SAE AS 6858 : 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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
INSTALLATION OF FUEL CELL SYSTEMS IN LARGE CIVIL AIRCRAFT
Hardcopy , PDF
03-05-2023
English
02-03-2017
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. REFERENCES
3. GENERAL
4. FCS INTEGRATION WITH THE AIRCRAFT
5. SAFETY
6. PROOF AND BURST
7. MATERIAL COMPATIBILITY
8. AFFECTED CERTIFICATION REQUIREMENTS
9. ENVIRONMENTAL
10. GASEOUS H2 STORAGE AND DISTRIBUTION
11. OXIDANT SUPPLY AND DISTRIBUTION
12. FUEL CELL MODULE CONSIDERATIONS
13. BALANCE OF PLANT CONSIDERATIONS
14. THERMAL MANAGEMENT CONSIDERATIONS
15. CONTROLLER / SYSTEM INTERFACE CONSIDERATIONS
16. SENSORS
17. ELECTRICAL POWER CONDITIONING
18. POWER STORAGE
19. ELECTRICAL POWER INTERFACE
20. MAINTENANCE
21. NOTES
Describes the technical requirements for the safe integration of gaseous hydrogen fueled Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS) within the aircraft.
| DocumentType |
Standard
|
| Pages |
35
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| EN 2282:1992 | Aerospace series - Characteristics of aircraft electrical supplies |
| SAE AIR 6464 : 2013 | EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES |
| RTCA DO 347 : 2013 | CERTIFICATION TEST GUIDANCE FOR SMALL AND MEDIUM SIZED RECHARGEABLE LITHIUM BATTERIES AND BATTERY SYSTEMS |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| ISO 11119-2:2012 | Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 2: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450 l with load-sharing metal liners |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| SAE AIR 825/13 : 2003 | GUIDE FOR EVALUATING COMBUSTION HAZARDS IN AIRCRAFT OXYGEN SYSTEMS |
| SAE AIR 1957 : 2015 | HEAT SINKS FOR AIRBORNE VEHICLES |
| SAE ARP 4418 : 2008 | PROCEDURE FOR SAMPLING AND MEASUREMENT OF ENGINE AND APU GENERATED CONTAMINANTS IN BLEED AIR SUPPLIES FROM AIRCRAFT ENGINES |
| SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| SAE AS 8010 : 2012 | AVIATOR'S BREATHING OXYGEN PURITY STANDARD |
| MIL-DTL-7891 Revision G:2008 | FILLER VALVE, AIRCRAFT OXYGEN |
| RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| RTCA DO 227 : A2017 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS (MOPS) FOR NON-RECHARGEABLE LITHIUM BATTERIES |
| IEC 60952-3:2013 | Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP) |
| SAE J 2601 : 2016 | FUELING PROTOCOLS FOR LIGHT DUTY GASEOUS HYDROGEN SURFACE VEHICLES |
| IEC 60952-2:2013 | Aircraft batteries - Part 2: Design and construction requirements |
| SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| SAE ARP 5021 : 2016 | OXYGEN CYLINDER INSTALLATION GUIDE |
| RTCA DO 293 : A2009 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR NICKEL-CADMIUM, NICKEL METAL-HYDRIDE, AND LEAD ACID BATTERIES |
| SAE ARP1870A:1987(S2012) | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)<br> |
| SAE AS 861 : 2016 | MINIMUM GENERAL STANDARDS FOR OXYGEN SYSTEMS |
| SAE AIR 1277 : 2005 | COOLING OF MILITARY AVIONIC EQUIPMENT |
| SAE ARP 1532 : 2015 | AIRCRAFT OXYGEN SYSTEM LINES, FABRICATION, TEST AND INSTALLATION |
| SAE AIR 1059 : 2014 | OXYGEN CYLINDER QUALITY, SERVICEABILITY, MAINTENANCE TRANSFILLING AND MARKING |
| EN 2570:1996 | Aerospace series - Nickel-cadmium batteries - Technical specification |
| FAA AC 20-184 : 2015 | GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT |
| SAE J 2579 : 2013 | STANDARD FOR FUEL SYSTEMS IN FUEL CELL AND OTHER HYDROGEN VEHICLES |
| SAE AIR 1168/8 : 2011 | AIRCRAFT FUEL WEIGHT PENALTY DUE TO AIR CONDITIONING |
| ISO 11119-1:2012 | Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 1: Hoop wrapped fibre reinforced composite gas cylinders and tubes up to 450 l |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| SAE AIR 64 : 1992 | ELECTRICAL AND ELECTRONIC EQUIPMENT COOLING IN COMMERCIAL TRANSPORTS |
| IEC 60952-1:2013 | Aircraft batteries - Part 1: General test requirements and performance levels |
| AIAA G 095 : 2004 | GUIDE TO SAFETY OF HYDROGEN AND HYDROGEN SYSTEMS |
| ISO 11119-3:2013 | Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 3: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450L with non-load-sharing metallic or non-metallic liners |
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