SAE ARP 5794 : 2014
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD
Available format(s)
Hardcopy , PDF
Superseded date
03-06-2018
Superseded by
Language(s)
English
Published date
01-01-2014
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Specifies the general design, testing, and safety requirements for aircraft tank mounted fuel booster pumps used for engine fuel feed, transfer, and jettison.
| Committee |
AE-5B
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| SAE ARP 6385 : 2017 | AIRCRAFT FUEL PUMP MECHANICAL AND ELECTRICAL SAFETY DESIGN |
| SAE ARP594 : 2017 | FUEL PUMP THERMAL SAFETY DESIGN |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| ASME Y14.35 : 2014 | REVISION OF ENGINEERING DRAWINGS AND ASSOCIATED DOCUMENTS |
| SAE AMS A 21180 : 2011 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| SAE ARP594 : 2016 | FUEL PUMP THERMAL SAFETY DESIGN |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| SAE AMS QQ P 416 : 2016 | PLATING, CADMIUM (ELECTRODEPOSITED) |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
| SAE AMS 2175 : 2010 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| SAE ARP 8615 : 2011 | FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
| SAE AMS 3216 : 2005 | ELASTOMER: FLUOROCARBON (FKM) RUBBER HIGH-TEMPERATURE - FLUID RESISTANT LOW COMPRESSION SET 70 TO 80 |
| MIL-STD-31000 Revision A:2013 | Technical Data Packages |
| SAE ARP594 : 2016 | FUEL PUMP THERMAL SAFETY DESIGN |
| SAE AMS R 83485 : 2014 | RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES |
| SAE AS 5440 : 2011 | HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
| FAA AC 20-152 : 2005 | RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| ASME Y14.24 : 2012 | TYPES AND APPLICATIONS OF ENGINEERING DRAWINGS - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| SAE J 1926/1 : 2016 | CONNECTIONS FOR GENERAL USE AND FLUID POWER - PORTS AND STUD ENDS WITH ASME B1.1 THREADS AND O-RING SEALING - PART 1: THREADED PORT WITH O-RING SEAL IN TRUNCATED HOUSING |
| ASME Y14.34 : 2013(R2018) | ASSOCIATED LISTS - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| ASTM D 910 : 2017-05 | SPECIFICATION FOR LEADED AVIATION GASOLINES |
| SAE ARP 5316 : 2014 | STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| 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 |
| 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) |
| SAE AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
| SAE ARP 1401 : 2012 | AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST |
| FAA AC 20-155 : 2013 | INDUSTRY DOCUMENTS TO SUPPORT AIRCRAFT LIGHTNING PROTECTION CERTIFICATION |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
| SAE AMS P 5315 : 2013 | ACRYLONITRILE-BUTADIENE (NBR) RUBBER FOR FUEL-RESISTANT SEALS 60 TO 70 |
| FAA AC 20-115 : 2017 | AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( ) |
| FAA AC 25.981-1 : 2008 | FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES |
| MIL-PRF-6855 Revision F:2009 | RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES, GENERAL SPECIFICATION FOR |
| MIL-DTL-25988 Revision C:2006 | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES |
| ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| SAE AIR 4246 : 2012 | CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING |
| MIL-S-7742 Revision D:1991 | SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
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