a service ceiling of 49,700 feet (15,149 meters). The YB-49 had a maximum fuel capacity of 14,542 gallons (55,047 liters) of JP-1 jet fuel. Its combat radius was 1,403 nautical miles (1,615 statute miles/2,598 kilometers).

The maximum bomb load of the YB-49 was 16,000 pounds (7,257 kilograms), though the actual number of bombs was limited by the volume of the bomb bay and the capacity of each bomb type. While the YB-35 Flying Wing was planned for multiple machine gun turrets, the YB-49 carried no defensive armament.

Only two Northrop YB-49s were built and they were tested by Northrop and the Air Force for nearly two years. Though an additional nine YB-35s were ordered converted, the B-49 was not placed into production.

The second ship, YB-49 42-102368, disintegrated in flight during a test flight north of Muroc Air Force Base, 5 June 1948, killing the entire crew, which included Captain Glen Edwards. The name of Muroc was changed to Edwards Air Force Base in his honor.

YB-49 42-102367 was destroyed by fire following a taxiing accident at Edwards, 15 March 1950. The program was cancelled on the same day.
This Day in Aviation - Page 2 of 306 - Important Dates in Aviation History

Northrop YB-49 42-102367 takes off from Northrop Field, Hawthorne, California, 21 October 1947. (Unattributed)

Chief Test Pilot Max R. Stanley. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

Northrop YB-49 42-102367 at Northrop Field, Hawthorne, California. (Unattributed)

Northrop YB-49 42-102367 takes off from Northrop Field, Hawthorne, California. Note the crowds of onlookers and residential housing along W. 120th Street, on the north side of the airport. (Unattributed)

Northrop YB-49 42-102367 in flight near Muroc Air Force Base. (U.S. Air Force)

 

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October 22, 1975

The lander from the Soviet space probe Venera 9 touched down on the surface of the planet Venus, at approximately 32° south latitude, 291° east longitude.

The images and other data was transmitted to an orbiting section of Venera 9 for relay to Earth. The lander sent signals for approximately 53 minutes before the orbiter traveled out of range.

Venera 9 had been launched from the Baikonur Cosmodrome aboard a Proton-K rocket, 8 June 1975. The space probe weighed 4,936 kilograms (10,882 pounds).

Once in orbit around Venus, the spacecraft separated into the orbiter and lander. As the lander descended to the surface, data was collected about the planet's atmosphere. A 40-kilometer (25-mile) deep layer of clouds was studied. The cloud bases were about 35–40 kilometers (22–25 miles) above the surface. The clouds contained hydrochloric and hydrofluoric acid, bromine and iodine.

At the planet's surface the atmospheric pressure was 90 times that of Earth's. The temperature was measured at 485 °C. (905 °F.).
October 22, 2020 - This Day in Aviation

Venera 9 lander. (NASA)

Venera 9 orbiter. (NASA)

Digitally enhanced image of the surface of Venus captured by the Venera 9 lander, 22 October 1975. (NASA)

Mosaic of images of the surface of Venus captured by the Venera 9 lander, 22 October 1975. The rocks are estimated to be 30–40 centimeters across. (NASA)

 

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October 22, 1968

The first manned mission of the Apollo Program, Apollo 7, "splashed down" in the North Atlantic Ocean. The three man crew, Walter M. Schirra, Donn F. Eisele, and R. Walter Cunningham, had completed 163 orbits in 10 days, 20 hours, 9 minutes, 3 seconds. The spacecraft landed 7 nautical miles (13 kilometers) from the recovery ship, USS Essex (CVS-9).
October 22, 2020 - This Day in Aviation

The Apollo 7 command module descends to the surface of the Atlantic Ocean under three parachutes, 22 October 1968. (NASA)

The crew of Apollo 7 on the flight deck of USS Essex (CVS-9), 22 October 1968. Left to right, Captain Walter M. Schirra, USN; Major Donn F. Eisele, USAF; Major R. Walter Cunningham, USMC. (NASA)

 

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October 22, 1955

At Edwards Air Force Base, in the high desert of southern California, Republic Aviation Corporation test pilot Russell M. ("Rusty") Roth took the first of two prototype YF-105A-1-REs, serial number 54-098, for its first flight.

Though equipped with an under-powered Pratt & Whitney J57-P-25 interim engine, the new airplane was able to reach Mach 1.2 in level flight.

Aerodynamic improvements to the engine intakes and redesign of the fuselage to incorporate the drag-reducing "area rule," along with the more powerful J75-P-5 turbojet engine allowed the production model F-105B to reach Mach 2.15.

The Thunderchief is the largest single-place, single-engine aircraft ever built. It was a Mach 2 fighter-bomber, designed for NATO defensive tactical nuclear strikes with a nuclear bomb carried in an internal bomb bay. The YF-105A was 61 feet, 0 inches (18.593 meters) long, with a wing span of 34 feet, 11 inches (10.643 meters) and overall height of 17 feet, 6 inches (5.334 meters). Its empty weight was 20,454 pounds (9,277 kilograms) and the Maximum Takeoff Weight (MTOW) was 41,500 pounds (18,824 kilograms).

The Pratt & Whitney Turbo Wasp JT3C (J57-P-25) was a two-spool axial-flow turbojet engine with a 16-stage compressor section (9 low- and 7 high-pressure stages) and a 3-stage turbine (1 high- and 2 low-pressure stages). The J57-P-25 had a Normal Power rating of 8,700 pounds of thrust (38.700 kilonewtons), and at Military Power produced 10,200 pounds of thrust (45.372 kilonewtons) (30-minute limit). The Maximum Power rating was 16,000 pounds of thrust (71.172 kilonewtons) with afterburner (5-minute limit). The J57-P-25 was 22 feet, 3.1 inches (6.784 meters) long, 3 feet, 3.8 inches (1.011 meters) in diameter, and weighed 5,120 pounds (2,322 kilograms).

