Thank you for your interest in Boeing Company The part number 17G130383-1, a Tool Spring Compres item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 5120-01-383-6388, 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 17G130383-1, you may browse our platform further for similar components produced by Boeing Company The under the CAGECode 88277, as well as additional products that are categorized under FSC 5120 Hand Tools Nonedged Nonpowered. If you have any questions regarding our services or the NSN 5120-01-383-6388 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 17G130383-1 at your earliest convenience.
MRC | Criteria | Characteristic |
---|---|---|
SR-5 | THE MANUFACTURERS DATA | |
SR-5 | MANUFACTURERS CODE | 88277 |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | SIZE: 2.5"" DIA X 3.75"" LENGTH; WEIGHT: 0.5 LBS; MATERIAL: ALUMINUM; FINISH: ANODIZE; THE C-17 A/C INCORPORATES A SHIMMY DAMPER ON EACH MAIN GEAR TODAMPEN VIBRATION/SHIMNY DURING TAKEOF F AND LANDING; A MEANS IS REQUIRED TO COMPRESS THE SPRINGS USING AN ARBOR PRESS IN ORDER TO REMOVE AND INSTALL THERESERVOIR CAP |
SR-5 | DESIGN CONTROL REFERENCE | 17G130383-1 |
ZZZV | III FSC APPLICATION DATA | TOOL,SPRING COMPRESSION - SHIMMY DAMPER RESERVOIR |
FTLD | III FUNCTIONAL DESCRIPTION | THE TOOL IS CYLINDRICALLY SHAPED WITH A 1.25"" DIA X 2.25"" DEEP MACHINEDHOLE; THE HOLE ALLOWS THE TOOL TO FIT OVER THE PISTON SHAFT AND COMPRESS THESPRINGS WITHIN THE CAP; ONCE THE SPRINGS ARE COMPRESSED, THE RETAINING RING CAN BE REMOVED AND THE SPRINGS RELEASED IN ORDER TO REMOVE THE CAP |
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