| Date: |
9-22-2020 |
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| Number of Hours: |
2.10 |
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| Brief Description: |
Service Letter SL-00014 |
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Installed two F-00773A stiffeners to the interior of the tailcone skin, directly below the access panel under the horizontal stabilizer, one on each side of the airplane, per Vans Service Letter SL-00014. Deburred stiffener edges and holes, and scuffed, cleaned, and primed the faying surface. The interior of the F-773 aft side skins had already been primed. Rivets Today: 10 |
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