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Date:  6-29-2012
Number of Hours:  2.00
Manual Reference:  Page 7-48
Brief Description:  Powerplant Break In Procedure

Engine break in procedure followed exactly. After procedure the exhaust manifold (header) bolts were re torqued to 210 in/lbs. Propeller bolts re torqued (1/4" to 120 in/lbs) (5/16" to 175 in/lbs).
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