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SAE ARP 492 : 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Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST
Available format(s)

Hardcopy , PDF

Superseded date

06-04-2021

Language(s)

English

Published date

18-07-2014

1. SCOPE
2. APPLICABLE DOCUMENTS
3. GENERAL REQUIREMENTS
4. DETAIL REQUIREMENTS
5. SUGGESTED TESTING TECHNIQUES
APPENDIX A - CALCULATION OF V/L RATIO
APPENDIX B - RECOMMENDED V/L METERS

Describes procedures for testing aircraft engine fuel pumps for the purpose of determining their resistance to deterioration, during steady state endurance test, while receiving MIL-T-5624 Grade JP-4 fuel as a homogenous mixture of gas and liquid expressed as a ratio of vapor volume to liquid volume (V/L).

Committee
AE-5B
DocumentType
Standard
Pages
14
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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)/7(2011) : 2011 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
MIL BULL 343 : A DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/11(2013) : 2013 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
DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
SAE ARP 4028 : 2014 AIRCRAFT/ENGINE FUEL PUMP TWO PHASE (SLUGGING FLOW) INLET PERFORMANCE TEST AND EVALUATION
SAE ARP 4024 : 2013 AIRCRAFT/ENGINE FUEL PUMP NET POSITIVE SUCTION PRESSURE PERFORMANCE TEST AND EVALUATION
SAE MAP 749 : 2015 AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)

SAE ARP 4024 : 2013 AIRCRAFT/ENGINE FUEL PUMP NET POSITIVE SUCTION PRESSURE PERFORMANCE TEST AND EVALUATION
SAE ARP 4028 : 2014 AIRCRAFT/ENGINE FUEL PUMP TWO PHASE (SLUGGING FLOW) INLET PERFORMANCE TEST AND EVALUATION
SAE AIR 1326 : 1997 AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER

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