Empennage : Horizontal Stabilizer & Elevator

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Posted by robert escobal (11) on 2000-09-14 23:27:26 24.25.71.225

1996 Cal told me that I had too many rivits on this end but was OK.


Posted by Terry L Carlson (21) on 2000-09-25 20:59:01 206.154.186.148

The elevator control attachment. Height of hole in vertical piece determines amount of movement. Reference plans for dimensions.


Posted by Terry L Carlson (21) on 2000-09-25 21:12:53 206.154.186.148

Horizontal stabilizer connection to fuselage on right side. I installed the doubler reinforcement on the inside rather than the outside. Threaded a 4130 rod and installed it through Bulkhead 'E' for attachment.


Posted by Terry L Carlson (21) on 2000-09-25 21:25:24 206.154.186.148

Horizontal stabilizer connection to fuselage on left side. Note my method of putting a drop of 'Bright Red' fingernail polish on the threads and nuts of all bolts. If you do this as you install them, you don't have to go back and check them because you know you already tightened them. You can also tell if they have loosened because the polish will crack. I use this method on the completed aircraft assembly.


Posted by Hector Mora (471) on 2000-11-07 05:01:05 193.153.147.142

I need opinions about this change.Thanks


Posted by Hector Mora (471) on 2001-06-23 13:22:11 213.99.163.81



Posted by Hector Mora (471) on 2001-06-23 13:23:56 213.99.163.81



Posted by Hector Mora (471) on 2001-06-23 13:31:44 213.99.163.81

My .020" channel spar,have 2 5/16"x 68".It is 5/16" more wide,and is fixed a little more back in the H.S.Near of 3" of edge


Posted by Hector Mora (471) on 2001-06-27 16:55:55 193.153.147.151

This is my particular measure for the H.S. spar


Posted by Hector Mora (471) on 2001-06-27 16:59:25 193.153.147.151

Measure of my H.S. skin


Posted by Hector Mora (471) on 2001-06-27 17:14:09 193.153.147.151

I make a line at one side of 3/4" (previus picture) and another in the opposite side at 2 7/8" of the same trailing edge.Total wide of the skin is 26"(development)


Posted by Hector Mora (471) on 2001-06-27 17:18:11 193.153.147.151

Elevator skin


Posted by Hector Mora (471) on 2001-06-27 17:20:24 193.153.147.151



Posted by Hector Mora (471) on 2001-06-27 17:23:58 193.153.147.151



Posted by Hector Mora (471) on 2001-06-27 17:28:59 193.153.147.151



Posted by Hector Mora (471) on 2001-06-27 17:31:40 193.153.147.151



Posted by Hector Mora (471) on 2001-06-27 17:33:31 193.153.147.151



Posted by Hector Mora (471) on 2001-08-11 17:42:20 213.99.226.57



Posted by Hector Mora (471) on 2001-08-11 17:44:23 213.99.226.57



Posted by Hector Mora (471) on 2001-08-11 17:45:46 213.99.226.57



Posted by Hector Mora (471) on 2001-08-11 17:46:54 213.99.226.57



Posted by Hector Mora (471) on 2001-08-11 17:48:03 213.99.226.57



Posted by Hector Mora (471) on 2001-08-11 17:49:58 213.99.226.57



Posted by Hector Mora (471) on 2001-08-11 17:51:20 213.99.226.57



Posted by Hector Mora (471) on 2001-08-11 17:52:52 213.99.226.57



Posted by Hector Mora (471) on 2001-08-21 18:41:54 193.152.183.212

Elevator ribs,maked in same form that H.S.


