I looked at the CAFE reports and at FAR 23.155 (the FAR which
regulates elevator forces in small airplanes). The
regulation requires a minimum of 15 pounds of aft stick force to go from
cruise to maximum G (4.5 G for the 320, per the POH). That would
represent 4.3 pounds per G if the stick force gradients were linear. It
also allows some decrease in stick force gradient (designers usually try to
avoid this) as long as it is not "excessive".
Here are the aft stick forces required to obtain one additional G (i.e.
to go from trimmed one-G flight to 2 Gs) for various airplanes.
1) The Cessna 152 -- 20 pounds of aft stick force
2) An RV-8 -- 11 pounds of aft stick force
3) An RV-6, a Lancair Legacy (N199L), and a Lancair 320 (Fred
Baron's airplane) -- all about 4 pounds of aft stick force
So it appears as though the Lancairs are at or very close to (and maybe
slightly below) the minimum stick force per G for a certified airplane, but
surprisingly similar to an RV-6. The RV-8 and the Cessna 152 are well
above the minimum stick force per G for certified airplanes.
But ...
Never forget that the FARs are intended to keep the lowest common
denominator safe. The "Joe bag of doughnuts" weekend VFR flyer who just
got his license. No offense is meant here. I was Joe for a
long time. (And my favorite is a chocolate glazed -- not chocolate
frosted -- doughnut.) That's why I flew Cessnas early in my flying
career. There is nothing inherently wrong with a more skilled pilot
flying a more maneuverable airplane. Lancairs have long been advertised
as the "Ferrari of the skies" and I'd never give my sixteen year old kid the
keys to my Ferrari (if I had one, that is). But it does suggest that the
safety margins are smaller in the less forgiving Lancair, but also for the
RV-6, which nobody thinks of as dangerous. It's obviously not the whole
story.
However ...
The CAFE guys did not go all the way to 4.5 G -- they stopped at 3.5
G. So the data is not 100% there. We have to extrapolate to
determine if the FAR requirement is met. The Legacy looks pretty
linear (stick force vs G) and appears as though the minimum stick force at
maximum G would be somewhere between 15 and 20 pounds at 4.5 G -- the FAR
requirement therefore appears to be met.
The 320, on the other hand, looks pretty good at
forward CG (extrapolates to 19 - 20 pounds at 4.5 G) but no so much at aft CG,
where the stick force gradient decreases (although not excessively) and it
extrapolates to only about 11 pounds for 4.5 G. Not so good.
That's troublesome, at least to me, and is why I have
strived to make my CG forward. Long engine mount, battery in the engine
compartment, hydraulic pump forward of the instrument panel are the big things
I've done. I also convinced my wife that I bought the higher-power 360
engine on the basis of safety, since it adds weight to the nose of the
airplane. (No, she didn't believe my rationale but agreed to look the
other way, and no, she does not have a sister.)
Take this data as you will. I think we all
agree that the Lancair is not for the beginner pilot, and here we have some
regulatory guidance suggesting why. Experience and training act together
to mitigate the reduced safety margins of a maneuverable airplane, and the
Lancair is no exception.
- Rob
Wolf