Bellanca produced the 14-passenger Airbus, a single engine behemoth that cruised at 150 mph.
The Airbus 14-passenger commercial transport that was developed into Aircruiser of early 1930s for commercial and military use
1 engine
Bellanca K

The new company also had two other models that were built for special orders, the Bellanca Model J and the Model K.
A transatlantic hopeful was the Bellanca K of 1932 which may be considered as the prototype for the P-200 Air bus. The Bellanca K c/n 117 NR4864 was originally named ‘Roma’ in connection with a proposed New York-Rome flight.
For the New York-Oslo attempt of 23 August 1932 the Model K was renamed ‘Enna Jettick’. Leaving New York, at 5.43am ‘Enna Jettick’ (piloted by Thor Solberg and Carl Petersen) reached Harbor Grace, Newfoundland, at 7pmm. The proposed landing for fuel before the transatlantic leg was frustrated by fog and the crew was forced to ditch, without injury, in Darby’s Harbor, 75 miles SW of Harbor Grace, with the loss of the Model K.
Engine: Pratt & Whitney Hornet, 500 hp
Wingspan: 64 ft 6 in
Length: 39 ft 1 in
AUW: 12,000 lb
Cruise: 115 mph
Bellanca CH Pacemaker

Disappointed because the ‘Columbia’ was not the first aircraft to accomplish the New York to Paris flight, Bellanca severed all relations with Levine, and started his own company, the Bellanca Aircraft Corporation of America, and rented facilities on Staten Island, NY. The new Bellanca model was designated the CH, and was basically a commercial version of the WB-2.
CH-200 Pacemaker
First flown in 1928
CH-300 Pacemaker

First flown in 1929
CH.300 six-seat Iightpiane, Pacemaker six-seater of 1929 and flown 1931 on an 84-hour 33-minute world non-refueled endurance record.
The CH-300, produced between 1928 and 1930, was powered by both the 330 hp Wright Whirlwind and the 450 hp Pratt & Whitney Junior.
The CH-400 was powered by the 450 hp Pratt & Whitney Junior or the 420 hp Wright Whirlwind.
Both Pacemaker and Pacemaker Senior are six-seat cabin monoplanes and generally similar externally.
PM-300 Pacemaker Freighter
E Senior Pacemaker
Senior Pacemaker Srs 8
JE-1
CH-400
Wingspan: 50 ft 6 in
Length: 27 ft 11 in
Empty weight: 3000 lb
Loaded weight: 5350 lb
Max speed: 165 mph
Cruise: 155 mph
ROC: 900 fpm
Range: 1360 mi
Wright-Bellanca WB-2 Columbia

During 1926, the WB-2 won two efficiency trophies at the National Air Races in Philadelphia. Wright considered putting the aircraft into production, but decided against it to avoid alienating other aircraft companies that were potential customers for their engines. Disappointed by Wright’s decision, Bellanca left the company and joined with a young businessman named Charles Levine to form the Columbia Aircraft Company. Wright sold the WB-2 and all drawings and production rights to the new company.

Built for the 1926 Nationals, the WB-2 won all efficiency events and the endurance title in 1927. The WB-2 went on to a long and fruitful flying career starting with establishing a new world’s non-refueled endurance record of 51 hours, 11 minutes, and 59 seconds in April of 1927, piloted by Clarence Chamberlin and Bert Acosta.
In the latter half of 1926, Charles Lindbergh wanted to buy the WB-2, now named the ‘Columbia’, for his proposed flight from New York to Paris. He was rebuffed by Levine who also had designs on the flight and the $25,000 prize money. When company president Charles Levine added a stipulation that he would supply the support crew, Lindy withdrew and went to Ryan Co instead. Lindbergh then went to Ryan for his “Spirit of St. Louis”. Meanwhile Levine, in choosing the crew, managed to promise two seats to three people. So while the Columbia was grounded by a court order brought by the third party, Lindbergh took off on his successful flight to Paris.