The YF-105A's wings were swept 45° at 25% chord. The angle of incidence was 0° and there was no twist. The wings had 3° 30′ anhedral. The total wing area was 385 square feet (35.8 square meters).

During testing, the prototype's maximum speed was 770 knots (886 miles per hour (1,426 kilometers per hour) at 35,000 feet (10,668 meters)—Mach 1.34—and 676 knots (778 miles per hour/1,252 kilometers per hour) at Sea Level—Mach 1.02. The YF-105A's service ceiling was 52,050 feet (15,865 meters). It's combat radius was 950 nautical miles (1,093 statute miles/1,759 kilometers), and the maximum ferry range was 2,321 nautical miles (2,671 statute miles/4,298 kilometers).
October 22, 2020 - This Day in Aviation

The first of two Republic YF-105A-1-RE Thunderchief prototypes, 54-098, on Rogers Dry Lake, Edwards Air Force Base, California, 1955. (U.S. Air Force)

Republic Aviation Corporation test pilot Russell M. "Rusty" Roth. (Jet Pilot Overseas)

Republic YF-105A 54-098 landing at Edwards Air Force Base. (Ray Wagner Collection, San Diego Air and Space Museum Archives)

 

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October 22, 1938

Lieutenant Colonel Mario Pezzi, Regia Aeronautica, set a Fédération Aéronautique Internationale (FAI) World Record for altitude when he flew an experimental Società Italiana Caproni Ca.161bis to an altitude of 17,083 meters (56,047 feet).

Pezzi was awarded the Medaglia d'oro al Valore Aeronautico and promoted to the rank of colonel.

The Caproni Ca.161bis was an experimental single-seat, single engine, two-bay biplane developed from the earlier Ca.113. It was 27 feet, ¾ inch (8.249 meters) long with a wingspan of 46 feet, 9 inches (14.249 meters) and height of 11 feet, 5¾ inches (3.500 meters). The airplane's empty weight was 1,205 kilograms (2,657 pounds) and gross weight was 1,650 kilograms (3,638 pounds).

The Ca.161bis was powered by an air-cooled, supercharged, 38.673 liter (2,359.97 cubic inch) Piaggio P.XI R.C.100/2v two-row 14-cylinder radial engine which produced 700 horsepower and drove a four-bladed propeller through a 0.62:1 reduction gear. This engine was a license-built version of the French Gnome-Rhône 14K Mistral Major.
October 22, 2020 - This Day in Aviation

Lieutenant Colonel Mario Pezzi, seated in a pressure vessel built into the cockpit of the Caproni Ca.161bis.

The Caproni Ca.161bis, with Lieutenant Colonel Mario Pezzi in the cockpit. (Mario Pezzi Family Archive)

Generale S.A. Mario Pezzi, Regia Aeronautica. (Mario Pezzi Family Archive)

 

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October 22, 1919

During a competition for the Coupe Deutsch de la Meurthe, Lieutenant Le Marquis Bernard Henri Marie Léonard Barny de Romanet of France's Aéronautique Militaire flew a Nieuport-Delâge Ni-D 29V to set two Fédération Aéronautique Internationale (FAI) World Records for Speed Over a Closed Circuit of 268.63 kilometers per hour (166.92 miles per hour).¹

De Romanet's Ni-D 29V was one of three racing variants of the highly successful single-engine, single-seat Ni-D 29C.1 biplane fighter, which was the fastest in the world at the time. The Ni-D 29V was 21 feet, 3.5 inches (6.489 meters) long, with a wing span of just 6.00 meters (19 feet, 8¼ inches), shortened from the 31 feet, 10 inch (9.703 meters) wingspan of the standard production chasseur.
October 22, 2020 - This Day in Aviation

A Nieuport-Delâge Ni-D 29V. This airplane, #10, was flown by Joseph Sadi Lecointe. (Unattributed)

Le Marquis Bernard Henri Marie Léonard Barny de Romanet with a Spad-Herbemont, (S.20bis6) 9 October 1920. (Agence Meurisse 84138/BnF)

Bernard Henri Barny de Romanet

 

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October 23, 1959

American Airlines accepted delivery of its first jet airliner, Boeing 707-123 N7501A (serial number 17628, line number 7). The new airplane had made its first flight on 5 October. Christened Flagship Michigan, American Airlines advertised its new 707 as the "Astrojet."

The Boeing 707 was developed from the earlier Model 367–80, the "Dash Eighty." It is a four-engine jet transport with swept wings and tail surfaces. The leading edge of the wings are swept at a 35° angle. The airliner had a flight crew of four: pilot, co-pilot, navigator and flight engineer. The airliner could carry a maximum of 189 passengers.

The 707-123 was 145 feet, 1 inch (44.221 meters) long with a wing span of 130 feet, 10 inches (39.878 meters). The top of the vertical fin stood 42 feet, 5 inches (12.929 meters) high. The 707 pre-dated the "wide-body" airliners, having a fuselage width of 12 feet, 4 inches (3.759 meters). The airliner's empty weight is 122,533 pounds (55,580 kilograms). Maximum take off weight is 257,000 pounds (116,573 kilograms).
October 23, 2020 - This Day in Aviation

American Airlines' first Boeing 707-123 airliner, N7501A, is rolled out. (Boeing)

Boeing 707-123 N7501A, American Airlines Astrojet, Flagship Michigan, at Seattle. (American Airlines)

 

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October 23, 1934

At Lago di Garda, Brescia, Italy, Warrant Officer Francesco Agello, Regia Aeronautica, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Course when he flew the Macchi Aeronautica M.C. 72 float plane, serial number MM 181, to an average speed of 709.21 kilometers per hour (440.68 miles per hour).

