Request a Quote on United Technologies Corporation Part Number 4082885 with the NSN 2840-01-440-1697 Today!

Part Number: 4082885

Manufacturer: United Technologies Corporation

NSN: 2840-01-440-1697

NIIN: 014401697

Item Name : Damper Turbine Blade Aircraft Tu

CAGE Code: 77445

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

FSG: 28 Engines Turbines and Components

Country: USA

NCB Code: 01

Thank you for taking an interest in the Damper Turbine Blade Aircraft Tu NSN parts that we carry here on Buy Military Ground Vehicle Parts. You have reached the RFQ page for part number 4082885, an item that traces back to the manufacturer United Technologies Corporation. Listed with NSN 2840014401697, this listing is available for purchase from our website at any time. If you are interested in part number 4082885 and wish to learn more, be sure to fill out and submit the RFQ form found on this page. By presenting us information such as your target price and expected delivery date, we can best formulate and present a solution that closely caters to your unique needs and restrictions alike.

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 Customer 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are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor.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.

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

Upload RFQ SHEET

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

Upload File

To make the part searching process as simple as possible, we choose to list offerings with as much relevant information as we can. For example, while part number 4082885 is manufactured by United Technologies Corporation, it is specifically listed along with CAGE Code 77445. With this identifier, you can trace this item back to the exact facility it was sourced from. Additionally, with the NSN 2840-01-440-1697, this signifies that the product belongs to the Federal Supply Class 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Alongside our easy-to-navigate database, we also offer highly competitive pricing and rapid lead times for the benefit of our customers. Get in touch with an industry expert today and see why so many customers steadily depend on us for their operational needs.

NSN Information for Part Number 4082885 with NSN 2840-01-440-1697, 2840014401697

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
2840-01-440-1697 Item PartTypeName: DAMPER,TURBINE BLADE,AIRCRAFT TU	2840	014401697	0	N
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
	U			A	0
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
4082885	2	2	3

Characteristics Data of NSN 2840-01-440-1697, 2840014401697

MRC	Criteria	Characteristic
ABHP	OVERALL LENGTH	0.565 INCHES MINIMUM AND 0.571 INCHES MAXIMUM
ABMZ	DIAMETER	16.788 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
APGF	DESIGN TYPE	AXIAL COMPRESSOR
CQFM	HARDNESS RATING	34.0 ROCKWELL C MINIMUM OVERALL AND 44.0 ROCKWELL C MAXIMUM OVERALL
CRTL	CRITICALITY CODE JUSTIFICATION	FEAT AND CZBJ
CZBJ	ENGINE SECTION LOCATION	COMPRESSOR
FEAT	SPECIAL FEATURES	T.O. 2J-F100-54, FIG 99, IND 21; REPL P/N 4074864 ONCE TCTO HAS BEEN ACCOMPLISHED; RETAINING PLATE DAMPER IS SYMMETRICAL IN SHAPE AND HAS 6 RETENTION TABS FORWARD AND AFT TO PRECLUDE POSSIBLE REVERSE INSTALLATION AND RESULTING CUT-OFF OF CO
MATT	III MATERIAL	NICKEL ALLOY OVERALL
MDCL	MATERIAL DOCUMENT AND CLASSIFICATION	AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL