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Viewing 1 to 30 of 47
CURRENT
2016-11-29
Standard
AS5877B
This SAE Aerospace Standard (AS) prescribes requirements for the various types of nozzles that are used for the refueling and defueling of aircraft fitted with pressure fuel servicing systems. It is to be used as a replacement for MIL-N-5877, MS29520 and for all commercial applications.
2016-05-25
WIP Standard
ARP5918A
This SAE Aerospace Recommended Practice (ARP) establishes the minimum recommended Test Stand Setup and Procedures for inspecting and testing Aircraft Refuelers. The inspection and test procedure shall be used to evaluate the operation and performance of an Aircraft Refueler to assure that it meets the minimum refueling performance criteria and is fit for aircraft fueling and/or defueling operations. These procedures shall be used to test new Aircraft Refuelers and may be used to perform routine tests to confirm that the Aircraft Refuelers comply with the minimum performance criteria as specified herein. This document covers all types of Aircraft Refuelers, stationary (e.g., cabinet type units) or mobile (e.g., hydrant service vehicles, tankers, etc). NOTE: Aircraft refueling vehicle design and operating requirements are provided in separate SAE ARP Documents.
2016-04-22
WIP Standard
AIR5691A
This document is applicable to commercial and military aircraft fuel quantity indication systems. It is intended to give guidance for system design and installation. It describes key areas to be considered in the design of a modern fuel system, and builds upon experiences gained in the industry in the last 10 years.
CURRENT
2015-10-21
Standard
J2600_201510
SAE J2600 applies to the design and testing of Compressed Hydrogen Surface Vehicle (CHSV) fueling connectors, nozzles, and receptacles. Connectors, nozzles, and receptacles must meet all SAE J2600 requirements and pass all SAE J2600 testing to be considered as SAE J2600 compliant. This document applies to devices which have Pressure Classes of H11, H25, H35, H50 or H70.
2015-09-24
WIP Standard
ARP5789A
This document contains general criteria for the planning, design, and construction of military and commercial ground based aviation fueling facilities that receive, store, distribute, and dispense liquid aviation turbine fuels at airports to both fixed and rotary wing aircraft.
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.
2015-08-21
WIP Standard
ARP6344
This Aerospace Recommended Practice (ARP) establishes a test procedure and recommended surge pressure limit value for the evaluation of fixed aircraft pressure fuel dispensing systems. Note: This ARP is not applicable to aerial refueling systems or mobile aircraft refueling systems (trucks, hydrant servicing vehicles, etc.). Testing of aerial refueling systems is addressed in ARSAG documents. Testing of mobile refueling systems is addressed in ARP 5918. Note: This ARP does not address requirements that may be specific to the testing of shipboard aircraft refueling systems.
CURRENT
2015-08-13
Standard
ARP5818A
This document is a guideline for the design and operation of Aviation Aircraft Refueling Vehicles and for the materials, components, and systems used thereon. The criteria set forth herein are the minimum recommendations for all types of aircraft refueling vehicles, including tanker vehicles, hydrant service vehicles, towable hydrant carts, fixed refueling cabinets, and any other type of aircraft refueling vehicles used at airports for aircraft refueling operations with nominal operating fuel pressures and flow rates as specified within this document.
CURRENT
2015-07-17
Standard
AS1284B
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.
CURRENT
2015-07-04
Standard
ARP694C
This ARP is intended to cover all external lights on the tanker and fixed wing receiver airplanes used to accomplish aerial refueling. This ARP describes lights used for two basic types of aerial refueling: The Probe and Drogue, and the Boom/Receptacle method.
2014-04-25
WIP Standard
AIR4782B
This SAE Aerospace Information Report (AIR) presents historical information and background data related to hydrant valves and couplers used in worldwide ground refueling of commercial aircraft (hereafter generically referred to as hydrant devices). Military hydrant devices are not included since their mission requirements demand approaches that may differ.
