Raymond Sievers - Experimental Aircraft Builder's Log

Raymonds Web Site


Date: 3-24-2010
Number of Hours: 10.00
Manual Reference: DRAWING 37
Brief Description: Manual section 8 page 15

Mounted bracket and phenolic bushing over fuel line penetration point thru firewall. Begun running fittings and hardware for permanent rudder pedal installation. Installed LH tank attach bracket permanently to fuselage.

Firewall Penetration

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