Request a Quote on Part Number PDO7WRGBZOENI12-TYPE-I with the NSN 6630-01-552-5360 by Warner Robins Air Logistics Center

Part Number: PDO7WRGBZOENI12-TYPE-I

Alternate P/N: PDO7WRGBZOENI12TYPEI

Manufacturer: Warner Robins Air Logistics Center

NSN: 6630-01-552-5360

NIIN: 015525360

Item Name : Testing Kit Petrole

CAGE Code: 98752

FSC: 6630 Chemical Analysis Instruments

FSG: 66 Instruments and Laboratory Equipment

Country : USA

NCB Code : 01

Thank you for your interest in Warner Robins Air Logistics Center part number PDO7WRGBZOENI12-TYPE-I, a Testing Kit Petrole item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 6630-01-552-5360, and you can obtain customized procurement solutions on this component from our team members by completing and submitting the form below. For our specialists to best deliver quotes that accommodate your specifications, please be sure we are presented with essential details like your target price, desired quantity, and anticipated fulfillment timeline. Once we have the opportunity to receive and review your submission, we will strive to provide a tailored response for your consideration within 15 minutes or less.

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Besides part number PDO7WRGBZOENI12-TYPE-I, you may browse our platform further for similar components produced by Warner Robins Air Logistics Center under the CAGECode 98752, as well as additional products that are categorized under FSC 6630 Chemical Analysis Instruments. If you have any questions regarding our services or the NSN 6630-01-552-5360 items that we sell, you may always give us a call or email, as we would be delighted to assist you in any way that we can. Otherwise, we encourage you to request a quote for part number PDO7WRGBZOENI12-TYPE-I at your earliest convenience.

Characteristics Data of NSN 6630-01-552-5360, 6630015525360

MRC	Criteria	Characteristic
RDAL	III REFERENCE DATA AND LITERATURE	ASTM D3241
ALCD	III USAGE DESIGN	ANALYSIS OF PETROLEUM PRODUCT
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 115.0V, 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
FCLS	III FUNCTIONAL CLASSIFICATION	AA-8.16