FAA AC 33.28-1 : 0
Current
The latest, up-to-date edition.
COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS
Hardcopy , PDF
English
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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SAE ARP6109 | Electronic Engine Control Hardware Change Management |
FAA AC 20-156 : 2006 | AVIATION DATABUS ASSURANCE |
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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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