Production rights were reacquired by Bellanca Corp to build NC/NX/NR237 Columbia for the 1927 New York-Berlin flight, piloted by Chamberlin with Charles A Levine, in which the useful load was increased to 3550 lb. Eventually, the ‘Columbia’ was cleared of litigation and took off on its successful transatlantic flight on June 4, 1927. In the cockpit were Clarence Chamberlin, one of the pilots of the endurance record and Charles Levine, who became the first transatlantic passenger. The plan was to fly all the way to Berlin, and Chamberlin had vowed to fly until they ran out of fuel. Forty-three hours later, they landed in Eisleben, Germany, the first of two successful Atlantic crossings for Bellanca’s most famous aircraft.

It was destroyed in a 1934 hangar fire.
Engine: 1 x Wright “Whirlwind” J5C, 165kW / 220hp
Wingspan: 14.0 m / 45 ft 11 in
Wing area: 25.3 sq.m / 272.33 sq ft
Length: 27’9″
Useful load: 1604 lb
Max speed: 126 mph
Cruise speed: 180 km/h / 112 mph
Stall: 47 mph
Range: 8050 km / 5002 miles
Crew: 2
Passengers: 4

Wright-Bellanca WB-1

In 1925, Bellanca went to work for the Wright Aeronautical Corporation of Paterson, NJ. His assignment there was to develop an aircraft around the new Wright Whirlwind engine. He already had a design in mind, which was an improved version of the CF, called the CG. This design evolved into the Wright-Bellanca WB-1.
First flying in September 1925 piloted by Lt Fred Becker, the WB-1 enjoyed a short, but successful flying career. The aircraft had already won one race and efficiency contest at the 1925 Nationals, piloted by Becker, before an untimely accident destroyed the craft during preparation for an attempt to break the world’s non-refueled endurance record. It was destroyed in a crash-landing during speed and payload trials in 1926 at Curtiss Field, seriously injuring Becker.
At the time of the crash, Bellanca was already working on an improved version of the WB-1 designated the WB-2.
Engine: Wright J-4, 200 hp
Wingspan: 45’0″
Length: 24’9″
Useful load: 1440 lb
Max speed: 132 mph
Cruise speed: 100 mph
Stall: 45 mph
Seats: 5
Bellanca CF

In 1921, a group of investors lured Bellanca westward to Omaha, NE, in hopes of establishing that town as a center for aircraft manufacture. Before the aircraft could be built, the company went bankrupt, but construction of the aircraft continued under the financial backing of a local motorcycle dealer named Victor Roos. The resultant aircraft, the Bellanca CF, was called by Janes’s All the World’s Aircraft “the first up-to-date transport aeroplane that was designed, built, and flown with success in the United States.” Among the local people helping to build the aircraft was the daughter of Bellanca’s landlord, Dorothy Brown. Giuseppe and she were married on November 18, 1922.
Despite its advanced design, the Bellanca CF could not compete with the economics of the time. In the days just after World War I, a surplus Curtiss Jenny could be purchased for as little as $250.00. A Bellanca CF, with a price tag of $5000.00, was just too expensive and the aircraft never went into production.
Bellanca 1912 Monoplane

At the urging of his brother Carlo, who was already established in Brooklyn, New York, Giuseppe Bellanca immigrated to America in 1911. Before the end of the year, he began construction of his third airplane design, a parasol monoplane. The engine was a 3-cylinder Anzani of 30 hp, mounted before the wing. Built in the backyard of his brother Carlo’s grocery shop in New York, after construction was completed, he took the small craft to Mineola Field on Long Island, NY, and proceeded to teach himself to fly.
He began by taxiing. He then, taxied faster, which gave way to short hops. The hops got longer, until, on May 19, 1912, there was not enough room to land straight ahead, and Bellanca had to complete a turn in order land safely. Having successfully taught himself to fly, Bellanca then set about teaching others to fly, and from 1912 to 1916, he operated the Bellanca Flying School with two more copies he built. One of his students was a young Fiorello La Guardia, the future mayor of New York City. In return for flying lessons, La Guardia taught Bellanca how to drive a car.
Engine: Anzani 30 hp
Bellanca 1909 Pusher
Bellanca’s first aircraft design was a “pusher” aircraft, somewhat similar to the Wright Flyer. Lacking funds for such an endeavor, he joined with two partners, Enea Bossi, and Paolo Invernizzi. The union of the three produced the first flight of a totally Italian-designed and Italian-built aircraft in December of 1909.
Bell X-5

