Thank you for taking interest in the Turbo Power And Marine System Inc part number 475603, a Seat Helical Compression Spring product that we stock that is presented alongside the NSN 5340-00-807-0925 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 475603 specifically traces back to Turbo Power And Marine System Inc through the CAGE Code 11449, a distinct identifier for one of their physical locations. Moreover, with the NSN 5340-00-807-0925, this listing falls within Federal Supply Code (FSC) 5340 Hardware Commercial, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 475603 here on Aero OEM Parts 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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