logo

Standards Manage Your Business

We Manage Your Standards

SAE

SAE AS5663A : 2012

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

Standard Details

In lieu of TSO-C135, this SAE Aerospace Standard (AS) prescribes the minimum performance StandardDetails 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 StandardDetails 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. This document does not address qualification of the EMAs or brake assembly to the landing gear environmental threats including, but not limited to, EMI/HIRF, failure mode operation or other application specific performance, or the qualification of software or of complex custom micro-coded components, including but not limited to, Programmable Logic Devices (PLD) and Application Specific Integrated Circuits (ASIC).

Cross Reference: 14CFRAC25-7A,FAATSO-C135

General Information

Status : Stabilized
Standard Type: Main
Document No: SAE AS5663A : 2012
Document Year: 2012
Pages: 16

Life Cycle

Currently Viewing

Stabilized
SAE AS5663A : 2012
Knowledge Corner

Expand Your Knowledge and Unlock Your Learning Potential - Your One-Stop Source for Information!

© Copyright 2024 BSB Edge Private Limited.

Enquire now +