Gary Christensen - Experimental Aircraft Builder's Log

RV-6A - GBC


Date: 10-1-2011
Number of Hours: 0.00
Manual Reference:
Brief Description: Ream nose gear retention hole

Reamed the hole in both the nose gear hole and the engine mount retention bolt hole. Test fit the engine/gear against firewall. Determined that fuselage would need to be raised 3" to be bolted on the firewall, and no need for that now.

Reamed retention - nose gear

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