You have arrived on the Request for Quote (RFQ) page for part number 8719, a Goodrich Corporation component that is listed with the product description “Torque Shaft Damper Nws” and NSN 1620-00-741-9181 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 Goodrich Corporation part number 8719, you can seamlessly search for more items from this manufacturer or CAGECode 13002 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 1620 Aircraft Landing Gear Components, which this component falls under having the NSN 1620-00-741-9181. Whether you desire part number 8719 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 |
---|---|---|---|---|---|---|
1620-00-741-9181 Item PartTypeName: TORQUE SHAFT,DAMPER,NWS | 1620 | 007419181 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
8719 | 6 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | T-38 ACFT |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
FEAT | SPECIAL FEATURES | BASED ON HOW THE ITEM IS USED ON THE AIRCRAFT |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 9H2-3-54-4 |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | MIL-S-5626 STEEL CHROME PLATED;HEAT TREAT TO 180000 PSI MIN;1.060 IN. DIA BY 4.294 IN. LG SHAFT;0.4065 IN. DIA LEVER PIVOT HOLE OFFSET 0.950 IN. FROM CENTER LINE OF SHAFT;3/4-16NF3 THD 0.625 IN. DEEP IN END OF SHAFT |
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