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1929 Curtiss Thrush J-6

1929 Curtiss Thrush J-6

Several Thrush J-6 airplanes were flown by female pilots during the early 1930s to make record-breaking endurance flights, including one in which the aircraft stayed aloft for almost 10 days.

A black and white photo of a 1929 Curtiss Thrush J-6 parked on a Curtiss Aeroplane airfield.

The 1929 Curtiss Thrush bridged the gap between small personal aircraft and larger commercial airliners. (Photo from the Paul S. Maynard archive)

BY MARK MAYNARD

The Curtiss Thrush exemplified the transitional phase of aviation in the late 1920s. The 1929 Thrush bridged the gap between small personal aircraft and larger commercial airliners. Its design innovations and contributions to endurance flying underscore its significance in aviation history.

Introduced in 1929, the Curtiss Thrush is a six-passenger, high-wing monoplane developed by the Curtiss Aeroplane and Motor Co. Based on an enlarged version of the Curtiss Robin, the Thrush aimed to serve as a light transport and utility aircraft. Its development featured both Curtiss and Wright engines, reflecting the era’s rapid advancements in aviation technology.

Aviation historian Joseph P. Juptner, in his work “U.S. Civil Aircraft: Vol. 3,” noted that “the fuselage of the Thrush formed the basis for the twin-engine Curtiss Kingbird.” The plane’s design would highlight its influence on subsequent aircraft developments.

Design and Development

The initial prototypes of the Curtiss Thrush were equipped with 170 horsepower Curtiss Challenger engines. However, these engines were found to be underpowered for the aircraft’s design. Consequently, the production models designated Thrush J were outfitted with more robust 225-hp Wright J-6-7 Whirlwind radial engines. This upgrade significantly enhanced the aircraft’s performance.

The fuselage construction utilized a Pratt truss frame made primarily from duralumin tubing, a high-strength, lightweight aluminum alloy. Chrome-molybdenum steel reinforced high-stress areas, all covered in fabric. The wings featured solid spruce spars and stamped Alclad ribs, with a semi-cantilever design supported by steel tube struts.

A black and white photo of a 1933 Curtiss Thrush J-6 flown by pilots Helen Richey and Frances Marsalis. The words "Outdoor Girl" are in large white font on the black plane's fuselage

The Curtiss Thrush J-6 “Outdoor Girl” flown by pilots Helen Richey and Frances Marsalis. (Photo courtesy of San Diego Air and Space Museum Archive)

Operational History

The Curtiss Thrush played a notable role in early aviation endurance records. In August 1932, pilots Louise Thaden and Frances Marsalis flew a Thrush J, named “I.J. Fox,” for 196 hours and 5 minutes. Their effort set an endurance record near Valley Stream, N.Y. This achievement contributed to Thaden receiving the Harmon Trophy in 1936. (“I. J. Fox” refers to their sponsor, a nationally known fur store operator founded by Isidore Joseph Fox.

Later, in December 1933, pilots Helen Richey and Frances Marsalis set another endurance record. The pair of women pilots flew another Thrush J, “Outdoor Girl,” for 237 hours and 42 minutes over Miami, Fla. (The plane was named for a brand of women’s cosmetics, a new sponsor.) Their Thrush J-6 was refueled from the air by a Curtiss Robin. The endurance flight further demonstrated the aircraft’s capabilities.

Internationally, the Thrush saw limited use. The China National Aviation Corp. ordered 12 units, but only 10 were produced, with just one making it to China in 1930.

Additionally, one Thrush was operated in Cuba by the Compañía Nacional Cubana de Aviación Curtiss. A subsidiary of North American Aviation Inc., the airline was the precursor to Cubana de Aviación, the national airline of Cuba.

1929 Curtiss Thrush Specifications

  • Crew: One to two (with dual controls)
  • Capacity: Six passengers
  • Length: 32 feet 7 inches
  • Wingspan: 48 feet 0 inches
  • Height: 9 feet 3 inches
  • Wing Area: 305 square feet
  • Empty Weight: 2,260 pounds
  • Gross Weight: 3,800 pounds
  • Fuel Capacity: 110 U.S. gallons
  • Powerplant: 1 225-hp Wright J-6-7 (R-760) radial engine.
  • Maximum Speed: 122 mph
  • Cruise Speed: 104 mph
  • Range: 900 miles
  • Service Ceiling: 13,200 feet
  • Rate of Climb: 650 feet per minute (3.3 meters per second)

SOURCE: Wikipedia.

