Monday, August 31, 2009
Sunday, August 30, 2009
Saturday, August 29, 2009
Planning ahead
This is to get an idea of the cost, which is obviously fairly scary.
But also determining the choices I'll need to make for the electrical components and any items I might need to factor in during the earlier parts of construction, such as wiring runs.
Right now my plan is to have a dual electrical system, and avoid any vacuum driven instruments, and not install a vacuum pump at all.
As for panel layout, I am currently looking at a variation on the 'standard six-pack'.
The standard six pack is how instruments are typically laid out in production aircraft and is how most instrument rated pilots learn to fly on the gauges.
It has six primary flight instruments in 2 rows, going from top left to right, we would have:
- Air speed Indicator ( aka the 'ASI', not powered )
- Artificial horizon - typically vacuum powered.
- Altimeter ( not powered )
- Turn Coordinator - typically electrically driven, this is used to determine 'standard rate' turns for Instrument ( IFR ) flying and also shows 'the ball' which shows if the aircraft is flying straight or 'skidding' or 'slipping'.
- Directional Gyro (DG) - This shows direction, like a compass, but stabilized with a gyroscope since a normal compass has lots of idiosyncracies ( spelling? ) when actually changing direction or under accelleration forces, this is typically vacuum powered.
- And finally on the lower right, the vertical speed indicator which shows the rate of climb or descent ( feet per minute here in the US ), not a powered instrument.
- The artificial horizon is replaced by an Electronic Flight Information System (EFIS), which may also include engine monitoring capability, the one i am currently investigating is the Advanced Flight Systems AF-3400.
This instrument will, on it's own, give me everything all of the other instruments listed above give, plus more, and as such will be placed top center of my instrument panel. - The DG is replaced with a combined HSI/DG.
A HSI, is a Horizontal Situation Indicator, it shows gyro stabilized direction plus the needles for the navigation radios VORs, Localizers and Glideslopes, and GPS courses.
Also investigating 2-axis auto pilot.
This full setup will give me plenty of redundancy both in terms of flight instruments and navigation aids, while still fitting into the limited space afforded by the Tandem ( as opposed to side-by-side ) seating in the RV-8.
Powerplant wise, I am looking at a 180 HP Lycoming IO-360 (Fuel Injected), with Unison electronic ignition, coupled to an MTV15 2-blade composite hydraulic variable pitch prop.
I prefer 2 blades over 3 for efficiency cross country, Composite in case I have a prop strike as it is less likely to cause major engine damage in that situation, and hydraulic variable pitch for efficiency and aerobatic capability, also planning for inverted oil and fuel.
Clearly, all of this is costing many $, so compromises are to come i am sure, but now i have a good idea of what i am looking for.
Friday, August 28, 2009
Last of the rudder stiffeners
Thursday, August 27, 2009
Drilling rudder skeleton
Tuesday, August 25, 2009
Monday, August 24, 2009
Sunday, August 23, 2009
Fabricating spacer and strips for the rudder
Utilized the bandsaw for the rudder bottom attach strips, which need to be fabricated.
The rudder has 2 parts which need to be fabricated from 2024-T3 aluminum, a spacer r-717 and these 2 strips.
Saturday, August 22, 2009
Rudder Stiffeners & new tools
Then continued the rudder stiffener trimming, using the snips, as it now seems like the easiest way.
Then cleco-d the stiffeners to the rudder.
Interesting to see how the trimming and the interlocking nature of the stiffeners means that the rudder skin can be closed very tightly and still have the stiffeners almost to the narrowest point.
Just ordered the last 2 needed stiffeners from Vans tonight.
Friday, August 21, 2009
Rudder Stiffener results
Well, after last nights difficulties with the rudder stiffeners, I consulted the good people on the RV-List at matronics.
The response was excellent, balanced between "buy a bandsaw and never look back" and "I was able to do it just fine with the snips using the appropriate left or right handed snips - Appropriately".
So tonight I found that by applying some patience, I was able to trim the stiffeners just fine with the snips and then use the scotchbrite wheel on the bench grinder to de-burr and soften the edges.
Still some more to do, and I need to get some extras from Vans.
Thursday, August 20, 2009
Rudder Stiffener woes
Wednesday, August 19, 2009
Tuesday, August 18, 2009
VS rear spar - final rivet
Monday, August 17, 2009
Rudder stiffeners
First step, cut the R815 rudder stiffeners to size, and, of course, &$@!?# it up, need to order more rudder stiffeners from vans tomorrow.
Sunday, August 16, 2009
Finished the skin rivets on the VS
Saturday, August 15, 2009
Friday, August 14, 2009
VS Spars and Ribs Rivetted
Thursday, August 13, 2009
Further rivets in the VS Spar
Wednesday, August 12, 2009
Riveting the VS spar
Sunday, August 9, 2009
Finished priming the VS spars and ribs
The primer has not set fully yet, so I am not proceeding to fully cleco it together for riveting tonight.
Dimpling and priming the VS
Friday, August 7, 2009
Dimpling the VS skin
Only hit my thumb with the hammer a few times, reminds me of the joke -"When I nod my head - you hit it."
Thursday, August 6, 2009
VS front spar countersinking and dimpling
Then machine countersunk the holes at the bottom - front facing holes in the front spar reinforcement bar and dimpled the corresponding holes in the front spar itself.
Wednesday, August 5, 2009
Drilled VS skin and disassembled
Made some marks with a Sharpie pen so that it can be re-assembled in the right orientation.
Also - need to consider lighting on the vertical stabilizer, as I will need to make allowances for wiring it up before i close the rear spar onto the VS.
Tuesday, August 4, 2009
VS initial assembly
Then attached the skin for the vertical stabilizer with clecos, ready to final size drill the skin holes ( to #40 )
Monday, August 3, 2009
Vertical Stabilizer spars and ribs
Fluted and edge-finished the ribs, and cleco-ed ribs and spar together for the vertical stabilizer.
Edge-finishing is to round-off the sharp edges left by the machines which press the parts at the factory.
Fluting is to straighten the ribs as they come out of the factory slightly bowed, again due to how they are stamped.
Sunday, August 2, 2009
Finished the Horizontal Stabilizer
Finished the first major sub-component of my new airplane.
On to the vertical stabilizer tomorrow night.
The blue tape over some of the holes in the top of the horizontal stabilizer is to remind me not to rivet them, they are attachment points for a fairing to be attached in final assembly.