02/19/20: 2.07Hrs 1: The tunnel cover assembly was riveted to the fuselage. 2: The grommet was installed on the firewall and CT-01200 was fed through it. 3: CT-01200 was attached to F-01246A. 4: CT-01200 was inserted in VA-219-2, adjusted so it extended 7/16" and then the hardware was tightened.
02/20/20: 2.08Hrs Worked on step 5.
03/23/20: 3.23Hrs 5: CT-01200 was secured to the engine mount.