 This is another image from my dad, Paul Smith Maynard, who worked as an engineer in aviation for four decades. Dad began his career in about 1943 after graduating from West Virginia University. He started with Curtiss-Wright Corp., a pioneer in making flying machines. He went on to work at North American Aviation and Rockwell International. See more of his vintage plane pics here.

1944 Curtiss SC Seahawk

1944 Curtiss SC Seahawk

The Curtiss SC Seahawk, capable of being fitted with a float or wheeled landing gear, was America’s best World War II floatplane scout

A 1942 Curtiss SC Seahawk floatplane scout in the air

More than 500 Curtiss Seahawk scout planes were built at the plant in Columbus, Ohio. The first flight of a prototype XSC-1 took place Feb. 16, 1944. (Photo from the Paul S. Maynard archive)

BY MARK MAYNARD

The Curtiss SC Seahawk was a scout seaplane launched from a Navy cruiser for observation. According to the plane’s page in Wikipedia, the single-seat seaplane landed in water and was retrieved by hoist. Though capable in concept, the Curtiss SC Seahawk did not see significant action during World War II. By the end of the war, helicopters were replacing seaplanes.

The Curtiss Aeroplane and Motor Co. designed the Seahawk for the U.S. Navy during World War II. In the late stages of the war and into peacetime, the Seahawk gradually replaced the existing Curtiss SO3C Seamew and Vought OS2U Kingfisher floatplanes.

A Curtiss Seahawk spotting plane hoisted aboard USS IOWA (BB-61), off San Francisco, July 1947. A second SC-1 is on the catapult at right.

A Curtiss Seahawk spotting plane hoisted aboard USS IOWA (BB-61), off San Francisco, July 1947. A second SC-1 is on the catapult at right. (Ted Huggins photo from the archive of Naval History and Heritage Command, Washington, DC)

Curtiss Production Order

Work began in June 1942 following a U.S. Navy Bureau of Aeronautics request for observation seaplane proposals. Curtiss submitted the Seahawk design on Aug. 1, 1942, and a contract for two prototypes and five service test aircraft was awarded on Aug. 25. Before the prototypes’ first flight, a production order for 500 SC-1s followed in June 1943.

While only intended to seat the pilot, a bunk was added in the aft fuselage for rescue or personnel transfer. Two .50 caliber M2 Browning machine guns were fitted in the wings, and two underwing hardpoints allowed the carriage of 250-pound bombs or surface-scan radar on the right wing. The wings were foldable. The main float, designed to incorporate a bomb bay, is claimed to have been prone to leaks. Curtiss modified the design to carry an auxiliary fuel tank.

A Seahawk is catapulted from the deck of the USS Missouri

Piloted by Ensign F.H. Gilkie, a Curtiss SC-2 Seahawk is catapulted from the USS Missouri (BB-63). The photo is dated Feb. 27, 1948. (Official U.S. Navy Photograph, from the archive of Naval History and Heritage Command, Washington, DC)

The first flight of a prototype XSC-1 took place on Feb. 16, 1944, at the Columbus, Ohio, Curtiss plant. Flight testing continued through April 28, when the last of the seven pre-production aircraft took to the air. Nine more prototypes were built under the designation SC-2 with a second seat and modified cockpit. Series production was not undertaken.

For retrieval, a Curtiss SC-1 Seahawk taxis up to a sea-sled towed by USS IOWA (BB-61), off San Francisco, July 1947.

For retrieval, a Curtiss SC-1 Seahawk taxis up to a sea-sled towed by USS IOWA (BB-61) off San Francisco in July 1947. (Ted Huggins photo from the archive of the Naval History and Heritage Command, Washington, DC)

Seahawk History

The first serial-production Seahawks were delivered to the USS Guam on Oct. 22, 1944. All 577 aircraft eventually produced for the Navy were delivered on conventional landing gear. The planes were then flown to the appropriate naval air station, where floats were installed for service as needed.

Capable of being fitted with a float or wheeled landing gear, the Seahawk was America’s best World War II floatplane scout. However, its protracted development time meant it entered service too late to see significant action in the war. It was not until June 1945, during the pre-invasion bombardment of Borneo, that the Seahawk was involved in military action. By the war’s end, seaplanes were becoming less desirable, with helicopters replacing the Seahawk soon afterward.

The Seahawk’s tri-color camouflage and markings were required by U.S. Navy regulations from 1944 to 1945 and later postwar regulations.

There are no known surviving examples of the Seahawk today.

A color image of the front engine area of a Curtiss Seahawk that shows a ladder to the float.

