6930-01-051-3542
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A rigid item designed to maintain a predetermined space between two vane, fan, aircraft gas turbine engine in a vane assembly or vane segment, fan, aircraft gas turbine engine. They also maintain the proper angle of the vane for proper air passage. They may be positioned at the outer or inner edge of the vane.
6930-01-051-3542, no name available
FAQs
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