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Date:  3-5-2008
Number of Hours:  7.00
Manual Reference:  
Brief Description:  V stab details

Layed up 1 bid carbon along v stab to fuselage joint, ahead of the h stab and behind h stab.
Layed up 3 bid carbon between left v stab skin and h stab.
Sanded glass on v stab leading edge.
Applied micro over v stab leading edge.
Applied superfil to rudder right skin.
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