Have procrastinated a little getting this post written but the good news
is, the first condition inspection has revealed no significant issues with the
DOG Aviation RV-12. However, I did run across a couple of speed bumps that
created delays. One time consuming task was looking up the torque values for
all the hardware on the airplane. I’m not referring to the standard torque
values for AN3 or AN4 bolts which builders have well memorized by the time the
airplane is completed … no, I’m talking about the myriad of parts that have
unique torques such as Matco brake hardware, the Rotax engine hardware,
propeller bolts, etc. Plus, there is the time spent sifting through the
documentation for additional information such as tire pressures, stabilator
cable tensions, nose gear breakout forces, etc.
Tip for builders: My suggestion is while assembling the RV-12 each time you
run across a nonstandard torque value, breakout force, gap measurement or
pressure reading document it on a list that can later be tailored to suit your
needs via a word processor or spreadsheet. Having a list that shows torque
values, clearances, breakout forces, spark plug gaps, etc. will make the first
condition inspection on your RV-12 or any kit aircraft move along so much
faster and all inspections thereafter. In fact, I would also suggest taking
things one step further by making a complete list or spreadsheet of inspection
due dates for items such as testing of the transponder and the required
quarterly ELT test … in addition, include expiration/replacement dates for
items such as the batteries in the ACK E-04 (I did record the main battery for
the ELT in the avionics log but did not record the battery dates for the
associated remote panel indicator or audio alert indicator) along with dates
for firewall forward items such as fuel pump replacement, rubber hoses, brake
fluid, coolant, etc. Wish I had thought about creating those lists during the
construction process. Moving forward, assembling a meaningful list related to
inspection items along with perhaps keeping a white board in the hangar will
make future inspections much less time consuming. I spotted a white board in
the hangar across from me and thought it was a good idea so took a photo of it
to use as a guideline for making my own white board.
Photo of a whiteboard spotted in a hangar across from me. There seems to
be merit in creating a white board for keeping a visual on major inspection due
dates and time related items such as oil changes.
Decided to begin the condition inspection at the nose of the aircraft
and move aft. Van’s documentation suggests checking the torque of the propeller
hub after the first six hours … I went beyond that knowing the annual was
nearing. For the benefit of non-aviation readers of the Blog, the two Sensenish
propeller blades are captured between two half hubs … the one called the mount
hub is bolted to a mounting flange attached to the propeller shaft coming out
of the gear reduction unit on the front of the Rotax 912ULS engine and the
other is called a clamp hub which captures the two propeller blades and is
bolted to the mount hub. Unfortunately, to check the mounting bolt torque on
the mount hub, it requires removing the clamp hub and both propeller blades. It
would be nice if the bolt heads sat in a recess or up against a stop so the
bolts would not rotate allowing the bolt torque to be checked without removing
the blades … but sadly, that is not the case so the clamp hub and blades need
to be removed to gain access to the mount hub bolt heads. As it turns out, the
nuts on two of the six bolts moved slightly when the torque was checked … the
required torque is 18-20 foot pounds so I was shooting for 19.5 lbs. to allow
for a little drag in the locknut.
These are the nuts and bolts that attach the mount hub onto the mounting
flange. Unfortunately, to properly check the bolt torque it requires the
removal of clamp hub and propeller blades to gain access to the heads of the
bolts.
Avid readers of the DOG Aviation blog may recall when the propeller
blades were first installed they were pitched wrong and after posting photos of
the work session, I received an Email from a fellow builder who caught the
error (thanks again Nick). This required loosening the clamp hub bolts a couple
of extra times while readjusting the blades. Unfortunately, Nord-Lock washers
self-destruct a little each time a bolt is loosened, so they are only effective
for a few cycles because the capturing ridges on the washers get worn down
easily. Knowing this, I figured the Nord-Lock washers should be replaced since
they had been exercised a few times already… so prior to beginning the
condition inspection, I purchased new Nord-Lock washers at a local bolt & nut
supply. Well, much to my surprise, when about to use the new Nord-Lock washers,
I discovered they were a much smaller outer diameter than the Nord-Lock washers
supplied by Sensenich with the propeller kit. This resulted in a parts delay
because I needed to order new Nord-Lock washers directly from Sensenich. So my
tip to fellow RV-12 builders is to plan ahead and have some spare Nord-Lock
washers on hand when planning to remove the prop mounting bolts … just make
sure the Nord-Lock washers are the larger diameter ones.
On the left is a used Nord-Lock washer removed from the propeller hub
and split in half to reveal the worn ridges on the washer. On the right is a
new Nord-Lock washer split in half so the locking ridges can be seen. Also note the outside diameter of the
standard Nord-Lock washer on the right that was procured locally has a much
smaller outside diameter than the Nord-Lock washers supplied by Sensenich on
the left.
The new Nord-Lock washers received from Sensenich were placed in the
digital caliper and measured in at 21/32". So fellow builders attempting
to locally source Nord-Lock washers for the propeller bolts, make sure you
purchase washers that have an outside diameter of 21/32" … otherwise you
will need to place an order through Sensenich.
The Nord-Lock washers that Sensenich supplies for the RV-12 propeller
utilizes a washer with an outside dimeter of 21/32" which is a larger OD
than typical for a 5/16" diameter bolt.
After replacing the Nord-Lock washers that hold the clamp hub in place,
the propeller blades were pitched with a digital level to 71.4° using the
method in Van’s plans along with the Van’s pitch tool. Got the pitch even
better than the first time around … now both blades are within .05° of one another.
For those not familiar with the process of adjusting the RV-12’s propeller
blades, the following is a link to a post that covers that procedure:
Link to the procedure for adjusting the Sensenich propeller blade pitch on the RV-12.
About the only item I found that NEEDED correcting was the temperature
thermostat for the Reiff heating system … it had popped off the oil tank.
Frankly, I was not surprised to see this because when installing the Reiff
heating system I began by scuffing up the aluminum on the bottom of the engine
and cleaning with Acetone then mixing the epoxy and attaching the heating pad
to the bottom of the engine. Then without thinking I slathered the thermostat
for the oil tank with epoxy and affixed it to the side of the oil tank …. only
to realize, darn (not the word I used at the time) I had not yet scuffed the
oil tank and cleaned it with Acetone before applying the epoxy. Figured it was
too late to do much of anything, so the thermostat would either stick, or not …
which ended up being the case. To correct the problem all the old epoxy was cut
off the thermostat and the oil tank with a razor and both the oil tank and
thermostat were roughed up with sandpaper and a jewelers file. Reiff suggests
using JB Weld as a substitute for the epoxy they supply with the heater kit, so
that is what was used for the repair. The JB Weld was applied in two
applications. The first application was to the bottom and sides of the thermostat
so a piece of safety wire could be placed around the oil tank and tightened to
keep the thermostat pressed against the oil tank while the epoxy cured. After
the epoxy cured, the safety wire was removed and a second application of epoxy
was used to cover the top and sides of thermostat. Hopefully this will no
longer be an issue … but moving forward, this will be an area I will be keeping
an eye on especially now that winter is coming and I’ll be using the heater.
My finger is pointing to the oil tank thermostat for the Rieff heating system that was epoxied back onto
the oil tank using JB Weld epoxy. This time both the thermostat and oil tank received a good scuffing and
cleaning with Acetone … hopefully the thermostat it will stay affixed to the
oil tank.