Fuselage : Bulkheads D & E

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Posted by Hector Mora (471) on 2000-11-05 08:38:29 193.152.182.177

Pattern of"D"


Posted by Hector Mora (471) on 2000-11-05 08:40:51 193.152.182.177

Bulkhead "D" in progress


Posted by Hector Mora (471) on 2000-11-05 08:45:35 193.152.182.177

Reinforcement angle of 3/4"x3/4"x.040" (2024 T3),from "D" to "E"


Posted by Hector Mora (471) on 2000-11-05 08:50:02 193.152.182.177

Reinforcement angle in the botton skin from "C" to "D" in diagonal


Posted by Hector Mora (471) on 2000-11-05 09:01:11 193.152.182.177

More of the same


Posted by Hector Mora (471) on 2000-11-05 12:42:15 193.153.147.190



Posted by Hector Mora (471) on 2000-11-05 12:44:18 193.153.147.190



Posted by Hector Mora (471) on 2000-11-05 12:47:00 193.153.147.190



Posted by Hector Mora (471) on 2000-11-05 12:50:21 193.153.147.190

This reinforcement angle, is one of my changes


Posted by Hector Mora (471) on 2001-04-21 17:58:36 193.152.182.31

The holes are of 2" of diameter.The distance from bottom is 5" to center in the left side.In the right side is 6", but 5 1/2" is better.My flat bottom skin is .025" Alclad.This is only with zinc cromate in the joint


Posted by Hector Mora (471) on 2001-04-21 18:19:52 193.152.182.31

This is a internal view of right side of bagage compartmen.The yelow (zinc cromate) angle is maked of a plate of 1/8" 2024 T3 x 3" of long and 1" of wide ,for fix the safety belt.Between bulkhead and skin there are a flat piece of .040" to prevent dents in the skin when you pull of rivets


Posted by Hector Mora (471) on 2001-04-21 18:24:37 193.152.182.31

Left side of bagage compartment, and how I fix to side of bulkhead "C"


Posted by Hector Mora (471) on 2001-04-21 18:26:39 193.152.182.31

Frontal view


Posted by Hector Mora (471) on 2001-04-22 15:46:56 213.99.226.139

Note the internal reinforcement plates


Posted by Hector Mora (471) on 2001-04-22 15:51:43 213.99.226.139

Union of skin "C-D" to "D-E"


Posted by andy jankowski (128) on 2002-05-16 08:26:47 198.142.113.92

View showing rudder tube and elavator tube in tailboom.


Posted by andy jankowski (128) on 2002-05-16 08:30:02 198.142.113.92

I put an inspection hole in the tail bottom next to bulkhead "E" to allow me to put in bolts, instead of a rod, to hold the rear stabiliser on. It has worked well.


Posted by Rick Stockton (70) on 2002-09-21 13:00:12 4.60.158.138

Top and side panels from "C" to "D"


Posted by Rick Stockton (70) on 2002-09-21 13:04:42 4.60.158.138

Top panel "C" to "D" going on


Posted by Jack Dernorsek (78) on 2004-08-12 12:49:33 65.209.67.185

From builder Lance Rademeyer in South Africa, "...notice on this Teenie's fuselage how he has rounded the skins, he says extremely difficult and it took him 3 attempts. This guy's name is Gavin Edwards; owned a Teenie which he did 500 hours in before losing a motor due to electrical problems.

This Teenie that he is building is 16% wider than standard he is using the same leaf gear spring arrangement as he had on the last one he says it never gave him a moments trouble. The aircraft is way past the stage of these photos and I would guess 90% complete."
Picture posted by Jack D


Posted by Jack Dernorsek (78) on 2004-08-12 12:51:22 65.209.67.185

From builder Lance Rademeyer in South Africa, "...notice on this Teenie's fuselage how he has rounded the skins, he says extremely difficult and it took him 3 attempts. This guy's name is Gavin Edwards; owned a Teenie which he did 500 hours in before losing a motor due to electrical problems.

This Teenie that he is building is 16% wider than standard he is using the same leaf gear spring arrangement as he had on the last one he says it never gave him a moments trouble. The aircraft is way past the stage of these photos and I would guess 90% complete."
Picture posted by Jack D


Posted by Hector Mora (471) on 2005-06-08 03:35:51 62.43.0.33

T2 Rafael Sajardo.
View from the access panel in botton fin to the internal reinforcement in the "E" bulkhead zone.Note the particular form to fix with bolts and internal reinforcement plates, the angles of the Horizontal Stabilizator



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