SAE ARP 6109 : 2014

Superseded

Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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ELECTRONIC ENGINE CONTROL HARDWARE CHANGE MANAGEMENT

Available format(s): Hardcopy, PDF

Superseded date: 07-07-2021

Language(s): English

Published date: 21-02-2014

Publisher: SAE International

Table of Contents - (Show below) - (Hide below)

1. SCOPE
2. REFERENCES
3. REGULATION AND GUIDANCE MATERIAL
4. DESIGN CHANGE EVALUATION
5. ASPECTS OF COMPLEXITY ANALYSIS
6. DECISION TOOL - CLASSIFICATION CRITERIA
7. NOTES

Abstract - (Show below) - (Hide below)

This document is intended for use by manufacturers of aircraft, engines and Electronic Engine Controls [EECs] as a component change process and evaluation guideline.

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Committee	E-36
Document Type	Standard
ISBN
Pages
Published
Publisher	SAE International
Status	Superseded
Superseded By	SAE ARP6109A:2014(S2021)

Standards Referencing This Book - (Show below) - (Hide below)

MIL-HDBK-61 Revision A:2001	CONFIGURATION MANAGEMENT GUIDANCE
MIL-STD-883 Revision K:2016	TEST METHOD STANDARD - MICROCIRCUITS
SAE ARP 4754 : 2010	GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
RTCA DO 254 : 2000	DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
IEC TS 62239-1:2015	Process management for avionics - Management plan - Part 1: Preparation and maintenance of an electronic components management plan
FAA AC 33.28-1 : 0	COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS

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