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Viewing 1 to 30 of 38
2010-05-11
WIP Standard
AIR6403
Develop a database which will be used to generate a set of predictive equations for a wide range of tire properties for modern (radial) aircraft tires. Methods and parameters to follow the tradition of NASA TR-R64, modified as appropriate/necessary. The application of the resulting paper will facilitate the estimation of radial tire mechanical properties for use in landing gear system models, thereby enhancing aircraft safety.
2014-10-29
WIP Standard
ARP6307
This document is for establishing and addressing anomalies on appearance of new and newly retreaded tires.
2015-02-13
WIP Standard
ARP4955B
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.
CURRENT
2014-12-01
Standard
ARP6265
This document describes a recommended test procedure to assess the burst characteristics of tires used on 14CFR Part 25 or similar transport airplanes.
CURRENT
2014-11-06
Standard
ARP6225
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.
CURRENT
2013-12-16
Standard
ARP6152
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.
CURRENT
2010-06-10
Standard
ARP6137
A tire pressure monitoring system (TPMS) is a means to electronically measure and report the current tire pressure. Some systems are capable of transmitting the information to the flight deck while other systems are for use on the ground by maintenance personnel (only). This SAE Aerospace Recommended Practice (ARP) document is intended to establish overall component and system function guidelines and minimum performance levels for a TPMS. The system should visually indicate the tire inflation pressure status. These guidelines include, but are not limited to: Design recommendations for system components, which: monitor tire inflation, and, are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment. Recommended performance and safety guidelines for a TPMS.
CURRENT
2010-07-13
Standard
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.
CURRENT
2014-06-16
Standard
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.)
CURRENT
2008-08-13
Standard
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.
CURRENT
2011-04-07
Standard
AIR5487B
This SAE Aerospace Information Report (AIR), is intended to provide a continuum on historical development of aircraft tires.
CURRENT
2008-08-21
Standard
AIR5797
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.
CURRENT
2015-08-10
Standard
AIR5800A
This SAE Aerospace Information Report (AIR) applies to landing gear tires and airframe structure for all types and models of civil and military aircraft having tires as part of the landing gear.
CURRENT
2009-07-29
Standard
AIR5651
This SAE Aerospace Information Report (AIR) is intended to provide a historical account of testing methods used during the years for Commercial Aircraft New Tire certification.
HISTORICAL
1997-11-01
Standard
ARP5257
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.
HISTORICAL
2009-02-17
Standard
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.)
HISTORICAL
2009-07-06
Standard
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.
HISTORICAL
1999-06-01
Standard
ARP5265
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.)
HISTORICAL
1997-12-01
Standard
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.
CURRENT
2007-08-22
Standard
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.
HISTORICAL
2009-10-29
Standard
AIR5800
This SAE Aerospace Information Report (AIR) applies to landing gear tires and airframe structure for all types and models of civil and military aircraft having tires as part of the landing gear.
HISTORICAL
2005-09-02
Standard
AIR5487A
This SAE Aerospace Information Report (AIR), is intended to provide a continuum on historical development of aircraft tires.
HISTORICAL
2002-06-27
Standard
AIR5487
This SAE Aerospace Information Report (AIR), is intended to provide a continuum on historical development of aircraft tires.
CURRENT
2012-10-22
Standard
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.
CURRENT
2002-08-19
Standard
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.
HISTORICAL
2004-08-04
Standard
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.
CURRENT
2011-03-28
Standard
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.
CURRENT
2012-04-05
Standard
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.
HISTORICAL
2005-01-05
Standard
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.
HISTORICAL
2001-07-01
Standard
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.
Viewing 1 to 30 of 38