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[4] The most widely used system is based on the Boeing 2707: Initial Cost of the Code Design System, Cat. No. Boeing 2707, Boeing Aircraft Company, Seattle, Wash. 1983... From the 1994 and 1995 editions of the Code Book, update of the "Mark II" Code Design System. [5] In an attempt to make all aspect of a pre-production aircraft as realistic as possible, the designer had to use as many different parts as possible: The Boeing 2707 contains numerous dual purpose parts that can be used in either the tail assembly or the wing assembly. [6] But in terms of landing gear design, such as a self-loading tractor gear system, the cost savings is only marginal. [7] When the conventional landing gear design is used, this "compromise" is even more necessary because the designer cannot use as many parts in one assembly as a drag assembly design. [8] However, the use of the McDonnell Douglas MD-11 design, which was too "large" for a design to be classified as a "basic design" was based on the concept that for such design: Initial Cost of the Code Design System, Cat. No. Boeing 2707, Boeing Aircraft Company, Seattle, Wash. 1983... From the 1994 and 1995 editions of the Code Book, update of the "Mark II" Code Design System. [9] As to the prototype design and the test flights, of course, a different design and a more costly design was used. [10] The original time schedule for the first flight of the prototype Boeing 757 was, as published in the April 19, 1962 issue of Flight International, "The first flight of the Boeing 757 is projected to take place in the second quarter of 1962." The first flight did take place on February 18, 1964. [11] In the early 1960s, the "horizontal stabilizer" was used for the first time, when the Boeing 707 was being developed. It is still being used in the Boeing 747. [12] The purpose of the original "delta" design was to make the aircraft "less stable" (both in the straight-and-level flight and on the ground) and, at the same time, to have more space for the main engines. [13] The major disadvantage of the twin-engine design is the need for two propellers instead of one. This

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Aerodrome Design Manual Doc 9157 Part 2