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Standard

Aircraft Tire Electrical Resistance Test

2022-02-14
CURRENT
ARP6404
This document points to a standard ASTM test method utilized by land vehicle manufacturers and others to provide the electrical resistance of a tire. It is desired that this ASTM test method is also used with aircraft tires. This method will assure that more accurate repeatable data is provided to those in the aerospace industry who request it.
Standard

Aircraft Wheel Inflation Valves Incorporating an Inflation Pressure Gauge

2020-10-26
CURRENT
ARP5543A
This specification covers the recommended design, construction, performance and testing requirements for aircraft wheel inflation valves incorporating an inflation pressure gauge which are mounted on the aircraft wheel. These valve/gauge assemblies should be appropriate for use on all aircraft types supported by tubeless tire/wheel assemblies.
Standard

Aircraft Wheel Inflation Valves Incorporating an Inflation Pressure Gauge

2015-01-12
HISTORICAL
ARP5543
This specification covers the recommended design, construction, performance and testing requirements for aircraft wheel inflation valves incorporating an inflation pressure gauge which are mounted on the aircraft wheel. These valve/gauge assemblies should be appropriate for use on all aircraft types supported by tubeless tire/wheel assemblies.
Standard

Aircraft Tire Wear Profile Development and Execution for Laboratory Testing

2018-08-06
CURRENT
AIR5797A
This SAE Aerospace Information Report (AIR) describes the current process for performing comparative wear testing on aircraft tires in a laboratory environment. This technique is applicable to both radial and bias tires, and is pertinent for all aircraft tire sizes. This AIR describes a technique based upon “wear” energy. In this technique, side wear energy and drag wear energy are computed as the tire is run through a prescribed test program. The specifics that drive the test setup conditions are discussed in Sections 4 through 7. In general, the technique follows this process: A test profile is developed from measured mechanical property data of the tires under study. Each tire is repeatedly run to the test profile until it is worn to the maximum wear limit (MWL). Several tires, typically 5 to 10, of each tire design are tested. Wear energy is computed for each test cycle and then summed to determine total absorbed wear energy. An index is calculated for each tire design.
Standard

Tube, Pneumatic Tire, Aircraft

2023-06-02
CURRENT
AS50141C
This SAE Aerospace Standard (AS) establishes requirements for manufacturing, testing, identification, packaging, and quality of tubes for application in commercial and military aircraft wheel assemblies.
Standard

Tube, Pneumatic Tire, Aircraft

2010-06-25
HISTORICAL
AS50141A
This SAE Aerospace Standard (AS) establishes requirements for manufacturing, testing, identification, packaging, and quality of tubes for application in commercial and military aircraft wheel assemblies.
Standard

Tube, Pneumatic Tire, Aircraft

2022-05-19
HISTORICAL
AS50141B
This SAE Aerospace Standard (AS) establishes requirements for manufacturing, testing, identification, packaging, and quality of tubes for application in commercial and military aircraft wheel assemblies.
Standard

Tube, Pneumatic Tire, Aircraft

2001-07-01
HISTORICAL
AS50141
This SAE Aerospace Standard (AS) establishes requirements for manufacturing, testing, identification, packaging, and quality of tubes for application in commercial and military aircraft wheel assemblies.
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