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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS
28-07-2022
English
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Superseded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 AS 1710 : 2014 | 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 | VALVES, CHECK, AIRCRAFT FUEL SYSTEM |
GEIASTD0007B:2013 | LOGISTICS PRODUCT DATA |
SAE AS 1650 : 2017 | 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 AS 5877 : 2016 | DETAILED SPECIFICATION FOR AIRCRAFT PRESSURE REFUELING NOZZLE |
SAE AIR 786 : 2014 | 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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