At Aviation Parts Circuit, we offer an unparalleled selection of parts for the aerospace, civil aviation, defense, electronics, and IT hardware markets. Owned and operated by ASAP Semiconductor, we have access to an inventory of more than two billion new and obsolete parts organized into an efficient, streamlined, and easy-to-navigate purchasing platform. Part numbers such as 34A12204, which is a Shroud Compressor B from manufacturer Triumph Engine Control Systems Llc, are in stock and ready to ship with short lead times and competitive prices. We specialize in leveraging our purchasing power with major suppliers, allowing us to offer lower costs and faster shipping on all orders, even in AOG situations. Our team at Aviation Parts Circuit is available 24/7x365 to provide you with a quick quotation on part 34A12204 and any other NSN part listed on our website.
To help users quickly locate the parts they need, our website offers a broad scope of parametric search measures, allowing customers to filter parts by their Federal Supply Group or Class, part type, part family, CAGE Code, NSN, and more. For example, if you are in need of Triumph Engine Control Systems Llc parts from NSN 2995003074902, our website can provide you with a selection of parts exclusively from that manufacturer and NSN. At Aviation Parts Circuit, our goal is not only to improve the parts procurement process, but to revolutionize it entirely. To begin the NSN part 34A12204 purchasing process instantly, submit an RFQ today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2995-00-307-4902 Item Description: Shroud Compressor B | 2995 | 003074902 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
34a12204 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | J-57 AIRCRAFT ENGINE |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | OVERALL LENGTH 1.130 TO 1.160 IN;OVERALL HEIGHT 2.270 TO 2.290 IN;OVERALL WIDTH 1.060 TO 1.070 IN;HOLE FOR OUTER GOVERNOR SHAFT 0.5905 TO 0.6000 IN;WALL THICKNESS 0.039 TO 0.057 IN;LIP OF SHAFT HOLE 0.110 TO 0.120 IN FROM SHROUD BODY,MATL S |
ZZZV | FSC APPLICATION DATA | CONTROL,COMPRESSOR BLEED A12110AAG,A12140KY,A12702AHF,A12715RR,A12902AJC,A12902AJJ,A17101RR |
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