• Shopping Cart
    There are no items in your cart

FAA AC 20-156 : 2006

Current

Current

The latest, up-to-date edition.

AVIATION DATABUS ASSURANCE

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2006

€35.89
Excluding VAT

1. PURPOSE
2. MOTIVATION FOR GUIDANCE
3. SAFETY REQUIREMENTS
4. DATA INTEGRITY REQUIREMENTS
5. DATABUS PERFORMANCE REQUIREMENTS
6. SOFTWARE AND HARDWARE ASSURANCE REQUIREMENTS
7. ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS
8. VERIFICATION AND VALIDATION REQUIREMENTS
9. CONFIGURATION MANAGEMENT REQUIREMENTS
10. SECURITY ASSURANCE REQUIREMENTS
11. PROCEDURES FOR MEETING REQUIREMENTS
12. RELATED DOCUMENTS AND HOW TO GET THEM

Provides means to gain Federal Aviation Administration (FAA) approval of your aviation databus by showing the databus design performs its intended function and satisfies the applicable airworthiness requirements when installed on an aircraft or aircraft engine.

DocumentType
Standard
Pages
10
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
ARINC 825 : 2015 GENERAL STANDARDIZATION OF CAN (CONTROLLER AREA NETWORK) BUS PROTOCOL FOR AIRBORNE USE
SAE ARP 6461 : 2013 GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT

FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
FAA AC 33.28-2 : 2003 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
FAA AC 20-152 : 2005 RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
FAA AC 33.75-1 : 2007 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.75, SAFETY ANALYSIS
FAA AC 33.28-1 : 0 COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.