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Aircraft Fuel System and Component Icing Test
- Aerospace Standard
Published December 04, 2007 by SAE International in United States
This Aerospace Recommended Practice (ARP) covers a brief discussion of the icing problem in aircraft fuel systems and different means that have been used to test for icing. Fuel preparation procedures and icing tests for aircraft fuel systems and components are proposed herein as a recommended practice to be used in the aircraft industry for fixed wing aircraft and their operational environment only. In the context of this ARP, the engine is not considered to be a component of the aircraft fuel system, for the engine fuel system is subjected to icing tests by the engine manufacturer for commercial and particular military applications.
|Aerospace Standard||Aircraft/Engine Fuel Pump Net Positive Suction Pressure Performance Test and Evaluation|
|Aerospace Standard||Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation|
|Aerospace Standard||Aircraft Inerting Systems|
Data Sets - Support Documents
No Datasets Available
|MIL-E-5272C||This document is not part of the subscrption.|
|MIL-F-17874B||This document is not part of the subscrption.|
|MIL-F-38336B||This document is not part of the subscrption.|
|MIL-F-8615C||This document is not part of the subscrption.|
|MIL-P-5238C||This document is not part of the subscrption.|
|MIL-S-8710B||This document is not part of the subscrption.|
|MIL-V-38003||This document is not part of the subscrption.|
|NRLReport3604||This document is not part of the subscrption.|
|WADD Tech. Rpt. 60-826||This document is not part of the subscrption.|
|WADDTech.Rpt.60||This document is not part of the subscrption.|
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