FAA AC 20-156 : 2006
Current
The latest, up-to-date edition.
AVIATION DATABUS ASSURANCE
Hardcopy , PDF
English
01-01-2006
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.