MIL-PRF-32020 Revision B:2011
Current
The latest, up-to-date edition.
Prover, Liquid Volumetric Positive Displacement Meter
04-05-2011
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Affirms readings on displacement and turbine meters such as permanently installed meters used with truck fill stand installations or meters mounted on mobile refueling equipment such as the R-11 6000 gallon refueler and R-12 Hydrant Refueler.
| DevelopmentNote |
B NOTICE 1 - Notice of Administrative Change. (12/2017)
|
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
The meter prover is used to verify readings on displacement and turbine meters such as permanently installed meters used with truck fill stand installations or meters mounted on mobile refueling equipment such as the R-11 6000 gallon refueler and R-12 Hydrant Refueler. The prover is designed for the verification of positive displacement and turbine meters within the operational flow range of 30 GPM to 600 GPM with operating pressures not to exceed 150 psi. The meter prover consists of a trailer chassis and running gear that contains a master meter, suitable inlet and outlet piping and connections, discharge hoses and nozzles, control valves, check valve after meter, and pressure and 2 temperature gages. The master meter prover will be designed in accordance with API MPMS 4-1 and 4-5.
| MIL-A-25896 Revision E:1983 | Adapter, Pressure Fuel Servicing, Nominal 2.5-Inch Diameter |
| API 1529 : 1998 | AVIATION FUELING HOSE |
| SAE AS8090A | Mobility, Towed Aerospace Ground Equipment, General Requirements For |
| FED-STD-297 Revision E:1985 | Rustproofing of Commercial (Nontactical) Vehicles |
| MIL-DTL-5624 Revision W:2016 | Turbine Fuel, Aviation, Grades JP-5 (NATO F-44) |
| A-A-59248 Base Document:1998 | Meter, Volumetric, Positive Displacement, Liquid, Fuel, 600 GPM |
| API MPM CH4.5 : 2016 | MANUAL OF PETROLEUM MEASUREMENT STANDARDS - CHAPTER 4.5: MASTER METER PROVERS |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-PRF-85285 Revision E:2012 | Topcoat, Aircraft and Support Equipment |
| SAE AS5877B | Detailed Specification for Aircraft Pressure Refueling Nozzle |
| A-A-59326 Revision D:2011 | Coupling Halves, Quick-Disconnect, Cam-Locking Type, General Specification for |
| API 2003 : 2015 | PROTECTION AGAINST IGNITIONS ARISING OUT OF STATIC, LIGHTNING, AND STRAY CURRENTS |
| MIL-DTL-25524 Revision F:2015 | Turbine Fuel, Aviation, Thermally Stable (JPTS) |
| MIL-DTL-83133 Revision J:2015 | Turbine Fuel, Aviation, Kerosene Type, JP-8 (NATO F-34) and NATO F-35 |
| A-A-50696 Revision D:2016 | Reels, Static Discharge, Grounding, 50, 75, and 100Foot Cable Lengths |
| ASTM F 1347 : 1991 : R2018 | Standard Specification for Manually Operated Fueling Hose Reels |
| MIL-DTL-83413 Revision C:2012 | Connectors and Assemblies, Electrical, Aircraft Grounding, General Specification for |
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