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Aviation Partners, LLC Project
RV-10
Fuselage
2-6-2011
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Date:
2-6-2011
Number of Hours:
7.00
Manual Reference:
Section 40
Brief Description:
Began flap system assembly
Began Section 40, Flap System. Completed all of the match drilling and priming of assemblies prior to installation. Specifically Section 40-2, Steps 1-6, Section 40-3, Step 1, and 40-4 Steps 1-4.
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69
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159
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67
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157
1972
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3
41
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22
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17
398
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1
140
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40
235
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