Welcome to our online Request for Quote (RFQ) service, where you can fill out and submit the form provided below to obtain tailored procurement options from our team of industry experts. You have taken interest in part number PD07WRGBZOENI12-TYPE-II, which is a Testing Kit Petrole item from Warner Robins Air Logistics Center that is listed with the NSN 6630-01-552-5367 for quick identification. Should you wish to move forward with quotation for this listing, be sure that you supply us with key details like your target pricing, quality, and delivery date. This information is what we will base presented quotes on, with responses offered shortly after the receipt and review of each form.
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To ensure that customers only procure exact items of need, we present our offerings with as much relevant data as possible. For example, part number PD07WRGBZOENI12-TYPE-II was specifically produced by Warner Robins Air Logistics Center under the CAGE Code 98752, providing traceability. Furthermore, with the NSN 6630-01-552-5367, one can also determine that this listing falls under Federal Supply Class (FSC) 6630 Chemical Analysis Instruments. Alongside such details, all purchases will come delivered with any applicable qualifying certifications, furthering the reliability of our purchasing options. With this in mind, be sure to request a quote on part number PD07WRGBZOENI12-TYPE-II, and we will be in touch.
| 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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