11.1 Engine Cowl Mod

This entry is part 6 of 17 in the series 11 - Fairings

Once the inside work was completed, I put the cowling back on to see how much room I’ve got.

It’s hard to tell from the picture, but there’s about 1/2″ clearance between the top of the intake and the inside of the cowling. It’s tight, but it should be enough.

The top needed a bit of work though. It was a bit bumpy with a couple low spots. So after consulting with Malcom, I filled the low spots with micro and covered the whole thing with  one layer of fine BID.

A little bit (hopefully, very little) of filler and it should be ready to move on to the next step.

11.1 Engine Cowl Mod

This entry is part 7 of 17 in the series 11 - Fairings

After the two outer layers of BID had cured, I filled the low spots with micro and covered the whole area with one layer of fine BID. Looks like a Turtle. I was tempted to put a head and legs on it and leave it. 🙂

Then it was time (once again) to fill. This is after the first layer of fill has been sanded and then another layer put down and guide coat and sanding.

Now it’s getting close. I had the shape worked out and all I’m doing at this point is fixing voids and a couple minor low spots.

I REALLY hate the spotted dog. But hopefully by next week I’ll be cutting the oil access door.

11.1 Engine Cowl

This entry is part 8 of 17 in the series 11 - Fairings

I finally got the top of the engine cowl fair. Before I cut the oil access door, I’m going to join the upper and lower cowl at the rear. First area around the openings for the prop and air are cleaned up.

Then duct tape is applied to the inside of the bottom half and the top half is sanded. The two cowl halves are installed and clamps are used to hold the rear of the cowl together. Then a five BID layup is used to create a flange on each side of the prop opening.

Once the layup has cured, a hole is drilled that will hold the two halves together and the manufacturing flange is cut away. Then the gap between the two halves is filled.

After filling and sanding are done, the air outlets are cut down to their final dimension. Malcolm suggested using 3/4″ masking tape on the step which provides a 3/4″ line.

11.1.6 Oil Access Door

This entry is part 9 of 17 in the series 11 - Fairings

I finally finished the finishing on the upper cowling. Until it’s in shiny white primer, I won’t know how good it is, but it feels like it has the right lines.

Now it’s time to cut the oil door. The manual has you draw a 6 inch diameter circle and flatten one edge and put a hinge on it. Then a screw is used to hold it closed. I picked up a hidden hinge and recessed push button latch from the RV guys. So the first thing is to determine the location of where the door will go. To do that I installed the upper cowling and reached up inside and marked the inside of the cowling where the oil filler cap is. Then I removed the cowling and drew out the shape of the door. I decided to go with a “D” shaped door.

Since black marker doesn’t show up on carbon, I used masking tape for the layout.

I then cut all the straight lines. Here’s the top view with only the curved parts left.

Then position the hinge and drill the holes before cutting away the door.

I don’t have a blade narrow enough to cut the curves near the hinge so I drilled a series of small holes.

To keep it from binding while making the final cuts, duct tape will hold it in position.

An oil filler access door.

To make sure it’s in the correct location, I installed the cowling to verified the position.

Then I covered the bottom of the door and made a flange with 4xBID. Once it was cured, I trimed away the excess leaving a flange (or lip) that the door would rest against.

Next I positioned and drilled for the recessed latch. Here’s everything held together with cleco’s.

I’m a bit concerned about the clearance with the J-hinge. It’s REALLY close.

But I’ll wait and see how much movement the engine has before I make the call on that. Best case is I have enough room. Next best is I could trim part of the hinge. Worst case is having to come up with a different hinge.

11.1.99 Cowling Baffle Treatment

This entry is part 15 of 17 in the series 11 - Fairings

I’m not using the standard Velocity cooling plenum.  I decided to use a more traditional approach where aluminum baffles create a box that mates with the upper cowling to create the high-pressure plenum.  The interface between the aluminum baffles and the inside of the cowling is a flexible baffle material that creates a relatively airtight seal.  On most other planes the cowling is sheet aluminum and the flexible baffle will slide up against the cowling.

But my cowling is a rather course fiberglass. So to allow the flexible baffle to slide, I decided to create a smooth surface on the inside of the cowling… but only where the baffle will contact.

I sanded down the inside of the cowling where the baffle material will contact the cowling. Then I used masking take to define the area and painted on epoxy.

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Once it dried, I removed the tape over the inner area, sanded the epoxy and painted on a second coat.

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Now (hopefully) the flexible baffle material will slide as needed.

