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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

INFORMATION ON ANTISKID SYSTEMS

1988-01-01
HISTORICAL
AIR1739
This Aerospace Information Report (AIR) has been prepared by a panel of the SAE A-5 Committee and is presented to document the design approaches and service experience from various applications of antiskid systems. This experience includes commercial and military applications.
Standard

DESIGN OF SKID CONTROL & ASSOCIATED AIRCRAFT EQUIPMENT FOR TOTAL SYSTEM COMPATIBILITY

1982-04-01
HISTORICAL
ARP1070A
This document covers the general requirements for aircraft skid control systems and their components. Methods of defining skid control system performance criteria for design and evaluation purposes are outlined and recommended. Design and operational goals, general theory, and functions, which must be considered by the aircraft brake systems engineer to attain the most effective skid control performance, are covered in detail. Recommended methods for measuring performance of skid control systems are included.
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 EQUIPMENT

1962-12-01
HISTORICAL
AS483
This specification 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 (See Paragraph 5.1) to determine the compatibility of these requirements with the applicable aircraft and to specify requirements in excess of these minimums as necessary.
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