| Date | Description of Task | Hours | 
			
				|  | Left Wing |  | 
			
				| 10/20/06 | Today I started by setting up the right wing on 
				the stand and clamped it down.  I decided to build up the 
				left wing and then with it on the cradle I can work on the 
				ailerons and flaps for both wings simultaneously.  Since 
				this is mostly a repeat of the steps with the right wing I will 
				not be posting as many pictures.  I will have pictures of 
				new issues as they present. 
    | 1.0 | 
			
				| 10/21/06 | I drilled the spar to #40 for all the 124 
				platenut rivets as well as all the other flange rivets top and 
				bottom.  Then I countersunk the rivets.  I then dabbed the 
				countersinks with Alodine using a Q-tip.  I began riveting 
				the #8 platenuts.  I started countersinking the 
				platenut hole for the #8 screw.  I used a cut-off #8 screw to gauge the countersink depth. 
    | 3.0 | 
			
				| 10/22/06 | Finished countersinking the spar for the #8 
				screws...all 62 of them.  Alodined each countersink.  
				I also riveted the #6 platenuts for the inspection covers. 
  
				Drilled and riveted the two center section platenuts on the 
				spar.  Drilled the tie-down bar to the spar and attached 
				the four platenuts and primed using the rattle can.  Bolted 
				the tie-down and torqued to 25 in/lbs.
     Began working on the left wing rear spar.  
				Drilled and clecoed the W-907D and W-907E doubler plates to the 
				spar.  Drilled the hole for the aileron pushrod using my 
				Unibit then cleaned it up with my Dremel tool.  Took 
				the whole assembly apart and deburred the spar and doubler 
				plates.   The rear spar is ready to chemically treat 
				with SanChem.
     | 5.0 | 
			
				| 10/27/06 | Using the SanChem, I chemically treated the rear 
				spar and doubler plates.  After drying, I countersunk the 
				holes in the rear spar where needed.  I used alodine to 
				spot-treat the countersunk holes and riveted the rear spar 
				assembly.  I saved myself 
				some time and just referenced
				
				Smitty's website to determine which holes received rivets 
				and which shouldn't. Next, I placed the main spar and rear 
				spar on the table and clecoed the ribs to the spars.  You 
				have to pay attention to the plans to arrange the ribs in the 
				proper orientation.  I was really proud when I had finished 
				to find that I had NO left-over ribs :)
 | 3.0 | 
			
				| 10/29/06 | Match drilled the main ribs to the front and 
				rear spars.  Disassembled the ribs and set aside for 
				chemical treating.   | 1.0 | 
			
				| 11/3/06 | Scotchbrite scrubbed all 15 main ribs with soap 
				and water. 
    | 2.5 | 
			
				| 11/4/06 | Etched and chemically treated the main ribs.  
				Clecoed the main ribs to the main spar and riveted.  
				Clecoed the rear spar to the main ribs and riveted. Drilled 
				the 1"x1" angle to the outboard rib and attached.  Hung the 
				left wing assembly on the wing stand.  Drilled the wing 
				walk doubler as per the plans.  Clecoed the inboard skin, 
				doubler and outboard top skin to the wing skeleton.   | 6.5 | 
			
				| 11/5/06 | Match drilled the inboard and outboard skins to 
				the ribs. 
				Cut, deburred and drilled the J-stringers to the top skins. 
   
 
					
					Gretz Pitot Install
					I am 
					attempting to determine the best location for mounting my
					
					Gretz pitot.  I basically have three options. 
					Option 1:  
					This is where Vans suggests installing the pitot and has 
					holes in the ribs to this bay for routing lines.  I feel the 
					pitot head will be too close to the tie-down ring.
  
					
					  
					Option 2:  
					This location is one bay outboard of an inspection panel and 
					plenty far from the tie-down, but is located in the center 
					of the wing (inboard to outboard).  Not sure if that really 
					matters.
  
					
					  
					Option 3:  
					This location is also one bay outboard of the 3rd inspection 
					panel and is the most outboard location.  It will require 
					routing the pitot tubing around the bellcrank.
   
