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Viewing 1 to 30 of 89
2015-09-23
WIP Standard
AIR4783A
This SAE Aerospace Information Report (AIR) presents a glossary of terms commonly utilized in the ground delivery of fuel to an aircraft and some terms relating to the aircraft being refueled. The purpose of this document is to provide background material for educational purposes to persons designing, building, and using aircraft ground refueling delivery systems.
2015-05-20
WIP Standard
AIR6510
This SAE Aerospace Information Report (AIR) comprises the technical terms and nomenclature, together with their definitions and abbreviations that are used in Aircraft Fuel Systems.
2010-08-09
WIP Standard
AIR6148
Informational discussion on Jet Fuels being introduced that are produced from feed stocks other than the traditional petroleum crude oils.
2015-04-21
WIP Standard
AIR6325
This Aerospace Information Report (AIR) is intended to provide comprehensive reference and background information pertaining to aircraft point level sensing
HISTORICAL
2011-02-10
Standard
AIR1660
A fuel level control valve/system controls the quantity of fuel in a tank being filled or emptied. This document provides a general familiarization with these mechanisms (e.g. forms they take, functions, system design considerations). This document provides the aircraft fuel system designer with information about these mechanisms/devices, so that he can prescribe the types of level control valves/systems which are best suited for his particular fuel system configuration.
2015-06-25
WIP Standard
ARP6340
This ARP provides recommended practice on the considerations and methodology to demonstrate acceptable performance of the Engine components / fuel system, and APU, whilst operating throughout the flight cycle / engine duty for continuous operation with iced fuel and short duration operation with a snowshower resulting from release of accreted ice from fuel washed surfaces, where no anti-icing additives are present (e.g. Fuel System Icing Inhibitor FSII or alternative). Two scenarios must be considered when demonstrating the capability of Engine components / fuel system, and APU to operate with fuel borne ice to satisfy certification regulations applications in support of FAA Part 23 and Part 25, CFR Part 33, and corresponding EASA CS-E regulations, and equivalent Military application requirements.
2007-10-24
WIP Standard
ARP5776
This document provides reccomended design critera, integration guidance and test methods for flames arrestors used in aircraft fuel systems.
2008-02-05
WIP Standard
AS5751
The document describes the pressure requirements for aircraft fuel systems as it relates to their refueling on the ground.
2017-06-30
WIP Standard
AIR7975
Generic overview of fuel system design and sizing, and guidelines for installation of various fuel system elements
2013-08-01
WIP Standard
AIR1408B
This report lists documents that aid and govern the design of gas turbine powered aircraft and missile fuel systems. The report lists the military and industry specifications and standards and the most notable design handbooks that are commonly used in fuel system design. The specifications and standards section has been divided into two parts, a master list arranged numerically of all industry and military specifications and standards and a component list that provides a functional breakdown and a cross-reference of these documents. It is intended that this report be a supplement to specifications MIL-F-8615; MIL-F-17874; MIL-F-38363 and MIL-F-87154. Revisions and amendments which are correct for the specifications and standards are not listed. The fuel system design handbooks are listed for fuels and for system and component design.
2017-03-07
WIP Standard
AIR1616B
This document defines design, performance, and test criteria for self-sealing breakaway valves.
2013-08-07
WIP Standard
ARP1665B
The test procedure applies to the refueling manifold system connectingn the receiver aircraft fuel tanks to the refueling source fuel pump(s) for both ground and aerial refueling. The test procedure is intended to verify that the limit value for surge pressure specified for the receiver fuel system is not exceeded when refueling from a refueling source which meets the requirements of AS1284 (reference 2). This recommended practice is not directly applicable to surge pressure developed during operation of an aircraft fuel system, such as initiating or stopping engine fuel feed or fuel transfer within an aircraft, or the pressure surge produced when the fuel pumps are first started to fill an empty fuel manifold.
HISTORICAL
1970-05-01
Standard
AIR1082
The importance of adequate component procurement specifications to the success of a hardware development program cannot be overemphasized. Specifications which are too stringent can be as detrimental as specifications which are too lax. Performance specifications, for instance, must not only identify all the component requirements, but they must also include sufficient quality assurance provisions so that compliance can be verified. It should be understood that in almost every case specifications for components will ultimately become part of a BINDING, WRITTEN CONTRACT (PO). The purpose of this document is to describe specifications, provide guidance for the preparation of fluid component specifications, and identify documents commonly referenced in fluid component specifications.
