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Flandy Rv-10
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Date:  7-11-2014
Number of Hours:  6.00
Manual Reference:  44
Brief Description:  Wing install cont.--wiring, flaps

Torqued all main wing bolts and checked with two different units

NAS 1309-58 bolts--960in/lbs
NAS 1306-58 bolts- 180in/lbs
AN6-11 rear spar - 175in/lbs with cotter key.

Threaded all cabin wires out to final location in each wing and threaded all pre-installed wing wires into cabin to be routed to final destination later.


Installed both flaps and rough filed inboard edge to allow clearance with fuselage- will need to check gap and finish install.
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