Consolidated 9 XPY-1 Admiral / 16 Commodore

The Commodore twin-engined flying boat were ordered by a US-owned South American-based airline called NYRBA which challenged Pan American’s regional dominance and was later leveraged to sell its assets to Pan Am (circa 1930). Subsequently Pan Am went on to operate Commodores up to and through World War II, and some machines had short careers with successor operators.
A total of 14 were ordered for commercial use.
The Commodore failed to gain military orders in the form of XPY-1.

Model 16-1 Commodore
Engine: 2 x 575hp Pratt & Whitney R-1860 Hornet radial
Take-off weight: 7983 kg / 17600 lb
Wingspan: 30.48 m / 100 ft 0 in
Length: 18.80 m / 61 ft 8 in
Height: 4.76 m / 15 ft 7 in
Max. Speed: 206 km/h / 128 mph
Ceiling: 3430 m / 11250 ft
Range: 1609 km / 1000 miles
Crew: 3
Passengers: 22

Consolidated TW-8 / PT-1 Trusty

Improvements to the Dayton-Wright Company TW-3 design continued and included the removal of the engine cowling (for improved forward cockpit visibility) and a redesigned fuselage in a slimmer form with tandem instructor/student seating (this model being known as the “Camel” for the visible bump appearing between the two seating areas). The Camel was evaluated under the (unofficial) designation TW-8 and accepted into service as the PT-1 with 221 being delivered beginning 1924 and replacing the TW-3’s in service. The PT-1 represented the first aircraft purchase of the Army Air Service since the closing shots of World War One.

The PT-1 was a biplane aircraft with a simple two-wheel undercarriage, an engine mounted at the front of the design, a traditional tail section and twin side-by-side seating for instructor and student. The aircraft featured a choice of a Clerget or Le Rhone engines. The PT 1 basic trainer included innovations like a fuselage framework from welded chrome molybdenum steel. Because of it was so sturdy and dependable, it was nicknamed “Trusty”.

The PT-1 would eventually be replaced itself by the Consolidated PT-3 from 1928 onwards.

Hollywood’s Paul Mantz owned PT-1E A.C.26-233 two-seater which appeared in the film ‘One Man Mutiny’.

PT-1E A.C.26-233

Consolidated PT-1 Trusty
Engine: 1 x Wright-Hispano E 8-cylinder water-cooled Vee, 180hp.
Length: 27.76ft (8.46m)
Width: 34.45ft (10.50m)
Height: 9.84ft (3.00m)
Empty Weight: 1,806lbs (819kg)
Maximum Take-Off Weight: 2,577lbs (1,169kg)
Maximum Speed: 92mph (148kmh; 80kts)
Cruising speed: 68 kt / 126 km/h
Maximum Range: 350miles (563km)
Rate-of-Climb: 690ft/min (210m/min)
Service Ceiling: 13,448ft (4,099m; 2.5miles)
Accommodation: 2

PT-1E
Engine: Wright V-720, 180 hp

Consolidated TW-3

The Dayton-Wright Company TA-3 (designated with an “A” for its air-cooled engine operation) was delivered by request with an uprated Le Rhone engine of 110 horsepower. Still further evaluation models were ordered, this time with the requested Wright-Hispano I V-8, 150 horsepower engine of increased power (designated TW-3 with the “W” standing for its water-cooled engine process) finally culminating in an official order by the USAAS.
Production rights for the trainer were secured by the newly-created Consolidated Aircraft Company (established by Reuben Fleet of the Gallaudet firm) as General Motors was reviewing their commitment to aircraft production in a post-war world and would eventually shut down operations at Dayton-Wright altogether. The TW-3 was delivered by 1923 and became the first notable variant of the “Trusty” production line.

