Find Part Number 6809081 With NSN 2840-00-877-0065 by Rolls Royce Corporation!

Part Number: 6809081

Manufacturer: Rolls Royce Corporation

NSN: 2840-00-877-0065

NIIN: 008770065

Item Name : Blade Compressor Aircraft Gas Tu

CAGE Code: 63005

FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components

FSG: 28 Engines Turbines and Components

Country: USA

NCB Code: 00

Welcome to National Stock Numbers Quotes, your go-to solution for Blade Compressor Aircraft Gas Tu components by Rolls Royce Corporation. With over 2 billion ready-to-purchase products in our inventory, customers can easily meet rigid time constraints and inflexible budget parameters. National Stock Numbers Quotes maintains a diverse database of items that suit a myriad of industry verticals, including aerospace, defense, and civil sectors, among others. On this page, you can submit a quote request for part number 6809081 with NSN 2840008770065 to receive a customized solution in as little as 15 minutes or less.

Note : We Will Not Share Your Information To Any Third Parties.

Product Details

“*” Required Fields Are Compulsory

Contact Information

* By clicking this box, I acknowledge that I have read and accept the ASAP Semiconductor Terms and Conditions and agree that all quotes and purchase orders are exclusively subject to the ASAP Semiconductor Terms and Conditions.

I consent to receive email communications from ASAP Semiconductor and can unsubscribe at any time.
ASAP Semiconductor is a wholly independent aftermarket parts distributor.
This website is intended for quotations based on part numbers only. Please DO NOT submit drawings, technical data, or other specifications through this portal.

Disclaimer: This is a quotation for the goods listed above. This quotation is meant as an estimate and does not reflect a final bill or invoice. All quotations are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor. This quotation is subject to the ASAP Semiconductor Terms & Conditions available at https://www.asapsemi.com/terms-conditions.aspx . All United States Government and Department of Defense bids are quoted as CAGE code 6RE77 from ASAP Semiconductor’s Anaheim, California facility. Any quotation from ASAP Semiconductor without 6RE77 is void.

Upload RFQ SHEET

If you have more than one item, upload your spreadsheet here

Upload File

At National Stock Numbers Quotes, we make it a priority to meet our customers’ operational requirements, so we keep catalogs fully stocked with in-demand NSN parts like those with the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components by Rolls Royce Corporation. For additional specification regarding your part needs, you can also find a wide range of items by their respective CAGE Code, such as 63005, and many other designations for your ease-of-search. Kick off the procurement process with a competitive quote for NSN 2840-00-877-0065 today and see why customers continuously rely on National Stock Numbers Quotes time and time again. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock!

NSN Information for Part Number 6809081 with NSN 2840-00-877-0065, 2840008770065

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
2840-00-877-0065 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU	2840	008770065	0	N
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
	U			A	0
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
6809081	2	2	3

Characteristics Data of NSN 2840-00-877-0065, 2840008770065

MRC	Criteria	Characteristic
ABHP	OVERALL LENGTH	3.753 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	T56 AIRCRAFT ENGINE
CXCY	PART NAME ASSIGNED BY CONTROLLING AGENCY	BLADE,COMPRESSOR-1ST STAGE
MATT	MATERIAL	STEEL CORROSION RESISTING OVERALL
ABMK	OVERALL WIDTH	1.197 INCHES NOMINAL
CRTL	CRITICALITY CODE JUSTIFICATION	AGAV
FEAT	SPECIAL FEATURES	CONTOUR OF CONCAVE AND CONVEX SIDES OF AIRFOIL SECTIONS MAY VARY WITHIN A .006 BAND PARALLEL TO BASIC; TOLERANCE BAND APPLIES TO SECTION CONTOURS UP TO TANGENT POINT OF LEADING AND TRAILING EDGE RADII; AIRFOIL SURFACES SHALL BLEND SMOOTHLY