| Date: |
2-13-2005 |
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| Number of Hours: |
5.00 |
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| Brief Description: |
Rudder Inspection Corrections |
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Drilled out rivets holding .040 doublers to spar. Removed doublers and corrected bend angle in doubler to more closely match angle in rudder spar. Re-revited doubler to spar. Riveted rear and leading edge skins to rudder skeleton. Left bottom 10% of skin unriveted per plans for access for final fit of rudder bearings for installation on fuselage. |
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