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Date:  12-13-2006
Number of Hours:  2.00
Manual Reference:  
Brief Description:  Final attachment/installation of VS...

...Filed stell weldments where they were striking the aft bulkhead prior to horn hitting up elevator stop. Drilled and forth hole for AN3-5A to attach tail tie-down/aft VS spar to fuselage. Reinstalled elevator pushrod after priming.
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Rudder needs 15 hours drying

Rudder needs 15 hours drying

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