SAE AS6858
Current
The latest, up-to-date edition.
Installation of Fuel Cell Systems in Large Civil Aircraft
Hardcopy , PDF
English
21-04-2023
Important note : Users cannot be edited or removed once added to your Multi user PDF.This is a joint SAE/EUROCAE development.
| DocumentType |
Standard
|
| Pages |
35
|
| PublisherName |
SAE International
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| Status |
Current
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| Supersedes |
This is a joint SAE/EUROCAE development. This document will be released as both an SAE Aerospace Specification (AS) and a EUROCAE Minimum Aviation System Performance Standard (MASPS).This document defines the technical requirements for the safe integration of gaseous hydrogen fueled Proton Exchange Membrane (PEM) Fuel Cell Systems (FCS) within the aircraft.Most of the technical concepts and approaches covered by this document represent current industry \"best practice\". Others require specific approval from the procuring activity before use. This requirement for approval is not intended to prohibit their use; but rather to ensure that the prime contractor has fully investigated their capability to perform reliably and to be sufficiently durable under the required conditions and that the prime contractor can present substantiating evidence for approval before the design is committed to.
| 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 |
| IEC 60079:1957 | Recommendations for the construction of flameproof enclosures of electrical apparatus |
| ISO 11119-1:2020 | Gas cylinders Design, construction and testing of refillable composite gas cylinders and tubes Part 1: Hoop wrapped fibre reinforced composite gas cylinders and tubes up to 450 l |
| SAE AIR 1957 : 2015 | HEAT SINKS FOR AIRBORNE VEHICLES |
| SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
| SAE AIR64C | Electrical and Electronic Equipment Cooling in Commercial Transports |
| SAE AIR1059F | Oxygen Cylinder Quality, Serviceability, Maintenance Transfilling, and Marking |
| IEC 60952-3:2013 | Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP) |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| SAE ARP 5021B : 2019 | Oxygen Cylinder Installation Guide |
| SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
| SAE AS 861 : 2016 | MINIMUM GENERAL STANDARDS FOR OXYGEN SYSTEMS |
| SAE AIR 1277 : 2005 | COOLING OF MILITARY AVIONIC EQUIPMENT |
| ISO 11119-2:2020 | Gas cylinders Design, construction and testing of refillable composite gas cylinders and tubes Part 2: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450 l with load-sharing metal liners |
| SAE ARP 1532 : 2015 | AIRCRAFT OXYGEN SYSTEM LINES, FABRICATION, TEST AND INSTALLATION |
| EN 2570:1996 | Aerospace series - Nickel-cadmium batteries - Technical specification |
| SAE AS 8010 : 2018 | AVIATOR'S BREATHING OXYGEN PURITY STANDARD |
| ASTM G 128 : 2002 | Standard Guide for Control of Hazards and Risks in Oxygen Enriched Systems |
| SAE J2601_202005 | Fueling Protocols for Light Duty Gaseous Hydrogen Surface Vehicles |
| SAE J2579_201806 | Standard for Fuel Systems in Fuel Cell and Other Hydrogen Vehicles |
| ISO 11119-3:2020 | Gas cylinders Design, construction and testing of refillable composite gas cylinders and tubes Part 3: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450 l with non-load-sharing metallic or non-metallic liners or without liners |
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