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 17G980525-501, which is a Fixture Aircraft Ma item from Boeing Company The that is listed with the NSN 4920-01-333-1975 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 17G980525-501 was specifically produced by Boeing Company The under the CAGE Code 88277, providing traceability. Furthermore, with the NSN 4920-01-333-1975, one can also determine that this listing falls under Federal Supply Class (FSC) 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. 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 17G980525-501, and we will be in touch.
MRC | Criteria | Characteristic |
---|---|---|
SR-5 | THE MANUFACTURERS DATA | |
FEAT | SPECIAL FEATURES | MATERIAL IS ALUMINUM AND STEEL; THIS ITEM IS USED IN CONJUNCTION WITH THE TRANSDUCER INDICATOR (4920012866545),THE TESTER BASE (4920012622655),THE HAND PUMP (4320009988206),THE HYDRAULIC HOSE (4720012058698),THE MULTIMETER (6625011960014),AND THE D.C. POWER SUPPLY (6130001481796) |
SR-5 | MANUFACTURERS CODE | 88277 |
SR-5 | DESIGN CONTROL REFERENCE | 17G980525-501 |
RDAL | REFERENCE DATA AND LITERATURE | 1C-17A-4-4; SERD:980525; 980611 |
CWFR | NOMINAL OVERALL LENGTH | 3.000 FEET |
FTLD | FUNCTIONAL DESCRIPTION | THIS FIXTURE IS USED TO SECURE TESTER BASE FOR VERIFYING THE LOAD CELL;THIS FIXTURE IS A MECHANICAL DEVICE WHICH RESTRAINS THE AIRDROP PLATFORM UNTIL A PRESET FORCE IS REACHED AND WHEN THE PRESET FORCE IS REACHED THE VRL AUTOMATICALLY TRIPS THE AIRDROP PLATFORMCH AUTOMATICALLY TRIPS THE AIRDROP PLATFORMS EXIT THE AIRCRAFT |
AGAV | III END ITEM IDENTIFICATION | C-17A AIRCRAFT |
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