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RV-12iS B
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10-4-2018
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Date:
10-4-2018
Number of Hours:
4.50
Manual Reference:
Brief Description:
23iS/U-06
1. The wing spar penetration holes were cut out.
2. A large hole was drilled.
3. A mark was made on the F-01270-L-1 & -R-1 both sides.
4. The screw was dimpled and then riveted F-01270-L-1 & R-1
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443
3643
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52
188
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55
331
.Finish
96
569
.Fuselage
115
758
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21
92
.PAP
11
1
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39
202
.Service Bulletin
14
15
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24
249
Batteries Log
1
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1
Finish Kit
1
612
None
1
0
Painting process
9
255
PAP
1
Powerplant
2
371
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