Consolidated Aircraft Corp

Gallaudet Airplane Corp was dissolved 1923 and factory acquired by Consolidated Aircraft Corporation with Reuben H.Fleet.
Original factory was quickly outgrown by the company formed May 29,1923 and moved to Buffalo, NY, in 1924, leasing part of a wartime Curtiss factory. In the 1920s and 1930s produced small numbers of civil types, but main output was military and between 1924-1932 included more than 770 PT-1 /311 and NY primary training biplanes for the USAAC and Navy, plus a small batch of similar 0- 17s for observation duties.
The creation of the civil Model 14 “Husky”trainer led to the creation of the Fleet Aircraft Division in 1929.
Thomas Morse Aircraft acquired 1929. In the 1930s Consolidated specialized in marine aircraft, P2Y twin-engined patrol flying-boats being built 1931-1933; followed by P-30 single-seat fighter monoplanes for the Army in 1933-1935.
In autumn 1935 company moved to San Diego, California, gaining a harbor for testing its maritime designs, which continued with the P3Y/PBY Catalina family. During a ten-year production life 2,400 Catalinas were built by Consolidated and hundreds more by other companies. Production of PB2Y Coronados began in 1939. In 1940 Hall Aluminium Co acquired. Company began a five-year program of building more than 11,000 B-24/C- 87/PB4Y/RY Liberator and Privateer bomber, transport, and patrol aircraft for the U.S. Services and the RAF. Liberator production was also undertaken by Ford, Douglas, and North American. Final wartime product was the TBY Sea Wolf. A 34 percent controlling interest in Consolidated acquired December 1941 by Vultee Aircraft Inc., and management links from then led to merger of the two companies on March 17,1943 as Consolidated Vultee Aircraft Corporation.
Amalgamation from March 17,1943 of Consolidated Aircraft Corporation and Vultee Aircraft Inc., whose wartime production programs are listed under these separate headings. By the end of Second World War Consolidated Vultee was largest aircraft manufacturing organization in the U.S.A., with factories at San Diego and Vultee Field, California; Fort Worth, Texas; Nashville, Tennessee; Wayne, Michigan; New Orleans, Louisiana; Miami, Florida; and Allentown, Pennsylvania; plus modification centers at Tucson, Arizona; Elizabeth City, North Carolina; and Louisville, Kentucky.
Late-war/early post-war programs included B-32 Dominator long-range bomber, L-13 liaison/observation aircraft and multi-engined B-36 intercontinental bomber. The company entered the commercial field with first flight, in summer 1946, of twin-engined Model 110, from which later stemmed well-known 240/340/440 Metropolitan series of medium-sized shorthaul airliners. Various noteworthy military prototypes included the XB-46 jet bomber, XP-81 single-seat mixed-power escort fighter, XF-92 rocket-powered interceptor, XA-41 close-support aircraft, and XF2Y Sea Dart hydro-ski fighter. A small number of R3Y Tradewind four-engined transport flying-boats Were built for the U.S. Navy. In the early 1950s Consolidated Vultee began calling its products “Convair” types, and on April 30,1954 it became the Convair Division of General Dynamics Corporation, which was then the major shareholder.

Conroy Aircraft

USA.

Formed 1968-1969 by Jack M. Conroy at Santa Barbara airport, California, offering aircraft and services for the petroleum and other “bulk” cargo industries. First ventures included turboprop conversions of Douglas DC-3 (Conroy Turbo Three) and Fairchild C-119 Flying Boxcar. Conroy developed original Guppy series of giant transports (see Aero Spacelines); also converted Canadair CL-44D- 4 swing-tailed, long-range freighter as Conroy CL-44-0, with enlarged-diameter fuselage (flown November 1969); and Stolifter (flown 1969) single-turboprop conversion of Cessna Super Skymaster, with upward-opening aft fuselage. Turboprop conversion of Grumman Albatross amphibian flown February 1970; company ceased trading shortly afterwards.

Conquest Conquest           

The Conquest is an advanced monoplane which was adapted from the Quicksilver. It is stressed for ridge soaring and thermal flying in as little as 12 mpd winds. The wing has a single surface, 12% airfoil and a load factor of 3.5.

The centre of gravity can be adjusted to the flyers weight. The Conquest goes to gether in under 15 minutes with a 7/16in spanner and a screwdriver. Optional extras were ailerons, wing fences and soaring wingtips. Landing wheels and tail skid were standard.

The airframe is made from 6061-T6 1 7/8in, 1 1/8in, 1in and 0.5in anodised aluminium, which came in a choice of colours: gold, blue, black, or red. Fully sleeved and doweled. Outer cables are 1/8in, inner cables are 5/32in, all 7 strand, stainless steel aircraft quality. All hardware is die-stamped, bent, hardened and anodised.

The sail is Howe and Bainbridge 3.8oz stabilised dacron. A fully adjustable seated harned was provided.

Conquest 52
Chord length: 4.33 ft
Wing span: 32.6 ft
Wing area: 140.8 sq,ft
Nose angle: 180˚
Weight: 63 lb
Pilot weight: 130-190 lb
Takeoff speed: 14 mph
Stall speed: 12 mph
Max speed: 30 mph
Best glide ratio (L/D): 8-1
Best L/D speed: 15 mph
Min sink: 250 fpm

Conquest 60
Chord length: 5 ft
Wing span: 32.6 ft
Wing area: 163 sq,ft
Nose angle: 180˚
Weight: 67 lb
Pilot weight: 160-225 lb
Takeoff speed: 14 mph
Stall speed: 12 mph
Max speed: 35 mph
Best glide ratio (L/D): 8-1
Best L/D speed: 15 mph
Min sink: 270 fpm