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Date:  3-12-2006
Number of Hours:  4.00
Manual Reference:  
Brief Description:  Set angle of incidence

Removed wings, drilled holes in fuselage for aileron pushrod and electrical conduit.
Drilled holes in gearbox for aft spars.
Reinstalled wings.
Measured angle of incidence as follows:
left wing root +0.9 left wing tip +0.5
right wing root +1.0 right wing tip +0.5

Reviewed manual on wing root fairings. Located fairing parts.
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