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SAE ARP6152
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SAE ARP6152 2012 Edition, December 1, 2012
Aircraft Tires Service Overload Capability
Description / Abstract:
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.
Purpose
The purpose of this ARP is to provide a recommended procedure for the testing of aircraft tires for multiple tire landing gears under the foreseeable condition that one of the tires on the landing gear loses its load carrying capability during normal operations of the aircraft, resulting in a condition where the remaining tire(s) on the landing gear must carry the landing gear loads for the remainder of the flight. It is the performance of the highest loaded remaining tire which is the focus of this ARP.
Compliance with this report is not considered approval for installation on any category aircraft. The OEM for the platform for which the equipment is intended should be consulted for concurrence with the approaches proposed herein as an acceptable qualification demonstration for aircraft tires under overload conditions.
Application
This ARP is applicable to aircraft tires subject to TSO-C62 and for installation on 14 CFR Part 25 aircraft and should be considered for any aircraft configuration changes that cause any re-assessment of the design data used for the approval of the tires (e.g., to achieve TSO-C62 approval) or for the installation approval of the tires on the aircraft.
The procedures recommended herein are considered to represent an acceptable performance standard in support of FAR 25.1309 (a) and (b). OEMs may have internal standards that differ from those prescribed herein based on company specific lessons learned.
Purpose
The purpose of this ARP is to provide a recommended procedure for the testing of aircraft tires for multiple tire landing gears under the foreseeable condition that one of the tires on the landing gear loses its load carrying capability during normal operations of the aircraft, resulting in a condition where the remaining tire(s) on the landing gear must carry the landing gear loads for the remainder of the flight. It is the performance of the highest loaded remaining tire which is the focus of this ARP.
Compliance with this report is not considered approval for installation on any category aircraft. The OEM for the platform for which the equipment is intended should be consulted for concurrence with the approaches proposed herein as an acceptable qualification demonstration for aircraft tires under overload conditions.
Application
This ARP is applicable to aircraft tires subject to TSO-C62 and for installation on 14 CFR Part 25 aircraft and should be considered for any aircraft configuration changes that cause any re-assessment of the design data used for the approval of the tires (e.g., to achieve TSO-C62 approval) or for the installation approval of the tires on the aircraft.
The procedures recommended herein are considered to represent an acceptable performance standard in support of FAR 25.1309 (a) and (b). OEMs may have internal standards that differ from those prescribed herein based on company specific lessons learned.
SAE ARP6152 2012 Edition, December 1, 2012
Aircraft Tires Service Overload Capability