The Bell X-5 was produced to investigate the aerodynamic consequences of altering the wing geometry in flight, and first flew on 20 June 1951. Work on the two X-5s began in 1948, the basis of the design being the Messerschmitt P.1101 prototype that had almost been completed by the Germans at the end of World War II. Two X-5s were manufactured by Bell, differing from their German ancestor primarily in being able to adjust their wing sweep angle in flight. The variable sweep wing could be adjusted to 20, 40 or 60 degrees the hydraulic operating mechanism automatically compensating for the inevitable shift in the position of the design’s centre of gravity.
Powered by a 4900-lb (2222-kg) thrust Allison J35-A-1; turbojet located in the lower fuselage and exhausting under the tail boom. Special fairings were also fitted to ensure that the leading and trailing edges of the wing roots presented smooth aerofoil surfaces at all times.
The first prototype (50-1838) was completed on February 15th, 1951 and first flown on June 20th, 1951. A second prototype (50-1839) followed into the air on December 10th, 1951. Both airframes accounted for some 200 total flights with the first prototype netting 133 flights alone. All three wing sweep positions were trialed on the first prototype’s ninth flight with success.

The Bell X-5 was produced to investigate the aerodynamic consequences of altering the wing geometry in flight, and first flew on 20 June 1951. Work on the two X-5s began in 1948, the basis of the design being the Messerschmitt P.1101 prototype that had almost been completed by the Germans at the end of World War II. Two X-5s were manufactured by Bell, differing from their German ancestor primarily in being able to adjust their wing sweep angle in flight. The variable sweep wing could be adjusted to 20, 40 or 60 degrees the hydraulic operating mechanism automatically compensating for the inevitable shift in the position of the design’s centre of gravity.
Powered by a 4900-lb (2222-kg) thrust Allison J35-A-1; turbojet located in the lower fuselage and exhausting under the tail boom. Special fairings were also fitted to ensure that the leading and trailing edges of the wing roots presented smooth aerofoil surfaces at all times.
The first prototype (50-1838) was completed on February 15th, 1951 and first flown on June 20th, 1951. A second prototype (50-1839) followed into the air on December 10th, 1951. Both airframes accounted for some 200 total flights with the first prototype netting 133 flights alone. All three wing sweep positions were trialed on the first prototype’s ninth flight with success.
In practice, it was found that the X-5 inherited some particularly vicious stall-spin instability characteristics. The cause was believed to be the positioning of the tail section within the design and compounded by the position of the vertical tail fin itself. As the wing sweep changed, essentially the entire aerodynamic qualities of the aircraft changed with it. The resulting action could lead the aircraft into an irrecoverable spin – this eventually occurring on October 14th, 1953 – the second prototype was lost to such a spin while running its wing sweep at 60-degrees, killing Air Force test pilot Captain Ray Popson.
The program was shelved and ultimately cancelled by the USAF. Testing did continue on with the first prototype into 1955 after which the aircraft served out the rest of her term as a chase plane until early 1958.
During Neil Armstrong’s first (and only) flight in the Bell X-5 in October 1955, the landing gear door fell off. Armstrong recalled;
“My checkout pilot was Jack McKay, and he explained that they often had trouble getting the nose gear tucked up. So, after take off, when retracting the gear, you were advised to nose over and go for about half a G. That would help get the nose gear in place, due to less download on the gear. So I attempted to do it, but it didn’t seem to be locking up. In thee meantime, I was nosing over, getting into a nose down position and, of course, the aircraft was speeding up, and I suspect that I actually ‘oversped’ the gear-limit speed, knocking the fairing door off. I never got the indication that the gear was completely retracted, so I put it back down and wasn’t able to conduct my flight plan. I never got a chance to fly the airplane again. They decided it was at the end of its research lifetime”.
The remaining Bell X-5 was handed over to the National Museum of the United States Air Force in Dayton, Ohio, in March of 1958 where it resides even today as part of the Research & Development Gallery at Wright-Patterson Air Force Base.
Engine: 1 x Allison J35-A-17 tubojet, 2223kg
Take-off weight: 4536 kg / 10000 lb
Wingspan: 5.66-9.39 m / 18 ft 7 in-30 ft 10 in
Length: 10.16 m / 33 ft 4 in
Height: 3.66 m / 12 ft 0 in
Max. speed: 1046 km/h / 650 mph

