Franklin Gaxiola - Experimental Aircraft Builder's Log

GA Aerospace’s Web Site


Date: 12-13-2018
Number of Hours: 18.80
Manual Reference:
Brief Description: 37iS/U-19, 37iS/U-20, 50iS/U-05, 50iS/U-07

37iS/U-19: 4: NA 5: Most of this was making sure there were no fiberglass spikes along the edges. 6: This had already been done on page 37iS/U-15, on this step we rounded a bit the corners no minimize stress. 7: NA 8: NA 9: NA 10: NA 11: NA 37iS/U-20: 1: NA 2: NA 3: NA 50iS/U-05: 10: This might have been a lot easier if the orange heat-shield wouldn't have been there. 11: It was torqued to 18.44 ft/lb 12: NA 13: NA 14: NA 15: NA 50iS/U-07: 2: NA 3: We would recommend doing the bends of step 7 before cutting at the specified length 4: We would recommend doing the bends of step 7 before beveling the end of the tube. 5: NA



Preformed radiator hose re-attached to the engine.

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