Thank you for your interest in part number 17G130383-1, a component manufactured by Boeing Company The that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 5120-01-383-6388 and features the description “Tool Spring Compres.” To request a quote for part number 17G130383-1, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 5120-01-383-6388 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from Boeing Company The, which is associated with the CAGECode 88277. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 5120 Hand Tools Nonedged Nonpowered part number 17G130383-1.
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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