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Gas Turbine Handbook : Principles and Practices

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Detectable Problems 191<br />

Figure 12-3. Dual spool gas turbine estimated parameter changes<br />

with low pressure-turbine nozzle area change.<br />

Corrective Action<br />

Geometry changes resulting from oxidation, corrosion, erosion,<br />

or impact damage can be corrected only during overhaul by removal<br />

<strong>and</strong> replacement of the damaged parts. Depending on the type of<br />

machine this could result in downtime of one day (aero-derivatives) to<br />

several weeks (heavy frame units) 4 . However, certain actions can be<br />

taken to maximize the time between overhaul <strong>and</strong> to minimize fired

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