Item 405 of Regulation S-K
is not
contained herein, and will not be contained, to the best of Issuer’s knowledge,
in definitive proxy or information statements incorporated by reference in
Part
III of this Form 10-KSB or any amendment to this Form 10-KSB. [ X
]
Indicated
by check mark whether the registrant is a shell company (as defined in Rule
12b-2 of the Exchange Act [ ]
Yes [ X ] No.
The
issuer’s revenues for its most recent fiscal year were $3,403,000.
The
aggregate market value of the voting stock, consisting solely of common stock,
held by non-affiliates of the issuer computed by reference to the closing
price
of such stock was $20,952,000 as of September 18, 2007.
The
number of shares outstanding of the Issuer’s no par value Common Stock as of
October 12, 2007 was 154,848,181.
Documents
Incorporated by Reference
None
Groen
Brothers Aviation, Inc.
Annual
Report on Form 10-KSB
Table
of Contents
|
Part
I
|
Page
No.
|
|
|
Item
1.
|
Description
of Business
|
1
|
|
Item
2.
|
Description
of Property
|
17
|
|
Item
3.
|
Legal
Proceedings
|
17
|
|
Item
4.
|
Submission
of Matters to a Vote of Security Holders
|
18
|
|
Part
II
|
||
|
Item
5.
|
Market
for Common Equity, Related Stockholder Matters and Small Business
Issuer
Purchases of Equity Securities
|
18
|
|
Item
6.
|
Management’s
Discussion and Analysis or Plan of Operation
|
20
|
|
Item
7.
|
Financial
Statements
|
36
|
|
Item
8.
|
Changes
in and Disagreements with Accountants on Accounting and Financial
Disclosure
|
36
|
|
Item
8A
|
Controls
and Procedures
|
36
|
|
Item
8B
|
Other
Information
|
37
|
|
|
||
|
Part
III
|
||
|
Item
9.
|
Directors,
Executive Officers, Promoters and Control Persons; Compliance with
Section
16(a) of the Exchange Act
|
37
|
|
Item
10.
|
Executive
Compensation
|
42
|
|
Item
11.
|
Security
Ownership of Certain Beneficial Owners and Management
|
45
|
|
Item
12.
|
Certain
Relationships and Related Transactions, and Director
Independence
|
46
|
|
Part
IV
|
||
|
Item
13.
|
Exhibits
|
47
|
|
Item
14.
|
Principal
Accountant Fees and Services
|
49
|
|
Signatures
|
50
|
|
PART
I
|
Item
1.
|
Description
of Business
|
Background
Groen
Brothers Aviation, Inc. (the
“Company") or (“GBA”) was originally incorporated in the State of Utah on July
28, 1980 as New Wave Energy. Separately, on March 21, 1986, Sego
Tool, Inc. was incorporated by brothers Jay1 and David Groen in order to enter
the
gyroplane business. On September 18, 1990, the Groen brothers
exchanged 100% of the common stock of Sego Tool, Inc. for 80% of the stock
of
New Wave Energy, an action that was in effect a reverse acquisition of New
Wave
by the owners of Sego Tool. On October 23, 1990, the name of New Wave
Energy was changed to Groen Brothers Aviation, Inc., and under this name,
the
Company became a fully reporting public corporation (stock symbol “GNBA”) to
facilitate the raising of capital and to give minority shareholders the
flexibility of owning publicly traded stock. Hereafter, the "Company"
refers to the small business issuer, Groen Brothers Aviation, Inc. (“GBA”) and
its wholly-owned subsidiaries, Groen Brothers Aviation USA, Inc. (“GBA USA”)
and, from December 2002 through November 2004, American Autogyro, Inc.
(“AAI”). Effective November 1, 2004, the Company merged AAI into GBA
USA. Unless otherwise stated, the financial activities described
herein are those of GBA USA, which is the sole operating entity of the
Company.
The
initial objective of the Company,
primarily through GBA USA, was to develop and market an easy-to-fly and
cost-efficient gyroplane2 that could
compete effectively in the general aviation market. Initially,
personal funds of the Groen brothers were used to build a proof-of-concept
aircraft incorporating a design for the first collective pitch controlled
semi-rigid teetering rotor system for a gyroplane. This first
prototype aircraft flew successfully in 1987, and as a result, the Company
was
able to obtain the support of private investors to begin the development
of its
second prototype gyroplane, the one-seat Hawk 1.
Following
the successful flight of the
Hawk 1 in 1992, the Company proceeded with the design of its third prototype,
the two-seat Hawk H2X, which first flew in February 1997, incorporating a
unique
airfoil design enabling a smooth vertical takeoff at a world record-breaking
density altitude for gyroplanes. At this point, management recognized
that the opportunities for gyroplanes, and for the Company, extended well
beyond
the original general aviation market objective, and had broad potential for
commercial, governmental and military applications. The Company’s
focus was thus reoriented to the design of a larger four-seat gyroplane,
the
Hawk 4, intended for Federal Aviation Administration (“FAA”) certification with
a wide range of potential commercial and public use applications.
Between
1997 and 2003 the Company
designed and manufactured two prototype Hawk 4 gyroplanes, the first with
a
piston engine first flight in 1999 and the second, powered by a Rolls-Royce
gas
turbine, had its first flight in 2000. Based on the superior
operating performance of the aircraft with the gas turbine engine, the Company
proceeded with its FAA certification program based on that
engine. While substantial progress was made in the lengthy and
expensive certification process in the following two years, the deterioration
in
the market for technical stocks, particularly aerospace, after 9/11, constrained
the Company’s funding capabilities. Although the Company had been
able to demonstrate the unique capabilities of the Hawk 4 through its
participation in the official security arrangements for the 2002 Winter
Olympics, the Company suspended its flight testing of the Hawk 4
during the first quarter of fiscal 2003 due to lack of financial
resources. Further development toward commercial certification of the
Hawk 4 has been deferred pending the obtaining of the funding necessary to
complete it.
