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  4. ›MH-139 Rotor Brake

U.S. Department Of Defense·Ohio

MH-139 Rotor Brake

Closes 7/24/2026$5M – $20MRequest for Information
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Description

The U.S. Air Force is conducting market research to identify sources capable of designing, integrating, and testing a rotor brake for the MH-139A. The objective of this effort is to integrate a rotor brake system on the MH-139A to support safe and efficient ground operations, particularly in high-wind environments. The addition of a rotor brake capability will optimize ground turn-around times, facilitate rapid refueling operations, reduce rotor system wear, and enhance overall ground safety for aircrew and support personnel. Key requirements for the modified system include procurement and installation, standardization, systems and software integration, airworthiness and structural integrity, support and fit-testing, certification and airworthiness pathway, and certification experience. Respondents are encouraged to provide comprehensive responses that demonstrate existing technology, qualifications, and experience. The response should include company information, technical capability, cost and schedule, and small business utilization.

Attached files

The solicitation documents live at the source — open the bid source above to download them.

Contact

Jeremy Perry

[email protected]

Key dates

Opened
6/25/2026
Closes
7/24/2026

Last updated

Details

Type
Request for Information
Industry
Aerospace and Defense
NAICS
336413
Solicitation №
MH139-CR05

Budget estimate

$5,000,000 – $20,000,000

The budget for this project can be estimated based on the scope of work, which includes designing, integrating, and testing a rotor brake for the MH-139A aircraft. The cost of the project may include non-recurring engineering costs, modification kit and installation costs, and testing and certification costs. Assuming the project requires significant design and testing efforts, the total cost may range from $5 million to $20 million. The factors that may influence the likely payment range include the complexity of the design, the number of aircraft to be modified, and the testing and certification requirements.

AI estimate from the solicitation

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