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CH701
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1-11-2010
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Date:
1-11-2010
Number of Hours:
2.00
Manual Reference:
N/A
Brief Description:
Fuselage Stiffeners
I decided to install "L" angles on the inside fuselage skins to avoid the "oil-canning" that is described by the other builders. Took a little work to align the angles and holes.
Layout holes
Drill
Reverse and rivet.
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247
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28
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25
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22
51
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24
70
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7
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37
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51
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20
54
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7
19
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22
51
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70
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23
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70
Prop
1
3
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7
19
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10
28
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19
61
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