CURRENT
2014-04-09
Standard
J2799_201404
This standard specifies the communications hardware and software requirements for fueling Hydrogen Surface Vehicles (HSV), such as fuel cell vehicles, but may also be used where appropriate, with heavy duty vehicles (e.g., busses) and industrial trucks (e.g., forklifts) with compressed hydrogen storage. It contains a description of the communications hardware and communications protocol that may be used to refuel the HSV. The intent of this standard is to enable harmonized development and implementation of the hydrogen fueling interfaces. This standard is intended to be used in conjunction with the hydrogen fueling protocol, SAE J2601, Compressed Hydrogen Light Duty Vehicle Fueling Protocol and SAE J2600, Compressed Hydrogen Surface Vehicle Fueling Connection Devices.
CURRENT
2013-12-19
Standard
AS47B
CURRENT
2013-09-10
Standard
AS1875A
This SAE Aerospace Standard (AS) presents all appropriate boss dimensions from .125 inch to 2.0 inch tube sizes.
CURRENT
2013-01-04
Standard
AIR5691
This document is applicable to commercial and military aircraft fuel quantity indication systems. It is intended to give guidance for system design and installation. It describes key areas to be considered in the design of a modern fuel system, and builds upon experiences gained in the industry in the last 10 years.
HISTORICAL
2012-11-19
Standard
J2600_201211
SAE J2600 applies to the design and testing of Compressed Hydrogen Surface Vehicle (CHSV) fueling connectors, nozzles, and receptacles. Connectors, nozzles, and receptacles must meet all SAE J2600 requirements and pass all SAE J2600 testing to be considered as SAE J2600 compliant. This document applies to devices which have Pressure Classes of H11, H25, H35, H50 or H70.
CURRENT
2012-01-03
Standard
AS1852D
This SAE Aerospace Standard (AS) defines the maximum allowable free opening dimensions for airframe fueling ports on civil aircraft that require the exclusive use of gasoline as an engine fuel, and the minimum free opening dimensions for airframe fueling ports on civil aircraft that operate with turbine fuels as the primary fuel type and with gasoline as the emergency fuel type. This SAE Aerospace Standard (AS) also defines the features and dimensions for airframe refueling ports on civil aircraft that require the exclusive use of turbine fuel as an engine fuel. In addition, this document defines the minimum fuel nozzle spout dimensions for turbine fuel ground service equipment, and the maximum fuel nozzle spout diameter for gasoline ground service equipment.
CURRENT
2011-08-10
Standard
ARP86C
These recommendations are written to cover the subject of engine exhaust gas to air type heat exchangers under the following classifications:
CURRENT
2008-08-12
Standard
AIR4782A
This SAE Aerospace Information Report (AIR) presents historical information and background data related to hydrant valves and couplers used in worldwide ground refueling of commercial aircraft (hereafter generically referred to as hydrant devices). Military hydrant devices are not included since their mission requirements demand approaches that may differ.
HISTORICAL
2007-05-24
Standard
J2799_200705
This technical information report specifies a guideline for the hardware requirements for fueling a Hydrogen Surface Vehicle (HSV) with compressed hydrogen storage at a Nominal Working Pressure of 70MPa. It contains a description of the receptacle geometry and optional communication hardware and communications protocol to refuel the HSV. The intent of this document is to enable harmonized development and implementation of the hydrogen fueling interfaces. It is intended to be utilized for the hydrogen vehicle field evaluation until enough information is collected to enable standardardization. The receptable portion of this TIR is to be reevaluated utilizing international field data in approximately 2 years and subsequently superseded by J2600 in the 2009 timeframe.
CURRENT
2006-07-24
Standard
ARP5918
This SAE Aerospace Recommended Practice (ARP) establishes the minimum recommended Test Stand Setup and Procedures for inspecting and testing Aircraft Refuelers. The inspection and test procedure shall be used to evaluate the operation and performance of an Aircraft Refueler to assure that it meets the minimum refueling performance criteria and is fit for aircraft fueling and/or defueling operations. These procedures shall be used to test new Aircraft Refuelers and may be used to perform routine tests to confirm that the Aircraft Refuelers comply with the minimum performance criteria as specified herein. This document covers all types of Aircraft Refuelers, stationary (e.g., cabinet type units) or mobile (e.g., hydrant service vehicles, tankers, etc). NOTE: Aircraft refueling vehicle design and operating requirements are provided in separate SAE ARP Documents.
