Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 26791-1, a Hamilton Sundstrand Corporation item with the NSN 2835009611464 that is listed alongside the description “Shield Turbine Nozzle.” If you are interested in part number 26791-1 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 26791-1 is specifically listed with the NSN 2835-00-961-1464, and this code can be used to determine that it falls under FSC 2835 Gas Turbines and Jet Engines Non Aircraft Prime Mover Aircraft Non Prime Mover and Components. Additionally, while tracing back to Hamilton Sundstrand Corporation, this NSN part was specifically produced under CAGE Code 55820. With our services and dedication to simple procurement in mind, get started with us today!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2835-00-961-1464 Item PartTypeName: SHIELD,TURBINE NOZZLE | 2835 | 009611464 | N | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | ||||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
26791-1 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CRES,MIL-S-6721 COMPOSITION 321 TEMPER T2,0.027 IN. MIN,0.035 IN.MAX THK MATERIAL,8.380 IN. MIN,8.440 IN. MAX FLANGE OD,4.804 IN. MIN,4.850 IN. MAX BODY OD,4.750 IN. MIN,4.780 IN. MAX ID,0.730 IN. MIN,0.790IN. MAX O/A LG,12 HOLES 0.100 IN. |
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