Category Archives: Section Ff1 – Engine Installation

Engine, Propeller and Final Preparations

The final installations have begun after many years of component fabrication.

My son and I carried the propeller out of basement storage for transport to the airport.

 

 

 

The unwrapped propeller on the floor was checked, then hung by Terry, Eric and I.  Sorry no photos were taken during that process.  Needless to say, everything went well and the prop looks great.  Easily the best looking thing about the aircraft!

 

 

High temperature RTV was applied to gaps in the baffling and between cylinder heads.  The engine was then filled with 12qts of Aeroshell 100 mineral oil, which will be used for the 25-30hour engine break-in period.

 

 

Final connections of the propeller governor cable and bracket adjustments were made. The air dams with their original heights were installed.  These were later reduced in size after some initial flight tests were performed.

 

 

EGT probes were installed in the exhaust manifold, then bundled with their corresponding CHT probe wires. The alternator belt was tensioned and Safe-T-Wired secure.

 

 

Measuring the leading edge of the wing provided a reference point for the CG calculations.

 

 

 

Intersection fairings for the gear legs were initially fit, then later painted and installed after the TS Flightlines stainless braided brake lines.

 

 

 

Final installation of the oil door with hidden hinge…

 

 

 

 

A 1/16″ ceramic mat was contact cemented in the lower cowl, then covered with Vans aluminum heat shielding.  This combination should prevent the cowl paint from being scorched by the exhaust manifold heat.  Lower cowl pins will be secured against these Adel clamps with tie wraps.

 

 

Final wiring for AeroLED VX landing lights were Solder Sealed, then run through conduit to the wingtips.

 

 

 

AeroLED VX landing and NS position lights/strobes…

 

 

 

 

Decals applied to flaps and doors…

 

 

 

 

Wiring from control sticks to system buses used DB15 connections for easy maintenance or removal.

 

 

 

Ground wires were covered in thick rubber fuel lines to prevent chaffing, then seat pans were installed.

 

 

 

Aerosport auxiliary seat handles were installed for easier operation. Then final inspection and review of everything to date.

 

 

 

All that’s left before first engine start is sit back and wait for good weather outside. It certainly has been a long time coming.  Very excited about this next major milestone.

Firewall Forward (1)

A variety of firewall forward components were added between paint preparation stages.

Here the standard oil plug was replaced with a quick-change unit.  Note the new unit is secured with .032 Safe-T wire tool.

 

 

 

Next the throttle and mixture levers were adjusted and tightened to final configuration. Castle nuts secure the levers and jam nuts immobilize the push-pull cables.

 

 

 

The sensor manifold contains units for oil (150psi), fuel (75psi) and MAP pressure (30psi).  All sensors were sealed with fuel resistant lubricant and torqued to appropriate tightness.  The manifold block was then fastened to the firewall through pre-installed (QB kit) AN3 nutplates.

 

 

The oil cooler unit was installed and feed lines attached from the engine block.  The right photo shows the manifold pressure line teed for a line to the Surefly magneto, which has the ability to adjust ignition timing based on MAP pressures.

 

 

 

A further complaint from many builders is oil leaking from the standard tube/hose/clamp configuration on Lycoming engines from cylinder heads to oil sump. I obtained the flexible SS hose kit from TSflightlines, then added fire sleeve myself prior to installation.  Two notes – the fire sleeve was probably not necessary (overkill on my part), and access to the oil sump fittings was much easier without the exhaust headers being installed.

 

 

This shows a provisional install of the primary alternator drive belt (Gates XL 7360). Final tightening of the belt and torquing the retainer bolts will occur once the propeller has been mounted.

 

 

 

The right photo shows the open ports for CHT probes in the cylinder head, plus the .032″ safety wire approach used to hold the forward cylinder baffle flange. The other photo shows the CHT probe installed with 30 lb-in torque (as per manufacturer instructions). The probes still need to be attached to the GEA24 engine monitoring system.

