If you are in search of dependable 9523M21P01 Shroud Segment Turbine Aircraft products, you can count on Rapid Mil Parts. You have taken a particular interest in part number 9523M21P01, a Unison Engine Components Inc component that is listed with the NSN 2840011753023 for identification purposes. When you are prepared to start the purchasing process for part number 9523M21P01, we provide online RFQ forms to fill out and submit for the means of receiving competitive quotes for your comparisons.
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Our dedication to quality is not merely a statement, and we strive to always exceed industry expectations for your benefit with the best NSN products, aerospace parts, military and defense parts, and other similar items on the market. For your convenience, part number 9523M21P01 is listed alongside the NSN 2840-01-175-3023 and is categorized under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components.
Additionally, this NSN part is specifically produced under CAGE Code 16190, which identifies the specific Unison Engine Components Inc facility it traces back to. If you are interested in kicking off procurement for your needs through phone or email or simply wish to discuss our diverse services and your purchasing options, do not hesitate to connect with a staff member of ours today!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-175-3023 Item PartTypeName: SHROUD SEGMENT,TURBINE,AIRCRAFT | 2840 | 011753023 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
9532M21P01 | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 0.254 INCHES MINIMUM AND 0.375 INCHES MAXIMUM |
ABPX | MATERIAL THICKNESS | 0.077 INCHES MINIMUM AND 0.085 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | B1B ACFT/F108 ACFT ENGINE |
APGF | DESIGN TYPE | COMPRESSOR |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
CZCJ | STAGE NUMBER | 1 |
FEAT | SPECIAL FEATURES | T.O. 2J-F108-4; HIGH PRESSURE TURBINE SHROUD AND 1ST STAGE L.P. TURBINE NOZZLE; U-SHAPED CLIPS |
MATT | MATERIAL | NICKEL ALLOY OUTER CASE |
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