Search Results

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

AUTOMATIC BRAKING SYSTEMS REQUIREMENTS

1993-04-01

HISTORICAL

ARP1907

This ARP covers the functional, design, construction, and test requirements for Automatic Braking Systems. Installation information and lessons learned are also included.

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

Aircraft Tire Inflation-Deflation Equipment

2014-07-11

CURRENT

AS1188A

This specification covers minimum design and test requirements for aircraft tire inflation-deflation equipment for use on 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 requirements in excess of these minimums as necessary.

Standard

Aircraft Tire Inflation-Deflation Equipment

2008-06-16

HISTORICAL

AS1188

This specification covers minimum design and test requirements for aircraft tire inflation-deflation equipment for use on 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 requirements in excess of these minimums as necessary.

Standard

Automatic Braking Systems

2016-01-25

CURRENT

ARP1907C

This SAE Aerospace Recommended Practice (ARP) covers the functional, design, construction, and test requirements for Automatic Braking Systems. Installation information and lessons learned are also included.

Standard

Automatic Braking Systems

2014-08-20

HISTORICAL

ARP1907B

This SAE Aerospace Recommended Practice (ARP) covers the functional, design, construction, and test requirements for Automatic Braking Systems. Installation information and lessons learned are also included.

Standard

Automatic Braking Systems Requirements

2006-10-26

HISTORICAL

ARP1907A

This ARP covers the functional, design, construction, and test requirements for Automatic Braking Systems. Installation information and lessons learned are also included.

Standard

DESIGN OF AIRCRAFT SKID CONTROL SYSTEMS FOR COMPATIBILITY WITH AIRPLANE EQUIPMENT

1969-04-01

HISTORICAL

ARP1070

Standard

Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility

2006-10-26

HISTORICAL

ARP1070B

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 should be considered by the aircraft brake system engineer to attain the most effective skid control performance, are covered in detail. Recommended methods for measuring performance of a skid control system are included.

Standard

Information on Electric Brakes

2019-02-15

CURRENT

AIR5937

This SAE Aerospace Information Report (AIR) describes the design, operation, and attributes of electrical braking systems for both military and commercial aircraft. At this time, the document focuses only on brakes utilizing electromechanical actuators (EMAs), as that is the present state of the art. As such, the discussions herein assume that EMAs can simply replace the hydraulic actuation portion of typical brake system leaving things such as the wheel and heat sink unchanged. Furthermore, the document provides detail information from the perspective of brake system design and operation. The document also addresses failure modes, certification issues, and past development efforts. Details on the design and control of electric motors, gear train design, ball or roller screw selection are available in the reference documents and elsewhere, but are outside the scope of this document.

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

Maintainability Recommendations for Aircraft Wheel and Hydraulically Actuated Brake Design

2022-07-13

WIP

ARP813D

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

Maintainability Recommendations for Aircraft Wheel and Hydraulically Actuated Brake Design

2019-02-15

CURRENT

ARP813C

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

Minimum Performance Recommendations for Part 23, 27, and 29 Aircraft Wheels, Brakes, and Wheel and Brake Assemblies

2012-07-19

CURRENT

ARP5381A

This Minimum Performance Document defines the testing required for wheels, brakes, and wheel and brake assemblies to be used on civil aircraft certified under 14 Code of Federal Regulations (CFR) Part 23, 27, and 29. Compliance with this document is recommended to assure that the equipment supplied will meet the intended design function when installed on aircraft. Compliance with this document does not constitute authorization for installation on an aircraft. The combined recommendations of this document provide an acceptable practice, but not the only practice, for obtaining authorization to apply TSO markings on the equipment.

Standard

Minimum Performance Recommendations for Part 23, 27, and 29 Aircraft Wheels, Brakes, and Wheel and Brake Assemblies

2006-03-17

HISTORICAL

ARP5381

This Minimum Performance Document defines the testing required for wheels, brakes, and wheel and brake assemblies to be used on civil aircraft certified under 14 Code of Federal Regulations (CFR) Part 23, 27, and 29. Compliance with this document is recommended to assure that the equipment supplied will meet the intended design function when installed on aircraft. Compliance with this document does not constitute authorization for installation on an aircraft. The combined recommendations of this document provide an acceptable practice, but not the only practice, for obtaining authorization to apply TSO markings on the equipment.

Standard

Minimum Performance Requirements for Transport Airplane Wheel and Brake Assemblies Using Electric Power Actuation

2012-07-11

CURRENT

AS5663A

In lieu of TSO-C135, this SAE Aerospace Standard (AS) prescribes the minimum performance standards for wheels, brakes, and wheel and brake assemblies using electric power actuation for transport category (14 CFR Part 25) airplanes. Testing is limited to that necessary to establish minimum performance related to strength, robustness, stopping capability, and energy absorption to ensure measurable, repeatable industry accepted standards for these aspects of wheel and brake performance. The test parameters associated with electric braking actuation are defined around the state of the technology at this time, typically comprised of an Electro-Mechanical Actuator (EMA) controlled by a control system delivering electric power and effecting motor control.