You are currently exploring our in-stock options for part number 475603 with the NSN 5340008070925. This product is listed with the description “Seat Helical Compression Spring” and is manufactured by Turbo Power And Marine System Inc. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number 475603 is listed alongside the NSN 5340-00-807-0925 and belongs to the FSC 5340 Hardware Commercial. Additionally, it is also under the CAGE Code 11449, which is assigned to Turbo Power And Marine System Inc. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number 475603 seamless.
| 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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