The recent comments regarding
the Small v. Big tail draw my attention to the fact that on a recent visit to
the wide brown land up over, LML lister Angier was privileged to see two
examples of large tail Lancair's. One belonging to me (didn’t build it), and the
other being the example quoted in the attached letter to Rob Wolf’s post “A
look at Lancair 360 Handling Qualities”. Now
owned by another lister here.
The only Lancair’s I have handled in the
air were all large tail versions, with one exception, that being N5ZQ in the
States. Bill will undoubtedly recall that I was – let’s say “ropey”
– to say the least. While I am prepared to accept that is my lack of
skill, and I reflect long and hard on this after each flight I have made over
forty odd years, I do come to the conclusion that there is a distinct
improvement in stability and handling of the Lancair with the large tail.
Over the past few months –almost
a year actually, there has been a slow but steady approach to the improvement
of training of, and understanding by, Lancair pilots here up over, brought on by the
historical global accident rate, and highlighted by two fatals within six days
in Australia, 20 months ago.
A Lancair Pilot Group has been
established, and having been asked to be involved, I have sought advice from
various sources regarding their views on the matter of Lancair training and opinions on
handling.
In this process I have had email
discussions with the test pilot who undertook some of the test flying on the Lancair which resulted in the recommendation
to enlarge the tail.
I quote from the email I
received from one him on 20 September 2007:
“…….When
the first example (a 320 I think?) was evaluated, it was found to have 2 major
design problems/defects. First the aft CG condition was unrealistic (in
excess of 30% MAC), and the horizontal stabiliser was too small. Combined
these resulted in neutral or negative stick free longitudinal stability.
Also manoeuvre stability (stick force per G) was at best measured in ounces per
G. Standard comment from then owners was"I like it like that because
it has fighter like feel." These pilots had obviously never flown a
fighter, at least not one built since about 1920, which all have positive long
stab, and minimum stick forces of about 7 lb/G.
CASA insisted
(under the good/bad old 101.28 rule) that stability be improved. I think
the aft CG limit was moved forward (not sure how much) and bigger tails were
required. The bigger tails (2 local REG 35 solutions by Graham Swannel
and Dave Simons) produced adequate solutions, but the practicalities of keeping
CG forward remained. The Lancair
235/230/360 models also have negative lateral sideslip stability; with
a low wing and no dihedral the predominant rolling force in a sideslip is
due to the rudder. This characteristic is rarely seen, and is disturbing
when deliberately sideslipping during cross wind approaches. For IFR
approval, CASA insisted this be fixed and a rudder/aileron interconnect was
developed (I think by Dave Simons) which produced apparent lateral sideslip
stability and hence predictable handling qualities in sideslip.
The kit
manufacturer was not amused by these criticisms of his creation and refused to
have anything to do with them. However, shortly after CASA came the
heavy, Aviation Consumer magazine in the US conducted some flight tests on the Lancair, and another fast plastic of similar size and shape, and
concluded their findings with some not very flattering remarks along the lines
of ......... how dare you foist on the unsuspecting public expensive machines
with such bad design features........ - I was very pleased to hear this as it
vindicated the position taken by CASA and other professional Test Pilots who
had flown the machines.
Very quickly the
manufacturer of kit X came out with a bigger tail (about 50% bigger!), and some
advice on how to fix the CG problem. Lancair eventually did the same……”
CASA is the current name for the
old CAA here up over. Under a Labour Government, the name changes every few
weeks to create jobs. Although the quote uses the current term CASA, at the
time of testing the authority was called CAA.
Hopefully this will help, if not
cause the usual broad-ranging hackles raising.
Cheers,
Dom Crain
VH-CZJ
Melbourne
Not Florida