AS1145A: AIRCRAFT BRAKE TEMPERATURE MONITOR SYSTEMS (BTMS) - Technical Standard

Features

Issuing Committee: A-5A Wheels, Brakes and Skid Controls Committee

Scope

Content: 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.

Meta Tags

Topics: Landing gear
Test procedures
Dampers and shock absorbers
Electronic equipment
Defense industry
Sensors and actuators

Details

DOI: https://doi.org/10.4271/AS1145A

Pages: 13

Citation: SAE International Technical Standard, AIRCRAFT BRAKE TEMPERATURE MONITOR SYSTEMS (BTMS), SAE Standard AS1145A, Revised March 1982, Issued April 1973, https://doi.org/10.4271/AS1145A.

Additional Details

Publisher: SAE International

Published: Jun 1, 1992

Product Code: AS1145A

Content Type: Technical Standard

Status: Revised

Language: English

Historical