DOD - A10 Fatigue Failure Analysis MRAS

The A-10 Fatigue and Failure Analysis (FFA) Program is seeking engineering failure analysis and testing engineering services for the A-10 Aircraft Structural Integrity Program (ASIP). The purpose of this effort is to address fleet deficiencies and unanticipated issues that arise in the aging A-10 fleet. The work includes strain surveys, failure evaluation, materials evaluation, fatigue testing, and component testing. The contractor will collaborate with the A-10 ASIP, Analysis and Structures teams, as well as the Hill Air Force Base (HAFB) maintenance community and materials lab. The period of performance is ongoing, and the place of performance is primarily at the contractor's site.

The A-10 Thunderbolt II aircraft has an average service life of over 12,000 flight hours, exceeding its original design service life. As the aircraft ages, issues related to fatigue, corrosion, and other damage mechanisms arise. The A-10 FFA Program aims to address these issues by providing engineering support on a contingency basis. The contractor will conduct strain surveys on aircraft assemblies/components, evaluate failures and nonconforming parts, perform materials testing and analysis, conduct fatigue testing, and test components as needed.

The government will provide access to relevant documents and equipment for evaluation purposes. The contractor will work closely with government personnel to address fleet issues in a timely manner. Monthly status reports will be submitted to update the government on the progress of each task. Security clearance is not required for this task order, but compliance with applicable DOD security regulations and procedures is necessary. Government furnished equipment, materials, property, and software will be provided as needed.

Overall, this opportunity provides a comprehensive range of engineering services to support the continued operational safety of the A-10 fleet. The contractor will play a critical role in identifying root causes of failures, evaluating nonconforming parts, and conducting necessary testing to ensure the structural integrity of the aircraft.