LASER AEROBATICS AKRO Model Z
If you wish to purchase a set of drawings
email for the address
to send the attached contract and a
bank draft for US$500.
The drawings offered for sale describe the construction of one of
the best aerobatic aircraft in the world. Already five aircraft
have been built in Australia and over eleven completed worldwide,
with many more under active construction.
The first of these aircraft was completed in late 1981 and was
flown in the 1982 and 1984 World Aerobatic Championships

The AKRO Z is a mid wing aerobatic monoplane whose ancestry can
be traced back to other homebuilt monoplanes developed in the USA.
The first AKRO Z was VH-AUZ, which flew in December 1981, after
much design and engineering work. The wing spars are of spruce
construction while the ribs are spruce and ply and wing skin is
plywood. The fuselage is welded steel tubing covered with sheet
metal aluminium forward of the cockpit and fabric aft. The tail
feathers are also built of steel tubing and are covered with
fabric. The aircraft has great structural strength and is
intended for advanced aerobatics. The fixed landing gear is of
tail wheel configuration. Construction should only be undertaken
by experience builders and may take approximately 3500 manhours.
The "LASER" Name and the AKRO Z.
The name "Laser" has become a generic term
for this family of aircraft, although it strictly relates to Leo
Loudenslager's original re-work of the Stephens Akro. A number of
aircraft constructed from modified Stephens plans, our own plans
or specialist manufacturers own plans have at times been called
"Lasers", "Laser 200's" and "Laser Z's".
Due to the parallel but independent development of these various
designs our aircraft is officially known as the Akro Z to avoid
any confusion with other aircraft within the "Laser"
family.
The Aircraft Design Background
The AKRO Z can trace its general evolution in
concept back to the Stephens
Akro, designed by Ed Allenbaugh and built by Clayton Stephens.
Using a Formula one air racer layout of monoplane & mid-wing
was a significant departure from the biplane layout immortalised
by Curtis Pitts, but the Stephens Akro's most interesting
departure from aerobatic standards was the use of airfoil NACA
23012, with asymmetric lift. The success of the Stephens Akro led
to great interest in the general layout, with the design being
extended by people such as Leo Loudenslager custom building their
own aircraft for world championship competition - the Laser. This
lead to a series of "homebuilt" aircraft which were
collectively known and often erroneously known as "Lasers",
although no formal design relationship actually existed between
them, other than the "Stephens" inspiration. One such
"Laser" aircraft was designed by Ray Parker & Gerry
Zimmerman, who redesigned the wing using the NACA 21012 aerofoil
section and by increased main spar depth at the root section.
This wing has no dihedral, zero incidence, and no sweepback at
the quarter chord line, providing excellent performance in
outside manoeuvres. The most instantly recognisable difference
between the Stevens Akro & the "Laser" series is
the bubble canopy versus raised rear decking. The Laser
Aerobatics AKRO Z is itself based on the Zimmerman/Parker design
concept, with the wing and structure developed by Ray & Gerry
being formalised by David Pilkington, twice Australian Advanced
Aerobatic Champion and holder of Bachelor & Master degrees in
Aeronautical Engineering. David further developed the design with
a number of local modifications to improve aerobatic flight
performance and ruggedness. The aircraft also differs
significantly from the Stephens Akro in the fuselage and tail
structure as well as having an elevator control system similar to
that used in the Pitts.

This aircraft was approved during the 1980's by the Australian
Civil Aviation Safety Authority - Amateur Built Aircraft Approval
Number 54 - and these plans are the only source for home builders
to build a "Laser" type aircraft. The AKRO Z has been
built and used by a number of successful international champion
pilots including Frank Fry of Australia and Mark Jefferies of the
UK.
The current CASA approval in Australia refers to drawings
initially submitted in the late 1980s. The current drawing set
incorporates later improvements and may be used as the basis for
an Experimental aircraft.
The package also contains: a Flight Manual & Operations
Manual, a set of photos of one airplane under construction, a
comprehensive set of over 40 drawings covering all aspects of the
aircraft construction other than the instrument panel, engine
cowl and fairings, as these tend to be hand fitted by the
constructor to ensure snug fit to the airframe, or to match
appropriate panel cutout to instruments & layout selected.

| Length | 19'5" | 5.92 m | Fuel Capacity | 20 US Gallons | 77 litres | |
| Wing Span | 24'4" | 7.42m | Engine | Lycoming | 200 hp | |
| Wing Area | 98.0 ft2 | 9.1m2 | Max. Speed | 155 kts | 286 kph | |
| Wing Loading | 14.29 lbs/ft2 | 69.80 kg/m2 | Stall Speed | 56 kts | 104 kph | |
| Aspect Ratio | 6.1 | Rate of Climb | 2,500 ft/min | 762 m/min | ||
| Gross Weight | 1400 Ibs | 635 kg | Aerobatic Weight | 1298 Ibs | 589 kg | |
| Useful Load | 430 lbs | 149 kg | Empty Weight | 970 lbs | 440 kg | |
| Takeoff Distance | 1,000 ft | 305 m | Landing Distance | 1,500 ft | 457 m | |
| Range | 308 nm | 572 km |