AviationWeek.com/awst AVIATION WEEK & SPACE TECHNOLOGY/JANUARY 15-FEBRUARY 1, 2015 33
Graham Warwick Washington
Weighty Matter
Terrafugia wants FAA to waive limits so its
flying car can still be called a light sport aircraft
D
esigning a flying car capable
of meeting both aviation and
highway safety requirements
is proving a weightier challenge than
imagined by startup Terrafugia when
it launched development of the Transi-
tion roadable aircraft in 2006.
The company has petitioned the FAA
for a waiver of the gross-weight and stall-
speed limits on the light sport aircraft
(LSA) category, arguing the design’s au-
tomotive crashworthiness features and
ability to land and drive through bad
weather will increase safety.
Terrafugia is requesting permission
for the two-seat Transition to have a
takeoff gross weight of 1,800 lb. and
stall speed of 54 kt., yet still be treat-
ed as an LSA that can be self-certified
by the manufacturer against industry
standards accepted by the FAA.
LSA rules limit landplanes to a max-
imum weight of 1,320 lb. and stall speed
of 45 kt. In 2010, to accommodate
road-safety features such as airbags,
Terrafugia successfully petitioned the
FAA to certify the Transition with a
gross weight of 1,430 lb., the limit for
seaplane LSAs.
“We now have quite a bit more infor-
mation about what it will actually take
to meet the level of safety that we be-
lieve is appropriate for this type of ve-
hicle, and it simply takes more weight
than we were previously allowed,” says
CEO Carl Dietrich.
“The Transition was designed to be
very simple to operate, in the spirit of
the LSA rule,” he says. “In my view, it
would be silly and unfortunate to allow
an arbitrary weight number associated
with a category to inhibit meaningful
improvements in safety and techno-
logical advancement.”
Established in 2005 in a bid to re-
vitalize general aviation by lowering
the cost of aircraft ownership and
pilot training, the LSA rule defines a
simple, low-performance aircraft that
the manufacturer can self-certify at a
significantly lower cost than for FAA
Part 23 certification.
Terrafugia states that even at a high-
er weight, the Transition “still belongs
in the LSA category. It is easy to fly,
maintains a comfortable stall margin
and benign stall characteristics, and
embodies the original intent of LSA
as a means to encourage innovation
and growth in the aviation industry.”
Since 2010, the FAA has granted
Icon Aircraft an exemption to LSA
rules to increase the maximum take-
of weight of its amphibious Icon A5
by 250 lb. to 1,680 lb. to accommodate,
among other features, a spin-resistant
airframe design.
“In 2010 the FAA did not want to set
a precedent beyond 1,430 lb. They have
now broken that rule and set a new
precedent with Icon at 1,680 lb.,” says
Dietrich. “In my view, our case is even
more compelling than Icon’s in terms
of improving safety and the clear con-
nection between the safety improve-
ments and weight requirements.
“I believe it would be a mistake
for the FAA to prevent this product
from coming to market as an LSA.
With LSA treatment, we will be able
to bring our safety improvements to
more people faster, so this exemption
request should be in line with the high-
level mission of the FAA.”
The Transition is being designed
to meet federal safety standards for
multi-purpose passenger vehicles, and
as a result “will set the highest bar for
occupant safety in general aviation,”
Terrafugia states in its petition. But
occupant-protection features add 121 lb.
A ballistic recovery parachute for im-
proved flight safety adds 36 lb., while the
aircraft’s roadability features, including
the ground drive system, add 266 lb.
“The primary driver for the additional
weight is the incorporation of the sys-
tems and structure necessary for safe
road use in general and crashworthiness
in particular,” says the petition. Meet-
ing frontal-impact standards requires a
safety cage that adds 44 lb. to the com-
posite structure, and a crumple zone and
bumpers that add 25 lb. Airbags, knee
bolsters, head-impact protection, self-
tensioning and load-limiting seatbelts,
and other features together add 52 lb.
Explaining the request to increase
stall speed, the petition states: “Due
to the dimensional constraints of road
use... it is not feasible to simply in-
crease wing area proportionally to the
increased weight. Based on a spectrum
of pilot experience, Terrafugia believes
the necessary stall speed increase will
not afect the underlying safety intent
of an easy-to-fly LSA.” c
TECHNOLOGY
NASA
The need to fold the wing for
road driving means Terrafugia
cannot increase the Transition’s
wingspan to maintain stall
speed at an increased weight.