Purpose of This Document

This document sets forth the basic features for a 4 MCU Inertial Reference System (IRS), consisting of the necessary inertial measuring devices and associated electronics specifically designed for installation in commercial transport-type aircraft, that may be used in place of an in-service 10 MCU ARINC 704 Inertial Reference System.

The intent of this document is to provide general and specific design guidance for the development of an IRS for airline use. It describes the desired operational capability of the system and the standards necessary to ensure interchangeability.

Customers who purchased ARINC 704A
also purchased

• ANSI A117.1 : BUILDINGS AND FACILITIES - PROVIDING ACCESSIBILITY AND USABILITY FOR PHYSICALLY HANDICAPPED PEOPLE; (REVISED AND REDESIGNATED TO ANSI/CABO A117.1-1992)
• AA ANSI H35.2 : Dimensional Tolerances for Aluminum Mill Products
• ANSI S3.6 : SPECIFICATIONS FOR AUDIOMETERS (R 1973) (REVISION OF Z24.5-51, Z24.12-52 AND Z24.13-53)
• ANSI Z136.1 : Safe Use of Lasers-This is now Copyrighted by LIA/LASER

See More Documents