Mark Byrne - Experimental Aircraft Builder's Log

DAVID'S WEB SITE


Date: 5-16-2015
Number of Hours: 2.00
Manual Reference: 5.2.O
Brief Description: WING FUEL VENT

INSTALL WING FUEL VENT INTO THE WING TIP THROUGH THE ACCESS PANEL. CONNECT THE CHECK VALVE TO THE FUEL TANK (545) WITH FLOW LINE TOWARDS THE TANK. CONNECT T FITTING (AN824-6D) TO THE CHECK VALVE. TUBING 5052-.375/.035 AS REQUIRED. FOR CORRECT ALIGNMENT. NUT COUPLING (AN818-6D AND SLEEVE (AN819-6D) AS REQUIRED FOR CORRECT ALIGNMENT

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