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Standard

AIRCRAFT BRAKE TEMPERATURE MONITOR SYSTEMS (BTMS)
1992-06-01
HISTORICAL
AS1145A
This specification covers minimum requirements for brake temperature monitoring equipment whenever used on any type and model of civil aircraft. It shall be the responsibility of the purchaser to determine the compatibility of these requirements with the application aircraft and to specify requirements in excess of these minimums as necessary.
Standard

Aircraft Brake Temperature Monitor Systems (BTMS)
2016-09-14
CURRENT
AS1145C
This specification covers minimum requirements for brake temperature monitoring equipment whenever used on any type and model of civil aircraft. It shall be the responsibility of the purchaser to determine the compatibility of these requirements with the application aircraft and to specify requirements in excess of these minimums as necessary.
Standard

Aircraft Brake Temperature Monitor Systems (BTMS)
2012-05-09
HISTORICAL
AS1145B
This specification covers minimum requirements for brake temperature monitoring equipment whenever used on any type and model of civil aircraft. It shall be the responsibility of the purchaser to determine the compatibility of these requirements with the application aircraft and to specify requirements in excess of these minimums as necessary.
Standard

Brake Systems, Wheel, Military Aircraft
2008-10-20
HISTORICAL
AS8584A
This SAE Aerospace Standard (AS) defines the requirements for brake systems used on military aircraft equipped with wheel-type landing gears.
Standard

Information on Parking Brake Systems
2020-09-16
CURRENT
AIR6441
This SAE Aerospace Information Report (AIR) provides information on the parking brake system design for a variety of aircraft including part 23, 25, 27, and 29. The document includes a discussion of key technical issues with parking brakes. This document does NOT provide recommended practices for parking brake system design.
Standard

MAINTAINABILITY RECOMMENDATIONS FOR AIRCRAFT WHEELS & BRAKES
1993-04-01
HISTORICAL
ARP813
This document suggests the maintainability features which should be considered in the design of aircraft wheels and brakes. The effect on such factors as cost, weight, reliability, and compatibility with other systems should be considered before incorporation of any of these features in the design.
Standard

MAINTAINABILITY RECOMMENDATIONS FOR AIRCRAFT WHEELS AND BRAKES
1993-04-01
HISTORICAL
ARP813A
This ARP suggests the maintainability features which should be considered in the design of aircraft wheels and brakes. The effect on such factors as cost, weight, reliability, and compatibility with other systems should be considered before incorporation of any of these features in the design.
Standard

Maintainability Recommendations for Aircraft Wheel and Brake Design
2010-06-25
HISTORICAL
ARP813B
This SAE Aerospace Recommended Practice (ARP) recommends the maintainability features which should be considered in the design of aircraft wheels and brakes. The effect on other factors, such as, cost, weight, reliability, and compatibility with other systems should be weighed before the incorporation of any of these maintainability features into the design.
Standard

SKID CONTROL EQUIPMENT
1975-01-15
HISTORICAL
AS483A
This standard covers minimum requirements for skid control equipment for use on all types and models of civil aircraft. It shall be the responsibility of the applicant to determine the compatibility of these requirements with the application aircraft and to specify requirements in excess of these minimums as necessary.
Standard

SKID CONTROL SYSTEM VIBRATION SURVEY
2008-06-16
HISTORICAL
AIR764C
This technical report documents three surveys to determine realistic vibration requirements for skid control systems specifications and obtain updated vibration information for locations in aircraft where skid control system components are mounted.
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