SAE ARP 8615 : 2011
Current
Current
The latest, up-to-date edition.
FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
11-08-2011
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.This document describes the requirements for air vehicle fuel, vent, and propulsion fuel system functional components.
| Committee |
AE-5A
|
| DevelopmentNote |
Supersedes MIL F 8615 (D). (06/2013)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| MIL-PRF-25439 Revision C:2013 | TRANSMITTER RATE OF FLOW, IN-FLIGHT REFUELING, 0-10,000 PPM, TYPE MB-3 |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| SAE ARP 6385 : 2017 | AIRCRAFT FUEL PUMP MECHANICAL AND ELECTRICAL SAFETY DESIGN |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MS29521 Revision H:2015 | DISK, VALVE |
| SAE AIR5691A : 2017 | GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS |
| SAE ARP594 : 2017 | FUEL PUMP THERMAL SAFETY DESIGN |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-DTL-7899 Revision D:2014 | Valve, Check, Aircraft Fuel System |
| SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
| SAE AS 7510 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-PRF-83323 Revision D:2016 | TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
| SAE AIR1184B : 2016 | CAPACITIVE FUEL GAUGING SYSTEM ACCURACIES |
| SAE ARP 5794 : 2014 | CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
| SAE AIR 4023 : 2016 | AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS |
| SAE AS5751:2018(R2023) | Design and Operating Requirements of the Onboard Aircraft Refueling System and Associated Ground Refueling Equipment Interface |
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