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Turbine Nozzle Tender, USA - 43349990

DEPT OF DEFENSE has floated a tender for Turbine Nozzle. The project location is USA and the tender is closing on 10 Jul 2020. The tender notice number is FD2030-20-01858, while the TOT Ref Number is 43349990. Bidders can have further information about the Tender and can request the complete Tender document by Registering on the site.

Procurement Summary

Country : USA

Summary : Turbine Nozzle

Deadline : 10 Jul 2020

Other Information

Notice Type : Tender

TOT Ref.No.: 43349990

Document Ref. No. : FD2030-20-01858

Competition : ICB

Financier : Self Financed

Purchaser Ownership : -

Tender Value : Refer Document

Purchaser's Detail

Purchaser : DEPT OF DEFENSE
Contracting Office Address : TINKER AFB, OK 73145-3070
Primary Point of Contact : Louis Colon
louis.colon.2@us.af.mil
Phone Number 4058553534

USA
Email :louis.colon.2@us.af.mil

Tender Details

Turbine Nozzle

Active Contract Opportunity

Notice ID : FD2030-20-01858

Related Notice : SPRTA1-20-Q-0367

Department/Ind. Agency : DEPT OF DEFENSE

Sub-tier : DEFENSE LOGISTICS AGENCY (DLA)

Major Command : DLA AVIATION

Sub Command : DLA AVIATION OKLAHOMA CITY

Office : DLA AVIATION AT OKLAHOMA CITY, OK

General Information

Contract Opportunity Type: Solicitation (Original)

All Dates/Times are: (UTC-05:00) CENTRAL STANDARD TIME, CHICAGO, USA

Original Published Date: Jun 10, 2020 09:26 am CDT

Original Date Offers Due: Jul 10, 2020 04:30 pm CDT

Inactive Policy: Manual

Original Inactive Date: Mar 30, 2021

Initiative: None

Classification

Original Set Aside:

Product Service Code: 2840 - GAS TURBINES AND JET ENGINES, AIRCRAFT, PRIME MOVING; AND COMPONENTS

NAICS Code: 336412 - Aircraft Engine and Engine Parts Manufacturing

Place of Performance: USA

Description

LENGTH ( IN )

3.0000

WIDTH ( IN )

3.5000

HEIGHT ( IN )

3.0000

WEIGHT ( OZ )

0.7000

ITEM MATERIAL

AMS 5388 NICKEL ALLOY OVERALL

ITEM FUNCTION

DIRECTS AIRFLOW TO TURBINE SECTION TO PRODUCE ENGINE THRUST

LEGACY ITEM DESCRIPTION

VANE IS A PRECISION CASTING WITH A CONTOURED IMPACT SURFACE & ANGLED TRAILING EDGE TO CONTROL EFFECTIVE AREA IN THE TOTAL NOZZLE WITHIN AN OUTER SHROUD. TF33P7/100