Bell X-2

Two X-2s were built by Bell Aircraft at their Niagara Falls, New York, facility. The airframes were composed primarily of stainless steel and “K-Monel,” an advanced lightweight heat-resistant stainless steel alloy swept wings.
The powerplant comprised a 15,500 lb (6804 kg) thrust throttable Curtiss-Wright XLR-25-CW-1 liquid propellant rocket.
The jettisonable cockpit can be separated from the fuselage in an emergency by an explosive charge, a ribbon-type parachute lowering the complete cockpit to a lower altitude at which the pilot can bale put.
The first X-2 was dropped into Lake Ontario on 12 May 1953 following an explosion and fire that also caused extensive damage to the EB-50A launch aircraft.
A leather gasket made by the Ulmer Company, when saturates with liquid oxygen, was so unstable that a shock of and magnitude caused the gasket to blow. A number of accidents occurred involving the X-1-3, X-1A, X-1D, and X-2, before the malfunctioning gasket was identified and a fix made.

The second aeroplane made the type’s first powered flight on 18 Novernber 1955, and recorded an altitude of 126,000 ft (38,465 m) as well as a speed of Mach 3.2 (2,094 mph; 3,370 km/h), the latter being recorded during the type’s fatal last flight on 27 Septernber 1956. This remained the highest speed at which man had flown until 1961. The aircraft experienced “inertia coupling” resulting in complete loss of control—pilot Milburn Apt was killed in the accident. No examples of the X-2 survive.
Dick Day warned his air force associates not to push ahead so fast with the X-2, piloted by Ivan Kinchloe, Frank ‘Pete’ Everest, and Milburn G. Apt. Data from their work was confirming evidence from NACA wind tunnel tests that the X-2 would experience ‘rapidly deteriorating directional and lateral (roll) stability near Mach 4’. On 25 April 1956, the X-2 broke the sound barrier for the first time. Less than a month later, it flew past Mach 2. By mid-summer it was pushing Mach 3. When Mel Apt took the X-2 up on 27 September 1956, for his very first flight in the aircraft, his flight plan called for ‘the optimum maximum energy flight path,’ one that would rocket him past Mach 3 – and into roll coupling. The fatal crash happened just as Dick Day thought it might. At 65,000ft and a speed of Mach 3.2, Apt lost control of the X-2 due to roll coupling and became unconscious. By the time he came to it was too late. He died instantly when the plane hit the desert floor.
The two X-2s achieved 20 flights in total between 1952 and 1956.

Engine: 1 x Curtiss-Wright XLR25-CW-1 rocket engine, 6804kg
Wingspan: 9.75 m / 31 ft 12 in
Length: 13.41 m / 43 ft 12 in
Height: 4.11 m / 13 ft 6 in
Max. speed: M3.2 (2,094 mph; 3,370 km/h).
Ceiling: 38405 m / 126,000 ft / 38,465 m
Crew: 1
