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DSCF0011

DSCF0011

Date: 10/24/2010 Views: 6222

Mass_Balance_Tower_48

Mass_Balance_Tower_48

Date: 01/23/2006 Views: 5139

DSCN6642

DSCN6642

Date: 10/25/2009 Views: 4214

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EAA SITE

EAA SITE

Date: 08/23/2023 Views: 765564

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EAA SITE

EAA SITE

Date: 08/23/2023 Views: 765564

Recent Updates

Date: 01/28/2026
Owner: Guest
Size: 400 items
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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: 10679
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: 9428
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: 9309
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: 9890
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: 9556
IMG_7231

IMG_7231

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

Date: 01/26/2014
Views: 9301
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: 9256
IMG_7312

IMG_7312

With one final overall fit of the tank.

Date: 02/17/2014
Views: 13038
IMG_7015

IMG_7015

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

Date: 10/23/2013
Views: 9895
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: 10938
IMG_7232

IMG_7232

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

Date: 01/26/2014
Views: 10343
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: 9687
IMG_7305

IMG_7305

Checked, double checked and again checked all the fits.

Date: 02/16/2014
Views: 9951
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: 9913
IMG_6995

IMG_6995

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

Date: 10/21/2013
Views: 13222
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: 9674
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: 10494
IMG_7005

IMG_7005

The space with the aileron tie rod and starboard side support removed.

Date: 10/22/2013
Views: 9891
IMG_7014

IMG_7014

Next catch was where the filler needed to go into its' position. There was a piece blocking which had to be removed.

Date: 10/23/2013
Views: 11743
IMG_6984

IMG_6984

But there's no way to get it in. It is too wide to go between the door sills.

Date: 10/21/2013
Views: 9452
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