A Seahawk scout warms up its engine at a Pacific Base circa 1944-45. Note beaching gear and ladder, with an APS-4 radar pod under the wing. While only intended to seat the pilot, a bunk was provided in the aft fuselage for rescue or personnel transfer. (Naval History and Heritage Command, Washington, DC)

Curtiss SC Seahawk Specifications

Crew: 1, with space for a single stretcher patient

Length: 36 feet, 4.5 inches

Wingspan: 41 feet

Height: 16 feet on beaching gear

Wing area: 280 square feet

Empty weight: 6,320 pounds

Gross weight: 9,000 pounds

PERFORMANCE

Powerplant: 1 1,300-hp Wright R-1820-62 Cyclone 9-cylinder air-cooled radial piston engine

Propellers: 4-blade constant-speed propeller

Maximum speed: 235 mph at 2,200 feet

Cruising speed: 125 mph

Range: 625 miles

Service ceiling: 37,300 feet

Rate of climb: 2,500 ft/min

ARMAMENT

Guns: 2 .50-caliber M2 Browning machine guns

Bombs: 2 325-pound bombs under-wing

Note: This is another image from my dad, Paul Smith Maynard, who worked four decades in aviation as an engineer. Dad began his career in about 1943 after graduating from West Virginia University. He started with Curtiss-Wright Corp., a pioneer in making flying machines. He went on to work at North American Aviation and Rockwell International.

Curtiss Robin

Curtiss Robin

During the ‘Golden Age of Flight,’ the Curtiss Robin made history for several endurance stunts, including a ‘wrong way’ record

A black and white photo of a Curtiss Robin monoplane at rest on a runway

The 1928 Curtiss Robin debuted innovative features and was known as a reliable workhorse aircraft, setting several endurance records and stunts. (Photo from the Paul S. Maynard archive)

BY MARK MAYNARD

The Curtiss Robin looks spartan, but this high-wing monoplane gained popularity for its innovative features and remarkable performance.

This workhorse Robin, in production from 1928 to 1930, was one of the first commercially successful light aircraft, debuting several aviation firsts. Among the Robin’s innovations was a retractable landing gear, one of the first aircraft to be so equipped in the Golden Age of Flight. The Robin was also one of the first to be powered by a radial engine.

Along the way, the Curtiss Robin set more than one aviation record, including a “wrong way” record.

According to a report at the National Air and Space Museum, the Curtiss Robin was a departure by the Curtiss Aeroplane and Motor Co. into the emerging civilian market of the late 1920s.

“This three-seat monoplane flew in the spring of 1928 with a 90-hp Curtiss OX-5, the engine that had powered Curtiss JN-4 Jenny trainers in World War I. Robins offered flight characteristics as straightforward as their appealing lines and modest performance. A distinctive feature was side cockpit windows that ran almost to the floor.”

Constructed of a wooden wing and steel tubing fuselage, the Curtiss Robin had an enclosed cabin that set it apart from other aircraft of its era. The cabin accommodated two passengers seated side-by-side behind the pilot. The cabin’s enclosed structure provided protection against the elements.

The Robin was produced in St. Louis, Mo., in association with the Robertson Aircraft Corp. The fixed-base operation ran the contract air mail route between St. Louis and Chicago.

Famous Robin Stunts

According to the Museum Of Flight, the Robin was a practical airplane, but best remembered for unusual endurance flights.

  • In 1930, Dale ‘Red’ Jackson performed more than 400 consecutive slow rolls in his Robin.
  • In 1929, Dale Jackson and Forrest O’Brine spent nearly 17 days circling over St. Louis. But that record was surpassed in 1935 by the brothers Fred and Al Key, who flew their Robin for more than 27 continuous days. Fuel was delivered from another Robin via hose; mail, food, oil, and spare parts came via container on a rope.
  • One of aviation’s most endearing records was set in a Curtiss Robin by Douglas “Wrong Way” Corrigan. He allegedly set off from New York for California in July 1938 and touched down in Ireland 28 hours later, claiming that he had accidentally read his compass backward. The plucky pilot — who had been denied official permission to fly the Atlantic — thus earned his nickname.

The ‘Newsboy’ Robin

From September 1929 to May 1930, a Robin C-2 was used to deliver the McCook, Neb., Daily Gazette to rural Nebraska and Kansas communities. Dubbed “The Newsboy,” the airplane flew a nonstop route of 380 miles daily, dropping bundles of newspapers out of a hole in the bottom of the fuselage from 500 feet to local carriers. The Robin C-2 was powered by a Curtiss R-600 Challenger, a six-cylinder, double-row, air-cooled, radial engine.

