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GA Aerospace’s Web Site
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Date: 5-5-2018
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Number of Hours: 16.00
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Manual Reference:
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Brief Description: Page 22iS/U-04
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Today, step 6 22iS / u-04 was finished, in which the parts wd-1204 were riveted. These parts had not been installed because they required some CR3213-4-3 squares, they were able to be placed after that. The area of u8203u8203 wings will lend us theirs and these will be replaced later.
Steps 4, and 5 22iS / U-05 were also carried out, first a light layer was applied between the piece F-01201B-1 and F-01201C-1, the sealant was mixed in a 100: 10 poportion of the components
A: B, both substances were weighed in a digital scale and then mixed homogeneously and finally applied in the aforementioned parts, this process took a little longer because when the sealant was spread, a topechap had to be made to achieve a aesthetic finish.
Finally steps 6, 7, 8, 9 22iS / U-05 were carried out in these steps 2 screws MS24694-C14 were placed pressing them with a torque of 32 Thready Qty Per Inch.
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