Posted by Hector Mora (471) on 2001-08-21 18:44:26 193.152.183.212

Ribs ready


Posted by Hector Mora (471) on 2001-08-21 18:51:20 193.152.183.212

To level out the H.S. I use two telescopic support


Posted by Hector Mora (471) on 2001-08-21 19:02:21 193.152.183.212

I fix first my hinges at tube with adhesive tape, and after fix to H.S..In this form they are straight.The central hinge is necessary maked more longer that 6" (7"-8")


Posted by Hector Mora (471) on 2001-08-26 03:10:04 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:15:22 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:20:09 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:22:27 213.99.163.71

Checking


Posted by Hector Mora (471) on 2001-08-26 03:24:31 213.99.163.71

Checking


Posted by Hector Mora (471) on 2001-08-26 03:26:55 213.99.163.71

And checking


Posted by Hector Mora (471) on 2001-08-26 03:29:02 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:30:25 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:35:13 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:36:48 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:38:10 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:39:41 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:42:00 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:44:29 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:52:48 213.99.163.71



Posted by Hector Mora (471) on 2001-08-26 03:56:30 213.99.163.71

Alternative??


Posted by Hector Mora (471) on 2001-08-29 13:49:53 193.152.182.145



Posted by Hector Mora (471) on 2001-08-29 13:52:10 193.152.182.145



Posted by Hector Mora (471) on 2002-04-12 07:30:57 213.96.80.15

Measurament respect to spar


Posted by Hector Mora (471) on 2002-04-12 07:34:13 213.96.80.15

1/8 x 12" bit it is crosing the angles and fuselage


Posted by andy jankowski (128) on 2002-05-16 08:34:49 198.142.113.92

I have balanced the elavators 100% using 1/4" alloy plate bolted on to 4130 steel elavator end caps, and 550 grammes of lead plate.That's about 1.2 lbs each end, total 2.4 lbs as opposed to 1 lb as per unbalanced plans.


Posted by andy jankowski (128) on 2002-05-16 08:37:30 198.142.113.92

The lead plates were cut with a knife and are bolted between a steel plate and alloy bar.I will put a fibre glass tip on both elavator and stabiliser.


Posted by andy jankowski (128) on 2002-05-16 08:39:39 198.142.113.92

The steel end caps with the weights on fit into the ends very well.


Posted by andy jankowski (128) on 2002-05-16 08:41:35 198.142.113.92



Posted by andy jankowski (128) on 2002-05-16 08:44:18 198.142.113.92

Full up elavator.


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

Underview of elavator.


Posted by andy jankowski (128) on 2002-05-16 08:49:07 198.142.113.92

Front view of weights.


Posted by andy jankowski (128) on 2002-05-16 08:53:31 198.142.113.92

Full down.


Posted by andy jankowski (128) on 2002-05-16 08:57:36 198.142.113.92

Rudder horn and turnbuckle.


Posted by andy jankowski (128) on 2002-05-16 08:59:02 198.142.113.92



Posted by andy jankowski (128) on 2002-05-16 08:59:53 198.142.113.92



Posted by andy jankowski (128) on 2002-05-16 09:03:12 198.142.113.92



Posted by andy jankowski (128) on 2002-05-16 09:03:40 198.142.113.92



Posted by Rick Stockton (70) on 2003-06-29 23:01:52 4.60.159.218

Rear view of Bulkhead "B"


Posted by Rick Stockton (70) on 2003-06-29 23:03:11 4.60.159.218

Another view of controls behind bulkhead "B"


Posted by Rick Stockton (70) on 2003-06-29 23:06:32 4.60.159.218

Ilder arm "not to plans" behind bulkhead "D" for elevator control.


Posted by Rick Stockton (70) on 2003-06-29 23:10:14 4.60.159.218

Elevator control horn and control tube.


Posted by Rick Stockton (70) on 2003-06-29 23:13:33 4.60.159.218

Cockpit control stick with brake grip.


Posted by Hector Mora (471) on 2005-06-07 11:17:51 62.43.0.33

From Rafael Sajardo´s Plane


Posted by Hector Mora (471) on 2005-06-07 11:25:36 62.43.0.33

The pieces with green protection are 4130 X .090 steel


Posted by Hector Mora (471) on 2005-06-07 11:34:33 62.43.0.33

The central screw replace the rivet. They fix the bulkhead "E", with nut plate inside.The frontal bolt take the reinforcement plate of .040", and another little plate of 1/8"


Posted by Hector Mora (471) on 2005-06-07 11:35:39 62.43.0.33



Posted by Hector Mora (471) on 2005-06-07 11:36:58 62.43.0.33




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