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SAE AS81366A

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Boundary Layer Control System; Pressure

Available format(s)

Hardcopy , PDF

Withdrawn date

07-02-2004

Language(s)

English

Published date

07-02-2004

NOTICE
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY (NOT APPLICABLE)
6 NOTES

Covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.

DocumentType
Standard
Pages
7
PublisherName
SAE International
Status
Withdrawn

This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.

MIL-B-81365 Base Document:1966 Bleed Air Systems, General Specification for
MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES

US$95.58
Excluding Tax where applicable

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