Aerospace Engineering Solutions is proud to offer immediate purchasing options on Warner Robins Air Logistics Center part number PD07WRGBZOENI12-TYPE-II, a Testing Kit Petrole product we carry that is listed with the NSN 6630-01-552-5367 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Warner Robins Air Logistics Center through the CAGE Code 98752, as well as categorized under FSC 6630 Chemical Analysis Instruments based on the first four digits of the NSN 6630-01-552-5367. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number PD07WRGBZOENI12-TYPE-II and other NSN items of need.
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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