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Larry Winger's 601XL Project
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Date:  10-15-2006
Number of Hours:  3.50
Manual Reference:  
Brief Description:  Riveted tip ribs and pre-drilled fiberglass tips

Even though the fiberglass tail tips do not get installed until after the stabilizer is installed on the fuselage, I decided to fit and pre-drill them. The installation took more time than I imagined, but it went well. The distance between tips came out to 2205mm, as called for in the plans. Now on to the elevator.
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