At
AirVenture 99 in Oshkosh, Wisconsin, the Ullmann Aircraft Company
announced the development of its new Panther kitplane. The Panther
is an all metal, four-place, high-wing, high performance (200 knot
cruise), fixed gear aircraft. The Panther is designed from the
ground up to satisfy the FAA’s FAR 23 certification standard in the
normal category (positive 3.8 g to negative 1.52 g)
The design team members are all aviation industry
veterans from companies such as Cessna, Lear, Raytheon Aircraft, and
Boeing. Collectively the team has 151 years of experience in the
design and testing of certificated aircraft. Their experience
combined with the known properties of all-metal construction, has
produced a unique aircraft that combines power, comfort, and
flexibility.
For a serious cross-country
airplane, speed is an essential attribute. The Panther is designed
for speed. You will be able to cruise to your destination in
car-like comfort at 200 knots (230 mph) in the new high-wing,
four-place, high-performance Panther.
In addition to its speed, the Panther has been designed to meet
FAA Part 23 certification standards by our team of professional
engineers. Kits will be delivered only after we have conducted
structural and flight testing of the Panther. The Panther uses a
space-frame welded steel truss to surround the passenger
compartment and provide additional strength and safety.
The Panther has been designed to
have superb handling characteristics (Class 1 on the Cooper-Harper
Scale – the highest possible rating). This prediction has been
confirmed by extensive wind tunnel testing at the Walter Beech
Memorial Wind Tunnel at Wichita State University.
All Panther kits have been designed
to take full advantage of the FAA’s 51% rule and minimize the
assembly labour. The steel space-frame truss and the engine mount
arrive completely welded and finished. The airframe components will
be preformed, the skin panels will be precut, and all will be pilot
drilled in precision factory jigs. The wing leading edge (which
includes the integral fuel tank) comes completely assembled.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
TCM IO-520-L or
IO-550-L
x
25 ft, 9 ins
9
ft, 7 ins
34
ft, 2 ins
x
x
x
1,010 lbs.
3,050 lbs.
x
800 nm
|
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
x
x
x
200 KTAS
x
x |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
58 KTAS
x |
All specifications are based on manufacturer's
calculation
|