Standard
Aircraft Recommended Practice, Ball-On-Cylinder (Boc) Aircraft Turbine Fuel Lubricity Tester
2002-12-16
CURRENT
MAP1794
Search Results
Standard
Recommended Practices for Lubricating Oil Filters, General Aviation Reciprocating Engine (Piston Type) Aircraft
2020-04-29
CURRENT
ARP1400B
This SAE Aerospace Recommended Practice (ARP) establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 345 to 689 kPa (50 to100 psig).
Standard
RECOMMENDED PRACTICES FOR GENERAL AVIATION FILTERS, RECIPROCATING ENGINE (PISTON TYPE) AIRCRAFT
1975-09-01
HISTORICAL
ARP1400
This recommended practice establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 50 - 100 psig.
Standard
AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS
2011-08-10
HISTORICAL
AIR4023
This AIR discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
Standard
AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS
1994-03-01
HISTORICAL
AIR4023A
This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
Standard
Aircraft Turbine Fuel Contamination History and Endurance Test Requirements
2007-10-18
HISTORICAL
AIR4023B
This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
Standard
Aircraft Turbine Fuel Contamination History and Endurance Test Requirements
2021-11-01
CURRENT
AIR4023C
This document discusses the history and development of endurance requirements, provides an analysis of test contaminant material and includes a discussion of future requirements.
Standard
Transmitter, Pressure, Fuel, 0-600 psi
2007-12-04
HISTORICAL
AS6302
This specification covers one type of fuel pressure transmitter designated MS28005-7.
Standard
Transmitter, Pressure, Fuel, 0-600 psi
2016-10-27
CURRENT
AS6302A
This specification covers one type of fuel pressure transmitter designated MS28005-7.
Standard
GLAND DESIGN, ELASTOMERIC O-RING SEALS, STATIC RADIAL AND FACE 800 PSI MAXIMUM SERVICE
2007-12-04
HISTORICAL
AS4873
This document establishes standard gland dimensions for low pressure static radial O-ring seal applications and provides recommendations for modifying these glands in special applications. No provisions are made in this document for anti-extrusion devices.
Standard
Impact of Copper Contamination on the Thermal Stability of Jet Fuels
2019-04-11
CURRENT
AIR6443
This SAE Aerospace Information Report (AIR) discusses the sources of Copper in aviation jet fuels, the impact of Copper on thermal stability of jet fuels and the resultant impact on turbine engine performance, and potential methods for measurement and reduction of the catalytic activity of Copper contamination in jet fuels. This document is an information report and does not provide recommendations or stipulate limits for Copper concentrations in jet fuels.
Standard
AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER
1974-01-01
HISTORICAL
AIR1326
The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system and the aircraft engine fuel system, and limitations in the usage of the V/L concept.
Standard
Aircraft Fuel System Vapor-Liquid Ratio Parameter
2020-04-29
CURRENT
AIR1326A
The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system and the aircraft engine fuel system, and limitations in the usage of the V/L concept.
Standard
Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations
2007-02-15
CURRENT
AS4273A
This document establishes requirements, test procedures, and acceptance criteria for the fire testing of fluid handling components and materials used in aircraft fluid systems. It is applicable to fluid handling components other than those prescribed by AS1055 (e.g., hoses, tube assemblies, coils, and fittings). It also is applicable to materials, wiring, and components such as reservoirs, valves, gearboxes, pumps, filter assemblies, accumulators, fluid-cooled electrical/electronic components, in-flight fluid system instrumentation, hydromechanical controls, actuators, heat exchangers, and manifolds. These components may be used in fuel, lubrication, hydraulic, or pneumatic systems.
Standard
Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard
2018-05-16
CURRENT
ARP5794A
This specification covers the general design, testing, and safety requirements for aircraft tank mounted fuel booster pumps used for engine fuel feed, transfer, and jettison.