The Macchi-Castoldi M.C.72 was designed by Mario Castoldi for Aeronautica Macchi. It was a single-place, single-engine, low-wing monoplane float plane constructed of wood and metal. It was 8.32 meters (27 feet, 3.5 inches) long with a wingspan of 9.48 meters (31 feet, 1.25 inches) and height of 3.30 meters (10.83 feet). The M.C.72 had an empty weight of 2,505 kilograms (5,512 pounds), loaded weight of 2,907 kilograms (6,409 pounds) and maximum takeoff weight of 3,031 kilograms (6,669 pounds).

It was powered by a 50.256 liter (3,067 cubic inch) liquid-cooled, supercharged Fiat S.p.A. AS.6 24-cylinder 60° dual overhead cam (DOHC) V-24 engine with 4 valves per cylinder. The engine produced 3,100 horsepower at 3,300 r.p.m. and drove two counter-rotating metal two-bladed fixed pitch propellers with a diameter of 8 feet (2.56 meters). The counter-rotating blades cancelled the torque effect of the engine.

Surface radiators were placed on top of each wing and surface oil coolers on the floats.
October 23, 2020 - This Day in Aviation

Warrant Officer Francesco Agello, Regia Aeronautica. (FAI)

Warrant Officer Francesco Agello, Regia Aeronautica, with the record-setting Macchi M.C.72, 23 October 1934. (Historic Wings)

Left rear quarter view of a Macchi M.C.72. (FAI)

Macchi M.C.72 MM 181 at the Museo Storico dell'Aeronautica Militare (Italian Air Force Museum) in Vigna di Valle, Italy. (Unattributed)

 

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October 23, 1911

For the first time, the airplane is used in warfare. Capitán Carlo Maria Piazza, a pilot commanding an aviation unit of the Regio Esercito (the Italian Royal Army), flew a Blériot Type XI on a reconnaissance mission over the Zanzur oasis, south west of Tripoli, Libya, during the Italo-Turkish War (1911–1912).

The Blériot XI was a single-seat, single-engine monoplane, designed by Raymond Saulnier and built by Louis Charles Joseph Blériot. It was 24 feet, 11 inches (7.595 meters) long with a wingspan of 27 feet, 11 inches (8.509 meters) and overall height of 8 feet, 10 inches (2.692 meters). It had an empty weight of 507 pounds (229.9 kilograms).

In its original configuration, the Type XI was powered by an air-cooled, 3.774 liter (230.273 cubic inches) Robert Esnault-Pelterie (R.E.P.) two-row, seven-cylinder fan engine (or "semi-radial"), which produced 30 horsepower at 1,500 r.p.m., and drove a four-bladed paddle-type propeller. The R.E.P. engine weighed 54 kilograms (119 pounds). This engine was unreliable and was soon replaced by an Alessandro Anzani & Co. W-3.

The Blériot XI Militaire was powered by a normally-aspirated, air-cooled, 7.983 liter (487.140-cubic-inch-displacement) Société des Moteurs Gnome Omega 7-cylinder rotary engine which produced 50 horsepower at 1,200 r.p.m. The direct-drive engine turned a two-bladed wooden propeller in a left-hand, tractor configuration. The Omega 7 is 79.2 centimeters (2 feet, 7.2 inches) long, 83.8 centimeters (2 feet, 9.0 inches) in diameter, and weighs 75.6 kilograms (166.7 pounds). The prototype of this engine is in the collection of the Smithsonian Institution National Air & Space Museum.

The Blériot XI had a maximum speed of 76 kilometers per hour (47 miles per hour) and its service ceiling was 1,000 meters (3,281 feet).

Captain Piazza was killed in action in 1917, during the First World War.
October 23, 2020 - This Day in Aviation

Capitán Carlo Piazza in the cockpit of his Blériot XI. (Aeronautica Militaire)

Capitán Carlo Maria Piazza (1871–1917)

Capitán Piazza with a Blériot XI, Tripoli, Libya, 17 February 1912.

 

[cammerjeff]

Obscure Balloon History; Source Abandoned & Little-Known Airfields

A 10/23/34 photo (courtesy of Mike Denja) of husband & wife balloon pioneer aviators Jean & Jeannette Piccard​

during their takeoff from Ford Airport on a record-setting flight to an altitude of 57,579', almost 11 miles up.​

The Piccards' intention was to reach the stratosphere, both to set an altitude record & to collect scientific data.​

Jeanette set the women's altitude record which held for almost 30 years.​

As the Piccards' pet turtle was also along for the ride, it is likely that it also set the unofficial altitude record for turtles or reptiles of any kind.​

They had been training at the airport where Jeannette, the pilot of the craft, worked to become the first licensed female balloon pilot in the U.S.​

Henry Ford even allowed them to use his hangar.​

The Site is now a Ford Motor Test track in Dearborn MI - Just stumbled on this photo while surfing - and noticed the date it was taken - hope know one minds my posting it.

 

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October 24, 2003

At 4:05 p.m. BST, the final commercial flight of the British Airways Concorde came to an end with the landing of G-BOAG at London Heathrow Airport. It landed third in sequence with G-BOAE and G-BOAF after all three supersonic airliners had made a low pass over London.

G-BOAG had flown from New York under the command of Captain Mike Bannister, with First Officer Jonathan Napier and Engineer Officer David Hoyle. There were 100 celebrity passengers on board.

