Download e-book for kindle: Airliners by John W. R. Taylor

By John W. R. Taylor

Well-known Airliners booklet from 1971 exhibiting an important airliners of that period DEPOSITили

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Air intake for third engine at base of fin. Tricycle undercarriage. Twin-wheel nose unit is offset to port and retracts sideways. Each main unit has two pairs of wheels side-by-side and retracts inward into fuselage. Wing span: 98'. Length: 114' 9". Height: 27'. Wing area: 1,461 sq. ft. WEIGHTS Basic operating weight: 73,200 lb. Max. take-off weight: 143,500 lb. PERFORMANCE Max. h. Take-off run: 6,400'. h. at 30,000' with full payload. A. in March 1964. t. 162 turbojet in the tail for improved take-off performance.

108 PERFORMANCE Max. h. Service ceiling: 37,750'. Max. h. at 30,000' with 17,640-lb. payload. Most of us had our first close look at a modern Soviet aircraft when a Tu-104 jet-liner visited London Airport in 1956. The original SO-passenger version entered regular service with Aeroflot on September 15 that year and was thus the world's second" jet transport, preceded only by the Comet 1. It was soon followed by the Tu-104A, as described above, which entered service in 1958, and by the 4-ft. longer Tu-104B with seating for 100 passengers, which entered service on Aeroflot's domestic routes inside Russia in the Spring of 1959.

Conventional control surfaces and double-slotted flaps. Tricycle undercarriage, with twin wheels on each unit. All units retract forward, main wheels into inner engine nacelles. PERFORMANCE Service ceiling: 25,000'. Take-off rlln: 5,930'. h. at 18,000' with full payload. ENGINES (Viscount 810). Four Rolls-Royce Dart Mk. p. and driving a four-blade reversiblepitch airscrew. , can be supplemented by two leading-edge slipper tanks with total capacity of 29U gal. PAYLOAD Crew of two on night deck. Seats for up to 73 passengers in pressurised cabin, with toilets, cloakroom, galley and underftoor baggage and freight holds with capacity of 25U cu.

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Airliners by John W. R. Taylor

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