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New and Newly Retreaded Tire Appearance

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP6307A
  • Current
Published 2019-07-02 by SAE International in United States
This document is for establishing and addressing anomalies on appearance of new and newly retreaded tires prior to installation on aircraft. It is intended to use cosmetics as well as functionality to make a determination of acceptability. However, if cosmetic appearance is not a requirement, use the inspection criteria from ARP6225. This ARP does not supersede (E)TSO-C62 minimum requirements, including marking requirements.
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Aircraft Tire Inspection - In-Service Removal Criteria

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP6225A
  • Current
Published 2019-02-13 by SAE International in United States
This document is for establishing tire removal criteria of on-wing civil aircraft tires only. This document is primarily intended for use with commercial aircraft, but may be used on other categories of civil aircraft, as applicable. The criteria are harmonized with the Care and Service Manuals of the tire manufacturers for both radial and bias tires.
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Aircraft Tires Service Overload Capability

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP6152
  • Current
Published 2018-09-02 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) defines a procedure for demonstrating service overload capability for new, main and nose landing gear, radial or bias tires fitted on multiple wheel landing gear of Part 25 certified aircraft.
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Recommended Practice for Measurement of Static and Dynamic Characteristic Properties of Aircraft Tires

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP4955A
  • Current
Published 2018-09-02 by SAE International in United States
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.
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Aircraft Tire Wear Profile Development and Execution for Laboratory Testing

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • AIR5797A
  • Current
Published 2018-08-06 by SAE International in United States
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. This is accomplished by dividing the total linear inches of wear…
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New and Newly Retreaded Tire Appearance

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP6307
  • Historical
Published 2018-02-06 by SAE International in United States
This document is for establishing and addressing anomalies on appearance of new and newly retreaded tires prior to installation on aircraft. It is intended to use cosmetics as well as functionality to make a determination of acceptability. However, if cosmetic appearance is not a requirement, use the inspection criteria from ARP6225, Aircraft Tire Removal Criteria. This ARP does not supersede (E)TSO-C62 minimum requirements including marking requirements.
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Hand Held Aircraft Tire Inflation Pressure Gauges

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP5542A
  • Current
Published 2017-09-15 by SAE International in United States
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.
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Tube, Pneumatic Tire, Aircraft

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • AS50141B
  • Current
Published 2017-09-13 by SAE International in United States
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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Aircraft Tire-to-Wheel Performance Characteristics

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP5507
  • Current
Published 2017-09-13 by SAE International in United States
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.
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Aircraft Tire Electrical Resistance Test

A-5C Aircraft Tires Committee
  • Aerospace Standard
  • ARP6404
  • Current
Published 2016-08-11 by SAE International in United States
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.
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