"Alpha Golf," British Aerospace serial number 100-214, was the final Concorde built in Britain, and, at its retirement, was the lowest-time Concorde in British Airway's fleet. It first flew at Filton, 21 April 1978, registered G-BFKW. It was delivered to British Airways 6 February 1980. In 1981, 100-214 was re-registered as G-BOAG. During the early 1980s, it was taken out of service and used as a source for parts for the other Concordes, but returned to airworthy status in 1985.

After a series of farewell flights, G-BOAG was retired to The Museum of Flight, Seattle, Washington. It had flown 16,239 hours, made 5,066 takeoffs and landings and had gone supersonic 5,633 times.
October 24, 2020 - This Day in Aviation

Concorde G-BOAG lands at LHR. (www.concordest.com)

Captain Bannister with Concorde, London Heathrow Airport, 2016. (British Airways)

 

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October 24, 1969

by Captain Sean M. Cross, United States Coast Guard (Retired)

At Da Nang Air Base, Republic of Vietnam, the 37th Aerospace Rescue and Recovery Squadron (ARRS) was coming up on their 500th "save" in mid-October 1969. Everyone was looking forward to it. They arrived at number 497, then hit a dry spell for about a week. On 24 October, MISTY 11 went down and through a connected series of events, Coast Guard exchange pilots Lieutenant Richard Victor Butchka retrieved numbers 498, 499, and 500, and Lieutenant (j.g.) Robert T. Ritchie claimed numbers 501 and 502.

Northeast of Saravane, Laos, MISTY 11, a U.S. Air Force North American Aviation F-100F Super Sabre "Fast FAC"—a jet Forward Air Controller) was designating targets along the Ho Chi Min Trail for ground interdiction strikes when it experienced engine failure due to antiaircraft fire. The stricken aircraft quickly descended to less than 1,000 feet (305 meters) above the terrain. The approximate time was 8:00 a.m. A MAYDAY was broadcast and the two crewmen ejected at low altitude. They parachuted into the jungle-covered mountainous terrain. MISTY 11 Alpha, 1st Lieutenant Alvin Donald Muller, and MISTY 11 Bravo, Captain Jack K. Clapper, were separated by about 800 yards (732 meters) due to the programmed delay in the ejection sequence between the front and rear ejection seats.

The survivors' position was in a small valley formed by two ridges about 100 meters long oriented north and south. At the north end where the ridges joined, a road was cut 20 meters from the top of the hill. MISTY 11A was on the east side of the valley and MISTY 11B was on the west side.

Each was equipped with a battery-powered radio and was contacted by an airborne Forward Air Controller (FAC), a North American Aviation OV-10A Bronco, NAIL 07, who had heard their pre-ejection call and was working in the area. The FAC said that he would notify Search and Rescue. MISTY 11A (Muller) informed MISTY 11B and the FAC that his leg was badly broken. MISTY 11B (Clapper) was unhurt.

Less than two hours from notification, two Douglas A-1 Skyraiders—call signs SANDY 11 and 12—and two Sikorsky HH-3E Jolly Green Giant helicopters—JOLLY 28 and 04—from strip alert in Quang Tri were on scene.

JOLLY 28 (HH-3E #66-13280) crew members: Captain Charles D. Langham, USAF (Pilot); Major Charles W. Bond (Co-Pilot); Staff Sergeant James E. Smith (Flight Engineer); and Technical Sergeant Donald G. Smith (Pararescueman)

JOLLY 04 (HH-3E #66-13290) crew members: Lieutenant Richard Victor Butchka, USCG (Pilot); Captain John K. Coder, USAF (Co-Pilot); Sergeant Joseph J. Vai (Flight Engineer); and Airman 1st Class George P. Hoffman III (Pararescueman)

The helicopters went into orbit. One Jolly Green, referred to as the "low bird," would make the rescue attempt while the second, the "high bird," would remain in a 3,000-foot (914 meters) orbit as backup. Before sending in JOLLY 28, the two A-1s trolled the area, but their repeated passes brought no response from enemy ground-fire. It was determined that Muller should be rescued first because of his broken leg and at about 11:00 a.m., JOLLY 28 descended toward MISTY 11A.

The terrain in the SAR area was rolling foothills with elevations varying from 1,500 feet MSL (Mean Sea Level: describes height above standard Sea Level) in the ravines, to 2,500 feet MSL on the hilltops (500 to 833 meters). The vegetation on these hills varied from dense triple-layered canopy jungles to open areas with tall jungle grass. The entire immediate area around MISTY 11A and B was defended by heavy small arms and automatic weapons as close as 50 feet to the survivors. The proximity of hostile forces to the survivors severely restricted the type of ordnance which could be delivered to protect them. There were scattered variable broken cumulus build-ups in the area with tops to 9,500 feet MSL and bases varying from 2,000 to 3,000 feet AGL (Above Ground Level: describes height above the ground). Visibility below the clouds was excellent.

Lieutenant Butchka, in the "high bird," JOLLY 04, watched his good friend, Captain Charles Langham, descend for the recovery. JOLLY 28 entered a hover over MISTY 11A and lowered the "PJ," Don Smith, by hoist. The PJ immediately had the downed airman on the canopy penetrator and gave the cable-up signal. Less than a minute had elapsed. When the penetrator was approximately 10 feet off the ground, the helicopter came under attack.

Butchka saw three sides of the blind canyon twinkling. It appeared that enemy forces had used the downed F-100F crewman as bait for a "flak trap." The Skyraiders rushed in to suppress the fire, but the opening enemy volley had shot the hoist assembly off its mounts, sending it crashing into the flight engineer's chest and dumping the PJ and MISTY 11A back on the ground. Realizing the hoist was inoperative, the flight engineer, SSGT James Smith, hit the switch shearing the hoist cable and yelled to Captain Langham to transition JOLLY 28 to forward flight.

