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SAE AIR 5924 : 2013

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

GUIDELINES FOR THE INTEGRATION OF ELECTRONIC ENGINE CONTROL SYSTEMS FOR TRANSPORT CATEGORY (PART 25) AND GENERAL AVIATION (PART 23) AIRCRAFT

Available format(s)

Hardcopy , PDF

Superseded date

19-01-2024

Superseded by

SAE AIR5924B:2024

Language(s)

English

Published date

16-01-2013

€171.21
Excluding VAT

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Superseded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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