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Port wingskin fill begins 4.

Port wingskin fill begins 4.

Date: 09/14/2010 Views: 6628

IMG_2312

IMG_2312

Date: 06/01/2005 Views: 6698

Panel_03

Panel_03

Date: 01/23/2006 Views: 5020

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EAA SITE

EAA SITE

Date: 08/23/2023 Views: 769144

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EAA SITE

EAA SITE

Date: 08/23/2023 Views: 769144

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Date: 02/02/2026
Owner: Guest
Size: 50 items
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IMG_2523

IMG_2523

But I'm still piddling around with the wiring and cabling. Found out today that the GRT Sport SX will control a Garmin SL30 radio and the Microair 760 will support SL30 type input/output. So, I'm working on adding the necessary wiring between the two.

Date: 01/03/2012
Views: 5516
IMG_2468

IMG_2468

Wiring begins in earnest. Color coding has been added to the switches. Red-Master, Blue-Ignition, Yellow-Starter, Green-Boost Pump & White-Lighting.

Date: 11/13/2011
Views: 5587
IMG_2513

IMG_2513

Had to make up a new cover plate for the back of the transmission where alternator #2 formerly resided.

Date: 12/16/2011
Views: 5594
IMG_2537

IMG_2537

Here you can see the numerous check lists used in the inspections laid out on the wing.

Date: 03/02/2012
Views: 5752
IMG_2437

IMG_2437

Eventually, the 2nd alternator and supporting H/W will go. Also, I have Parahelion copper-clad aluminum fat wire which will replace the existing fat wire.

Date: 10/15/2011
Views: 5553
IMG_2461

IMG_2461

The two main panels cut, poked and in place.

Date: 10/27/2011
Views: 10723
IMG_2470

IMG_2470

Another test fit. Getting better. Still waiting on the electroluminescent light ring for the altimeter.

Date: 11/13/2011
Views: 5557
IMG_2554

IMG_2554

After a preliminary W&B done last week, the CG was now somewhat aft. After all, I had removed almost 40 lbs (18 Kilos) from the instrument panel and another 7 lbs (3 kilos) from the engine compartment. So I pulled the battery from below the baggage

Date: 02/21/2012
Views: 5574
IMG_2491

IMG_2491

Other wing. I'll only show a few of the pics from the annual.

Date: 02/24/2012
Views: 6084
IMG_2460

IMG_2460

Used our hydraulic punch to poke out the round holes. The rectangular holes were corner drilled and cut out with aircraft shears. Files were used to clean up the holes in shape and size.

Date: 10/27/2011
Views: 10559
IMG_2525

IMG_2525

Wiring in the instrument panel. From a couple weeks ago, not the final iteration.

Date: 01/14/2012
Views: 5520
IMG_2313

IMG_2313

Panel plates were cut from aluminum and fitted to the fiberglass.

Date: 10/06/2011
Views: 7614
IMG_2522

IMG_2522

Spent several weeks identifying and relabeling aircraft wiring. Talk about tedious...

Date: 01/03/2012
Views: 5534
IMG_2456

IMG_2456

Drilling for the rivets to hold the anchor nuts required novel technique. Eventually, all anchor nuts were installed.

Date: 10/25/2011
Views: 6882
IMG_2524

IMG_2524

Maybe by the end of the week I can have the shell installed and wired into the aircraft so I can plug these into it. We'll see. These 26ºF (-3.3ºC) mornings have been limiting me to only 4 or 5 hours of afternoon work a day.

Date: 01/03/2012
Views: 5531
IMG_2526

IMG_2526

Again a picture from a couple weeks ago. One of the initial test fit of the panel and check of wiring runs.

Date: 01/14/2012
Views: 5748
IMG_2309

IMG_2309

The obvious place to begin weight reduction was the ridiculously heavy instrument panel. Removed it and put the Garmin radios, etc. up for sale. Meanwhile, I began to lay out the instrument configuration in the old panel.

Date: 10/06/2011
Views: 10581
IMG_2582

IMG_2582

Brought the pitot/static manometer out to test the P/S system.

Date: 02/27/2012
Views: 5564
IMG_2559

IMG_2559

Add the 2 meter extension to the 1 meter length and run the viewer down to the brake area.

Date: 03/12/2012
Views: 6314
IMG_2517

IMG_2517

This is 160 Kts on the manometer (right on)

Date: 02/28/2012
Views: 5648
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