Search Results

Standard

Recommended Wheel Tie Bolt Preload Procedure

2007-08-09

HISTORICAL

ARP5481

This SAE Aerospace Recommended Practice (ARP) provides the recommended procedure for obtaining desired preloads in aircraft wheel tie bolts when mounting tires and assembling the wheel. It is generally referred to as the snug-angle bolted joint assembly procedure. It is also known as the “torque-turn” procedure in the heavy equipment ground vehicle industry.

Standard

Recommended Wheel Tie Bolt Preload Procedure

2020-09-17

CURRENT

ARP5481A

This SAE Aerospace Recommended Practice (ARP) provides the recommended procedure for obtaining desired preloads in aircraft wheel tie bolts when mounting tires and assembling the wheel. It is generally referred to as the snug-angle bolted joint assembly procedure. It is also known as the “torque-turn” procedure in the heavy equipment ground vehicle industry.

Standard

BRAKE DYNAMICS

1979-07-01

HISTORICAL

AIR1064A

Standard

USAF Aircraft Wheels

2012-05-09

HISTORICAL

AIR4012B

This SAE Aerospace Information Report (AIR) documents general technical data associated with many of the wheels used in the Air Force.

Standard

USAF Aircraft Wheels

2012-07-19

CURRENT

AIR4012C

This SAE Aerospace Information Report (AIR) documents general technical data associated with many of the wheels used in the Air Force.

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

Wheels and Brakes, Supplementary Criteria for Design Endurance Civil Transport Aircraft

2006-10-26

HISTORICAL

ARP597C

This document recommends supplementary design criteria to enhance endurance and reliability of transport aircraft wheels and brakes.

Standard

Selection, Testing, Lubrication, and Sealing of Single Row Tapered Roller Bearings for Aerospace Wheel Applications

2022-09-08

CURRENT

AIR4403B

This SAE Aerospace Information Report (AIR) describes available technology and current aerospace industry practices used for the selection, testing, lubrication, and sealing of single row tapered roller bearings to reduce bearing damage as a problem in the aircraft industry.

Standard

Minimum Performance Standard for Parts 23, 27, and 29 Aircraft Wheels, Brakes, and Wheel and Brake Assemblies

2022-09-08

CURRENT

AS5714A

This SAE Aerospace Standard (AS) prescribes the Minimum Performance Standards (MPS) for wheel, brake, and wheel and brake assemblies to be used on aircraft certificated under 14 CFR Parts 23, 27, and 29. Compliance with this specification is not considered approval for installation on any aircraft.