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MG_2946

MG_2946

Date: 03/17/2008 Views: 4041

2010_12250006

2010_12250006

Date: 12/25/2010 Views: 22813

FWF-10 (2)

FWF-10 (2)

Date: 11/28/2009 Views: 5277

Newest Image

EAA SITE

EAA SITE

Date: 08/23/2023 Views: 693393

Most Viewed Image

EAA SITE

EAA SITE

Date: 08/23/2023 Views: 693393

Recent Updates

Date: 09/13/2025
Owner: Guest
Size: 400 items
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IMG_7285

IMG_7285

The new sight gage running up the back rest. 2 P-clips hold it in place. The new sight gage is also back lit with a strip of LED lights.

Date: 02/13/2014
Views: 6528
IMG_6962

IMG_6962

Old 1/4 in (6.4 mm) vent on the top. Totally inadequate for the job. New 3/8 in (9.5 mm) vent on the bottom.

Date: 11/13/2013
Views: 6631
IMG_7281

IMG_7281

This picture illustrates how the new vent will be installed to obtain the best venting possible within the limits of the tank.

Date: 02/13/2014
Views: 6828
IMG_6858

IMG_6858

The old fittings as removed from the old tank. Vent on left, starboard outlet in the middle and port outlet on the right.

Date: 10/01/2013
Views: 7954
IMG_7027

IMG_7027

The underside of the fuel tank is covered in plastic wrap which will prevent the tank from bonding to the epoxy in the micro.

Date: 10/30/2013
Views: 6837
IMG_7030

IMG_7030

The tank was then put in place so that the urethane and micro could shape themselves to the bottom of the tank

Date: 10/31/2013
Views: 5838
IMG_6956 1

IMG_6956 1

With the tank removed, the micro and urethane could be covered with cork. The cork serves to protect the tank from abrasion by the support materials. You can also see the strip of urethane applied to the top of the aluminum support for the tank ledge.

Date: 11/10/2013
Views: 7401
IMG_7226

IMG_7226

Here the urethane on the aluminum ledge has also been covered with cork. The cork both served to protect the tank and the urethane.

Date: 01/19/2014
Views: 6961
IMG_7231

IMG_7231

One final check to make sure everything fits and supports the tank.

Date: 01/26/2014
Views: 6841
IMG_7029

IMG_7029

Supporting material in the form of rigid polyurethane sheet and micro/epoxy mix are laid out on the bottom of the fuselage.

Date: 10/31/2013
Views: 6271
IMG_7312

IMG_7312

With one final overall fit of the tank.

Date: 02/17/2014
Views: 9507
IMG_7015

IMG_7015

Finally, the new tank is in place. More or less.

Date: 10/23/2013
Views: 7280
IMG_7230

IMG_7230

It was determined that a 1/4 in (6.4 mm) thick piece of rigid urethane foam topped with cork was needed to support the front "ledge" of the tank so it wouldn't sag.

Date: 01/26/2014
Views: 8143
IMG_7232

IMG_7232

Must have had the tank in/out two dozen times determining necessary clearances and supports.

Date: 01/26/2014
Views: 7629
IMG_7290

IMG_7290

Bonded in the foam and cork support for the "ledge" at the front of the tank.

Date: 02/14/2014
Views: 7087
IMG_7305

IMG_7305

Checked, double checked and again checked all the fits.

Date: 02/16/2014
Views: 7393
IMG_6994

IMG_6994

Seeing where the passenger door sill will have to be cut to allow the tank to go in.

Date: 10/21/2013
Views: 7248
IMG_6995

IMG_6995

The cutout in the passenger door sill now allows entry of the tank.

Date: 10/21/2013
Views: 9751
IMG_6996

IMG_6996

You also have to make sure you clear all the cables, plumbing and wiring in the "tunnel" area.

Date: 10/21/2013
Views: 6991
IMG_7004

IMG_7004

Here you see that the fuel outlets won't go past the pitch connection rod between the sticks. And this can not be removed to be replaced at a later date. The outlets have to be trimmed back by about 1/4 in (6.4 mm).

Date: 10/22/2013
Views: 7701
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