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FuelSystemMod45Ann

FuelSystemMod45Ann

Date: 04/30/2004 Views: 3280

DSCN5794Ann

DSCN5794Ann

Date: 04/25/2007 Views: 6970

IMG_2090

IMG_2090

Date: 08/18/2009 Views: 5044

Newest Image

EAA SITE

EAA SITE

Date: 08/23/2023 Views: 789723

Most Viewed Image

EAA SITE

EAA SITE

Date: 08/23/2023 Views: 789723

Recent Updates

Date: 03/15/2026
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: 9814
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: 9696
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: 9825
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: 11102
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: 9869
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: 9775
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: 10298
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: 10007
IMG_7231

IMG_7231

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

Date: 01/26/2014
Views: 9741
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: 9681
IMG_7312

IMG_7312

With one final overall fit of the tank.

Date: 02/17/2014
Views: 13611
IMG_7015

IMG_7015

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

Date: 10/23/2013
Views: 10328
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: 11412
IMG_7232

IMG_7232

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

Date: 01/26/2014
Views: 10852
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: 10097
IMG_7305

IMG_7305

Checked, double checked and again checked all the fits.

Date: 02/16/2014
Views: 10379
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: 10352
IMG_6995

IMG_6995

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

Date: 10/21/2013
Views: 13738
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: 10147
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: 10928
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