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FAA AC 20-145 : 2003

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS

Superseded date

28-10-2010

Superseded by

FAA AC 20-170 : 2010

Published date

12-01-2013

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1 PURPOSE
2 RELATED DOCUMENTS
   a Code of Federal Regulations
   b FAA Technical Standard Orders (TSO)
   c FAA Policy Documents
   d FAA Advisory Circulars (AC)
   e RTCA, Inc. Documents
   f SAE Documents
3 DEFINITIONS
4 ACRONYMS
5 SCOPE
6 BACKGROUND
7 DOCUMENT OVERVIEW
8 IMA SYSTEM APPROVALS AND AUTHORIZATIONS
   a TSO-C153 Authorization
   b Functional TSO Authorization
   c Installation Approval
9 SAFETY ASSESSMENT PROCESS GUIDANCE
10 CONFIGURATION MANAGEMENT GUIDANCE
11 ELECTRONIC IDENTIFICATION GUIDANCE
12 SOFTWARE GUIDANCE
   a Software Assurance
   b Software Levels
   c Field-Loadable Software (FLS)
   d Partitioning and Protection
   e Software Reuse
13 ELECTRONIC HARDWARE GUIDANCE
14 IMA DESIGN GUIDANCE
   a Electrical Power for IMA Systems
   b Recovery Features
   c Built-In Test (BIT)
   d Maintenance Diagnostics
   e Failure Detection and Annunciation
   f Functional Partitioning
   g Functional Isolation
   h Intentional Transmitters
   i Visual and Aural Alerting
15 ENVIRONMENTAL QUALIFICATION GUIDANCE
Figure 15-1 RTCA/DO-160D Environmental Qualification
            Requirements
16 HUMAN FACTORS AND FLIGHT CREW INTERFACE GUIDANCE
   a Human Factors Background
   b Potential Human Factors and Flight Crew Interface
     Issues with IMA Systems
   c Testing Considerations for Human Factors and Flight
     Crew Interface Issues
   d Methods of Compliance with Controls Regulations
17 TESTING PRACTICES
   a IMA Hardware Element Testing
   b Individual System Testing
   c IMA System Integration Testing
   d Aircraft Ground Testing
   e Aircraft Flight Testing
   f Configuration Control During Flight Testing
18 ROLES AND RESPONSIBILITIES OF IMA SYSTEM APPLICANTS
   a TSO-C153 Applicant Roles and Responsibilities
   b Functional TSO Applicant Roles and Responsibilities
   c TC, STC, ATC, ASTC Applicant Roles and Responsibilities
19 ADDITIONAL GUIDANCE FOR THIRD-PARTY MANUFACTURERS
20 AIRWORTHINESS CONSIDERATIONS
   a Initial Installation
   b Follow-on Installations
   c Change Impact Analysis
   d Change Classification
21 MAINTENANCE AND CONTINUED AIRWORTHINESS GUIDANCE
   a Maintenance Instructions
   b Maintenance Diagnostics
   c Master Minimum Equipment List (MMEL)
APPENDIX 1 PARTIAL LIST OF FUNCTIONAL TSOs

Provides an acceptable means, but not the only means, to obtain Federal Aviation Administration's (FAA) airworthiness approval for the installation of an Integrated Modular Avionics (IMA) System that uses hardware elements authorized under Technical Standard Order (TSO)-C153, Integrated Modular Avionics Hardware Elements.

DocumentType
Standard
PublisherName
Federal Aviation Administration
Status
Superseded
SupersededBy

FAA AC 20-170 : 2013 INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153
FAA N 8110.110 : 2010 SOFTWARE APPROVAL GUIDE LINES, CONTINUED
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA

FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
FAA AC 23.1311-1 : 2011 INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES
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 20-88 : A GUIDELINES ON THE MARKING OF AIRCRAFT POWERPLANT INSTRUMENTS (DISPLAYS)
FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
FAA 8110.4 : 2011 TYPE CERTIFICATION
SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
RTCA DO 254 : 2000 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 21-40 : 2007 GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE
FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
FAA AC 120-64 : 0 OPERATIONAL USE AND MODIFICATION OF ELECTRONIC CHECKLISTS
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 8150.1 : 2017 TECHNICAL STANDARD ORDER PROGRAM
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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