Vans Aircraft RV-12 Airplane Build: Newest RV-12 in the World (at least for a short time)

With the RV-12 completed, I've been working with Gary Brown a DAR in Independence Oregon to obtain a airworthiness inspection and certification. Today was the day for the inspection. After looking it the airplane, Builder's Log, Maintenance Logbooks and covering the Operating limitations and other paperwork I was awarded an Airworthiness Certificate!



Gary had a few suggestions that make sense. First Van's Aircraft is working on a split baggage compartment bulkhead. He said get it or build it, as it will allow inspection of the tailcone without removing the fuel tank. I'm planning to do this at the first conditional inspection.

In the picture below you can see the split floor panel that Van's offers that I installed previously.



Second tie-wrap the fuel pressure sensor to the radiator hose (as pictured below.) This will help reduce vibration on the sensor.



With the inspection out of the way next is to get myself ready for flying the RV-12. For this I have scheduled time with Mike Seager

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 16) Elevator trim Indicator, Run Up and Finish Up

Reference: RV-12 Acceptance Procedures

Working on the RV-12 today I notice there was no indication for the Elevator trim. And no mention of calibrating it in the plans. Looking at the Dynon guide there was a brief statement about calibrating it.



So following the setup wizard in the hardware calibration menu I set the calibration up but didn't set a take off mark as I have no idea were it will need to go.





First conditioned the brake pads per Matco brake instruction. Then came the time to warm the engine up and do a full power run up at operating temperature. My max rpm was 5100 rpm with the prop set at 71.4 degrees. This is too high and out of range. So I added 0.3 degree of coarseness to the pitch and reran it. This time I had 5010 rpm which is in the acceptable range. During this process I also went out to the compass rose and calibrated the magnetometer.

After removing the cowl and inspecting the engine I found some wear on the cowl from an exhaust spring. So I rotated the spring 180 degrees and put some RTV on it. Also put a aluminum foil patch over the wear. If this doesn't solve the problem I will need to reform a deeper impression in the fiberglass.









Removed the gascolator and cleaned the screen. Then Safety wired it back in place.





Next came the mapping of the fuel gauge. Sorry no pictures. Basically I pumped the system dry and then added 2 gallon at a time and told the EFIS system of each addition. Then at 4 gallons I also checked that the "NO FLY" indicator was in the correct spot in the mechanic fuel gauge. After that continue adding fuel up to 16 gallons were the electric gauge won't read any fuller. Followed the guide lines in the RV-12 Acceptance Procedures as it is required to roll the plane up on blocks and then off at certain time in the process.

8/13/15: Closing thought: I received word from Gary Brown the FAA accepted my paperwork and we scheduled for the inspection. Also I am schedule at the end of the month for transition training with Mike Seager. This project is finally winding down after 4 and a half years.

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 15) Final EAA inspection

Reference: Page 11-09, 33-02, 35-05, 37-10, 42N-20

In preparation for the Final EAA technical inspection I installed all of the inspection panels, cowl and the interior. Thus all of the reference listed above. Also I didn't take many pictures today.



First came the weighing of the airplane. Wait for it... total 763.8 pounds. Heavier than I hoped. Next Ernie showed me how to sync the carburetors and set the idle. Running it through the various RPM upto 3000 rpm. Below is the tool he used to sync the carbs and hose hookup.





Last but not least we safety wired the throttle nuts.



After all of this Ernie left me to finish the measuring for the weight and balance.



Finished up the measurements and calculation and submitted the paperwork to Gary Brown who is a DAR here in Oregon to get my DAR inspection. I'm not going to go into detail of how to complete the paperwork because I think this varies a little from region to region. As the old saying goes "your milage may vary". So talk it through with your DAR or FAA examiner.

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 14) First Engine Start!

Reference: RV-12 Production Acceptance Procedures, Rotax SI-912-018

Today is a big day for the RV-12 airplane. I have been working through the Production Acceptance Procedures step by step. I'm now up to the point of starting the engine for the first time.

Couple of highlights. I used Dex Cool mixed 50/50 with distilled water for the cooling system and added 3.2 liters of AeroShell Oil Sport Plus 4 to the oil (it came with the engine.) Then purged the oil system per SI-912-018. This requires building (or buying) some oil lines and fittings to pressurize the oil reservoir with up to 15 psi of air and rotating the prop until oil pressure registers on the EFIS system.



Next came the big moment, with extinguishers on hand we started the engine. Oil pressure came right up. But there was a problem. Why is the battery not charging?



After some searching the problem was a loss wire on the regulator pictured below.



With that fixed the charging system worked just fine. I have started going through all of the Service Bulletins to ensure everything is done and documented in the maintenance records. I am also continuing with the Production Acceptance Checklist. Next time will cover the final technical inspection and weight and balance.

