Standard
Uniform Measurement Units for Leakage Rates
2016-10-27
CURRENT
MAP4053A
Applications include specifications, reports, ratings, texts etc., where fluid leakage rates are treated.
Search Results
Standard
UNIFORM MEASUREMENT UNITS FOR LEAKAGE RATES
2007-12-04
HISTORICAL
MAP4053
Applications include specifications, reports, ratings, texts etc., where fluid leakage rates are treated.
Standard
Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel Systems
2012-01-03
HISTORICAL
AIR1616A
This document defines design, performance, and test criteria for self-sealing breakaway valves.
Standard
SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL SYSTEMS
1983-04-04
HISTORICAL
AIR1616
This document defines design, performance, and test criteria for self-sealing breakaway valves.
Standard
SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS
2007-12-04
HISTORICAL
ARP1616A
This document defines design, performance, and test criteria for self-sealing breakaway valves for use in crash-resistant aircraft fuel systems.
Standard
Recommended Materials and Practices for Use with Cryogenic Propellants
2000-08-01
CURRENT
AIR839C
No scope available.
Standard
RECOMMENDED MATERIALS AND PRACTICES FOR USE WITH CRYOGENIC PROPELLANTS
1965-01-10
HISTORICAL
AIR839
Standard
Pressure Fueling Simulator for Evaluating Aircraft Fuel Systems Under Design Pressure Fueling Conditions
2002-12-16
CURRENT
ARP816
Standard
PERFORMANCE TESTING OF GAS TURBINE LUBE OIL FILTER ELEMENTS
1994-07-01
HISTORICAL
AIR1666
This SAE Aerospace Information Report (AIR) reviews performance testing parameters for noncleanable, often referred to as disposable, aircraft gas turbine engine lubricant filter elements.
Standard
Nozzles and Ports – Gravity Fueling Interface Standards for Civil Aircraft
2012-01-03
CURRENT
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.
Standard
Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft
1997-08-01
HISTORICAL
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.
Standard
Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft
2006-03-24
HISTORICAL
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.
Standard
Minimization of Electrostatic Hazards in Aircraft Fuel Systems
2013-08-09
HISTORICAL
AIR1662A
This SAE Aerospace Information Report (AIR) provides background information, technical data and related technical references for minimization of electrostatic hazards in aircraft fuel systems. Techniques used to minimize the electrostatic hazard include: a Reducing fueling rate into tank bays including use of multiple refueling inlet nozzles. b Reducing refuel plumbing flow velocities. c Introducing fuel into the tank at a low velocity near the bottom and directing it to impinge upon a grounded conducting surface. d Avoiding electrically isolated conductors in the fuel tank. e Using conductivity additives in the fuel.
Standard
Method-Pressure Drop Tests for Fuel System Components
2020-05-18
CURRENT
ARP868D
This document describes recommended methods, associated equipment, and test setups to assist in understanding and conducting pressure drop tests on fuel system components. Background information and suggestions are provided to improve accuracy and repeatability of test results. Although written specifically for fuel system components, the methods, equipment, and suggestions presented herein apply equally to pressure drop tests conducted on any equipment utilizing incompressible fluids.
Standard
Method-Pressure Drop Tests for Fuel System Components
2013-08-09
HISTORICAL
ARP868C
This document provides recommended methods and describes associated equipment and test setups to assist in understanding and conducting pressure drop tests on fuel system components. Background information and suggestions are provided as means of improving accuracy and repeatability of test results. Although written specifically for fuel system components, the methods, equipment and suggestions presented herein apply equally to pressure drop tests of other liquid-handling devices.
Standard
MINIMIZATION OF ELECTROSTATIC HAZARDS IN AIRCRAFT FUEL SYSTEMS
1991-05-28
HISTORICAL
AIR1662
Standard
METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS
1994-09-01
HISTORICAL
ARP868B
To describe useful methods for conducting pressure drop tests of fuel system components for MIL-F-8615 or similar requirements and to present general suggestions for improving accuracy of test results.
Standard
METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS
1983-06-01
HISTORICAL
ARP868A
To describe useful methods for conducting pressure drop tests of fuel system components for MIL-F-8615 or similar requirements; and to present general suggestions for improving accuracy of test results.
Standard
Impact of Changes in Test Dust Contaminants and Particle Counter Calibration on Laboratory Filter Element Performance and Fluid Cleanliness Classes
2003-07-03
HISTORICAL
AIR5455
This SAE Aerospace Information Report (AIR) discusses the impact of the ISO Test Dusts, chosen as replacement contaminants for the Arizona Test Dusts (AC Test Dusts), and the ISO calibration procedure ISO 11171 for automatic particle counters, which replaces the calibration procedure ISO 4402 (1991), on laboratory performance of filter elements utilized in aerospace lubrication, hydraulic and fuel systems, and fluid cleanliness levels determined with automatic particle counters.
Standard
Impact of Changes in Test Dust Contaminants and Particle Counter Calibration on Laboratory Filter Element Performance and Fluid Cleanliness Classes
2012-01-03
CURRENT
AIR5455A
This SAE Aerospace Information Report (AIR) discusses the impact of the ISO Test Dusts, chosen as replacement contaminants for the Arizona Test Dusts (AC Test Dusts), and the ISO calibration procedure ISO 11171 for automatic particle counters, which replaces the calibration procedure ISO 4402 (1991), on laboratory performance of filter elements utilized in aerospace lubrication, hydraulic and fuel systems, and fluid cleanliness levels determined with automatic particle counters.
