SAE ARP 1401 : 2012
Current
The latest, up-to-date edition.
AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST
Hardcopy , PDF
English
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ASTM D 1064 : 1997 | Standard Test Methods for Iron in Rosin Tall Oil Fatty Acids and Other Related Products (Withdrawn 2002) |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 AIR790C | 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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