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RV-10 Firewall Forward Kit
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This page documents the installation of the Lycomming IO-540 engine and Grand Rapids Engine Information System (EIS-6000).
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Hours |
Sect. |
Notes and Photos
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3/4/10
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2 hrs
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Inventory
The engine was delivered to my door by a young man that backed a full-sized semi-tractor trailer truck through a 20' gate,
and down 200' of driveway without putting a scratch on anything. Great job! The engine comes hermetically sealed in plastic
inside a sturdy crate. The FWF kit came via Fedex in two boxes direct from Vans. It includes the exhaust system, baffles, alternator,
and stuff like that to make your engine complete.
Engine.
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Firewall Forward Kit.
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3/14 to 3/27/10
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35 hrs
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Sec FF1
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Engine Installation
The actual hanging of the engine was easy. It was all the work leading up to it that was hard. I wanted to make sure I had my
firewall finalized and that involved having the EIS holes and grommets in place as well as the manifold pressure port. I also
found that the upper forward fuselage riveting that I deferred had to be completed. Some of the rib rivets were now behind
the brake reservoir. Some others were difficult to reach with just the enging mount in place. With help from Pete, we
managed to get them all. The hours I list for this section include 20 hrs of upper forward fuselage work and 15 hours of FF1 work.
Attaching the mounts to the engine was a bit of a PITA because they are angled forward which makes it difficult to
tighten the forward nuts. The bottoms were worse than the top and I had to grind down an open end wrench to get it to fit to tighten.
Pete and I then hoisted the engine in position and tackled the upper motor mounts first. Then we put a floor jack under the bottom mount and used it
to nudge the engine into position to get the bottom bolt to slip through. The actual attaching of the engine did not take much time at all. Make
sure you have the torque wrench on the nut and not the bolt because in this case it makes a big difference.
Firewall Finalized
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Attaching Fittings
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Motor Mounts
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All Done!
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I did not order any engine hoses with the kit. I chose to have custom hoses made from a certified shop using
Stratoflex teflon hose with integral firesleeve. I ordered them from Precision Hose Technology. They pressure test the hoses
before shipping. Here is what I ordered:
Stratoflex Teflon with Integral Firesleeve Hoses for RV-10
- 124-4J hose, 524-4CR fitting, 15.50" Long (124J001-4CR0154) (Fuel Press. VA-102)
- 124-4J hose, 524-4CR fitting, 27.25" Long (124J001-4CR0272) (Oil Press. VA-133)
- 124-6J hose, 524-6CR fitting, 14.00" Long (124J001-6CR0140) (Fuel Supply VA-138)
- 124-6J hose, 524-6CR and 528-6CR fitting, 25.50" Long (124J002-6CR0254) (Fuel Line VA-189)
- 124-8J hose, 524-8CR fitting, 16.50" Long (124J001-8CR0164) (Oil cooler VA-135)
- 124-8J hose, 524-8CR fitting, 27.00" Long (124J001-8CR0270) (Oil cooler VA-190)
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5/27 to 8/8/10
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85 hrs
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Sec FF2
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Cowel Baffle
I am really enjoying this section of the plans and feel that I have finally escaped fiberglass hell. This section takes you back to pulling blue plastic off of parts, drilling, deburring, bending, machining and priming – the good old days of airplane building.
The building of the cylinder baffles is straight forward per the plans. They are then cut to fit to the engine and top cowl. I had no problem with bracket alignment as reported by Tim Olsen. I did find a crack in bracket CB-1010D at a flange bend and replaced the flanges with 0.060" angle so check for that.
I have been trimming the height of each cylinder baffle to fit the cowl as each one is installed. This is different from the plans which has them all installed and then trimmed. I think my method is better because it isolates the high points and once a particular baffle is cut, it is finished for good.
Cyl 5,6
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Cyl 1,2,3,4
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Left Air Ramp
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Initial Trim
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To fabricate the tension rods you will need a 6-32 die to thread the ends. I used my lathe to turn the rods at a slow speed and held the die holder by hand. When I installed the tension
rods there we interference with the cylinder oil return tubes. I found removing them, holding them in a vice and adding more twist
to them was the best way to obtain clearance.
