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Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems
- Aerospace Standard
- ARP1616B
- Cancelled
Sector:
Issuing Committee:
Language:
English
Scope
This document defines design, performance, and test criteria for self-sealing breakaway valves for use in crash-resistant aircraft fuel systems.
Rationale
This document should have been cancelled previously, when it was replaced by AIR1616A, which contains the same information, with updated references to other specifications, and was stabilized in 2012. It is now confusing to have two specifications covering exactly the same subject, which are virtually word for word identical. Since AIR1616A has been more recently updated than ARP1616A, then ARP1616A should be cancelled. AIR1616A will be updated to state that it supersedes ARP1616A.
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Topic
Data Sets - Support Documents
No Datasets Available
Issuing Committee
AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee
Welcome to the AE-5A, Aerospace Fuel, Inerting and Lubriation Systems public forum area.
Scope: Has responsibility for the resolution of problems in either design or service usage of aerospace fuel, oil and oxidizer systems, their components such as valves, pumps, couplings, fuel cells, quantity and flow gages, and tanks, and related problems as presure surger, icing, electrification, and safety. Develops standards addressing fuel, oil and oxidizer 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" link 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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