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 13) Closing Forward Fuselage

Reference: Page 45A-10, 42C-16, 34-11; 4.0 hours

Now that the RV-12 is at the airport I can adjust the radio volume for the EFIS as it requires a radio signal and ATIS is ideal for this.



This completes page 45C-10.

Reference: Page 42C-16

Next came the testing and final install of the ELT. To complete the G switch test I fabricated my own test plug using a 15 pin female D-Sub and a jumper wire. And of course the test have to be done 5 minutes after the hour. Sorry I didn't photograph the test plug.



Then came the install of the Forward fuselage.



Reference: page 34-11

Now with the forward fuselage on I can ensure the canopy handle works prperly with just one hand. And after some adjustment it works fine.

This completes this entry for the RV-12 final assembly.

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 12) Moving to Airport

Today was the big move of the RV-12 airplane from the warehouse to the airport. First I moved the wings using my Tacoma truck and the rack pictured below. It sits on the rack with the spar pointing forward into the truck cabin.



Next I rented a 17 foot U Haul truck to move the fuselage.The two outside ramps are the same length as the truck ramp.



Then with a little help it was time to install the wings.



That's it for todays work.

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 11) New Vernier Throttle

Reference: Notifications 14/09/24 and 14/09/25; 3.5 hours

Had a nice visit with Ken Scott at Van's Aircraft yesterday about flying the RV-12 and he suggested going to the new vernier throttle. The reasoning is this, on final approach the RV-12 need to be slown down, however the old throttle would creep forward and increase the engine rpm especially with the older Rotax throttle springs. After flying 50 plus hours with the old throttle he was surprised at what a difference the new vernier throttle made.

So today I'm removing the old throttle and installing the new setup which includes the new carburetor springs.



Out with the old.,br/>


Builder's note: The new throttle is a larger diameter than the old one. And the hole needs to be moved downward to allow the nut the backside of the control panel to turn freely and not interfere with the instrument panel floor. So I used a Dremel to enlarge the hole and lower it off center. Ithink the new panels have this clearance issue solved.



Of course the firewall needs to be resealed with fire proofing.



And the extra cable cut off.



New springs installed and the throttle cables rigged per page 50-05 and 50-06.



The new throttle cable comes pre-labeled. So that's one less thing to worry about. This complete this entry and installation of Notification 14/09/24 and 14/09/25 and page 50-05 and 50-06. The feel of the new vernier throttle cable is great!

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 10) SB 15-03-05

Reference: Pages 50-05, 50-06; 5.0 hours

Today's work on the RV-12 involved installing the air cleaners and installing the new carburetor floats for Service Bulletin 15-03-05. My RV-12 engine was effect by this due to the serial number range of the carburetors. I ordered the floats back in March, April and they finally arrived this week.



Builder's note: Note lack of marks on old floats in picture above. New floats and gaskets are pictured below.



Reference: Builder's note: I wanted to hid the exposed fiberglass that shows through the inside of the canopy. SO I purchased black contact paper from Home Depot, cut patterns and the cover the area to mach the curve of the layup.









This concludes this entry for working on the RV-12 airplane.

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 9) Old Notification Completion

Reference: Notifications dated 8/31/12 and 2/11/13; 1.5 hours

I've been going through and checking the documentation of all the service bulletin and notifications for the RV-12 and preparing logbook entries for these. In my search, I came across two older notifications dealing with the electrical harness. Both apply to my RV-12 airplane because of the date these harnesses were received.

UPDATE: There is a GOTCHA for Notification 2/11/13. Even though my harness fit the dates of the Notification, so I changed the wires, the harness was correct before the change. Swapping the wires caused the problem outlined in the notification. So check the light operation first before changing the wiring!

Reference: Notification dated 8/31/12

This notification requires swapping two of the wires in the WH-00045 or WH-00026 harness. It depends on which Skyview harness system you have. Mine is the older conversion from the D-180 EFIS to the Skyview so it involves the WH-00026.

In light of the problem I had with the other wiring notification I called Van's to find out if there was any test that would show if these two wires needed changing or not. I was told if the wires are backwards then the Skyveiw will give a 4/8 error message.





Reference: Notification dated 2/11/13

This notification dealt with to wires that needed to be changed in the lighting harness WH-00031. Again my airplane was included because the harness was received before 2/11/13. The two wire are extracted using a extractor tool and swapped.

As noted above: I had to reverse the wires back to the original configuration as my wiring harness was wired correctly to start with.



This completes the work and rework for these two notifications on the RV-12 airplane.

Vans Aircraft RV-12 Airplane Build: Final Assembly (part 8)

Reference: Interior Instructions 3.5 hours

My wife really liked the look of the full interior kit for the RV-12 airplane so today will show the steps of how I did it. If you are wondering it to total kit (not including the seats) adds ~12 pound to the airplane.







Builder' note: the picture below show how I had to cut the back panel to accommodate to newer fuel vent system.































This completes the install of the RV-12's interior. Of course most, if not all, of it will come back out for the DAR inspection.