01/07/19: 2.66Hrs 1. The bracket assemblies were riveted to the forward spar. 2. Hinge stop hardware was installed. 3. Forward counterbalance bracket was riveted to the front spar. 4. Aft counterbalance bracket was riveted to the aft spar.
01/08/19: 2.42Hrs 5. Horn doublers, forward and aft spar were clecoed again to the spar cap assembly. 6. Spar box assembly was riveted as instructed on step 6, a total of 40 holes were riveted using LP4-3. 7. Inboard horn attach angle, upper and lower horn were clecoed to the assembly. 8. The inboard attach angle was riveted to the aft spar. 9.The horns were riveted to the assembly.
