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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.
Standard

Tube, Pneumatic Tire, Aircraft

2005-01-05
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

2012-04-05
CURRENT
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

Tire Burst Test Methodology

2014-12-01
CURRENT
ARP6265
This document describes a recommended test procedure to assess the burst characteristics of tires used on 14CFR Part 25 or similar transport airplanes.
Standard

Aircraft Tire Electrical Resistance Test

2011-03-28
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 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

Recommended Practice for the Measurement of Static and Dynamic Properties of Aircraft Tires

1997-12-01
HISTORICAL
ARP4955
The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish guidelines for the measurement of static and dynamic characteristic properties of aircraft tires. It is intended as a general guide toward standard practice, but may be subject to frequent changes to keep pace with experience and technical advances. It replaces the previous SAE document, AIR1380.
Standard

Recommended Practice for Measurement of Static and Dynamic Characteristic Properties of Aircraft Tires

2007-08-22
CURRENT
ARP4955A
The purpose of this SAE Aerospace Recommended Practice (ARP) is to establish guidelines for the measurement of static and dynamic characteristic properties of aircraft tires. It is intended as a general guide toward standard practice, but may be subject to frequent changes to keep pace with experience and technical advances. This revision (Revision A) is also intended to provide suggested guidelines for synthesizing tire dynamic data necessary for landing gear shimmy analyses.
Standard

Minimum Operational and Maintenance Responsibilities for Aircraft Tire Usage

2020-01-24
WIP
ARP5265C

This SAE Aerospace Recommended Practice (ARP) sets forth criteria for the installation, inflation, inspection, and maintenance of aircraft tires as well as criteria for the maintenance of the operating environment so as to achieve the purpose stated in 1.1. (Definitions of terms related to aircraft tires are found in 2.2.)

Standard

Minimum Operational and Maintenance Responsibilities for Aircraft Tire Usage

2009-02-17
HISTORICAL
ARP5265A
This SAE Aerospace Recommended Practice (ARP) sets forth criteria for the installation, inflation, inspection, maintenance and removal of aircraft tires as well as criteria for the maintenance of the operating environment so as to achieve the purpose stated in 1.1. (Definitions of terms related to aircraft tires is found in 2.2.)
Standard

Minimum Operational and Maintenance Responsibilities for Aircraft Tire Usage

2014-06-16
CURRENT
ARP5265B
This SAE Aerospace Recommended Practice (ARP) sets forth criteria for the installation, inflation, inspection, and maintenance of aircraft tires as well as criteria for the maintenance of the operating environment so as to achieve the purpose stated in 1.1. (Definitions of terms related to aircraft tires are found in 2.2.)
Standard

Aircraft Tire-to-Wheel Performance Characteristics

2002-08-19
CURRENT
ARP5507
The performance of an aircraft tire/wheel assembly in service is dependent on the geometrical fit, load distribution, and performance at the tire/wheel interface while rolling. This document focuses on the tire-to-wheel circumferential movement for a new tubeless tire.
Standard

Hand Held Aircraft Tire Inflation Pressure Gauges

2012-10-22
CURRENT
ARP5542A
This SAE Aerospace Recommended Practice (ARP) covers the design, construction, performance and testing requirements for hand held aircraft tire inflation pressure gauges with valve stem attachment chuck to be used with all aircraft types. The ground-based gauges in this specification are those which are designed to read the tire inflation pressure from a position adjacent to the tire.
Standard

Hand Held Aircraft Tire Inflation Pressure Gauges

2004-08-04
HISTORICAL
ARP5542
This SAE Aerospace Recommended Practice (ARP) covers the design, construction, performance and testing requirements for hand held aircraft tire inflation pressure gauges with valve stem attachment chuck to be used with all aircraft types. The gauges in this specification are those which are designed to read the tire inflation pressure from a position adjacent to the tire.
Standard

Aircraft Wheel Inflation Valves Incorporating an Inflation Pressure Gauge

2020-09-16
WIP
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

2008-08-13
CURRENT
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 Retreading Practice - Bias and Radial

2008-09-11
HISTORICAL
ARP4834A
This SAE Aerospace Recommended Practice (ARP) sets forth criteria for the selection, inspection, retread and repair of worn civil aircraft tires, and the means to verify that the retreaded tire is suitable for continued service. This document is applicable to both bias ply and radial aircraft tires qualified subsequent to the adoption of this document.
Standard

Tire Overspeed Landing Test

2010-07-13
CURRENT
ARP5257B
This document covers the basis of, and test procedure for, an overspeed landing test on aircraft tires with rated speeds of 190 mph (306 km/h) and above. The conditions requiring an overspeed test, alternatives, test requirements and pass/fail criteria are addressed.
Standard

Aircraft Tire Retreading Practice - Bias and Radial

1995-11-01
HISTORICAL
ARP4834
This SAE Aerospace Recommended Practice (ARP) sets forth criteria for the selection, inspection, retread and repair of worn civil aircraft tires, and the means to verify that the retreaded tire is suitable for continued service. This document is applicable to both bias ply and radial aircraft tires qualified subsequent to the adoption of this document.
Standard

Tire Overspeed Landing Test

2009-07-06
HISTORICAL
ARP5257A
This document covers the basis of, and test procedure for, an overspeed landing test on aircraft tires with rated speeds of 190 mph (306 km/h) and above. The conditions requiring an overspeed test, alternatives, test requirements and pass/fail criteria are addressed.
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