1932 CURTISS ROBIN SPECIFICATIONS

Mission: Pilot plus 2 passengers

Wingspan: 41 feet

Length: 25 feet 9 inches

Engine: Curtiss 90-hp OX-5 V-8 water-cooled piston engine

Maximum speed: 99.7 mph

Range: 785 miles cruising; 580 miles at full throttle

Source: Wikipedia; “Curtiss Robin 1932 – Specifications,” Aviation Heritage Foundation

This is another image from my dad, Paul Smith Maynard, who worked as an engineer in aviation for four decades. Dad began his career in about 1943 after graduating from West Virginia University. He started with Curtiss-Wright Corp., a pioneer in making flying machines. He went on to work at North American Aviation and Rockwell International.

Curtiss O-52 Owl Observation Aircraft

Curtiss O-52 Owl Observation Aircraft

The 1941 Curtiss O-52 Owl two-seat observation aircraft played a crucial role in U.S. Air Force intelligence gathering, but technological advancements made it obsolete at its debut

A 1941 black and white photo of a Curtiss O-52 on a runway during winter

The 1941 Curtiss O-52 Owl was a large, advanced two-person observation aircraft ordered by the U.S. Air Force. The monoplane was ordered into production in 1939, but it was obsolete at its launch in 1940 and mainly saw use as a trainer. (Photo from the Paul S. Maynard archive)

BY MARK MAYNARD

TThe Curtiss O-52 “Owl,” introduced in 1941, is a testament to the United States’ commitment to advancing its military aviation capabilities during World War II. A reconnaissance aircraft, the O-52 played a crucial role in intelligence gathering and surveillance operations, showcasing technological advancements of its time.

The O-52 Owl evolved from the earlier Stinson O-49 Vigilant and was designed by the renowned American aircraft manufacturer Curtiss-Wright Corp. The Owl’s robust construction and impressive performance made it an integral part of the U.S. Army Air Corps’ reconnaissance fleet. The plane’s distinctive features included a high-wing monoplane design, fixed landing gear, and an enclosed cockpit for the crew of two. A total of 203 O-52s were built.

In 1941, however, the aircraft became unsatisfactory to modern combat situations in overseas areas, according to a report in AeroCorner.com. Consequently, the aircraft was consigned to perform courier roles inside the United States and for anti-submarine warfare (A/S) on the Gulf of Mexico, Atlantic, and Pacific oceans. In November 1942, the Soviet Union ordered 30 aircraft in the Lend-Lease policy.

Performance

The Curtiss O-52 boasted a maximum speed of 220 mph and was powered by a 600-horsepower Pratt & Whitney R-1340-51 Wasp nine-cylinder radial engine. Its endurance and range were vital for long-duration reconnaissance missions, providing critical information for military strategists during global conflict.

The importance of the Curtiss O-52 in wartime operations cannot be overstated. As aviation historian John M. Andrade notes in his book “U.S. Military Aircraft Designations and Serials: 1909 to 1979.”  “The O-52 was a significant improvement over its predecessor, the O-49 Vigilant.” The book highlights how the O-52 offered enhanced capabilities, demonstrating Curtiss-Wright’s commitment to innovation in military aviation.

According to a report in HistoryOfWar.org, the O-52 two-person cockpit was extensively glazed, and the wing was mounted on top of the cockpit glazing. The Owl had a retractable undercarriage, with the wheels pulling back into wells in the side of the fuselage. There were dual controls and doors on the cockpit floor to use a camera.

“To give the plane good low-speed handling, it had full-length automatic leading-edge slots linked to wide-span trailing-edge flaps that operated whenever the slots were extended.

“It was armed with one fixed forward-firing machine gun and one flexibly mounted machine gun in the observer’s position. It had a retractable turtle back, first developed for the [Curtiss] SOC Seagull scout observation seaplane, which improved the observer’s field of fire.

In the ever-evolving landscape of military aviation during World War II, the Curtiss O-52 Owl was pivotal in shaping the success of reconnaissance and intelligence operations. Its design, performance, and adaptability underscored the United States’ commitment to staying at the forefront of aviation technology during global conflict, leaving an enduring legacy in the annals of military history.

1941 CURTISS O-52 OWL SPECIFICATIONS

Mission: Reconnaissance aircraft used by the United States Army Air Corps during World War II

Crew: 2, pilot and observer/rear gunner

Length: 26 feet 4.75 inches

Wingspan: 40 feet 9 inches

Height: 9 feet 11.5 inches

Empty weight: Approximately 3,437 pounds

Maximum takeoff weight: 4,725 pounds

Engine: 1 600-hp Pratt & Whitney R-1340-51 Wasp nine-cylinder radial engine

Maximum speed: 220 mph

Cruising speed: 192 mph

Fuel capacity: 115 gallons

Range: 700 miles

Service ceiling: 21,000 feet

Owl Armament:

  • One .30 caliber M1919 Browning machine gun in the forward fuselage;
  • One .30 caliber M1919 Browning machine gun in the rear cockpit;
  • Bombs or photo-reconnaissance equipment could be carried under the wings.