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11.1.2 Cowling attach mod

This entry is part 16 of 17 in the series 11 - Fairings

I used the cowling to the fuselage attachment method described in the book.  I thought about using approaches that other builders have used but decided to just get it done.

One of the things that I wish I had done was a captive flange at the fuselage attach point instead of a bunch of screws. Since I haven’t painted yet, I could to that but so far I’ve been deferring that decision.

But I do have one place on the lower cowl that I have to deal with. When the hole were being drilled in the lower cowling, one of them ended up being directly under the electric fuel boost pump.  There’s not enough room for a regular nutplate.  Even a a low profile tinnerman would probably not fit.

So I decided to do a captive flange under the fuel pump. FIrst I made a spacer with a couple layers of triax and BID.  This has to be the same thickness as the cowl flange. Then I cut a piece of leftover titanium that would extend aft from the firewall past the fuselage flange by about a half inch. Next I drilled four holes through the fuselage, spacer and titanium. Finally I put a film of structural adhesive between all the parts and riveted them in place.

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Filling the countersunk rivets will be done during paint prep in the fall.

If I like how this works, I may do this all around the fuselage/cowling attach area. Then maybe use piano hinge at the wingroot.

11.1.8 Cowling Attachments

This entry is part 17 of 17 in the series 11 - Fairings

One of the changes I made during my build was to replace the screws which attach the doghouse cover to the canard with piano hinges with pins that are removed from inside the nose.

6.8.2 Doghouse Attach Points

I also used an internal J-hinge for the nose hatch and a hidden latch. This means there are no visible screws on the forward part of the aircraft.

When the cowling was being prepared, I considered using piano hinges there as well. But three things stopped me. One was that I couldn’t figure out how to deal with the cowl to fuselage attachment. I knew from experience that the slight curve of the hinge for the doghouse cover made for a bit of challenge getting the pin to slide into the hinge easily. The fuselage curve would be significantly more difficult.

The second was how to access that cowl-fuselage pin. There would have to be some type of hole in the cowl to insert the pin and you need a latch of some sort.  Malcolm said he built one and that it was inserted from below the wing and you had to use a drill to get in fully inserted.

And the third was time. At this point I was about 5 years into the build.  The plane was at Hangar 18 (Malcolm Collier’s shop) so I was commuting from Chicago to work on it. The engine hadn’t been hung yet, the first electrical wire had yet to be pulled and I was looking to get finished. So I made the decision to go with the method called out in the manual which is to use screws with nutplates to attach the cowling.

I used #8 truss head stainless steel screws. I picked up some nylon washers to try and keep the cowling finish somewhat presentable.

And it works.  There’s nothing wrong with the book solution.

But like many aspects, it could be better. In my opinion, the biggest drawback is time.  There are a little over 40 screws holding the upper and lower cowling in place.  I eventually purchased an electric screwdriver to speed up the cowling removal process. But even with that it still takes a long time to remove all those screws.  The heads of the screws round out. Which means I had to constantly replace screws when the head became so damaged that I couldn’t tighten it anymore.   Finally, it just looks… not bad… but not good.

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What alternatives are there?

Piano hinge retrofit

I could use piano hinges on the wing roots and where the two cowl halves meet.  Then the screws would just be at the cowl-fuselage junction. The problem with that is trying to install hinges with the engine in place would be very difficult if not impossible.

Camloc’s, Dzus or quarter-turn fasteners

These have been around airplanes for years. Basically they are spring loaded, quarter turn fasteners. They are available in many styles.  The problem is that they aren’t cheap.  But I found the racing version isn’t too expensive. So I got a couple samples.

jegs flatheadjegs oversizedjegs spring

The spring gets riveted to the underside of the lower panel. Then the fastener gets inserted from the outside and picks up the spring.  But here’s the big problem: This would be fine with a sheet metal airplane where the thickness of the panels doesn’t vary.  But with a composite airplane, there are variations in the thickness of all the parts. So you would either need a number of different length fasteners.  And of course you would need to remember which length went in which hole.  Or you could measure and then use shims to create an identical thickness. The other issue is that they are HUGE.  Some of the heads of the fasteners are one inch in diameter.

Then I decided to look into aircraft versions.  Reiff Lorenz gave me a tip for Skybolt located nearby in Leesburg, FL so I started looking at their offerings.  They have a number of different types.  But the one which has the most promise is their Cloc 4000 Series Fasteners.  The best part is they have an adjustable receptacle (like the nutplate for quarter turn fasteners) which can accommodate a wide range of panel thicknesses. I ordered two fasteners, two floating receptacles and two grommets. The grommets are the ring that the fastener goes through on the outer panel.  Kind of like a bezel.