Above, Butchka punched off his auxiliary fuel tanks and went into a plunging autorotative descent. Seeing Langham's aircraft smoking and streaming fluid (was hit in the main gearbox and was losing oil pressure), Butchka told him to put the helicopter on the ground. Langham searched for a clear spot and put the aircraft into a small punch bowl-shaped valley. Langham and crew jumped out of the helicopter into the elephant grass, looking up for high bird. They did not have far to look. Butchka's helicopter was in a 25-foot hover on the left side of Langham's helicopter with its hoist cable waiting. Butchka expected ground fire from the enemy at any moment. During the swift pick up, the helicopter shuddered with a jolt to the right side. The aircraft's skin was holed with a gash eight inches long by two inches wide.

Major Charles W. Bond had the honor of being the 500th save.

With the men safely on board, the next problem was getting out of there. Butchka did not want to go back out the way he came because of heavy enemy fire. Weather was hot and humid, pressure altitude was high, and the only other way out presented him with a vertical face rising about 130 feet. It was decision time. Butchka said; "I headed for the face, pulled every bit of power I could ('pulled the collective to my arm pit' was the description in another interview), and with a little bit of airspeed drooped the rotor to 94-percent — and just cleared the top." As he eased over the ridgeline, the JOLLY immediately came under heavy ground fire from a different direction. SANDY lead hadn't reported anything because he didn't know where Butchka was. Miraculously they were not hit. However, JOLLY 04 "caught his blades in some trees and is requesting escort out of the area." A forward air controller, COVEY 297, escorted JOLLY 04 to Lima Site 61, an Air Force TACAN navigation site at Muang Phalan, Laos.

There were still two MISTY crewmembers and Langham's PJ on the ground at the initial recovery spot. The PJ, Technical Sergeant Donald G. Smith, using his handheld radio, reported "contact with bad guys 35 meters to my west" and directed air strikes bracketing their position. JOLLY 76, a Sikorsky HH-53C Super Jolly Green Giant from the 40th ARRS at Udorn, Thailand, made three recovery attempts but each time received intense ground fire resulting in extensive battle damage to the helicopter. JOLLY 76 sustained severe battle damage, loss of hydraulic systems and associated tail rotor control problems that forced the aircraft to withdraw. JOLLY 76 was escorted out of the area by JOLLY 72 and A-1s SANDY 01 and 04, and successfully recovered at Lima Site 44, an unimproved covert landing strip near Saravane, Laos.

JOLLY 76 (Sikorsky HH-53C Super Jolly Green Giant) crewmembers: Captain Donald R. Almanzar (Pilot); Captain Peter L. Fekke (Co-Pilot); Staff Sergeant Harold R. Hailey (Flight Engineer); Sergeant Anthony J. McFarr (Pararescueman); Sgt. Douglas W. Crowder (Pararescueman); and Sergeant Gregory Lee Anderson (Aerial Photographer).

JOLLY 15 (Sikorsky HH-3E Jolly Green Giant) crew members: Coast Guard Lieutenant (j.g.) Robert T. Ritchie, USCG (Pilot); Lieutenant Colonel Sidney S. Sosnow , USAF (Co-Pilot); Technical Sergeant Frank Gaydos, Jr. (Flight Engineer); Staff Sergeant Jon K. Hoberg (Pararescueman); and Sgt. Edward K. Rendle (Pararescueman).

Later that afternoon the JOLLIES tried again. After multiple A-1 passes dropping CBU-19s ( a 130-pound modified dispenser containing 528 canisters with an incapacitating chemical CS—"tear gas") SANDY 06 and 05 escorted "low bird" JOLLY 15 with Coast Guard Lieutenant (j.g.) Rob Ritchie into the rescue area.

Rob said; "The previous attempts that day were all into the wind approaches. I chose a downwind approach because all indications were the 'bad guys' were set up for us to come into the wind and were waiting." The SANDYs made suppression runs and laid smoke as had been requested – then they joined in a daisy chain of passes that provided protective fire. Ritchie used the smoke for cover, swooped in fast and quickly put the aircraft into a hover over Smith and MISTY 11A. TSgt. Gaydos fearlessly operated the rescue hoist while completely exposed to the hostile fire impacting about him. His reassuringly calm hover instructions to the pilots, ensured Smith and MISTY 11A were quickly brought on board with only slight damage to the aircraft. During Ritchie's next approach to pick up MISTY 11B they began taking very heavy ground fire on the way in. The element of surprise was no longer there and the North Vietnamese had repositioned. SANDY Lead called the approach off and both A-1s made several suppression runs.

Ritchie commenced his third approach immediately after the suppression runs. He said it was much quieter this time and he came to a hover over MISTY 11B. As the penetrator went down the ground fire became much heavier and the helicopter was taking numerous hits. The utility hydraulics to the hoist was disabled due to ground fire damage to a pressure line and fluid flow was lost. Unable to complete the pickup Ritchie exited the area. JOLLY 15 notified SANDY 03 that he would be unable to remain in the area and commenced a rendezvous for air refueling with KING 03, a Lockheed C-130 Combat King. JOLLY 15 landed at Lima Site 61 at 3:35 p.m.

Two additional tries to pick up MISTY 11B were made to no avail. A tropical thunderstorm moved in and heavy rain fell for the next 30 minutes. A third attempt was made while the squall was passing through and as the storm began to subside, the winds became relatively calm and the previously laid smoke screen began to envelope the area – adversely impacting the rescue helicopters' visibility and making it more difficult to locate MISTY 11B.

