Date:	12-18-2012
Number of Hours:	4.00
Brief Description:	SB 12-11-09
SB 12-11-09 Step 29: Vacuumed the rivet tails and drill shavings from the interior of the fuselage. Step 30: Tapped the Spar Pin Bushings in the Center Section foreward slightly to provide access to the fwd most rivets on the F-1204U-B and F-1204T-2 Angles. Riveted the angles to the Center Section using CR 3213-4-5 rivets. Then tapped the Spar Pin Bushings back in place.