I tested them out on some mockup panels and they work great. I simulated different panel thicknesses by adding washers between the two test panels.  The receptacle adjusted for every thickness I threw at it.  But there were two problems: 1) Countersinking the grommet.  The bottom of the grommet is a 120 degree countersink. But I don’t have a countersink that size and I don’t have one with a 15/32” guide to keep it centered.  2) Cost. Each position was going to cost about $10.  That would work out to over $400 for entire cowling.

As is usually the case in aviation, almost all problems can be solved using the acronym which is well known to boaters. BOAT: Break Out Another Thousand (dollars). Fortunately, it wasn’t that bad.  On the runup to Sun-n-Fun, Skybolt was having a sale. 10% off.  And they have a special tool for countersinking for the grommets.  And it’s ONLY $145.

Since there is a price break at 50, I bumped up the number of parts so I would have some spares. The parts came out to about $440.

Here is the receptacle.

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The small stud on the housing prevents a spring clip from engaging. This allows you to turn the receptacle in or out to adjust it. Once you have it at the correct depth, you remove the stud, rotate the receptacle 90 degrees in or out (whichever is closer) and the clip engages the receptacle locking it in position.

I installed two on the upper cowling just to see how difficult the install would be, how it would look and most importantly, how it would hold up. The installation was too bad, but the results were very nice.

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After about 4 hours of flight time, I could see no adverse wear or stress as a result of the two fasteners. So now it’s time to get serious about installing.

The first task was to make a drill guide. It would have been nice if the rivet holes matched the existing nutplates, but with the size of the receptacle housing, that wasn’t going to happen.  Skybolt sells a drill guide but I spent my lunch money for the year on their countersink tool. So I grabbed some steel (never make a guide you need to use more than two times out of aluminum) marked, drilled and cut.

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I filed down one corner so it would fit close if there was a raised edge.  Now, all I have to do is attach this guide to the flange with a #8 screw into the existing nutplate.

If the rivet holes were farther apart, I could mount  the receptacle in the same orientation. But because they’re just a little farther apart, that won’t work. I tried rotating the receptacle 90 degrees but in many cases there wasn’t enough room.  So I had to settle for rotating it about 40 degrees off of the existing nutplates.

Installation

Here’s one of the nutplates on the flange of the wingroot.

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After the two #30 mounting holes have been drilled.

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Next, remove the old nutplate by drilling out the rivets with a #41 drill bit and enlarge the center hole to 15/32”.

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Then countersink for the new rivets and install the receptacle.

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I’m not a fan of pop rivets. So whenever possible, I use solid rivets. Pop rivets are used for places that I can’t get the rivet squeezer into.

Preparing the outer panel for the fastener.

Here is the cowling where the #8 screw was used to attach the cowling. Notice how the screw head/washer has displaced the paint (actually primer since I haven’t painted yet).

Because the new fastener will be in the exact same position as the old screw, it’s a simple matter of enlarging the hole to accommodate the grommet. A step drill gets the opening to within about a 32nd of an inch.  Then a 15/32” drill bit finishes the opening.

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Finally the incredibly, insanely expensive special tool is used to create the bevel for the grommet.

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This is the same type of bit used with the micro-stop countersink tool.  But it has a number of different sized guides which attach to the pilot. Once the micro-stop is adjusted, it only takes a second to create the bevel.

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Once that’s done, it’s time to put the cowling on, insert the fastener, and then tighten until the head of the fastener is flush with the grommet. Then remove the fastener without rotating the receptacle. This is accomplished by pushing in firmly while releasing the fastener. Remove the cowling and then remove the stud. Insert a flat blade screwdriver into the receptacle and turn in or out a quarter turn to let the spring clip latch into the receptacle. That’s it.

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Repeat about 40 times and you’re done.

I think that when the engine comes out for overhaul, I’ll retrofit piano hinges on the wing roots and upper/lower cowl joint. But until then, this solution will work nicely.

Here’s a split screen view of the left and right side.

Before-After

Parts:
SK245A161A  –  Receptacle $4.20
SK40S5-3S  –  Fastener $3.29
SK-GS – Grommet $1.99
MS20426AD4-5835 Solid Rivets

Tools:
#30 drill bit
#41 drill bit (to drill out old nutplates)
Step drill bit
15/32” drill bit
Rivet Squeezer
Counter sink for 3/32” hole
SKC4S (Counter sink for grommet)
Drill
#2 Phillips Head Screwdriver
Large Flat Blade Screwdriver