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

Cavity Design and O-ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels

2005-01-05

HISTORICAL

AS666C

This AS applies to the cavity design and the selection of O-rings for tubeless tire wheels.

Standard

Compilation of Freezing Brake Experience and Potential Designs and Operating Procedures to Prevent Its Occurrence

2016-05-24

CURRENT

AIR4762A

This Aerospace Information Report (AIR) describes conditions under which freezing (frozen) brakes can occur and describes operating procedures which have been used to prevent or lessen the severity or probability of brake freezing. This document also identifies design features that some manufacturers implement to minimize the occurrence of freezing brakes. This document is not an Aerospace Recommended Practice (ARP) and therefore does not make recommendations based on a consensus of the industry. However, part of this document’s purpose is to describe the design and operational practices that some are using to minimize the risk of frozen brakes. NOTE: The following information is based upon experience gained across a wide-range of aircraft types and operational profiles, and should NOT take precedence over Aircraft Flight Manual or Flight Operations Procedures.

Standard

Compilation of Freezing Brake Experience and Suggested Designs and Operating Procedures Required to Prevent Its Occurrence

2014-08-20

HISTORICAL

AIR4762

This AIR describes conditions under which freezing brakes can occur and offers suggested design features to minimize occurrence. It also suggests operating procedures which have been shown to prevent or lessen the severity of brake freezing.

Standard

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

2013-04-22

HISTORICAL

ARP1070C

This document recommends minimum requirements for antiskid brake control to provide total aircraft systems compatibility. 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. Methods of determining and evaluating antiskid system performance are discussed. While this document specifically addresses antiskid systems which are a part of a hydraulically actuated brake system, the recommended practices are equally applicable to brakes actuated by other means, such as electrically actuated brakes.

Standard

MILITARY SERVICE EXPERIENCE - AIRCRAFT WHEELS

2011-08-10

HISTORICAL

AIR4012

Standard

Military Service Experience - Aircraft Wheels

2000-10-01

HISTORICAL

AIR4012A

This SAE Aerospace Information Report (AIR) is intended to provide general background on aircraft wheel service lives on military aircraft and wheel laboratory test requirements as specified by military procurement agencies or aircraft manufacturers. Wheel service life in this document refers to the lowest life wheel half or flange in a wheel assembly measured in years (excluding bearing, bolt, and other removals). This information is intended as a reference guide for those responsible for specifying original equipment (OE) wheel laboratory test requirements.

Standard

NONDESTRUCTIVE INSPECTION (NDI) METHODS USED DURING PRODUCTION AND OPERATION OF AIRCRAFT WHEELS AND BRAKES

1994-09-01

HISTORICAL

AIR4777

This SAE Aerospace Information Report (AIR) identifies current nondestructive inspection (NDI) methods used to insure product integrity and maximize "in service" life of the major structural components of aircraft wheel and brake assemblies.

Standard

Nondestructive Inspection (NDI) Methods Used During Production and Operation of Aircraft Wheels and Brakes

2012-05-11

HISTORICAL

AIR4777A

This SAE Aerospace Information Report (AIR) identifies current nondestructive inspection (NDI) methods used to insure product integrity and maximize "in service" life of the major structural components of aircraft wheel and brake assemblies.

Standard

OVERPRESSURIZATION RELEASE DEVICES

1975-01-01

HISTORICAL

ARP1322

This ARP specifies the minimum design and test recommendations for aircraft tubeless tire and wheel overpressurization release devices to protect from possible explosive failure of the contained air chamber due to overinflation. This device will not protect against flash fire explosive conditions within the air chamber which may occur due to extremely overheated brakes. To protect against this condition, nitrogen or other inert gas should be used for inflation.

Standard

Overpressurization Release Devices

2007-08-09

HISTORICAL

ARP1322A

This SAE Aerospace Recommended Practice (ARP) specifies the minimum design and test recommendations for aircraft tubeless tire and wheel overpressurization release devices to protect from possible explosive failure of the contained air chamber due to overinflation. This device will not protect against flash fire explosive conditions within the air chamber which may occur due to extremely overheated brakes. To protect against this condition, nitrogen or other inert gas should be used for inflation.

Standard

Overpressurization Release Devices

2018-06-21

CURRENT

ARP1322C

This SAE Aerospace Recommended Practice (ARP) specifies the minimum design and qualification test recommendations for aircraft wheel overpressurization release devices used with tubeless aircraft tires to protect from possible explosive failure of the contained inflation chamber due to overinflation. Devices of this type provide a means, but not the only means, for showing compliance to Subsection 25.731(d) of Part 25 of Title 14 of the Code of Federal Regulations. Devices of this type will not protect against flash fire explosive conditions within the inflation chamber which may occur due to extremely overheated brakes or spontaneous combustion caused by a foreign substance within the inflation chamber. To help protect against this condition, nitrogen (N2) or other inert gas should be used for inflation.

Standard

Overpressurization Release Devices

2014-08-20

HISTORICAL

ARP1322B

This SAE Aerospace Recommended Practice (ARP) specifies the minimum design and test recommendations for aircraft wheel overpressurization release devices used with tubeless aircraft tires to protect from possible explosive failure of the contained air chamber due to overinflation. Devices of this type provide a means, but not the only means, for showing compliance to Subsection 25.731(d) of Part 25 of Title 14 of the Code of Federal Regulations. Devices of this type will not protect against flash fire explosive conditions within the air chamber which may occur due to extremely overheated brakes. To help protect against this condition, nitrogen or other inert gas should be used for inflation.

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.

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.