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SAE ARP 1401 : 2012

Current
Current

The latest, up-to-date edition.

AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

06-06-2012

1. SCOPE
2. REFERENCES
3. BRIEF HISTORY
4. NEED FOR TEST STANDARDIZATION
5. WATER TO ICE EVOLUTION
6. RECOMMENDATIONS
7. TEST PROCEDURES
8. ADDITIONAL NOTES ON TEST CONSIDERATIONS
9. NOTES
APPENDIX A - MODIFIED KARL FISCHER WATER ANALYSIS METHOD

Specifies a brief discussion of the icing problem in aircraft fuel systems and different means that have been used to test for icing.

Committee
AE-5A
DocumentType
Revision
Pages
15
PublisherName
SAE International
Status
Current
Supersedes

SAE ARP 5757 : 2016 GUIDELINES FOR ENGINE COMPONENT TESTS
SAE ARP 5794 : 2014 CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD

MIL-S-8710 Revision B:1969 STRAINER, AIRFRAME FUEL SYSTEM, GENERAL SPECIFICATION FOR
ASTM D 1064 : 1997 Standard Test Methods for Iron in Rosin Tall Oil Fatty Acids and Other Related Products (Withdrawn 2002)
MIL-P-5238 Revision C:1974 PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR
SAE AIR 790 : 2006 CONSIDERATIONS ON ICE FORMATION IN AIRCRAFT FUEL SYSTEMS
MIL-F-17874 Revision B:1965 FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF
MIL V 38003 : NOTICE 1 VALVE, FUEL LEVEL CONTROL, FUEL TANK, AIRCRAFT GENERAL SPECIFICATION FOR
MIL F 38363 : B (3) FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-F-8615 Revision D:1976 FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]

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