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Date:  6-14-2004
Number of Hours:  4.00
Manual Reference:  DWG 34A
Brief Description:  Test fit landing gear mount to fuselage.

Test fit and adjust socket holes for landing gear mount. The flange of the geat leg mount along the upper edge of the spar does not lay flat against the spar. Took a long time to diagnose the problem. Talked to Van's several times. Bruce suggested to just pull the 1/16 gap in with the bolts. Will use clamps when drilling the fuselage side skin to the gear leg mount.
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