06/17/19: 3.16Hrs 1: F-12127D was created by cutting a 84 27/32" length of 3/8" aluminum tubing, the 25degree bend was made and that end of the tube was flared with its corresponding hardware. 2: The 88.2degree bend was made. 3: The other 3 bends were made and the snap bushing location was marked on the tube.
02/12/20: 1.25Hrs 4: The fuel line was fed forward through the snap bushings on the fuselage, then the forward end was flared with its hardware installed. 5: F-12127D was attached to the bypass fitting assembly. and the tube's clearance with F-12108A was confirmed 6: F-12127D was secured to F-01207D-L-1 with the called out cushion clamp.
