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CH17_34

CH17_34

Date: 12/31/1969 Views: 4669

Raimo 7

Raimo 7

Date: 05/22/2007 Views: 6392

Aeropoxy 458 Splining Compound 2.

Aeropoxy 458 Splining Compound 2.

Date: 08/24/2009 Views: 8722

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EAA SITE

Date: 08/23/2023 Views: 704649

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EAA SITE

Date: 08/23/2023 Views: 704649

Random Items

Date: 11/06/2025
Owner: Guest
Size: 50 items
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IMG_2528

IMG_2528

View from the other side. Must have down 5 test fit by the last one. Each resulted in finding things to correct. So I've been correcting things for a couple weeks now. More wire labels, adding connectors, checking pinouts, testing switches, finding is

Date: 01/14/2012
Views: 5543
IMG_2501

IMG_2501

The full panel. Instrument final fit.

Date: 11/23/2011
Views: 6491
IMG_2454

IMG_2454

I had some maple veneer from another project which came in handy to cover the sheet aluminum plates. I think it's much more attractive than painted aluminum.

Date: 10/24/2011
Views: 5256
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: 5337
IMG_2313

IMG_2313

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

Date: 10/06/2011
Views: 7073
IMG_2565

IMG_2565

You can see the bubbles of air coming from the brake line as you push fluid in from below. You can also manipulate the brake master to assist the flow of air out of the system.

Date: 03/12/2012
Views: 8087
IMG_2522

IMG_2522

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

Date: 01/03/2012
Views: 5122
IMG_2463

IMG_2463

Here's why the bottom breakers are upside down. It puts the buss bars connecting the inputs together. The first breaker in the bottom row is the main output from the alternator so it is right side up so the output goes to the buss bars.

Date: 10/28/2011
Views: 5893
IMG_2447

IMG_2447

Started to make up the switch and breaker panel.

Date: 10/24/2011
Views: 7545
IMG_2571

IMG_2571

The nasty job of bleeding brakes. How do you do it without assistance? You get out the inspection camera and point the camera head at the brake reservoir.

Date: 03/12/2012
Views: 6138
IMG_2525

IMG_2525

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

Date: 01/14/2012
Views: 5067
IMG_2125

IMG_2125

These 8 lbs of instruments were removed from the old panel along with the approximately 35 lbs of Garmin H/W.

Date: 11/24/2011
Views: 5025
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: 9571
IMG_2462

IMG_2462

Here is the switch & breaker panel all nicely assembled. Don't know if you can tell, but the bottom row of breakers (except for the first one) are all upside down.

Date: 10/28/2011
Views: 5546
IMG_2495

IMG_2495

496 Mount, Microair Comm & Xponder, GRT EIS 4000, Fuel Pressure, Prop Controls.

Date: 11/22/2011
Views: 5118
IMG_2307

IMG_2307

Cardboard cutouts and templates were used to shape and size the panels and to decide where instruments should go.

Date: 10/06/2011
Views: 6283
IMG_2491

IMG_2491

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

Date: 02/24/2012
Views: 5611
IMG_2452

IMG_2452

The Garmin equipment sold very quickly and the proceeds were used to buy the new instruments. Here are the 2 1/2" "backup" gauges with the Microair Comm & Xponder as well as the GRT EIS 4000 from the old panel. At this point I was sti

Date: 10/24/2011
Views: 7080
IMG_2571

IMG_2571

Opened all the inspection holes to ensure all is well inside.

Date: 02/24/2012
Views: 5695
IMG_2512

IMG_2512

Did numerous test fit insertions of the instrument panel shell. I think I finally have it ready to install.

Date: 12/16/2011
Views: 5118
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