					I have just 
					about ruled out Option 1 due to the close proximity of the 
					tie-down.  Option 2 or Option 3 are still possibilities.  | 5.0 | 
			
				| 11/18/06 | Today my friend, Anton D'Allen came over to help 
				me out and proved to be a great helper.  We started out by 
				match drilling the bottom skins. After much debate I decided to go with Option 1.  This 
				is the only option that avoids running the pitot tube and wiring 
				through the bellcrank area.  I fabricated the attach angle 
				and drilled the bracket for riveting to the skin.  I then 
				reattached the bottom skin and marked it for the pitot bracket 
				cutout.  Cut the skin for the bracket and drilled for 
				rivets.  I primed the pitot mounting tube and riveted the 
				platenuts.  I will set the assembly aside until I rivet the 
				bottom skins.
  We clecoed the ribs in the leading edge assembly and mounted 
				to the spar and clecoed.  Fabricated the W-919 splice strip 
				and drilled and clecoed with the W-908 rib. More Gretz Pitot install
				
				here. | 6.0 | 
			
				| 11/19/06 | Match drilled left wing 
				leading edge. | 2.0 | 
			
				|  | Total Hours | 35.0 | 
			
				|  | Left 
				Tank |  | 
			
				| 11/18/06 | I put the left tank skin in the cradle and clecoed the ribs.  
				I had to use my board and clamping technique in order to get the 
				clecos in but it worked.  Next, I trimmed the T-911 and 
				T-911-INBD stiffeners, deburred and match drilled them to the 
				tank skin.  Next, I carefully oriented the attach angles on the rear 
				baffle.  Then, using the W-932DG drill guide, I drilled 
				each attach angle to #30. 
 | 2.0 | 
			
				| 11/19/06 | Drilled attach angles to 3/16" for spar attach 
				and clecoed to tank baffle.  Back-drilled attach brackets, 
				removed and deburred.  Deburred tank baffle.  
				Re-attached baffle and clecoed to tank skin.  Pop-riveted 
				the attach brackets to baffle.  Installed tank to wing spar 
				and clecoed through spar with 3/16 clecos and through tank skin 
				to spar with 1/8 clecos. 
 | 2.0 | 
			
				| 12/2/06 | Drilled the tank attach brackets through the 
				spar and then removed the tank from the spar.  I had only 
				put one pop rivet in each bracket and as a result the brackets 
				moved as they were drilled.  Sooo, off goes an order to 
				Vans for replacement brackets.  I decided to go ahead and 
				order replacement elevator counterbalance weights since I seem 
				to have trimmed them to be too light.  Started to 
				countersink the tank skin at the baffle attach. 
 | 2.0 | 
			
				| 12/3/06 | Finished countersinking the baffle attach rivet 
				line.  Drilled out the bad tank attach brackets.  
				Trimmed the T-410 reinforcement plates. 
 | 2.0 | 
			
				| 12/9/06 | I'm still waiting for the replacement tank 
                attach brackets so on to other tasks.  I deburred the 
                bottom skin ribs and began deburring the bottom skins. 
                TruTrak Roll Servo Bracket InstallationI received my servo bracket assembly and soon 
                discovered I had been sent the support bracket for the right 
                wing install.  I fired off an email to Stein so I expect to 
                get this resolved quickly.  The installation is really a 
                mental challenge because the bracket comes with no instructions.  
                After some time, this is the final result...minus the support 
                bracket. (UPDATE: Received a replacement bracket from 
				TruTrak... Great service!)
 
   | 5.0 | 
			
				| 12/10/06 | Deburred the left wing bottom skins, then 
                dimpled. 
 | 3.0 | 
			
				| 12/21/06 | Disassembled and deburred the leading edge skin, 
				ribs and splice plate.  Drilled the splice plate for rivets 
				and deburred.  Dimpled the splice plate.  Used a 
				reamer to enlarge the hole for the tie-down bolt to final size.  
				Set aside for priming. My replacement tank attach brackets 
				finally arrived today so I'm back in business.  I drilled 
				the brackets and pop riveted to the tank (using two (2) 
				rivets this time).  After back drilling through the spar, I 
				removed the tank from the spar and placed in the cradle. 
				 I removed the attach brackets from the baffle by drilling out 
				the pop rivets.  Drilled the attach brackets for K1000-3 
				platenuts.  Countersunk the brackets and washed down with 
				MEK.  Set the brackets aside for priming. Fabricated the T-905 attach angle.  I used the bench 
				grinder to finish trim the angle.  
				I match drilled the attach angle to the inboard rib and set 
				aside for priming.
 | 7.0 | 
			