Fortunately, the survivor's emergency radio was operational and the pilot knew how to use it. By coordinating voice guidance from MISTY 11B on the ground and SPAD 09 (circling overhead), JOLLY 19, another HH-3E, flew over Clapper and lowered a canopy penetrator to him. He climbed onto the device and the helicopter quickly exited the area as soon as Clapper was clear of the trees. The gunner on the rescue helicopter pulled him in the door and the MISTY 11 rescue was successfully concluded at around 6:00 p.m.

JOLLY 19 (Sikorsky HH-3E Jolly Green Giant) from Detachment 1, 40th Aerospace Rescue and Recovery Squadron. Crewmembers: Major Ted L. Smith (Pilot); Major Edward B. Robbins (Co-Pilot); Staff Sergeant Robert E. Hunt (Flight Engineer); Master Sergeant Paul L. Jenkins (Pararescueman); and Sergeant Leland H. Sorensen (Pararescueman).

The following A-1 SANDY forces participated in the event:

SANDY 01 1st Lieutenant Rex V. Huntsman
SANDY 04 Lieutenant Colonel Dick Michaud
SANDY 03 Major Nelson Moffatt
SANDY 07 1st Lieutenant Noel Frisbie
SANDY 05 Captain Bob Crowder
SANDY 06 Captain Glenn C. Dyer
SANDY 11 Captain Jack L. Hudson
SANDY 12 Lieutenant Colonel George D. Miller

Epilogue: For their efforts during this combat rescue the following medals were awarded:

Technical Sergeant Donald G. Smith, USAF, Pararescueman from JOLLY 28 was awarded the Air Force Cross:

The President of the United States of America, authorized by Section 8742, Title 10, United States Code, awards the Air Force Cross to Technical Sergeant Donald G. Smith for extraordinary heroism in military operations against an opposing armed force as a Pararescueman on a HH-3E Rescue Helicopter in Southeast Asia on 24 October 1969. On that date, Sergeant Smith voluntarily descended to the surface on a forest penetrator to assist a downed pilot. As he and the pilot were being raised, hostile fire rendered the hoist inoperative and the cable was sheared, dropping them fifteen feet to the ground. Sergeant Smith's position was surrounded by hostile forces, and his helicopter was downed by hostile fire. Remaining exceptionally calm, his resolute and decisive presence encouraged other survivors, while his resourcefulness in controlling and directing the aircraft providing suppressive fire, resulted in the safe recovery of all downed personnel. Through his extraordinary heroism, superb airmanship, and aggressiveness in the face of the enemy, Sergeant Smith reflected the highest credit upon himself and the United States Air Force.

Lieutenant Robert T. Ritchie, USCG, was awarded the Silver Star.

The President of the United States of America takes pleasure in presenting the Silver Star (Air Force Award) to Lieutenant, Junior Grade, Robert T. Ritchie, United States Coast Guard, for gallantry in connection with military operations against an opposing armed force while attached to the 37th Aerospace Rescue and Recovery Squadron (USAF). Lieutenant, Junior Grade, Ritchie distinguished himself as Aircraft Commander of an HH-3E rescue helicopter in Southeast Asia on 24 October 1969. On that date, Lieutenant, Junior Grade, Ritchie repeatedly penetrated an area of intense hostile fire in an effort to rescue three downed airmen before battle damage rendered his aircraft incapable of further rescue operations. By his gallantry and devotion to duty, Lieutenant, Junior Grade, Ritchie has reflected great credit upon himself and the United States Air Force.

Captain Charles D. Langham, USAF, earned the Silver Star:

Captain Charles D. Langham distinguished himself by gallantry in connection with military operations against an opposing armed force as Aircraft Commander of an HH-3E helicopter in Southeast Asia on 24 October 1969. On that date, while attempting to recover two downed Air Force pilots., Captain Langham's aircraft was subjected to intense hostile fire. Displaying superb airmanship, Captain Langham nursed his critically damaged aircraft way from the immediate hostile area and effected an emergency landing in a confined, remote area which saved his crew from probable serious injury or possible death. By his gallantry and devotion to duty, Captain Langham has reflected great credit upon himself and the United States Air Force.

LT Richard V. Butchka, USCG, earned the Distinguished Flying Cross with Combat V.

The President of the United States of America takes pleasure in presenting the Distinguished Flying Cross with Combat "V" (Air Force Award) to Lieutenant Richard V. Butchka, United States Coast Guard, for heroism while participating in aerial flight as aircraft Commander of an HH-3E helicopter, attached to the 37th Aerospace Rescue and Recovery Squadron, United States Air Force, in Southeast Asia on 24 October 1969. On that date, in the face of known hostile forces, who had just shot down another rescue helicopter, Lieutenant Butchka, with complete disregard for his own personal safety, skillfully and expeditiously effected the rescue of three crewmen from the downed helicopter. The outstanding heroism and selfless devotion to duty displayed by Lieutenant Butchka reflect great credit upon himself and the United States Coast Guard.

The following Distinguished Flying Cross recipients were also confirmed for this mission: Major Charles W. Bond; Captain John K. Coder; Technical Sergeant Frank Gaydosl Jr.; Sergaeant Joseph J. Vai; Airman 1st Class George P. Hoffman III; Staff Sergeant Jon K. Hoberg; and Lieutenant Colonel. Sidney S. Sosnow.

Misty #132 Jack K. Clapper left the USAF in 1974, went to law school and is a trial lawyer in Novato, California. Donald G. Smith passed away on 12 March 2016 at the age of 80. Richard V. Butchka passed away 28 July 2007 at the age of 66. Misty #119 Alvin Donald ("Devil") Muller passed away on 16 November 2010 at the age of 67.

