KC135 APU Repair

Closed Pre-Solicitation Posted

Solicitation number
MM08152024
Agency
Responses due
Set-aside
No set-aside

Opportunity facts

Place of performance
Hill AFB, Utah 84056, United States

Notice details come from SAM.gov. Updated .

About this opportunity

The Department of the Air Force Materiel Command Air Force Sustainment Center is seeking information and potential sources for the repair of the KC-135 Auxiliary Power Unit (APU), a critical component within the KC-135 aircraft's Secondary Power and Engine Start System. This is not a solicitation, but rather a Sources Sought Announcement to gather information for future acquisition planning purposes. A Repair Qualification Requirement (RQR) is attached, which details the process for vendors to become qualified approved sources for the APU repair work. The RQR outlines the key qualification requirements, including demonstrating repair capabilities, testing and verification, and providing a qualification article within a 180-day timeframe and $6,000 cost estimate. Potential sources may also apply for a qualification waiver if they meet certain criteria.

This opportunity is not set-aside and does not currently have any identified incumbent contractors. The NAICS code is 336413 - Other Aircraft Parts and Auxiliary Equipment Manufacturing, and the PSC code is 2835-P - Gas Turbines And Jet Engines; Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, And Components. The sources sought announcement is posted on August 15, 2024, with responses due by September 16, 2024.

Notice text

This is not a solicitation but rather a Sources Sought Announcement to determine potential sources for information and planning purposes only.  A Repair Qualification Requirement (RQR) is also attached to this notice, detailing the process to become a qualified approved source or if applicable, submit a source qualification waiver.

The KC-135 Auxiliary Power Unit (APU) is a major /end item component within the KC-135 aircraft Secondary Power and Engine Start System. It is a small gas turbine engine that is used to start the main (propulsion) aircraft engines. The APU provides compressed air and generates electrical power for starting aircraft main engines and running aircraft systems. The APU consists of three major assemblies: turbine assembly, reduction drive unit, and combustor assembly.

Files

File Type Posted
RDL_KC 135 APU.pdf PDF
KC-135 APU Repair Qualification Requirements (RQR) signed.pdf PDF

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