42MiS/U-14: The cushion clamps were installed as instructed.
42MiS/U-16: The harness was routed as shown.
42MiS/U-21: HW-00004 was installed The cables for the USB port and the flap controls were routed aft. Switch gasket was installed under the flap switch and the terminals were connected to it. C6286 was grounded to the fuselage using the hardware for the cushion clamp. The wires on the flap motor were stripped. The terminals were crimped onto the wires. The spade terminals on the flap wires were connected to the spade terminals on the harness and to the terminals on the flap switch.
39iS/U-16 & 17 The canopy fairing is being sanded on its most aft edges for a smoother transition.
