If your operations demand part number 17G980525-501, an item produced by Boeing Company The and listed with the description “Fixture Aircraft Ma,” look no further than this page. At your convenience, you can complete the Request for Quote (RFQ) form below with details like your budget, desired quantity, and anticipated fulfillment timeline to receive customized procurement options on part number 17G980525-501. Our representatives will happily treat you to competitive pricing and swift lead times upon their receipt and review of a completed form, regularly responding in 15 minutes or less.
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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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