SAE AIR 5774 : 2012
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS
Superseded date
20-05-2019
Superseded by
Published date
01-01-2012
Publisher
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1. SCOPE
2. REFERENCES
3. DISCUSSION AND PREFERRED PRACTICES
4. NOTES
Provides guidance to airframe and equipment manufacturers for the design and installation of fuel systems into composite structure.
| Committee |
AE-5A
|
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| FAA AC 25.981-2 : 2008 | FUEL TANK FLAMMABILITY REDUCTION MEANS |
| SAE AIR 5128 : 2012 | ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS |
| SAE AMSC27725D | Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C) |
| FAA AC 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
| SAE ARP8615 | Fuel System Components: General Specification For |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-C-27725 Revision B:1969 | COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| GOST 10227 : 1986 AMD 6 2012 | |
| SAE AMSS7124B | Sealing Compound, Polysulfide, Accelerator Required, For Aircraft Structures |
| SAE AIR1662A | Minimization of Electrostatic Hazards in Aircraft Fuel Systems |
| SAE ARP 5413 : 1999 | CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| ASTM D 910 : 2017-05 | SPECIFICATION FOR LEADED AVIATION GASOLINES |
| SAE ARP4043B | Flight Line Grounding and Bonding of Aircraft |
| SAE AMSS4383B | Sealing Compound, Topcoat, Fuel Tank Buna-N Type |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| DEFSTAN 91-91/7(2011) : 2011 | TURBINE FUEL, KEROSINE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| SAE AIR4069C | Sealing of Integral Fuel Tanks |
| SAE AMSS29574A | Sealing Compound, Polythioether, for Aircraft Structures, Fuel and High Temperature Resistant, Fast Curing at Ambient and Low Temperatures |
| 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) |
| ASTM D 4154 : 2014 : REDLINE | Standard Performance Specification for Men’s and Boys’ Knitted and Woven Beachwear and Sports Shirt Fabrics |
| SAE ARP5583A | Guide to Certification of Aircraft in a High-Intensity Radiated Field (HIRF) Environment |
| SAE ARP5416A | Aircraft Lightning Test Methods |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| SAC GB 6537 : 1994 | NO.3 JET FUEL |
| SAE ARP 5577 : 2002 | AIRCRAFT LIGHTNING DIRECT EFFECTS CERTIFICATION |
| SAE ARP5414A | Aircraft Lightning Zone |
| SAE AMS3279D | Sealing Compound, Sprayable For Integral Fuel Tanks and Fuel Cell Cavities, For Intermittent Use to 350 °F (177 °C) |
| FAA AC 25.981-1 : 2008 | FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES |
| ASTM D 6469 : 2017 : REDLINE | Standard Guide for Microbial Contamination in Fuels and Fuel Systems |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
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