SAE AIR1662A
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Minimization of Electrostatic Hazards in Aircraft Fuel Systems
Hardcopy , PDF
31-12-2022
English
09-08-2013
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1. SCOPE
2. REFERENCES
3. PHYSICS OF ELECTROSTATIC CHARGE GENERATION
AND ACCUMULATION IN AIRCRAFT FUEL SYSTEMS
4. INCENDIVITY OF ELECTROSTATIC DISCHARGES
5. CRITERIA FOR IGNITION
6. CAUSE AND PREVENTION OF ELECTROSTATIC
HAZARDS IN AIRCRAFT
7. DESIGN AND OPERATING RECOMMENDATIONS
Provides background information, technical data and related technical references for minimization of electrostatic hazards in aircraft fuel systems.
| DocumentType |
Standard
|
| Pages |
24
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This SAE Aerospace Information Report (AIR) provides background information, technical data and related technical references for minimization of electrostatic hazards in aircraft fuel systems.Techniques used to minimize the electrostatic hazard include:aReducing fueling rate into tank bays including use of multiple refueling inlet nozzles.bReducing refuel plumbing flow velocities.cIntroducing fuel into the tank at a low velocity near the bottom and directing it to impinge upon a grounded conducting surface.dAvoiding electrically isolated conductors in the fuel tank.eUsing conductivity additives in the fuel.
| DEFSTAN 00-970(PT1)SEC5/13(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/11(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| SAE AIR 5128 : 2012 | ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS |
| DEFSTAN 00-970(PT1)SEC5/8(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5 - POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/9(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| DEFSTAN 00-970(PT1)SEC5/6(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| SAE AIR 1664 : 2013 | AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS |
| DEFSTAN 00-970(PT1)SEC5/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| SAE AIR4170B | Reticulated Polyurethane Foam Explosion Suppression Material for Fuel Systems and Dry Bays |
| DEFSTAN 00-970(PT1)SEC5/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5: POWERPLANT |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| DEFSTAN 00-970(PT1)SEC5/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 5 - POWERPLANT |
| SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
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