Aerial Photographer Staff Sergeant Gregory Lee Anderson, crewman on JOLLY 76, was aboard Jolly Green 71, an HH-53B, when it was shot down over Laos, 28 January 1970. SSGT Anderson is listed as Missing in Action. (Active Pursuit)

HH-3E 66-13280 caught fire in flight, 15 April 1970, and crashed near Kontum, Republic of Vietnam. Two of the five crewmen died.

HH-3E 66-13290 was retired to Davis Monthan Air Force Base, Tucson, Arizona, 18 March 1991. It was withdrawn from storage and placed on display with the New York Air National Guard at Westhampton Beach, New York.
October 24, 2020 - This Day in Aviation

A Sikorsky HH-3E Jolly Green Giant, 66-13290, of the 37th ARRS, hovering in ground effect at Da Nang, circa 1968. This helicopter was JOLLY 04, flown by Lt. R. V. Butchka, USCG, on 24 October 1969.(U.S. Air Force)

Lieutenant Richard Victor Butchka, United States Coast Guard, in the cockpit of a Sikorsky HH-3E Jolly Green Giant. (Butchka Collection)

LT Richard Butchka, USCG is congratulated by CPT Charles Langham, USAF following the recovery of his JOLLY 28 aircrew during the MISTY 11 combat rescue. (Butchka Collection)

1LT Don Muller, USAF, MISTY 11A, is assisted down from LTJG Ritchie's HH-3E, JOLLY 15. (Rotor Review Magazine, Spring '19)

Master Sergeant Donald G. Smith, United States Air Force.

CPT Charles D. Langham Silver Star medal ceremony

SSGT Gregory Lee Anderson, USAF

 

[DerAdlerIstGelandet]

October 24, 1953

At Edwards Air Force Base, California, Richard Lowe Johnson, Chief Test Pilot for the Convair Division of the General Dynamics Corporation, took the first prototype YF-102 Delta Dagger, serial number 52-7994, for its first flight.

The YF-102 was a single-seat, single-engine, delta wing fighter designed as an all-weather, missile-armed, Mach 2 interceptor. It was developed from the earlier, experimental, Convair XF-92 Dart. The F-102 was planned for a Westinghouse XJ67-W-1 engine, but when that was not ready in time, a Pratt & Whitney J57-P-11 afterburning turbojet engine was substituted. The J57 was a two-spool, axial-flow engine with a 16-stage compressor section (9 low- and 7-high-pressure stages) and a 3-stage turbine section (1 high- and 2 low-pressure stages). The J57-P-11 was rated at 10,000 pounds of thrust (44.482 kilonewtons), and 16,000 pounds (71.172 kilonewtons) with afterburner.

The prototype had finished assembly at the Convair plant in San Diego, California, on 2 October 1953. It was then shipped by truck to Edwards Air Force Base in the high desert of southern California where final preparations and testing was carried out.

The National Advisory Committee for Aeronautics (NACA) had tested scale models of the YF-102 in the 8-foot HST wind tunnel at the Langley Memorial Aeronautical laboratory and found that significant shock waves were produced at near-sonic speeds. Surprisingly, shock waves were created at the trailing edge of the delta wing. The shock waves caused very high drag that would keep the aircraft from reaching Mach 1, even with the more powerful engine planned for production models.

Several problems showed up on the YF-102's first flight. Severe buffeting was encountered at high sub-sonic speed. As predicted by NACA, aerodynamic drag prevented the YF-102 from reaching Mach 1 in level flight. There were also problems with the landing gear, the fuel system, and the J57 engine did not produce the rated power.

The production F-102A was considerably larger than the YF-102. The fuselage was lengthened, the wing area and span were increased, and the vertical fin was taller. A more powerful J57-P-23 engine was used. These and other changes increased the F-102A's gross weight by nearly 1,800 pounds (815 kilograms).
October 24, 2020 - This Day in Aviation

Convair YF-102 52-7994 on Rogers Dry Lake, Edwards Air Force Base, California. (San Diego Air and Space Museum Archive)

The first prototype Convair YF-102 Delta Dagger, 52-7994, was completed at the Convair plant in San Diego, 2 October 1953. (Convair Division of General Dynamics)

Convair YF-102 53-1785 with the original fuselage, photographed 31 December 1954. (NASA)

The first prototype Convair YF-102 Delta Dagger, 52-7994, on Rogers Dry Lake, October 1953. (U.S. Air Force)

Convair YF-102 52-7994 parked on the dry lake bed, Edwards AFB, California. (U.S. Air Force)

Convair YF-102 Delta Dagger 52-7994 just before touchdown on Rogers Dry Lake. (U.S. Air Force)

Convair Chief Test Pilot Richard Lowe Johnson. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

 

[DerAdlerIstGelandet]

October 24, 1947

First flight, prototype Grumman Model G-64, the XJR2F-1 Pelican. This amphibian would become the Grumman UF-1 Albatross. (In U.S. Air Force service, the Albatross was designated SA-16A. In 1962, this was changed to HU-16A for Navy, Coast Guard and USAF.)
October 24, 2020 - This Day in Aviation

Grumman Model G-64, XJR2F-1 Pelican. (Уголок неба)

Grumman G-64, XJ2RF-1 Pelican (U.S. Coast Guard)

 

[DerAdlerIstGelandet]

October 24, 1946

At 12:18 p.m., Mountain Standard Time (17:18 UTC), a captured V-2 rocket was launched from the U.S. Army's White Sands Missile Range, east of Las Cruces, New Mexico. The rocket, identified as Upper Air Rocket Number 13, carried a 35-millimeter DeVry Corporation cine camera set to expose one frame every second-and-a-half.

