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FAA AC 33.28-1 : 0

Current

Current

The latest, up-to-date edition.

COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS

Available format(s)

Hardcopy , PDF

Language(s)

English

€53.84
Excluding VAT

1 PURPOSE
2 RELATED REGULATIONS
3 RELATED REFERENCE MATERIAL
4 APPLICABILITY

Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with Section 33.28 of Title 14 of the Code of Federal Regulations (14 CFR 33.28), Electrical and electronic engine control systems.

DocumentType
Standard
Pages
50
PublisherName
Federal Aviation Administration
Status
Current

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FAA AC 23-16 : 0 POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS
FAA 8110.49 : 2011 SOFTWARE APPROVAL GUIDELINES
FAA AC 00-66 : 2015 SELECTION OF CYCLIC REDUNDANCY CODE AND CHECKSUM ALGORITHMS TO ENSURE CRITICAL DATA INTEGRITY
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
SAE ARP6109 Electronic Engine Control Hardware Change Management
FAA AC 20-156 : 2006 AVIATION DATABUS ASSURANCE
SAE AIR5924A Guidelines for the Integration of Electronic Engine Control Systems for Transport Category (Part 25) and General Aviation (Part 23) Aircraft
FAA AC 20-145 : 2003 GUIDANCE FOR INTEGRATED MODULAR AVIONICS (IMA) THAT IMPLEMENT TSO-C153 AUTHORIZED HARDWARE ELEMENTS

MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS

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