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Date:  1-31-2009
Number of Hours:  1.50
Manual Reference:  
Brief Description:  Optional aft fuselage belly stiffeners

Optional aft fuselage belly stiffeners

Fabricated formed angle stiffeners for the last and second last compartment belly skins. These prevent 'oil canning' of the aft floor areas and reduce noise during taxi.

I fluted the formed 0.032" angle to remove slight bows (or the 0.025" skin would take on the bow). I then turned the fuselage over to locate the end holes, deburred, dimpled and primed. The other holes need to be drilled from the inside (or they wouldn't line up).
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Positioning the stiffeners

Positioning the stiffeners

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