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Craigs RV-8 Web Site
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Date:  11-13-2010
Number of Hours:  3.00
Manual Reference:  8s8-1r1 12/02/08
Brief Description:  Preparing fuselage parts for final assembly

Page 8-31

Machine countersunk #30 for dimples the 1/8 holes on the side web of the F887-L1 abd R-1 upper longerons that are common with the WD-802- L 1 and R-1 upper engine mount brackets and #30 dimple countersunk holes in the F-820-L-1 and R-1 fwd side skins.
Deburred all match drilled and final drilled holes in all loose fuselage substructure parts
Deburred all holes in all fuselage skins
Trimmed the index tabs from the bottom of the F-820 L-1 and R-1 fwd side skins
Deburred the holes in the fwd and aft bottom flanges of the center section bulkhead assembly
Deburred the #30 holes in the F-814 E-L 1 and R-1 Seat ramp supports
Deburred the rivet holes at the fwd and aft ends of the F-826-1 and F-827-1 mid bottom skins
Deburred all open rivet holes on the fwd fuselage substructure
Dimple countersunk the #40 holes in the firewall assembly side flanges
Dimple countersunk the 4 #40 holes at the center aft end of the F-822-1 fwd floor panel located between the center section
Dimple countersink the 5 #30 holes on each side of the F-822-1 fwd floor panel
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dimpling the firewall flange

dimpling the firewall flange

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Dimpling the 5 holes with a hand dimpler to be able to reach them

Dimpling the 5 holes with a hand dimpler to be able to reach them

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Trimming the tabs

Trimming the tabs

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