Wings & Fins Subassemblies

This notice serves as a formal SOLICITATION for the procurement of Wing and Fin Sub-Assemblies. These critical sub-components are required to support the AIM-120X and CATM-120X series of the Advanced Medium Range Air-to-Air Missile (AMRAAM).

The Government intends to award a single contract for the scope of work identified within the Attachment 2 Statement of Work (SOW) as a result of this solicitation.

2. Source Selection Procedures

This acquisition will utilize the Lowest Price, Technically Acceptable (LPTA) source selection procedure in accordance with:

• FAR 15.103-2
• DoD Source Selection Procedures referenced in DFARS 215.200 and DFARS PGI 215.200

These procedures will be used to make an integrated assessment for a best value award decision. Please refer to sections L and M of the solicitation for additional information.

3. Evaluation and Award Criteria

The Government shall evaluate proposals in accordance with the provisions outlined in this notice. A detailed and complete analysis of each offeror's proposal will be performed.

Key Evaluation Parameters:

• Proposal Limit: The Government will only evaluate one proposal from each offeror.
• Award Basis: Award will be made to the responsible offeror whose proposal:
  1. Is determined to be technically acceptable.
  2. Conforms to all solicitation requirements (terms and conditions, representations, certifications, and technical requirements).
  3. Has the lowest Total Evaluated Price among the technically acceptable offerors.
• Evaluation Sequence: The Government does not imply, nor is it the Government's intention, to conduct the evaluations in sequential order (i.e., technical evaluation does not necessarily have to precede price evaluation).

4. Technical Evaluation Factors

The Government's technical evaluation will be based on the following four equally important subfactors:

Subfactor

Description

Subfactor One

Wing and Fin Packaging, Handling, Shipping and Transportation Solution

Subfactor Two

Wing and Fin Production Plan

Subfactor Three

Finished/In Process Product Verification Plan

Subfactor Four

Honeycomb Implementation