We are pleased to offer procurement for Goodrich Corporation part number 2887071 here on NSN Portal, a Ball Joint product that is listed with the NSN 3040-01-560-7936 for ease of identification. You have reached our Request for Quote (RFQ) form for this listing, where you are encouraged to submit details on your requirements to receive tailored purchasing options from our staff. As you will see, we ask that you offer key information on your pricing target, desired quantity, and more, as this will ensure that the representative who responds to your request is able to provide the most fitting solutions for your needs.
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Whether you procure part number 2887071 or other NSN products from our website, you can rest assured that we uphold full traceability for all items. For example, this particular listing traces back to Goodrich Corporation through the CAGE Code 99551, as well as falls under FSC 3040 Miscellaneous Power Transmission Equipment based on having the NSN 3040-01-560-7936. Furthermore, every purchase will be delivered with any applicable qualifying certifications or manufacturer trace documentation as per our NO CHINA SOURCING pledge. If you are ready to experience why professionals rely on us for their needs, request a quote for part number 2887071 today and take advantage of our industry-leading services.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 3040-01-560-7936 Item PartTypeName: BALL JOINT | 3040 | 015607936 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 2887071 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | End Item Identification | F-22 RAPTOR |
| CXCY | Part Name Assigned By Controlling Agency | ADAPTER STRAIGHT FLANGE INPUT COUPLING |
| MRC | Decoded Requirement | Clear Text Reply |
| FEAT | Special Features | MATERIAL IS PRIMARILY TITANIUM WITH SOME STEEL COMPONENTS. ITEM CONNECTS TO PTO SHAFT CENTER TUBE ON ONE END AND IS BOLTED TO THE EMAD (ENGINE SIDE) ON THE FLANGE END. ASSEMBLY CONTAINSA BALL AND SOCKET WHICH REQUIRES REPLACING EVERY 1,000 FLIGHT HOURS. ITEM TRANSMITS THE AXIAL LOAD THROUGH THE SHAFT WHICH OCCURS FROM THE THERMAL CYCLING OF THE ENGINE. |
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