SAE AIR 5924 : 2013
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
GUIDELINES FOR THE INTEGRATION OF ELECTRONIC ENGINE CONTROL SYSTEMS FOR TRANSPORT CATEGORY (PART 25) AND GENERAL AVIATION (PART 23) AIRCRAFT
Hardcopy , PDF
19-01-2024
English
16-01-2013
1. SCOPE
2. REFERENCES
3. APPLICABILITY
4. THRUST AND POWER CONTROL
5. USE OF SENSORS, AIRCRAFT SIGNALS, AND DATA
6. INSTRUMENTATION AND FLIGHT-CREW INTERFACES
7. MAINTENANCE CONSIDERATIONS
8. HARDWARE AND ENVIRONMENTAL ISSUES
9. CERTIFICATION
10. NOTES
Specifies methodologies and approaches that have been used to install and integrate full-authority-digital-engine-control (FADEC) systems on transport category aircraft.
Committee |
E-36
|
DocumentType |
Revision
|
Pages |
81
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
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" |
SAE ARP 5107 : 2006 | GUIDELINES FOR TIME-LIMITED-DISPATCH (TLD) ANALYSIS FOR ELECTRONIC ENGINE CONTROL SYSTEMS |
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 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
SAE AIR 6181 : 2011 | ELECTRONIC PROPULSION CONTROL SYSTEM/AIRCRAFT INTERFACE CONTROL DOCUMENTS |
SAE AS 755 : 2014 | AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION |
FAA AC 25-13 : 0 | REDUCED AND DERATED TAKEOFF THRUST (POWER) PROCEDURES |
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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