MIL-PRF-7024 Revision F:2012
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS
07-28-2022
English
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Specifies the requirements for three types of calibrating fluid used in the calibration of aircraft fuel system components.
| Committee |
FSC 6850
|
| DevelopmentNote |
Supersedes MIL C 7024 (D). (01/2012)
|
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AS1710D | COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY, THREADED TYPE WITH FERRULES |
| MIL-DTL-22263 Revision C:2009 | Coupling Fuel Line, Flexible, 125 PSI General Specification for |
| SAE AS 5304 : 2011 | STANDARD SPECIFICATION FOR TURBINE FLOWMETERS |
| MIL-DTL-85061 Revision C:2009 | COUPLING, FUEL LINE, FLEXIBLE, 125 PSI |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| MIL-DTL-7899 Revision D:2014 | Valve, Check, Aircraft Fuel System |
| GEIASTD0007B:2013 | LOGISTICS PRODUCT DATA |
| SAE AS1650E | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING, PROCUREMENT SPECIFICATION |
| SAE ARP 1827C : 2014 | MEASURING AIRCRAFT GAS TURBINE ENGINE FINE FUEL FILTER ELEMENT PERFORMANCE |
| SAE AS 7510 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| MIL-PRF-83323 Revision D:2016 | TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
| MIL-PRF-62625 Revision B:2009 | VALVE, FUEL-DRAIN |
| MIL-PRF-25017 Revision H:2011 | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (NATO S-1747) |
| MIL-DTL-24788 Revision B:2017 | Coupling Assembly, Semi-Dry-Break, Quick-Disconnect Fuel, with or without Continuity Switch |
| SAE MAP 749 : 2015 | AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL) |
| SAE AS5877B | DETAILED SPECIFICATION FOR AIRCRAFT PRESSURE REFUELING NOZZLE |
| SAE AIR786B | ELASTOMER COMPATIBILITY CONSIDERATIONS RELATIVE TO ELASTOMERIC SEALANT SELECTION |
| SAE ARP 1953 : 2014 | ACCEPTANCE TEST PROCEDURES AND STANDARDS TO ENSURE CLEAN FUEL SYSTEM COMPONENTS |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| SAE ARP 1797 : 2014 | AIRCRAFT AND AIRCRAFT ENGINE FUEL PUMP LOW LUBRICITY FLUID ENDURANCE TEST |
| ASTM D 5452 : 2012 : REDLINE | Standard Test Method for Particulate Contamination in Aviation Fuels by Laboratory Filtration |
| ASTM D 3227 : 2016 : REDLINE | Standard Test Method for (Thiol Mercaptan) Sulfur in Gasoline, Kerosine, Aviation Turbine, and Distillate Fuels (Potentiometric Method) |
| ASTM D 156 : 2015 : REDLINE | Standard Test Method for Saybolt Color of Petroleum Products (Saybolt Chromometer Method) |
| ASTM D 86 : 2017-06 | TEST METHOD FOR DISTILLATION OF PETROLEUM PRODUCTS AND LIQUID FUELS AT ATMOSPHERIC PRESSURE |
| MIL-PRF-25017 Revision H:2011 | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (NATO S-1747) |
| ASTM D 2386 : 2015 | Standard Test Method for Freezing Point of Aviation Fuels |
| ASTM D 5191 : 2015-10 | TEST METHOD FOR VAPOR PRESSURE OF PETROLEUM PRODUCTS (MINI METHOD) |
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