				| 12/22/06 | Primed the tank attach brackets.  Riveted 
				the platenuts to the attach brackets. Fabricated the T-410 
				reinforcement plates to the inboard and outboard ribs and test 
				fit/ground down until the fit was perfect.  Deburred and match 
				drilled the T-410 reinforcement plates to the inboard and 
				outboard ribs.   I match drilled the capacitive sender plates to the second 
				and sixth ribs per the plans.  Drilled the 3/8" hole for the BNC 
				connector in the inboard rib.  Deburred, dimpled and riveted the 
				platenuts in the capacitive plates.   Used the fly cutter to cut the access hole in the inboard #1 
				rib.  Match drilled the T-411 plate.  Drilled the 3/8" 
				holes in the inboard rib for the fuel vent fitting and the fuel 
				vapor return fitting. Fit and drilled the T-406B fuel cap flange.  Deburred and 
				countersunk the flange.  I also fabricated the T-914 clip from a 
				scrap of .020.
 | 7.0 | 
			
				| 12/23/06 | Countersunk the T-407 stiffener ring for the 
				platenuts.  Deburred and countersunk the T-407 and riveted the 
				platenuts.  Drilled the hole for the fuel pick-up since the 
				T-411 plate did not have it pre-drilled. Fit and match drilled 
				the VA-112 drain flange. Drilled the holes in ribs #2 and #3 for the fuel return line 
				and deburred. Chemically treated leading edge ribs, splice plate, T-905 
				attach angle and T-411 cover plate. Disassembled tank and deburred stiffeners and ribs.  
				Deburred skin.  Fabricated the small plate for covering the 
				tooling hole in the outboard rib.  Drilled and deburred cover 
				plate.  Scuffed skin along rib and stiffener line.
 | 6.0 | 
			
				| 12/26/06 | Dimpled leading edge and left tank skins.  
				Set up area and prosealed and riveted stiffeners, fuel flange, drain flange 
				and cover plate for tooling hole in outboard rib.  I used 
				my new (used) pneumatic Semco dispensing gun for dispensing the 
				proseal and it worked great. Riveted the platenuts on the 
				splice plate.
 | 6.0 | 
			
				| 12/27/06 | Prosealed and riveted tank ribs #2-#6.  
				Drilled anti-rotation bracket to T-411 tank access cover plate. 
 | 5.0 | 
			
				| 12/30/06 | Prosealed and riveted the inboard and outboard 
				ribs.  Riveted the T-905 attach angle and the T-410 
				reinforcement plates. Prosealed and riveted the anti-rotation bracket to T-411 tank 
				access cover plate.
  
 | 3.0 | 
			
				| 12/31/06 | Capacitive 
				Sender Installation I wanted to detail the installation of the capacitive senders 
				for the fellow builders who would like to see the details.
 I 
				started by loosely installing the inboard and outboard 
				capacitive plates.  Then installed the BNC sender in the 
				inboard rib. 
    I rough installed the vent tube and when I had the proper 
				length I flared the end and loosely installed to the AN-4 
				bulkhead fitting.
     Next, I crimped and then soldered the ring connectors on the 
				wire ends.
    I then twisted the 18 AWG wire around the vent tube to secure 
				the wire and remove the excess slack.  Then I loosely 
				connected the connectors to the capacitive plates.
    Then I installed the plates permanently.
   Next, I installed the fuel vapor return line.  Like the 
				right wing tank, I ran the return to the middle of the third 
				bay.
   Finally, I mixed up 4 oz. of proseal and coated the bulkhead 
				fittings of the vent tube and vapor return line and torqued to 
				55 in/lbs.  Then I covered the entire fittings with 
				proseal.  I also covered the ring connectors and connector 
				screws and nuts.  I also prosealed the wire in places where 
				it could rub against the tank skin.
     Here is the final shots before I close up.
   Installed the fuel sender with proseal and safety wired.
   
