01/17/20: 1.63Hrs 1: Three F-01276C were final-drilled 5/16 and installed on the fuselage. Steps 2 and 3 were worked on but after routing the tube it was noted that the start bend line was not correct and the tube ended up shorter than needed. These will have to be reworked.
02/12/20: 2.95Hrs 2, 3: F-12127A was created by cutting a 42 1/2" of 3/8" aluminum tubing and one pair of nut and sleeve was installed, then the tube was flared. 4: The tube was fed forward through the snap bushings on the fuselage. 5: F-12127A was attached to the fuel tank, then it was bent accordingly to fit in the recesses of F-12076C-1. 6: F-12127A was detached from the fuel tank, F-12127A was pushed a bit forward and bent so the tools to cut it and flare it could fit. The tube was cut and flared with its appropriate hardware installed. 7: F-12127A was attached to the bypass fitting assembly. 8: F-12127A was attached to the fuel tank in order to check its clearance on the aft most bushing it passes through.
