You have arrived on the Request for Quote (RFQ) page for part number 17G130383-1, a Boeing Company The component that is listed with the product description “Tool Spring Compres” and NSN 5120-01-383-6388 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside Boeing Company The part number 17G130383-1, you can seamlessly search for more items from this manufacturer or CAGECode 88277 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 5120 Hand Tools Nonedged Nonpowered, which this component falls under having the NSN 5120-01-383-6388. Whether you desire part number 17G130383-1 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
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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