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34A12204 by Triumph Engine Control Systems Llc - Receive a Competitive Quote

We’re excited to announce that 34A12204 NSN part is now available and ready for immediate shipping. Part number 34A12204 is a Shroud Compressor Bleed Governor manufactured by Triumph Engine Control Systems Llc with NSN 2995003074902. Are you interested in a quick and competitive quote for this part?

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Just NSN Parts, owned and operated by ASAP Semiconductor, is a leading distributor of NSN (National Stock Number) parts, new and obsolete. Because of our dedication to quality, we’re the only independent distributor in the United States with a strict No China Sourcing Pledge. We’re also an AS9120B, ISO 9001:2015 certified, and FAA AC 0056B accredited member of the Aviation Suppliers Association (ASA). Our vast and comprehensive inventory of over 2 billion parts coupled with our shipping facilities in Washington, Oregon, California, New Maxico, Nevada, Arizona, Illinois, Minnesota, Pennsylvania, and New York, allow us to offer you some of the fastest delivery times in the industry.

If you’d like to learn more about NSN part number 34A12204 Shroud Compressor Bleed Governor, feel free to call us at our toll-free number, +1-714-705-4780, or email us at sales@justnsnparts.com. And, if you’d like to stay informed on new inventory or any promotions, feel free to download the ASAP Semiconductor App from Google Play or the App Store.

NSN Information for Part Number 34A12204 with NSN 2995-00-307-4902, 2995003074902

NSNFSCNIINCLSHazmatDEMILCancelled NSN
2995-00-307-4902

Item PartTypeName:

SHROUD,COMPRESSOR BLEED GOVERNOR

29950030749020N
CIICHCCESDPMICCriticalityENAC
UA
Part NumberISCRNVCRNCCHCCMSDSSADC
34A12204623

Characteristics Data of NSN 2995-00-307-4902, 2995003074902

MRCCriteriaCharacteristic
AGAVEND ITEM IDENTIFICATIONJ-57 AIRCRAFT ENGINE
TEXTGENERAL CHARACTERISTICS ITEM DESCRIPTIONOVERALL 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
ZZZVFSC APPLICATION DATACONTROL,COMPRESSOR BLEED A12110AAG,A12140KY,A12702AHF,A12715RR,A12902AJC,A12902AJJ,A17101RR