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A method and apparatus are provided for inspecting a coated substrate such as a multi-layer coating on a substrate of a turbine airfoil. At each of a number of locations along the airfoil a number of frequencies of alternating current are passed through the airfoil. At least one impedance parameter

A method and apparatus are provided for inspecting a coated substrate such as a multi-layer coating on a substrate of a turbine airfoil. At each of a number of locations along the airfoil a number of frequencies of alternating current are passed through the airfoil. At least one impedance parameter is measured. The measured impedance parameters are utilized to determine a condition of the coating.

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1. A method for inspecting a muli-layer coating on a substrate of a turbine element airfoil comprising:for each of a plurality of locations along the airfoil: for each of a plurality of frequencies of alternating current: passing said current through the airfoil; and measuring at least one impedance

1. A method for inspecting a muli-layer coating on a substrate of a turbine element airfoil comprising:for each of a plurality of locations along the airfoil: for each of a plurality of frequencies of alternating current: passing said current through the airfoil; and measuring at least one impedance parameter; and determining a condition of the coating; wherein said current is passed between first and second electrodes, and wherein an ionically conductive liquid is applied at contact points of the first and second electrodes with the coating. 2. The method of claim 1 wherein said determining comprises determining a thickness of at least one layer of the coating.3. The method of claim 1 wherein said determining comprises identifying a void within the coating or between the substrate and the coating.4. The method of claim 1 performed while the turbine element is installed on a turbomachine.5. The method of claim 4 performed seriatim on a plurality of turbine elements on said turbomachine.6. The method of claim 1 performed while the turbine element is installed on a gas turbine engine.7. The method of claim 1 wherein for each said location the current is passed between a first electrode uniquely positioned relative to said location and a second electrode commonly positioned.8. The method of claim 1 wherein for each said location the current is passed between a first electrode uniquely positioned relative to said location and a second electrode uniquely positioned.9. The method of claim 1 further comprising:approving or rejecting the turbine element. 10. The method of claim 1 further comprising:determining a remaining useful life of the turbine element. 11. A method for inspecting a coated item comprising:electrically coupling first and second electrodes of a test apparatus to the item; passing an alternating current between the electrodes, the current passing through at least: a ceramic layer; a metallic substrate; a bondcoat layer between the ceramic layer and the metallic substrate; and an additional layer between the bondcoat layer and the ceramic layer; and measuring an impedance parameter. wherein said electrically coupling comprises applying ionically conductive liquid at contact location betweenthe first and second electrodes and thecoated item. 12. The method of claim 11 wherein said liquid is applied prior to contacting the item with the electrodes.13. The method of claim 11 further comprising:responsive to said impedance parameter, approving or rejecting the item. 14. A method for inspecting a coated item, the item comprising:a ceramic layer; a metallic substrate; a bondcoat layer between the ceramic layer and the metallic substrate; and an additional layer between the bondcoat layer and the ceramic layer, the method comprising: a step for electrically coupling a test apparatus to the item via two electrode, each using an ionically conductive liquid; and a step for obtaining an impedance spectrum characteristic for a location on the item. 15. The method of claim 14 wherein the method further comprises a step for identifying a physical characteristic of the item related to the impedance spectrum characteristic.16. The method of claim 15 wherein said physical characteristic comprises a thickness of at least one of the bondcoat layer, the additional layer, and the ceramic layer.17. The method of claim 15 wherein said physical characteristic comprises a size characteristic of a void.18. The method of claim 15 wherein said physical characteristic comprises a size characteristic of a void between an adjacent two of the substrate, the bondcoat layer, the additional layer, and the ceramic layer.19. A method for inspecting a coated item, the item comprising:a ceramic layer; a metallic substrate; a bondcoat layer between the ceramic layer and the metallic substrate; and an additional layer between the bondcoat layer and the ceramic layer, the method comprising: a step for electrically coupling a test apparatus to the item; and a step for obtaining an impedance spectrum characteristic for a location on the item; and a step for identifying a physical characteristic of the item related to the impedance spectrum characteristic, said physical characteristic comprising a size characteristic of a void between an adjacent two of the substrate, the bondcoat layer, the additional layer and; the ceramic layer. 20. A method for inspecting a multi-layer coating on a substrate of a turbine element airfoil comprising:for each of a plurality of locations along the airfoil: for each of a plurality of frequencies of alternating current: passing said current through the airfoil; and measuring at least one impedance parameter; and determining a condition of the coating, including identifying a physical characteristic of the airfoil related to the impedance parameter, said physical characteristic comprising a size characteristic of a void between an adjacent two of the substrate, a ceramic layer, a bondcoat layer between the substrate and the ceramic layer, and an additional layer between the bondcoat layer and the ceramic layer.