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SAE ARP 5757 : 2016

Current

Current

The latest, up-to-date edition.

GUIDELINES FOR ENGINE COMPONENT TESTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

16-10-2016

€135.68
Excluding VAT

1. SCOPE
2. REFERENCES
3. APPLICABILITY
4. HISTORICAL PERSPECTIVE
5. APPROACH
6. SUMMARY
7. NOTES

This SAE Aerospace Recommended Practice (ARP) provides guidance for substantiating the airworthiness of aircraft engine components.

Committee
E-36
DocumentType
Revision
Pages
27
PublisherName
SAE International
Status
Current
Supersedes

FAA AC 33.91-1 : 2010 ENGINE SYSTEM AND COMPONENT TESTS

FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
SAE MAP 749 : 2015 AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)
SAE ARP 5107 : 2006 GUIDELINES FOR TIME-LIMITED-DISPATCH (TLD) ANALYSIS FOR ELECTRONIC ENGINE CONTROL SYSTEMS
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
ISO 2685:1998 Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones
SAE AS 4273 : 2007 FIRE TESTING OF FLUID HANDLING COMPONENTS FOR AIRCRAFT ENGINES AND AIRCRAFT ENGINE INSTALLATIONS
FAA AC 33.17-1 : 2009 ENGINE FIRE PROTECTION SECTION 33.17
SAE AIR1639A : 1999 SAFETY CRITERIA FOR PNEUMATIC STARTING SYSTEMS
FAA AC 33.63-1 : 2007 TURBINE ENGINE VIBRATION
FAA AC 20-104 : 1978 REVISED POWER PLANT ENGINEERING REPORT NO. 3A, STANDARD FIRE TEST APPARATUS AND PROCEDURE (FOR FLEXIBLE HOSE ASSEMBLIES)
FAA AC 33.91-1 : 2010 ENGINE SYSTEM AND COMPONENT TESTS
FAA AC 33.28-3 : 2014 GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS
MIL-E-8593 Revision A:1975 ENGINE, AIRCRAFT, TURBOPROP, GENERAL SPECIFICATION FOR [ASG]
MIL-E-5007 Revision D:1973 ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
SAE ARP 1401 : 2012 AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST
ISO 2669:1995 Environmental tests for aircraft equipment — Steady-state acceleration
FAA AC 20-147 : 2014 TURBOJET, TURBOPROP, TURBOSHAFT, AND TURBOFAN ENGINE INDUCTION SYSTEM ICING AND ICE INGESTION
FAA AC 20-135 : 0 POWERPLANT INSTALLATION AND PROPULSION SYSTEM COMPONENT FIRE PROTECTION TEST METHODS, STANDARDS AND CRITERIA
SAE AIR 4246 : 2012 CONTAMINANTS FOR AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT TESTING
SAE AIR 4023 : 2016 AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS

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