Inactive

The Government is conducting market research to identify potential sources that possess the expertise, capabilities, and experience to meet the requirements for the remanufacture readiness effort for ... The Government is conducting market research to identify potential sources that possess the expertise, capabilities, and experience to meet the requirements for the remanufacture readiness effort for the EAC, part number 2117580-2-1 and NSN 1420-01-098-5936GF. The Flight Control Servo Assembly (FCSA) consists of two identical linear actuators, driven by a common electronic control unit, the Elevon Actuator Controller (EAC). The controller consists of circuits to perform actuator position signal summing, error signal amplification, servo loop compensation, and power drive stages for the servo motors, current limiting, and buffer circuits to output position, motor current monitor signals and motor voltage monitor signals. The EAC accepts analog voltage inputs proportional to the elevon position command, 28 VDC power, and +- 15 VDC power. The 28 vdc and +- 15 dc grounds are isolated outside of the servo assembly. The FCSA controls the elevon which guides the missile to its intended target. The purpose of this remanufacture readiness effort is to prove that a remanufactured EAC meets the original design requirements and all nuclear hardness requirements in preparation for a full rate production effort of the remanufactured EACs. The contractor shall be capable of producing a number of remanufactured EACs for prototyping purposes with the work to include disassembly, cleaning, inspection, assembly, testing, troubleshooting, and root-cause failure analysis to return an unserviceable EAC to a serviceable or like-new condition. The contractor shall be capable of furnishing all labor, materials, facilities, and equipment required to accomplish the remanufacture and all required testing to include functional testing and product reliability verification testing (PRVT). Additionally, the contractor may be responsible for supply chain management, logistics planning, long-lead time parts procurement, diminishing manufacturing sources, and material shortage issues. At this time, the Government does not possess a complete technical data package for the EAC. Throughout this effort, the contractor will be responsible for refining the remanufacturing procedures and test procedures as well as finalizing and updating all EAC drawings to reflect the new configuration of the remanufactured EAC to produce the complete technical data package at the conclusion of this effort. Furthermore, in updating the EAC drawings, there may be a need to re-derive and update the requirements as the drawings were originally developed in the 1980s.