Thank you for considering Warner Robins Air Logistics Center part number PD07WRGBZOENI12-TYPE-II, a component we stock that is further identified by the NSN 6630-01-552-5367 and product description “Testing Kit Petrole.” This item is currently available for purchase on our website today, and you can obtain a tailored quote at any time by completing the form on this page. To help us provide the best solution, please include critical details like your quantity requirements, target pricing, and delivery preferences within the submitted request. Once we receive your form, our team will promptly review provided information and respond with a quote that aligns with your needs.
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Alongside part number PD07WRGBZOENI12-TYPE-II, we encourage you to explore other offerings we carry from Warner Robins Air Logistics Center that have been produced under CAGE Code 98752, as well as similar products classified under FSC 6630 Chemical Analysis Instruments that may suit your projects. We can help you obtain pricing on all items that you are interested in, securing the most optimal solution for you. We are also happy to discuss any requirements that you may have, presenting specialized options for many restrictions and needs alike. With our services in mind, please submit your request for part number PD07WRGBZOENI12-TYPE-II today and discover why Marine Defence Parts is a trusted partner for naval and defense procurement.
MRC | Criteria | Characteristic |
---|---|---|
RDAL | III REFERENCE DATA AND LITERATURE | ASTM D3241 |
ALCD | III USAGE DESIGN | ANALYSIS OF PETROLEUM PRODUCT |
FCLS | III FUNCTIONAL CLASSIFICATION | AA-8.16 |
FTLD | III FUNCTIONAL DESCRIPTION | EVALUATES THE OXIDATION STABILITY OF AVIATION TURBINE FUELS |
FEAT | SPECIAL FEATURES | TEMPERATURE MEASUREMENT RANGE SHALL BE +212 DEG F TO +716 DEG F, SAMPLE CAPACITY SHALL BE 500ML MINIMUM, DIFFERENTIAL PRESSURE SHALL BE 0 TO 300 MMHG, POWER REQUIRED SHALL BE 230.0V, WEIGHT OF THE SYSTEM SHALL NOT EXCEED 200 LBS, FUEL LEAK AUTOMATIC SHUT-OFF MECHANISM SHALL BE INCLUDED, TESTER SHALL BE CAPABLE OF AUTOMATIC PERFORMANCE OF PREPROGRAMMED TESTS AND USER DEFINED TESTS, SHALL HAVE A 15 INCH MINIMUM DIAGONAL DISPLAY SCREEN OF CRT OR BETTER, TESTERS OPERATING SYSTEM SHALL BE COMPATIBLE WITH THE LATEST AIR FORCE STANDARD, TESTER SHALL PROVIDE A MEANS OF CONNECTING A STANDARD PRINTER VIA USB OR PARALLEL PORT, TESTER SHALL HAVE A STANDARD KEYBOARD FOR DATA INPUT |
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