Sources: Wikipedia and HistoryOfWar.org

Note: These specifications reflect the Curtiss O-52 Owl’s design and performance characteristics, highlighting its role as a reconnaissance aircraft during a critical period in aviation history. Specific details might vary slightly depending on the variant and modifications made to individual aircraft during their operational lifespan.

 This is another image from my dad, Paul Smith Maynard, who worked as an engineer in aviation for four decades. Dad began his career in about 1943 after graduating from West Virginia University. He started with Curtiss-Wright Corp., a pioneer in making flying machines. He went on to work at North American Aviation and Rockwell International.

See more of his vintage plane pics here.

Curtiss XP-934: A Bold Experiment

Curtiss XP-934: A Bold Experiment

 The 1932 XP-934 is based on the Curtiss XP-31 Swift, the airplane maker’s first monoplane fighter

A vintage black and white photo of a 1932 Curtiss XP-934 fighter aircraft

The 1932 Curtiss XP-934 was a bold but failed experiment in aircraft design. Despite its problems, the plane’s engineering helped pave the way for future fighter designs. (Photo from the Paul S. Maynard archive)

BY MARK MAYNARD

The Curtiss XP-934 Swift was a bold but failed experiment in World War II aircraft design. Built in 1932, the XP-934 is based on the Curtiss XP-31 Swift, the airplane maker’s first monoplane fighter.

In 1932, the world is still reeling from the Great Depression, but aviation is booming. New aircraft designs are always emerging, and the Army Air Corps is eager to stay ahead of the curve. To seek innovation in aircraft design and manufacturing, the United States Army Air Corps held several competitions in the 1930s to develop new aircraft for the service. In addition to the competitions, the Army Air Corps also worked directly with aircraft manufacturers to develop new aircraft.

The newly formed Curtiss-Wright Corp. was among the makers to join the competition in 1932. The mission was to create an experimental pursuit-attack aircraft.

Pursuit aircraft became vital for their nimbleness for such duty missions as dive-bombing troops on the ground, escorting bombers to their targets in enemy territory, taking reconnaissance imagery, and clearing the airspace of opposing aircraft.

The Curtiss-Wright entry, designated XP-934 by the Army, is the first enclosed cockpit fighter aircraft for the USAAC. It was also one of the last pursuit aircraft with fixed landing gear and externally braced wings.

Why the XP-934 Failed

For the USAAC competition, Curtiss proposed a radical design that featured a low-wing monoplane configuration with a retractable landing gear. The XP-934 was powered by a 700-horsepower Wright XR-1510 Cyclone radial engine, giving the plane a top speed of more than 200 mph.

After the Curtiss XP-934’s first flight on July 25, 1932, however, it was immediately apparent that the aircraft was underpowered and overweight. The single-seat fighter weighed around 850 pounds and carried 125 gallons of fuel, four .30 caliber machine guns, and ammunition. The retractable landing gear also proved to be problematic, and it was eventually removed.

However, according to a report on Aviatar.org, the sole airframe was re-engined with a 447kW Curtiss V-1570 Conqueror V-12 powerplant. In 1933 flight tests, the V-12 offered no improvement.

The Curtiss XP-934 is never ordered into production. Despite its problems, however, the XP-934 was a significant aircraft in aviation history. It was the first enclosed cockpit fighter aircraft for the USAAC, and it helped to pave the way for future fighter designs.

Curtiss XP-934 Specifications

Crew: 1

Length: 23 feet 9 inches

Wingspan: 35 feet 3 inches

Height: 8 feet 10 inches

Wing area: 226 square feet

Empty weight: 3,334 pounds

Gross weight: 4,143 pounds

Powerplant: 1 700 hp Wright XR-1510 Cyclone 9-cylinder radial engine

Performance

Maximum speed: 215 mph

Initial climb rate: 2,130 feet per minute

Service ceiling: 22,700 feet

Range: 396 miles

Armament

4 .30 caliber machine guns

Source: Wikipedia

Note: This is another image from my dad, Paul Smith Maynard, who worked four decades in aviation as an engineer. Dad began his career in about 1943 after graduating from West Virginia University. He started with Curtiss-Wright Corp., a pioneer in making flying machines. He went on to work at North American Aviation and Rockwell International.

See more of his vintage plane pics here.