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VALVE, STARTER CONTROL, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR
- Aerospace Standard
- AS1607A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers the general requirements for pneumatic control valves for use with the starters on aircraft gas turbine engines.
This specification shall be used in conjunction with AS943, ARP949, and AIR1639.
Topic
Data Sets - Support Documents
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| TABLE 1 |
Issuing Committee
AE-6 Starting Systems and Auxiliary Power Committee
Welcome to the SAE AE-6, Starting Systems and Auxiliary Power Committee public forum area.
Scope: Devotes itself to aircraft engine starting by electrical, hydraulic, or pneumatic means using stored energy sources such as batteries, hydraulic accumulators, solid or liquid propellants, stored gas, or small gas turbine engines. Develops standards for aircraft starting systems. Charter: Establish standards for aerospace and industrial engine starting, auxiliary power, and related secondary systems. For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright, and Membership" line in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.Reference
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