Removed rigging hardware from main wing spars through the three center holes in the spar webs. Slid RH wing out slightly for better access to fuselage side. Located wing root electrical connector and cut out hole for pass through. Drilled mounting holes then used 8-32 screws to attach bulkhead connector to fuselage side. Measured out pitot and AOA tube bulkhead connectors and drilled mounting holes. Trimmed pitot and AOA tubes then tested fit by sliding wing into position; fit checked good. Reversed wing attach pins then slid out LH wing and repeated the process for the smaller LH wing electrical bulkhead connector. Checked fitment the reinstalled wings. Verified proper clearance of connections in both wings with borescope.
Hours Worked: 3.27
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