SAE AIR 5924 : 2013

Superseded

View Superseded by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Superseded date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

Language(s)

English

Published date

16-01-2013

Publisher

SAE International

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Status	Superseded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	SAE AIR5924B:2024
Supersedes	SAE AIR 5924 : 2004

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