HISTORICAL
2006-03-24
Standard
AS1852C
This SAE Aerospace Standard (AS) defines the maximum allowable free opening dimensions for airframe fueling ports on civil aircraft that require the exclusive use of gasoline as an engine fuel, and the minimum free opening dimensions for airframe fueling ports on civil aircraft that operate with turbine fuels as the primary fuel type and with gasoline as the emergency fuel type. This SAE Aerospace Standard (AS) also defines the features and dimensions for airframe refueling ports on civil aircraft that require the exclusive use of turbine fuel as an engine fuel. In addition, this document defines the minimum fuel nozzle spout dimensions for turbine fuel ground service equipment, and the maximum fuel nozzle spout diameter for gasoline ground service equipment.
CURRENT
2006-01-27
Standard
ARP5789
This document contains general criteria for the planning, design, and construction of military and commercial ground based aviation fueling facilities that receive, store, distribute, and dispense liquid aviation turbine fuels at airports to both fixed and rotary wing aircraft.
HISTORICAL
2003-10-17
Standard
ARP5818
This document is a guideline for the design of an Aviation Aircraft Refueling and Defueling Tanker Vehicle and for the materials and components used thereon. The criteria set forth herein are the minimum recommendations and are limited to aircraft refueling vehicles for airport operations with operating fuel pressures and flow rates as specified within this document.
HISTORICAL
2002-10-04
Standard
J2600_200210
SAE J2600 applies to design, safety and operation verification of Compressed Hydrogen Surface Vehicle (CHSV) refuelling connection devices hereinafter referred to as nozzle and receptacle. CHSV Refuelling nozzles and receptacles shall consist of the following components, as applicable. Alternatives may be used as long as the alternative geometries shall not be interchangeable with the standard geometry specified in this SAE Standard and the standard geometry in Section 6 provides insufficient flow rates: a. Receptacle and protective cap (mounted on vehicle) (see Section 6 and 7); b. Nozzle (see Section 5). This document applies to devices which have Working Pressures of 25 MPa, 35 MPa, 50 MPa or 70 MPa hereinafter referred to in this document as the following (see 9.1c): H25 - 25 MPa at 15 °C; H35 - 35 MPa at 15 °C; H50 - 50 MPa at 15 °C; H70 - 70 MPa at 15 °C.
HISTORICAL
1997-08-01
Standard
AS1852B
This SAE Aerospace Standard (AS) defines the maximum allowable free opening dimensions for airframe fueling ports on civil aircraft that require the exclusive use of gasoline as an engine fuel and the minimum free opening dimensions for airframe fueling ports on civil aircraft that operate with turbine fuels as the primary fuel type. In addition, this document defines the minimum fuel nozzle tip dimensions for turbine fuel ground service equipment and the maximum fuel nozzle tip diameter for gasoline ground service equipment. This document establishes the essential interface dimensions for airframe refueling ports and ground refueling nozzles that are intended for use on civil aircraft with gravity fuel servicing provisions. Primary intent of the standardized interface limits detailed in this document is the prevention of misfueling reciprocating engine powered aircraft with turbine fuel when exclusive use of aviation gasoline is required for safe operation.
HISTORICAL
1996-11-01
Standard
ARP86B
These recommnedations are written to cover the subject of engine exhaust gas to air type heat exchangers under the following clasifications: Cabin Heating: (All occupied regions and windshields heating). Wing and empennage heating. Engine and Accesory Heating: (When heater is installed as part of the aircraft). These recommendations are not intended to cover the design of secondary exchangers which may be required when engine exhaust gas to air type heat exchangers are used in supplying ventilating air.
HISTORICAL
1996-11-01
Standard
ARP86A
null, null
These recommnedations are written to cover the subject of engine exhaust gas to air type heat exchangers under the following clasifications: Cabin Heating: (All occupied regions and windshields heating). Wing and empennage heating. Engine and Accesory Heating: (When heater is installed as part of the aircraft). These recommendations are not intended to cover the design of secondary exchangers which may be required when engine exhaust gas to air type heat exchangers are used in supplying ventilating air.
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