Find the standard you are looking for at Engineering360. Documents are available for purchase from the IHS Standards Store.

1 - 20 of 290 results

SAE AIR5487 - (R) AIRCRAFT TIRE HISTORY Organization: SAE
Date: 2011-04-01
Description: This SAE Aerospace Information Report (AIR), is intended to provide a continuum on historical development of aircraft tires.
SAE AS1188 - AIRCRAFT TIRE INFLATION-DEFLATION EQUIPMENT Organization: SAE
Date: 2014-07-01
Description: This specification covers minimum design and test requirements for aircraft tire inflation-deflation equipment for use all types of aircraft. It shall be the responsibility of the airframe manufacturer to determine the compatibility of the requirement with the applicable aircraft and to specify requirement in excess of these minimums as necessary.
SAE ARP6404 - AIRCRAFT TIRE ELECTRICAL RESISTANCE TEST Organization: SAE
Date: 2011-03-01
Description: 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.
SAE ARP6152 - AIRCRAFT TIRES SERVICE OVERLOAD CAPABILITY Organization: SAE
Date: 2012-12-01
Description: 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.
NPFC - MS 14113 - TAPE, IDENTIFICATION, COLOR CODED, FOR AIRCRAFT TIRES Organization: NPFC
Date: 2013-02-19
Description: This specification sheet establishes requirements for color coded aircraft tire identification tape which applies to all aircraft tires manufactured/retreaded for the Department of Defense.
SAE AIR4830 - (R) AIRCRAFT TIRE PRESSURE MONITORING SYSTEMS Organization: SAE
Date: 2011-04-01
Description: The intent of this SAE Aerospace Information Report (AIR) is to inform the aerospace industry about various systems available to monitor the inflation pressure and/or temperature of an aircraft tire. The tire pressure monitoring system (TPMS), with cockpit display, is the most widely used of all aircraft tire monitoring systems, and is detailed in this document more than other systems.
SAE ARP6225 - AIRCRAFT TIRE INSPECTION - IN-SERVICE REMOVAL CRITERIA Organization: SAE
Date: 2014-11-01
Description: 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.
SAE ARP4834 - AIRCRAFT TIRE RETREADING PRACTICE - BIAS AND RADIAL Organization: SAE
Date: 2015-04-01
Description: 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.
SAE ARP5507 - AIRCRAFT TIRE-TO-WHEEL PERFORMANCE CHARACTERISTICS Organization: SAE
Date: 2002-08-01
Description: 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.
SAE ARP5542 - (R) HAND HELD AIRCRAFT TIRE INFLATION PRESSURE GAUGES Organization: SAE
Date: 2012-10-01
Description: 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.
SAE ARP5265 - (R) MINIMUM OPERATIONAL AND MAINTENANCE RESPONSIBILITIES FOR AIRCRAFT TIRE USAGE Organization: SAE
Date: 2014-06-01
Description: 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.
SAE AIR5797 - AIRCRAFT TIRE WEAR PROFILE DEVELOPMENT AND EXECUTION FOR LABORATORY TESTING Organization: SAE
Date: 2008-08-01
Description: 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.
DOT - TSO C62 - AIRCRAFT TIRES Organization: DOT
SAE AS4833 - AIRCRAFT NEW TIRE STANDARD - BIAS AND RADIAL Organization: SAE
Date: 2014-11-01
Description: Purpose This document establishes the minimum recommended performance standards for new tires to be used on civil aircraft. All new or requalified tires shall meet these standards.
NASA-TN-D-7351 - CORNERING CHARACTERISTICS OF A 40 X 14-16 TYPE VII AIRCRAFT TIRE AND A COMPARISON WITH CHARACTERISTICS OF A C40 X 14-21 CANTILEVER AIRCRAFT TIRE Organization: NASA
Date: 1973-01-01
Description: The results of this investigation indicated that the cornering capability of the 40 x 14-16 type VII aircraft tire is degraded by high ground speeds, thin-film lubrication and tire hydroplaning effects on the wet surfaces, and brake torque.
NASA-TR-R-64 - MECHANICAL PROPERTIES OF PNEUMATIC TIRES WITH SPECIAL REFERENCE TO MODERN AIRCRAFT TIRES Organization: NASA
Date: 1960-01-01
Description: A study is presented of most of the properties of pneumatic tires which are of interest to aircraft designers. The principal topics discussed are tire vertical-force-deflection characteristics; lateral, fore-and-aft, and torsional spring constants; footprint-area properties; relaxation lengths; rolling radius; cornering force, cornering power, self-aligning torque, and pneumatic caster for yawed rolling conditions; effects of wheel tilt; and tire radial growth under the influence of centrifugal forces.
NASA-TN-D-2770 - AN INVESTIGATION OF THE INFLUENCE OF AIRCRAFT TIRE-TREAD WEAR ON WET-RUNWAY BRAKING Organization: NASA
Date: 1965-01-01
Description: Aircraft tire tread wear effect on wet-runway braking.
AIR FORCE - MIL-STD-878B - METHOD OF DIMENSIONING AND DETERMINING CLEARANCE FOR AIRCRAFT TIRES AND RIMS Organization: AIR FORCE
Date: 2006-11-21
Description: The methods covered in this standard are intended to determine the clearance for aircraft tires and rims. These methods apply to all military aircraft for dimensioning and determining this clearance requirement.
NASA-TP-1569 - WEAR, FRICTION, AND TEMPERATURE CHARACTERISTICS OF AN AIRCRAFT TIRE UNDERGOING BRAKING AND CORNERING Organization: NASA
Date: 1979-01-01
Description: An investigation to evaluate the wear, friction, and temperature characteristics of aircraft tire treads fabricated from different elastomers is presented.
SAE ARP4955 - (R) RECOMMENDED PRACTICE FOR MEASUREMENT OF STATIC AND DYNAMIC CHARACTERISTIC PROPERTIES OF AIRCRAFT TIRES Organization: SAE
Date: 2007-08-01
Description: 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 peace with experience and technical advances.

1 - 20 of 290 results