The V-2's engine burned for 59.8 seconds, by which time the rocket had reached an altitude of 17.0 miles (27.4 kilometers) and a velocity of 3,990 feet per second (1,216 meters per second). Continuing upward on a ballistic trajectory, the rocket reached a maximum altitude of 65.0 miles (104.6 kilometers) after 180.0 seconds. This is just above the 100-kilometer Kármán Line which is the arbitrary beginning of Space.

Falling back to Earth, Number 13 impacted approximately 17 miles north-northwest of the White Sands V-2 Launching Site and was completely destroyed. Although debris from the rocket was scattered widely, the film cassette was recovered.

The image below is a still frame from the recovered film. It shows the curvature of the Earth. This was the highest altitude a photograph had been made since Captain Albert W. Stevens photographed the Earth from a balloon, Explorer II, 20 July 1935.
October 24, 2020 - This Day in Aviation

First photograph of the Earth taken from an altitude of 65 miles (105 kilometers). (White Sands Missile Range/Applied Physics Laboratory)

A captured German V-2 rocket is launched from the White Sand Proving Grounds, 10 May 1946. (Popular Science)

V-2 rocket body at White Sands.

V-2 Number 3 is prepared for launch at White Sands Proving Grounds, New Mexico, 10 May 1946. With a burn time of 59 seconds, the rocket reached an altitude of 70.9 miles (114.1 kilometers) and traveled 31 miles (49.9 kilometers) down range. (The Space Race – Rockets)

 

[DerAdlerIstGelandet]

October 25, 1994

At Bell Helicopter Textron's plant at Mirabel, Quebec, Canada, the prototype Bell Model 430, registered C-GBLL, made its first flight.

The Bell Model 430 ("Four-Thirty") is a twin-engine intermediate-weight helicopter, operated by one or two pilots, and which can be configured to carry from 6 to 11 passengers. It has advanced avionics. The standard helicopter is equipped with skid landing gear, and retractable tricycle gear is optional. The 430 was the first helicopter to be certified for instrument flight with a single pilot, without a stability augmentation system. The aircraft is also certified for Category A operations, meaning that if one engine were to fail during takeoff, the helicopter could continue to fly with the remaining engine.

The 430 was developed from the preceding Model 230 (and the 230 from the 222). It was lengthened 1 foot, 6 inches (0.457 meters) and uses a four-bladed semi-rigid main rotor. Instead of a mechanical rotor head of trunnions, bearings and hinges, the 430 has a "soft-in-plane" fiberglass rotor yoke that is flexible enough to allow the blades to flap, feather and lead/lag.
October 25, 2020 - This Day in Aviation

The prototype Bell Model 430, C-GBLL, in flight, circa 1994. (Bell Helicopter TEXTRON)

 

[DerAdlerIstGelandet]

October 25, 1979

The 5,057th and very last Phantom II—an F-4E-67-MC, U.S. Air Force serial number 78-0744—was rolled out at the McDonnell Douglas Corporation plant, Lambert Field (STL), St. Louis, Missouri, and the production line was closed.

78-0744 was transferred to the Republic of Korea Air Force (ROKAF) under the Foreign Military Sales program Peace Pheasant II and assigned to the 17th Tactical Fighter Wing based at Cheongju International Airport (CJJ). One source says that it was "written off" but details are lacking.
October 25, 2020 - This Day in Aviation

McDonnell Douglas F-4E-67-MC Phantom II, 78-0744, the last of 5,057 Phantoms built at St. Louis, 25 October 1979. (McDonnell Douglas Corporation)

 

[DerAdlerIstGelandet]

October 24-25, 1928

Captain Charles B.D. Collyer, Air Service, United States Army, and Harry J. Tucker flew Tucker's Lockheed Vega, X4769, from New York to Los Angeles, non-stop, in 24 hours, 55 minutes.

A contemporary newspaper article reported the event:

YANKEE DOODLE SETS NEW MARK​

Monoplane Flies Across Continent to Los Angeles in 24 Hours, 55 Minutes
Mines Field, Los Angeles, Oct. 25—(AP)—Setting a new record for a trans-continental non-stop airplane flight from the Atlantic coast to the Pacific, the monoplane Yankee Doodle arrived here at 2:12 p.m. today from New York.
The unofficial time of the flight as announced by Capt. C.D.B. Collyer, pilot and Harry Tucker, owner and passenger, was 24 hours 55 minutes. The best previous time for the westward flight was 26 hours and 50 minutes, made in 1923 by Lieutenants John MacReady [John A. Macready] and Oakley Gelley [Oakley George Kelly].

530 Gallons Carried​

The Yankee Doodle hopped off at Roosevelt Field at 4:16:35 p.m. Eastern Standard Time yesterday. The little cigar-shaped white-winged plane was loaded with 530 gallons of gasoline, just about enough for a 24-hour flight, and a check began shortly after landing to determine how much of the fuel was left.
The westward flight covered approximately the course flown over by Col. Arthur Goebel when he piloted his plane to a new West-East non-stop trans-continental record of 18 hours and 55 minutes several weeks ago.
This was the fourth time Tucker has sent his plane into a coast-to-coast grind. The first West to East attempt was unsuccessful but on the second attempt Goebel piloted the machine through to the record.
—The Cornell Daily Sun, Ithaca, New York, Friday, October 26, 1928, Volume XLIX, Number 29 at Page 1, Column 5
October 25, 2020 - This Day in Aviation

Harry Tucker's Lockheed Vega, X4769. (National Archives)

Captain Charles B.D. Collyer

Harry J. Tucker