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dscn2189
Date: 12/31/1969
Views: 3896
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Duxford_17_8_09_167
Date: 08/23/2009
Views: 4508
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Oshkosh_2009_041
Date: 07/29/2009
Views: 9537
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GasCap1
Date: 10/29/2007
Views: 7299
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20050215_IMG_0013
Date: 02/15/2005
Views: 4366
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IMG_2263
Date: 02/23/2005
Views: 6224
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DSCN5280Ann
Date: 12/19/2006
Views: 3972
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Door hinge rebates 57.
Date: 11/12/2009
Views: 4559
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Found many voids and bad areas of layups on doors.
Date: 08/24/2009
Views: 9458
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dscn1887
Date: 12/31/1969
Views: 3793
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IMG_6786smal
Date: 02/23/2008
Views: 4711
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Alan's finger was part of the clamp.
Date: 10/16/2009
Views: 6269
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Option A) Electrical Box install 2 of 2.
Date: 08/12/2003
Views: 8601
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IMG_6973_em_sa
Here I have annotated the important elements. The red outlines the fiberglass support bonded to the bottom of the tank. Blue arrow points to the blue crack. The crack formed exactly as a stress analysis says it should, at 45ยบ to the corner of that supp
Date: 10/18/2013
Views: 7434
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Airbrake Terry 3.
Date: 09/07/2010
Views: 3870
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D-sub shell could be 180 degree or converted to 90 degree.
Date: 03/13/2009
Views: 11976
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Bat6
Date: 01/15/2009
Views: 5808
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Upholstery 2
First step is to do everything around the instrument module where it will be difficult to get at once it is installed. Finish of the plane is critical since no matter how well built, the finish is wahta you will be looking at the rest of your flying life.
Date: 03/05/2018
Views: 7998
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Time to start taper sanding 1.
Date: 10/22/2009
Views: 5295
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dscn0321
Date: 12/31/1969
Views: 4004
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