SAE ARP 4028 : 2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AIRCRAFT/ENGINE FUEL PUMP TWO PHASE (SLUGGING FLOW) INLET PERFORMANCE TEST AND EVALUATION
Hardcopy , PDF
02-05-2020
English
01-01-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS/CONSIDERATIONS
4. TECHNICAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. TEST DATA
7. TEST PROCEDURE
Pertains to all engine or airframe mounted fuel pumps and controls when required by the applicable specification.
| Committee |
AE-5B
|
| DocumentType |
Standard
|
| Pages |
19
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE ARP 492 : 2014 | AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST |
| SAE MAP 749 : 2015 | AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL) |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| ASTM D 86 : 2017-06 | TEST METHOD FOR DISTILLATION OF PETROLEUM PRODUCTS AND LIQUID FUELS AT ATMOSPHERIC PRESSURE |
| SAE ARP 492 : 2014 | AIRCRAFT ENGINE FUEL PUMP CAVITATION ENDURANCE TEST |
| SAE AIR 1326 : 1997 | AIRCRAFT FUEL SYSTEM VAPOR-LIQUID RATIO PARAMETER |
| MIL-G-5572 Revision F:1969 | GASOLINE, AVIATION, GRADES 80/87, 100/130, 115/145 |
| MIL T 83133 : D | TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
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