Accession Number:

AD0827436

Title:

SUPERSONIC TRANSPORT DEVELOPMENT PROGRAM. PHASE III. BOEING MODEL 2707. AIRCRAFT ENGINE INSTALLATION SUBSYSTEM SPECIFICATION,

Descriptive Note:

Corporate Author:

BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV

Personal Author(s):

Report Date:

1966-12-31

Pagination or Media Count:

69.0

Abstract:

This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification for the Aircraft Engine Installation Subsystem AEIS for the prototype model supersonic transport airplane. Differences between the prototype and production airplanes are described. The subsystem provides the total propulsive power required by the airplane for accomplishing its intended functions. The subsystem also provides mechanical and pneumatic power for supporting airframe accessory, environmental and air inlet subsystems. The subsystem contains the engine, exhaust and thrust reverser assembly, engine accessories, engine mounting provisions, engine controls, cowling, bleed air ducting, instrumentation plumbing and wiring.

Subject Categories:

  • Civilian Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE