FAA AC 20-145 : 2003
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS
28-10-2010
12-01-2013
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 ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING 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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