Request a Quote for Hamilton Sundstrand Corporation Part Number 160009-5 with the NSN 2835-01-053-7558

Part Number: 160009-5

Alternate P/N: 1600095

Manufacturer: Hamilton Sundstrand Corporation

NSN: 2835-01-053-7558

NIIN: 010537558

Item Name : Diffuser Turbine Engine

CAGE Code: 55820

FSC: 2835 Gas Turbines and Jet Engines Non Aircraft Prime Mover Aircraft Non Prime Mover and Components

FSG: 28 Engines Turbines and Components

Country : USA

NCB Code : 01

Aerospace Engineering Solutions is proud to offer immediate purchasing options on Hamilton Sundstrand Corporation part number 160009-5, a Diffuser Turbine Engine product we carry that is listed with the NSN 2835-01-053-7558 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.

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are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor.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

For your reference, this product is traceable to Hamilton Sundstrand Corporation through the CAGE Code 55820, as well as categorized under FSC 2835 Gas Turbines and Jet Engines Non Aircraft Prime Mover Aircraft Non Prime Mover and Components based on the first four digits of the NSN 2835-01-053-7558. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 160009-5 and other NSN items of need.

NSN Information for Part Number 160009-5 with NSN 2835-01-053-7558, 2835010537558

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
2835-01-053-7558 Item PartTypeName: DIFFUSER,TURBINE ENGINE	2835	010537558	0	N
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
	U			A
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
160009-1	5	9	5

Characteristics Data of NSN 2835-01-053-7558, 2835010537558

MRC	Criteria	Characteristic
AGAV	END ITEM IDENTIFICATION	JET FUEL STARTER PN5902924A F16 ACFT,T.O. 2JA3-57-3
FTLD	FUNCTIONAL DESCRIPTION	FOR ACFT. STARTING AND MAIN ENGINE MOTORING
RTSE	RELATIONSHIP TO SIMILAR EQUIPMENT	SIMILAR TO PN105772-100 &-200,MAIN DIFFERENCE BETWEEN-100 &-200 IS THROAT SPACING AND L.E. DIA
TEXT	GENERAL CHARACTERISTICS ITEM DESCRIPTION	DIFFUSER 17 VANE AIRFOIL; LENGTH AS INSTALLED 2.250 IN. MIN AND 2.310 IN. MAX; OUTER DIA 11.150 IN. MIN AND 11.160 IN. MAX; INNER HOLE DIA 6.980 IN. MIN AND 7.020 IN. MAX; A THROAT SPACING OF 0.420-0.426 IN. AT 17 PLACES; MATL IS ALUM ALLY