Thank you for your interest in Turbo Power And Marine System Inc part number 475603, a Seat Helical Compression Spring item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 5340-00-807-0925, 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 475603, you may browse our platform further for similar components produced by Turbo Power And Marine System Inc under the CAGECode 11449, as well as additional products that are categorized under FSC 5340 Hardware Commercial. If you have any questions regarding our services or the NSN 5340-00-807-0925 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 475603 at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-807-0925 Item PartTypeName: SEAT,HELICAL COMPRESSION SPRING | 5340 | 008070925 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 475603 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 0.1900 INCHES NOMINAL |
| ABXV | BORE DIAMETER | 0.2460 INCHES MINIMUM AND 0.2510 INCHES MAXIMUM |
| APGF | DESIGN TYPE | SOLID |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| FEAT | SPECIAL FEATURES | THIS PART MEETS THE Y REQUIREMENTS DUE TO CRITICAL FEATURES,TOLERANCES,FIT RESTRICTIONS,MATERIAL PROPERTIES AND MANUFACTURING PROCESS. FAILURE COULD RESULT IN LOSS OR SUBSTANTIAL DAMAGE TO WEAPON SYSTEM,DEATH OR SERIOUS INJURY |
| MATT | MATERIAL | STEEL COMP 1212 |
| ABPR | FIRST STEP DIAMETER | 1.0200 INCHES MINIMUM AND 1.0400 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | W/S: AIRCRAFT,STRATOLIFTER C-135; AIRCRAFT,STARLIFTER C-141; JOINT STARS TARGET RADAR SYSTEM; ENGINE,AIRCRAFT,TF-33-P-7 (C-141A/B); ENGINE,AIRCRAFT,TF33-P-3/5/9 (C/EC-135,B-52H); ENGINE,AIRCRAFT,TF33-PW-102 (C-135E,EC-135H/K/P) |
| BBRB | END DIAMETER | 0.5600 INCHES MINIMUM AND 0.5800 INCHES MAXIMUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5010 ASSN STD SINGLE MATERIAL RESPONSE |
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