There was no guidance in the plans for the width of the baffle material so I copied what was done on my Piper Dakota,
1 inch over the metal baffle and 2 inches extended over the baffle. I did not make paper layouts except for the forward air dam which
was the most complicated shape. I mounted the baffle material to the metal baffle on the workbench rather than on the airplane and that
worked out OK.
Alt Blast Air
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Magneto Blast Air
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Tension Rod Interference
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Almost done.
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I aborted a trip to Oshkosh this week due to various reasons but used my already scheduled vacation to make headway on this
section of the plans. The only remaining tasks are to run the spark plug wires, wire the SlickStart and wire the ignition switch. These
should be finished this week and then it is on to FF3 Controls.
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8/15 to 8/27/10
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12 hrs
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Sec FF3
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Control Cables
There are no directions in the kit concerning mounting of the throttle body. After consulting with the Lycoming service manual and looking at
the gaskets provided with the kit, this is what I concluded. From the intake manifold down goes gasket, bracket, gasket, throttle body, two
washers, star washer, then nut. Standard torque applies as there is no special call out in the service manual.
I've gotten really good at installing control cables. Mainly because after I installed them all, I had to remove them to put a nut
and washer on that has to be in place before pass through. Then they were removed and reinstalled for routing around the engine mount. The plans
depict the cables passing above the engine mount which I think pinches them to the engine casing so I moved them to below the engine mount
cross brace. Then
they were removed and installed to add the nut for the firewall eyeballs that I forgot to put on. All in all, they were on and off quite a
few times.
The propeller governor and the throttle control arms needed to be reclocked from the positions installed at the factory. The prop
governor was way out of position and to adjust it you remove safety wire from 6 screws that need to be loosened and then rotate the body to a position
that puts the least stress on the propeller cable. The throttle arm is removed by a single nut and I moved it 3 teeth aft for better throttle control.
The mixture arm did not need any adjustment.
The propeller cable is slightly long and the cockpit control does not completely seat in the full forward position. I'm not
going to worry about it right now until the governor stops are actually adjusted in test flight. The throttle cable that comes with the RV-10 Firewall
Forward Kit is definitely too short. The mixture cable they ship is 51.5" long and the throttle cable is 47.5" long. This makes no sense to me as
both cables start in the same place and one goes to the right side of the throttle body and the other to the left. Van's sells a throttle cable for
the RV-7 that is 50.5" long and I have ordered one to replace that which came with the kit. The RV-7 cable was a much better fit and allowed the cable
to go below the engine mount.
I am also hooking up the air vent control cables for the firewall flapper valves. This is a real PITA with the engine in the way
and I wish I could have done it sooner. The reason I didn't is that I didn't have the cockpit cross brace in place to keep access to the sub-panel
for ease of wiring.
Mixture Control
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Cockpit Controls
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Prop Control
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The predecessor to any action is a thought. |
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date
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hrs
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Sec FF4
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Fuel System
Type something intelligent here.
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date
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hrs
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Sec FF5
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Oil System
Type something intelligent here.
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date
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hrs
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Sec FF6
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Exhaust System
Type something intelligent here.
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3/7 to 8/15/10
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26 hrs
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Sec EIS
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Engine Information System (EIS)
This may sound odd, but I started the Grand Rapids EIS-6000 install by relocating my fuel filter out of the forward tunnel. It all started
because I am going to locate my EIS in a console above the forward tunnel. I don't want to have to go into the tunnel for
a maintenance item so I decided to move the filter to a more accessable place. It only took 8 hours labor, three orders from
aircraft spruce, an order from summit racing, an order from a hose supplier and 53 trips in and out of the airplane to install.
Fuel Filter Relocation

I ran all the wires along cushion clamps at the bottom of the subpanel. Cockpit wiring included OAT, Manifold Pressure,
and Amp Sensor. Running from the cockpit to the engine compartment were fuel pressure, oil temperture and oil pressure sensors. Then
all the EGT and CHT probes for the cylinders. I ran the CHT wires along the bottom of the engine along with the heavy starter and alternator
wires. The EGT's were a little different in that the left side EGT sensor are aft of the exhaust tube and the right side sensors are forward
of the exhaust tube. I ran these wires along with the spark plug wires.
EIS-6000
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Subpanel Wiring
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Right Side
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Left Side
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