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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: 7085
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IMG_2495
496 Mount, Microair Comm & Xponder, GRT EIS 4000, Fuel Pressure, Prop Controls.
Date: 11/22/2011
Views: 3833
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IMG_2491
Other wing. I'll only show a few of the pics from the annual.
Date: 02/24/2012
Views: 3483
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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: 4048
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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: 3531
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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: 3581
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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: 4207
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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: 4593
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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: 7046
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IMG_2490
Altimeter has been installed. Added a USB port for the GRT Sport. Began the label process.
Date: 11/22/2011
Views: 3741
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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: 3666
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IMG_2582
Brought the pitot/static manometer out to test the P/S system.
Date: 02/27/2012
Views: 3411
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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: 4550
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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: 4257
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IMG_2501
The full panel. Instrument final fit.
Date: 11/23/2011
Views: 4659
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IMG_2461
The two main panels cut, poked and in place.
Date: 10/27/2011
Views: 6721
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IMG_2456 1
This is a picture from the first big "smoke test."
Date: 02/10/2012
Views: 3339
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IMG_2522
Spent several weeks identifying and relabeling aircraft wiring. Talk about tedious...
Date: 01/03/2012
Views: 3405
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IMG_2123
And then another 7 lbs of alternator H/W and about 4 lbs of Whelen strobe/lights/power supply. That sleek piece in the lower left is one of the 6 oz AEROLED Nav/Strobe units replacing the Whelens.
Date: 11/24/2011
Views: 3673
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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: 4654
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