MIL-STD-1530C(USAF)
5.1.5.1 Corrosion Prevention and Control Plan.
A Corrosion Prevention and Control Plan shall be prepared and corrosion prevention and control processes shall be used in accordance with this standard, MIL-HDBK-1568, and JSSG-2006. The plan shall be consistent with the design service life and shall define corrosion prevention and control requirements and considerations for the System Development & Demonstration and Production & Deployment phases. The plan shall specify actions to delay the onset of corrosion and minimize
corrosion maintenance costs through the selection of materials, fabrication techniques, sealants, protective coatings, design features, and other measures that minimize the potential for corrosion throughout the structure.
5.1.5.2 Evaluation of corrosion susceptibility.
An evaluation of the susceptibility of the aircraft structure to corrosion shall be conducted as part of the CPCP. The evaluation shall identify locations where the structure might be susceptible to corrosion and the expected type(s) of corrosion (e.g., exfoliation, uniform, crevice, intergranular, and stress-corrosion cracking, etc.) that could occur at these locations. To identify potential corrosion damage locations, the evaluation shall account for the materials, manufacturing processes, corrosion prevention systems (e.g., coatings, sealants, etc.), preventative maintenance approaches (e.g., hangaring, wash cycles, wash fluids, etc.), the inspectability of the location, and structural fabrication techniques as well as the expected operational environments to which the aircraft are subjected.
5.1.6 Nondestructive Inspection (NDI) Program.
An NDI Program shall be established in accordance with MIL-HDBK-6870 and consistent with direction in AFI 21-105. The NDI Program will consider and implement appropriate nondestructive inspection processes into all phases of the program (design, engineering development, production, and in-service operation). The program shall establish a Nondestructive Inspection Requirements Review Board (NDIRRB) responsible for oversight and execution the program. The NDIRRB shall be formed early in the design phase to review and assess product form concepts for inspectability in terms of production process control and quality monitoring. The NDIRRB shall also be responsible for review and approval of inspection methods and detectability assumptions implemented in the Force Structural Maintenance Plan. The board's decisions are subject to USAF approval.
5.1.7 Selection of materials, processes, joining methods, and structural concepts.
Materials, processes, joining methods, and structural concepts shall be selected to result in a structurally efficient, cost-effective aircraft structure that meets the strength, rigidity, observability, durability, and damage tolerance requirements of the applicable specifications. Prior to a commitment to new materials, processes, joining methods, and/or structural concepts (i.e., those not previously used in the military and/or commercial aviation industry), an evaluation based on their stability, producibility, inspectability, supportability, and mechanical and physical properties shall be performed. The risk associated with the selection of the new materials, processes, joining methods and/or structural concepts shall be estimated and risk mitigation actions defined. The trade studies performed as part of the durability and damage tolerance control described in 5.1.4 shall be a major driver in the final selection of materials, processes, joining methods, and structural concepts. The detailed rationale for the individual selections and any proposed risk mitigation actions shall be submitted in the proposals of prospective contractors. Each rationale and all supporting data shall become part of the design database after contract award and during the design of the aircraft.
16
For Parts Inquires submit RFQ to Parts Hangar, Inc.
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business