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Standard Test Procedure and Limit Value for Shutoff Surge Pressure of Pressure Fuel Dispensing Systems
- Aerospace Standard
- AS1284B
- Stabilized
Sector:
Issuing Committee:
Language:
English
Scope
The test procedure and related limit value are intended to apply to fixed and mobile ground pressure fuel dispensing systems and to aerial refueling tankers.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature.
Recommended Content
Aerospace Standard | Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft |
Aerospace Standard | Method-Pressure Drop Tests for Fuel System Components |
Data Sets - Support Documents
No Datasets Available
Issuing Committee
AE-5C Aviation Ground Fueling Systems Committee
Welcome to the AE-5C, 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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