HISTORICAL
1976-03-01
Standard
AIR1408
This report lists military and industry specifications and standards which are commonly used in aerospace gas turbine fuel systems. It is intended as a supplement to specifications MIL-F-3863, MIL-F-17874 and MIL-F-8615. Revisions and amendments which are current for these specifications and standards are not listed.
HISTORICAL
1966-06-25
Standard
ARP868
No scope available.
HISTORICAL
1965-01-10
Standard
AIR839
No scope available.
HISTORICAL
1978-12-01
Standard
ARP1482
This ARP includes symbols for components and lines which are commonly used in the fuel and oil systems of airborne aerospace vehicles.
HISTORICAL
1973-01-01
Standard
AIR1184
It is intended to provide capacitance gaging system "specifiers" with the necessary tools to make value judgements concerning the various errors typically encountered in systems of this type. Thus, in addition to merely identifying the error-causes, descriptions are given concerning the basic factors from which these error-causes derive. This knowledge, when complemented with appraisals of the relative costs of minimizing the error-causes, will furnish the system specifier with a powerful tool with which to optimize gaging system accuracy, and thus, to obtain the "best possible" overall system within the constraints imposed by both design and budgetary considerations. Since the subject of capacitance gaging accuracy is quite extensive, and in some instances very complex, no attempt is made herein to present an all-inclusive and fully comprehensive evaluation of the subject. Rather, the major contributors to gaging system inaccuracy are discussed.
2017-06-30
WIP Standard
ARP8615A
This document describes the requirements for air vehicle fuel, vent, and propulsion fuel system functional components.
CURRENT
2012-01-03
Standard
AIR1616A
This document defines design, performance, and test criteria for self-sealing breakaway valves.
HISTORICAL
1997-12-01
Standard
AIR1660B
A fuel level control valve/system controls the quantity of fuel in a tank being filled or emptied. This document provides a general familiarization with these mechanisms (e.g. forms they take, functions, system design considerations). This document provides the aircraft fuel system designer with information about these mechanisms/devices, so that he can prescribe the types of level control valves/systems which are best suited for his particular fuel system configuration.
CURRENT
2016-05-17
Standard
AIR1660C
A fuel level control valve/system controls the quantity of fuel in a tank being filled or emptied on the aircraft. This document provides a general familiarization with these mechanisms (e.g., forms they take, functions, system design considerations). This document provides the aircraft fuel system designer with information about these mechanisms/devices, so that he can prescribe the types of level control valves/systems which are best suited for his particular fuel system configuration. The scope has been expanded as different aircraft manufacturers may use different type of fuel system architectures. Their refueling and defueling systems may take different configurations, may require different types of fuel control valves and may require different types of interface with the onboard Fuel Measurement System. They must also limit pressure surges and be compatible with ground refueling equipment which have varying surge potentials and create surges.
HISTORICAL
1987-04-21
Standard
AIR1660A
CURRENT
2012-12-11
Standard
AIR5774
This SAE Aerospace Information Report (AIR) is a compilation of engineering references and data useful to the technical community that can be used to ensure fuel system compatibility with composite structure. This AIR is not a complete detailed design guide and is not intended to satisfy all potential fuel system applications. Extensive research, design, and development are required for each individual application.
CURRENT
2000-08-01
Standard
AIR839C
No scope available.
CURRENT
1994-03-01
Standard
AIR4783
This SAE Aerospace Information Report (AIR) presents a glossary of terns commonly utilized in the ground delivery of fuel to an aircraft and some terms relating to the aircraft being refueled.
CURRENT
1986-09-01
Standard
AIR1408A
This report lists documents that aid and govern the design of gas turbine powered aircraft and missile fuel systems. The report lists the military and industry specifications and standards and the most notable design handbooks that are commonly used in fuel system design. The specifications and standards section has been divided into two parts, a master list arranged numerically of all industry and military specifications and standards and a component list that provides a functional breakdown and a cross-reference of these documents. It is intended that this report be a supplement to specifications MIL-F-8615, MIL-F-17874, MIL-F-38363 and MIL-F-87154. Revisions and amendments which are correct for the specifications and standards are not listed. The fuel system design handbooks are listed for fuels and for system and component design.
Viewing 1 to 30 of 89