 | 7.0 | 
			
				| 1/1/07 | Prosealed along rivet lines and attached baffle 
				with clecos in every hole.  Attached and prosealed tank 
				attach brackets.  Riveted baffle to tank, riveted baffle to 
				rib flanges and riveted tank attach brackets to baffle/rib 
				flanges. 
 | 4.0 | 
			
				| 1/5/07 | Mixed 2.0 oz of proseal and applied to the 
				inboard rib around the cover plate.  Applied the cover 
				plate and, after swirling each screw in proseal, attached 
				permanently.  Now to let the proseal cure for about a week 
				and test for leaks. 
   LEFT 
				TANK DONE!
 | .5 | 
			
				| 1/13/07 | Tested tank for leaks.  NO LEAKS! 
 | .5 | 
			
				|  | Total Hours | 62.0 | 
			
				|  | Closing Left 
				Wing |  | 
			
				| 1/6/07 | Deburred top outboard wing skin and began 
				dimpling. 
 | 2.0 | 
			
				| 1/7/07 | Dimpled top outboard wing skin.  Deburred 
				top inboard wing skin and the wing walk doubler and dimpled 
				both. Deburred J-stringers and dimpled.  Began deburring 
				wing ribs and rear spar in preparation for dimpling. 
 | 7.0 | 
			
				| 1/11/07 | Received notification from Van's 
				yesterday that my fuselage kit will be shipped the week of February 
				5th.  I had better get moving to finish the wings.  I 
				finished deburring the main wing ribs and rear spar and started 
				dimpling. 
 | 1.0 | 
			
				| 1/12/07 | Finished dimpling main wing ribs and rear spar.  
				Used deburring tool to "ream" the dimples in the rear spar.  
				Now it's time to prime! 
 | 2.0 | 
			
				| 1/13/07 | Chemically treated the leading edge skin. Polished one of my fuel tank caps.  Several builders are 
				opting to buy the Van's "deluxe" fuel caps.  I couldn't 
				justify spending an additional $100 per cap so I made my 
				own.  I started by disassembling the cap.  Next I 
				started sanding with 240 grit sandpaper.  I progressed 
				through 320 grit, 400 grit, 600 grit and finally wet sanded with 
				1000 grit.  All in all it took 30 minutes for the first 
				cap.
   
 | 3.0 | 
			
				| 1/14/07 | Began riveting the leading edge together. 
 | 1.0 | 
			
				| 1/19/07 | I finished riveting the leading edge and placed 
				on the spar.  I started riveting the leading edge to the 
				spar and riveted all that I could reach by myself. I began the 
				process of chemical treating the inside of the top skins as well 
				as the wing walk doubler and the J-stringers.  Since it was 
				around 26º 
				outside and the water froze on contact with the skins, I was 
				only able to clean scuff the skins and chemically clean/etch the 
				skins.
 | 3.0 | 
			
				| 1/20/07 | Today my friend and fellow EAAer, Jim Olsen, 
				came over to help me rivet the top skins.  I started by 
				chemically treating the inside of the skins and set them aside 
				to dry.  Jim helped me by bucking the inside spar flanges 
				of the leading edge.  We then used the pneumatic squeezer 
				to rivet the top and bottom to the spar flange. Next we 
				mounted the fuel tank and bolted it to the spar.  The bolts 
				were torqued to 25 in/lbs.  Next we screwed the tank top 
				and bottom to the spar flange.  I was pleased to see there 
				was no gap between the leading edge and the tank. We then clecoed the inboard and outboard skins to the spars 
				and ribs.   My EAA Technical Counselor, Kyle Boatright, called as 
				he was heading our way for a visit so we met him at Copperhill 
				airport.  Kyle had not seen the project since I had 
				received the wing kit so he looked it over pretty well.  I 
				really like having Kyle looking over my shoulder not only 
				because he has built an RV but because he is exceptionally 
				knowledgeable in so many areas of aircraft construction.  
				With Kyle's letter of approval, we returned him to the airport. After a great Mexican food lunch, Jim and I returned home and 
				riveted the top skins.  Like the right wing, we 
				back-riveted the top skins and then riveted the J-stringers.  
				We then removed the wing from the stand and placed it in the 
				cradle.  After Jim left, I finished riveting the skins to 
				the rear spar.
  
 | 8.0 | 
			
				|  | Total Hours | 307.2 | 
			
				|  | Next: Wings 3 |  |