Franklin Gaxiola - Experimental Aircraft Builder's Log

GA Aerospace’s Web Site


Date: 12-13-2019
Number of Hours: 8.30
Manual Reference:
Brief Description: 46iS-05

12/10/19 1. force was applied upwards to be able to make contact between the WD-1201 and the background of the firewal. 2. The WD-1201a was temporarily secured the background of the firewall as shown in Figure 1. 3. The hole on the left side was used as a guide to do final drill on the fuselage. 4. Temporarily the WD-1201 was secured to the firewall fiondo and the bold and nut on the right side was removed. 12/13/19 5. Step 3 was repeated to do the same on the right side. 6.The WD-1201 was removed and the holes deburred. 7.The WD-1201 was reisntalo and the two bolds were inserted as was done in step 4. 8.The engine was raised using the suspension points on the left and right side. 9. First the two bolds of the lower part of the WD-1201 were installed and then the two above installed.

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