The objective of this task is to perform a technical assessment of turbine blading for advanced second generation PFBC conditions, identify specific problems/issues, and recommend an approach for solving any problems identified. A literature search was conducted, problems associated with hot corrosion defined and limited experiments performed. (1) The conditions that favor sulfidation corrosion are present in PFBC turbines. Sulfidation corrosion occurs in industrial, marine and aircraft gas turbine engines and is due to the presence of condensed alkali (sodium) sulfates. The principle source of the alkali in industrial, marine and aircraft gas turbine engines is sea salt crystals. The principle source of the sulfur is not the liquid fuels, but the same ocean born crystals. Moreover deposition of the corrosive salt occurs primarily by a non-equilibrium process. Sodium will be present in the cleaned combusted gases that enter the PFBC turbine. Although equilibrium condensation is not favored, deposition via impaction is probable. (2) Accelerated oxidation associated with the presence of chlorine or chlorides is not anticipated. Marine gas turbines operate in sodium chloride rich environments without experiencing the accelerated attack noted in coal fired boilers where condensed chlorides contact metallic surfaces. Gaseous mixtures of sodium chloride and air are reported to mitigate sufidation corrosion. (3) Calcium sulfate can be an aoaressive corrodent, The sulfates of calcium and magnesium are the products of the reactions used to control sulfur. Based upon industrial gas turbine experience and laboratory tests, calcium and magnesium sulfates are, at temperatures up to 1500°F (815°C), relatively innocuous salts. In this study it is found that at 1650°F (900°C) and above, calcium sulfate becomes an aggressive corrodent. (4) The ternary sulfates of calcium, magnesium and sodium are very aggressive corrodents. Calcia and magnesia are used to capture the oxides _,I sulfur. The presence of sodium and the formation of sulfates can lead to the formation of corrosive salts which will attack turbine components. (5) The anticipated materials for advanced DOE engines are the high temperature single crystal alloys used in advanced aircraft gas turbines. A noteworthy observation is that th6 single crystal alloy appears to be more resistant to the combined calcium-magnesium-sodium sulfate corrosion that the industrial alloys developed to resist sulfidation corrosion. The resistance of the current families of coatinas with respect to the mixed sulfate corrodentis not v known, (6) Engine manufacturers establish parameters that relate turbine ai,"foil life with laboratory data. The data when used to rank materials is generally in agreement. However, the deposition of the corrosive salt is a non-controllable variable which differs from machine to machine. Therefore improvements in life associated with material selection by one manufacturer need not translate to another manufacturer. Improvements in life are related to the understa...