Chyetverikov TA

TA
Role	Transport Amphibian
National origin	USSR
Manufacturer	Chyetverikov
Designer	Igor Vyacheslavovich Chyetverikov
First flight	June 1947
Number built	3

The TA (Transportnaya Amfibiya – transport amphibian) was an amphibious transport designed and built in the USSR from 1945.

Development

Chyetverikov designed and built the TA immediately after World War II, as an amphibious transport, using Duralumin stressed skin construction. The capacious hull had seats for six to eight passengers and room for 1,000 kg of cargo as well as the electrically operated retractable undercarriage which retracted into the sides of the hull vertically. The untapered wing sat atop a short pylon braced by 'N' struts and had electrically operated slotted flaps and fixed floats, as well as the engine nacelles. The first aircraft was completed in June 1947 and carried out sea and flight trials until the undercarriage collapsed on landing in November 1947, repairs were carried out but the Chyetverikov OKB was closed at the end of 1948, before flight trials could resume. The second aircraft, designated TA-1, had semicircular wing-tips added, retrtactable wing-tip floats and area increasing flaps, (similar to Fowler flaps), as well as other minor changes. Trials were completed and a report submitted by 20 June 1948 but production was not authorised. The third prototype was completed as the TAF (Transportnaya Amfibiya Fotografichyeskii – transport amphibian, photographic), for use as a reconnaissance or survey aircraft, with greater span, tapered, outer wings. The TAF was flown successfully late in 1948 but the OKB was closed before any further work could be carried out.

Variants

• TA – The first prototype of the TA.
• TA-1 – The second prototype of the TA with retractable floats, area increasing flaps and other changes.
• TAF – The third of the TA family was a photographic (possibly survey) aircraft with tapered outer wings of greater span.

Specifications (TA)

Data from Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995”. London, Osprey. 1995. ISBN 1-85532-405-9

General characteristics

• Crew: 2
• Capacity: 6 – 8 + 1,000kg of cargo
• Length: 14 m (45 ft 11 in)
• Wingspan: 17.2 m (56 ft 5-1/4 in)
• Wing area: 43 m² (463 ft²)
• Empty weight: 4,658 kg (10,269 lb)
• Gross weight: 6,255 kg (13,790 lb)
• Powerplant: 2 × Shvetsov ASh-21, 522.2 kW (700 hp) each

Performance

• Maximum speed: 328 km/h (204 mph)
• Range: 700 km (435 miles)

See also

Aircraft of comparable role, configuration and era

• Grumman HU-16 Albatross
• Grumman G-73 Mallard

Related lists

• List of aircraft
• List of seaplanes and flying boats

References

• Gunston, Bill. “The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995”. London, Osprey. 1995. ISBN 1-85532-405-9
• Taylor, Michael J.H. . “ Jane's Encyclopedia of Aviation. Studio Editions. London. 1989. ISBN 0-517-69186-8