01/02/19: 2Hrs 1. FLF-00017 on the tank was capped using the hardware provided in the fuel tank test kit. 2. A 3/8 piece of tube was trimmed and flared, then the hardware shown on figure 1 was attached. 3. A condom with a rubber band was used to create an air-tight reference. 4. The tank was filled with air using a pump until the condom inflated and the former was then sprayed with soapy water to check for any leaks, even so, tomorrow it will need to be checked again at the same temperature to confirm that the condom is still inflated.
11/29/19: 10Hrs 5. The F-01229A and F-01229-1 were screwed to the baggage floor. 6. The fuel tank was attached to the fuselage at the top two attachment point using bolts, and inserting clecos in the four holes in the F-01229A.
12/02/19: 7.5Hrs 7. Match-drilled #12 the screw hole in the hole F-01227 into the F-01229A and F-01229-1. 8. The F-01229-1 and F-01229A were removed, the nutplate rivet holes were match-drilled on both parts and finally deburred.
12/03/19: 4.5 Hrs 9. The F-01229A was countersunk. Then the F-01229A and F-01229-1 were dimpled for the other two flush rivets and finally both were riveted together.
01/14/20: 1.33Hrs New F-01229A and F-01229-1 were match-drilled using F-01227 once again, a nutplate was used to match-drilled its holes, then F-01229A was countersunk and the parts were riveted as previously mentioned.
