SAE AIR5691A : 2017
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS
Hardcopy , PDF
14-10-2022
English
18-05-2017
1. SCOPE
2. REFERENCES
3. OVERVIEW OF GAUGING TECHNOLOGIES AND
FUEL CHARACTERISTIC MEASUREMENTS
4. SYSTEM DESIGN CONSIDERATIONS
5. INSTALLATION CONSIDERATIONS
6. IN-TANK ENVIRONMENT
7. LESSONS LEARNED
8. NOTES
APPENDIX A - COMMON JET FUEL TYPES
APPENDIX B - AVIATION JET FUEL ADDITIVES NOT
COMPREHENSIVE - BASED ON ASTM D1655
Pertains to commercial and military aircraft fuel quantity indication systems.
Committee |
AE-5A
|
DocumentType |
Revision
|
Pages |
73
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
FAA AC 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
ARINC 611 : 1988 SUPP 1 | GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY SYSTEMS |
MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
SAE ARP 8615 : 2011 | FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR |
SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
SAE AIR1184B : 2016 | CAPACITIVE FUEL GAUGING SYSTEM ACCURACIES |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE AIR 4170 : 2016 | RETICULATED POLYURETHANE FOAM EXPLOSION SUPPRESSION MATERIAL FOR FUEL SYSTEMS AND DRY BAYS |
SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
BS 5501-7:1977 | Electrical apparatus for potentially explosive atmospheres Intrinsic safety \'i\' |
ASTM D 910 : 2017-05 | SPECIFICATION FOR LEADED AVIATION GASOLINES |
SAE ARP1870A:1987(S2012) | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)<br> |
MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
SAE ARP 5577 : 2002 | AIRCRAFT LIGHTNING DIRECT EFFECTS CERTIFICATION |
SAE ARP 5414 : 2012 | AIRCRAFT LIGHTNING ZONE |
ARINC 429 : 2001 | ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS |
FAA AC 25.981-1 : 2008 | FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES |
SAE ARP 5412 : 2013 | AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS |
SAE AIR 4246 : 2012 | CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING |
MIL-G-7940 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE, INSTALLATION AND CALIBRATION OF |
MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
ARINC 609 : 1987 | DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS |
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