 

 

Exhaust headers and exhaust pipes with heat muffs were installed. Then 2″ SCAT tubes were connected between the engine baffles and the exhaust muffs.  Finally additional SCAT tubing was run to the heater vent distribution box.

 

 

The exhaust pipes have a flexible ball connection with the rigid exhaust headers. An isolation kit resides between the engine mount and exhaust stack to correctly position the output orientation. It also serves to keep high temperatures off the engine mount.  About 1/2″ – 3/4″ separation was achieved between the exhaust pipes and the lower cowl sections. Later the cowls will be covered with a thin ceramic blanket and reflective aluminum shielding to keep engine heat from discoloring the cowl paint.

Engine Installation (1)

International travel to visit family (first time in two years), supply chain issues and the Thanksgiving holidays have slowed the progress towards mounting the engine.  Many of the jobs performed before the engine was mounted would have been nearly impossible with restricted access from the motor mount and in close proximity to the firewall.  Advice to any builder – attach as many components as possible while the engine is still not mounted! Also pay attention to the sequence of attaching oil filter base, magneto work, tachometer port adjustments, and vacuum pad alternator.

After three years of storage in my garage, it was finally time to move the Lycoming YIO-540-D4A5 engine to the shop for installation.  My sons helped me load and unload the palleted engine onto Tal’s trailer for transport.

 

 

My biggest fear from the whole storage period was corrosion of the camshaft due to moisture exposure over time. This proved not to be the case, as Lycoming had done an excellent job of sealing the engine in the crate.  The dessicant indicators looked just like new when the protective plastic was unsealed!

 

 

One glitch in the process was Lycoming had sent incorrect 19770 mounting brackets (2″diameter hole) packaged inside the plastic seal instead of the correct 70456 (1.25″ diameter) intended for the Dynafocal mount on an RV10.  Because of holiday staffing at the factory, it took over two weeks to receive the proper brackets.  The time was used to connect as many items as possible on the firewall side of the engine.  At right are the fittings to the engine-mounted fuel pump.

 

Additional fittings were installed for the oil cooler lines, manifold pressure and tachometer port. I decided to use a magneto mounted Hall Effect RPM sensor instead of a mechanical tachometer converter simply because of eliminating moving parts where possible.

 

 

Oil thermostat and temperature sensor on the left.  The Airwolf remote oil filter base adapter in the right photo proved difficult to mount.  The lower right bolt required a special crows foot wrench and many 1/6 increment turns to get attached, then torqued properly.

 

 

Safety wiring the oil base adapter was also a challenge – mostly because of my inexperience with the process, but also because of confined geometry.

 

 

 

The remote oil cooler fittings were attached and clocked to point towards the direction of the remote housing.  Next was installing the RPM sensor on the right magneto, then fastening with safety wire.

 

 

 

Originally I wanted to install a 60amp backup generator (BC462-H), but the diameter of the main housing was about 1/8″ too big.  It bumped up against the Airwolf base adapter just enough to prevent a clean insertion of the spline and flat attachment against the pad. The smaller 40amp BC410-H fit perfectly. The space to access the lower left stud is very cramped.

 

 

Tools were modified to achieve some attachments. A normal 9/16″ box wrench was ground to gain access to the back nuts on the engine dog ears, especially the lower ones.  A 7/16″ wrench was cut to 3″ to allow the open ended portion to tighten the backup alternator lower left nut.  This was the most difficult task of all.

 

 

The engine is shown on the hoist ready for attachment.  The Lord J3804-20 isolators were taped into place to facilitate the mount process, which I was able to do by myself. The AN7-26A bolts took a bit to align, but eventually slide into place.  The actual mounting task lasted about one hour.

 

 

Here is the engine installed after so many years of preparation. Quite a satisfying accomplishment.

Other builders have suggested  allowing about a month before the cowling should be fit.  This time allows the rubber isolators and engine to settle into their final configurations. Next up will be baffle configurations and more painting.

 

 

MISCELLANEOUS

Custom brackets were fabricated to hold the aft door open sensors.