Franklin Gaxiola - Experimental Aircraft Builder's Log

GA Aerospace’s Web Site


Date: 12-14-2018
Number of Hours: 18.80
Manual Reference:
Brief Description: 50iS/U-07, 50iS/U-08, 50iS/U-10, 50iS/U-11

50iS/U-07: 6: NA 7: A template that can be found on 50iS/U-14 was made to replicate this bend. 8: Torque for both was of 18.44ft/lbs 9: Does not apply for this aircraft. 10: NA NOTE: Torque for all of the screws that go to the cushion clamps was of 25in/lbs. The one that clamps FF-00022 has not been torqued as specified. 50iS/U-08: 1: NA 2: Instead of drilling on the center of the cap Van's confirmed that a pilot hole that had been drilled into it had to be used for this. 3: NA 4: NA 5: NA 6: NA 7: NA 8: NA 9: NA 10: NA 11: NA 50iS/U-10: 1: NA 2: NA 3: NA 4: NA 50iS/U-11: 1: NA

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