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Tender Details
- Country: USA
- Summary: CH-53K Hybrid Inlet Particle Separator (IPS) Development
- UST Ref No: 118953589
- Deadline: 19 May 2025
- Competition: ICB
- Financier: Self Financed
- Purchaser Ownership: Public
- Tender Value: Refer Document
- Notice Type: Tender
- Document Ref. No.: N00019-25-RFPREQ-APM261-0204
- Purchaser's Detail :
- Description :
- Description
Disclaimer
THIS SOURCES SOUGHT IS FOR INFORMATIONAL PURPOSES ONLY. THIS IS NOT A REQUEST FOR PROPOSAL. IT DOES NOT CONSTITUTE A SOLICITATION AND SHALL NOT BE CONSTRUED AS A COMMITMENT BY THE GOVERNMENT. RESPONSES IN ANY FORM ARE NOT OFFERS AND THE GOVERNMENT IS UNDER NO OBLIGATION TO AWARD A CONTRACT AS A RESULT OF THIS ANNOUNCEMENT. NO FUNDS ARE AVAILABLE TO PAY FOR PREPARATION OF RESPONSES TO THIS ANNOUNCEMENT. ANY INFORMATION SUBMITTED BY RESPONDENTS TO THIS TECHNICAL DESCRIPTION IS STRICTLY VOLUNTARY.
Introduction
The Naval Air Systems Command (NAVAIR), Program Executive Office (PEO) Assault (A), H-53 Joint Program Office (PMA-261) announces its intention to award a contract for development and integration of an improved engine inlet system to increase particle separation efficiency and improve engine Time-On-Wing (TOW), particularly in austere/desert environments on CH-53K aircraft.
THIS SOURCES SOUGHT IS NOT A REQUEST FOR PROPOSAL. It is a market research tool being used to determine potential and eligible businesses capable of providing the services described herein prior to determining the method of acquisition and issuance of a Request for Proposal. The Government is not obligated to and will not pay for any information received from potential sources as a result of this notice.
Background
As the CH-53K operational testing in austere/desert environments has progressed, there have been impacts to the reliability and maintainability of the aircraft precipitating the need for a new engine inlet system to limit the amount of dust and sand ingested. The CH-53K engine inlet system must function both as a combined inlet and particle separator. The engine inlet system must provide clean airflow compatible with the CH-53K engine requirements for operability and performance throughout the flight envelope. The CH-53K engine inlet system must be safe, reliable, cost effective, and sustainable, and ensure maximum utiliz... - Documents :
Purchaser : DEPT OF DEFENSE | DEPT OF THE NAVY
NAVAL AIR SYSTEMS CMD HEADQUARTERS NAVAL AIR STATION, PATUXENT RIVER , MD 20670-5000, USA
Primary Point of Contact: Bryson Shibe, bryson.j.shibe2.civ@us.navy.mil
Secondary Point of Contact: Christopher J Harritt, christopher.j.harritt.civ@us....
Email :bryson.j.shibe2.civ@us.navy.mil
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