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Removing_Gel_Coat_for_Carbon_Fibre_Layup

Removing_Gel_Coat_for_Carbon_Fibre_Layup

Date: 09/02/2004 Views: 6350

Landing_Gear_16

Landing_Gear_16

Date: 01/23/2006 Views: 6891

2005_1_16_10

2005_1_16_10

Date: 02/03/2009 Views: 6444

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EAA SITE

EAA SITE

Date: 08/23/2023 Views: 792562

Most Viewed Image

EAA SITE

EAA SITE

Date: 08/23/2023 Views: 792562

Recent Updates

Date: 03/20/2026
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: 9880
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: 9784
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: 9893
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: 11170
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: 9954
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: 9861
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: 10383
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: 10083
IMG_7231

IMG_7231

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

Date: 01/26/2014
Views: 9829
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: 9760
IMG_7312

IMG_7312

With one final overall fit of the tank.

Date: 02/17/2014
Views: 13689
IMG_7015

IMG_7015

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

Date: 10/23/2013
Views: 10417
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: 11490
IMG_7232

IMG_7232

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

Date: 01/26/2014
Views: 10919
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: 10157
IMG_7305

IMG_7305

Checked, double checked and again checked all the fits.

Date: 02/16/2014
Views: 10453
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: 10432
IMG_6995

IMG_6995

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

Date: 10/21/2013
Views: 13819
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: 10216
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: 11003
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