Aerospace Performance Parts is pleased to offer immediate purchasing options for Boeing Company The part number 17G130383-1, which you have taken interest in. This Tool Spring Compres item is listed alongside the NSN 5120-01-383-6388 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 17G130383-1 or any other FSC 5120 Hand Tools Nonedged Nonpowered components we carry from Boeing Company The under CAGE Code 88277, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 5120-01-383-6388 part number 17G130383-1 today, knowing we will support all your operational needs with care.
| 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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