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A system and method of removing a predetermined amount of material from a bottom portion of a dovetail slot in a gas turbine engine disk, including the steps of configuring a designated flow path through the dovetail slot and providing a flow of abrasive media through the flow path a designated numb

A system and method of removing a predetermined amount of material from a bottom portion of a dovetail slot in a gas turbine engine disk, including the steps of configuring a designated flow path through the dovetail slot and providing a flow of abrasive media through the flow path a designated number of cycles so that a substantially uniform amount of material is removed from the dovetail slot bottom portion. The method also includes the step of sealing a pressure surface of the dovetail slot to prevent the abrasive media from flowing thereagainst.

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1. A method of removing a predetermined amount of material from a bottom portion of a dovetail slot in a gas turbine engine disk, comprising the following steps:(a) configuring a designated flow path through said dovetail slot; and,(b) providing a flow of abrasive media through said flow path a desi

1. A method of removing a predetermined amount of material from a bottom portion of a dovetail slot in a gas turbine engine disk, comprising the following steps:(a) configuring a designated flow path through said dovetail slot; and,(b) providing a flow of abrasive media through said flow path a designated number of cycles so that a substantially uniform amount of material is removed from said dovetail slot bottom portion. 2. The method of claim 1, further comprising the step of sealing a pressure surface of said dovetail slot to prevent said abrasive media from flowing thereagainst. 3. The method of claim 1, further comprising the step of inserting a pin member into said dovetail slot so as to form areas of reduced cross-section in said flow path. 4. The method of claim 3, wherein said pin member is retained in a pressure face of said dovetail slot. 5. The method of claim 3, further comprising the step of maintaining a minimum gap between a bottom surface of said pin member and a surface of said dovetail slot bottom portion. 6. The method of claim 1, further comprising the step of maintaining a minimum cross-section in said flow path. 7. The method of claim 1, further comprising the step of measuring a depth for said dovetail slot bottom portion prior to providing said abrasive media through said flow path. 8. The method of claim 7, further comprising the step of measuring a depth for said dovetail slot bottom portion after providing said abrasive media through said flow path. 9. The method of claim 1, further comprising the step of determining said designated number of cycles required in order for said predetermined amount of material to be removed from said dovetail slot bottom portion. 10. The method of claim 1, further comprising the step of confirming that at least said predetermined amount of material is removed from said dovetail slot bottom portion. 11. The method of claim 1, further comprising the step of shot peening said dovetail slot bottom portion after said predetermined amount of material is removed therefrom. 12. The method of claim 1, wherein said flow path has a variable cross-section along a longitudinal axis through said dovetail slot. 13. The method of claim 1, wherein said flow path has a variable cross-section in a direction substantially perpendicular to a longitudinal axis through said dovetail slot. 14. The method of claim 1, wherein said predetermined amount of material removed from said dovetail slot bottom portion is at least approximately 2 mils. 15. The method of claim 1, wherein said predetermined amount of material is removed from a targeted area in said dovetail slot bottom portion. 16. An apparatus for removing a predetermined amount of material from a bottom surface of a dovetail slot in a gas turbine engine disk, wherein a longitudinal axis extends through said dovetail slot, comprising:(a) a fixture for providing a flow of abrasive media back and forth through a designated path at a predetermined pressure and flow rate;(b) a cradle for retaining said gas turbine engine disk in position so that said dovetail slot is in flow communication with said designated path; and,(c) a device for defining a designated flow path through said dovetail slot for said abrasive media;wherein said flow of abrasive media removes a substantially uniform amount of material from a bottom surface of said dovetail slot. 17. The apparatus of claim 16, wherein said apparatus seals a pressure face of said dovetail slot from said flow of abrasive media. 18. The apparatus of claim 16, wherein said abrasive media flows through said flow path of said dovetail slot for a designated number of cycles. 19. The apparatus of claim 16, wherein said predetermined amount of material removed from said dovetail slot bottom surface by said abrasive media is at least approximately 2 mils. 20. The apparatus of claim 16, wherein said apparatus provides a minimum cross-section through said designated flow path of said dovetail slot. 21. The apparatus of claim 16, wherein said apparatus provides said designated flow path through said dovetail slot with a variable cross-section along said longitudinal axis of said dovetail slot. 22. The apparatus of claim 16, wherein said apparatus provides said designated flow path through said dovetail slot with a variable cross-section in a direction substantially perpendicular to said longitudinal axis of said dovetail slot. 23. The apparatus of claim 16, wherein designated flow paths through each of said dovetail slots in said disk are in flow communication with said designated path of said abrasive flow fixture so that abrasive media flows therethrough substantially simultaneously.