You have arrived on the Request for Quote (RFQ) page for part number 475603, a Turbo Power And Marine System Inc component that is listed with the product description “Seat Helical Compression Spring” and NSN 5340-00-807-0925 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 Turbo Power And Marine System Inc part number 475603, you can seamlessly search for more items from this manufacturer or CAGECode 11449 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 5340 Hardware Commercial, which this component falls under having the NSN 5340-00-807-0925. Whether you desire part number 475603 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.
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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