1
Jay Groen, founder
and Chairman, died in October 2006. David Groen, President and CEO,
took on the additional title and duties of Chairman.
2 Descriptions
of the characteristics of a gyroplane and its derivative, the gyrodyne,
and a
history of the development of these two aircraft types are provided at
the end
of this Background section.
The
Company continues to believe that there is a substantial and potentially
profitable market for the Hawk 4 and its derivatives, both for commercial
and
for so-called “Public Use” applications that do not require commercial
certification. The latter includes federal, state and local agencies
across the nation, particularly Homeland Defense, and also governments of
foreign countries. In this context, the Company has had conversations
with representatives of several countries with respect to setting up one
or more
joint ventures (“JV”) to certificate, manufacture and sell the Hawk series of
gyroplanes. As described below under “Company Products,” considerable
progress has been made with certain Spanish entities in this
regard.
While
recognizing in fiscal year 2003 the infeasibility of continuing at that time
with FAA certification of the Hawk 4, the Company also noted that the general
aviation kit-plane market, which does not require the costly certification
process of the Hawk 4, still lacked the safe, economical, easy-to-fly gyroplane
that the Company originally intended to produce. In the opinion of
management, the kit-plane market could expand significantly as a result
of new less restrictive FAA regulations. Although thousands of
kit-built small gyroplanes have been produced by a variety of manufacturers
over
many years, for the most part, the Company believed these gyroplanes did
not
incorporate a full understanding of gyroplane dynamics and that this contributed
to the fact that fatality statistics of kit gyroplanes did not reflect the
inherent safety of the gyroplane. Because the Company has an
important vested interest in the reputation for safety of gyroplanes in general,
management believed that both to protect the reputation of the gyroplane
and to
take full advantage of an underserved market, the Company should enter this
market.
To
take advantage of these
opportunities through utilization of its very considerable knowledge of
gyroplane dynamics and aerodynamics built up over the years, the Company
established American Autogyro, Inc. (“AAI”) in December
2002. AAI started with the design and manufacture of a
modification kit to enhance flight stability for another manufacturer’s
home-built gyroplane and initiated delivery of such a kit in April
2003. The Company reported its first revenues in the fiscal year
ended June 30, 2003, largely from AAI flight training and the sales of these
modification kits. AAI was then tasked with developing a new small
gyroplane, designed to aerospace standards, that would set a new standard
for
safety in that class of aircraft. The Company’s activities with this aircraft,
later called the ‘SparrowHawk,’ and its derivatives are described under “Company
Products.” Effective November 1, 2004, the Company merged AAI into GBA
USA. GBA USA is continuing the manufacturing, sales and marketing,
and customer support functions of the SparrowHawk.
The
Company also recognized that the
knowledge and experience that it had gained from its work with the Hawk 4
had
made it the preeminent authority on gyroplane technology and that that in
the
post 9/11 defense environment this technology had substantial
military potential. It could serve in a wide variety of roles ranging
from gyroplanes as unmanned air vehicles (“UAV”s) and to gyrodynes as heavy lift
Vertical Take-off and Landing (“VTOL”) transports and as high speed
helicopters. Furthermore, the technology could be further developed
to enable the design of runway independent commercial aircraft.
Starting
in fiscal 2003, the Company made presentations to the U.S. Defense Advanced
Research Projects Agency (“DARPA”) and to other military agencies and also to
public aerospace companies. Emerging from these efforts, on November
7, 2005, the Company announced that DARPA had selected a Company-led team
to
design a proof of concept high-speed, long range, VTOL aircraft. This
modern rotorcraft, named the “Heliplane” by DARPA, is intended as a demonstrator
aircraft for potential use in combat search and rescue roles and is designed
to
fly at a forward speed of 400 mph with a 1,150 mile range, a speed twice
as fast
as a helicopter, to offer the VTOL capability of a helicopter, the fast forward
flight of an airplane, and the safety, simplicity and reliability of a GBA
gyroplane, and is designed to exploit the Company’s gyrodyne
technology. On August 31, 2007, the DARPA contract was modified to
extend the term of Phase One thereunder from a period of 15 to 23 months
and to
increase the total funding in Phase One from $6.4 to $10.4
million. The Company is nearing the end of Phase One of the four
Phase program, and anticipates a Phase Two award by mid fiscal year
2008. There can be no guarantee, however, that Phase Two will be
awarded.
DARPA
is
the central research and development organization for the US Department
of
Defense (“DoD”). It manages and directs select basic and applied
research for DoD, emphasizing technology development projects where payoff
is
high and where success may provide dramatic advances in the capabilities
of this
country’s combat forces. Under its DARPA contract, the Company
retains the rights for both military and commercial use of the technology
emerging from the Heliplane contract and continues to pursue potential
opportunities for this and other of its technologies in the UAV and VTOL
fields. Under this contract, DARPA retains a “paid up for life”
license to the military use of this technology.
Gyroplane
and Gyrodyne Technology
Autorotative
flight was developed in 1919 by Spanish aviator, Juan de la Cierva, with
the
objective of eliminating the risk of stalling inherent in all fixed wing
aircraft when forward speed drops below a critical speed. De la
Cierva named and trademarked his invention as the “autogiro,” which means “self
turning” or “autorotation.” The rotary wing of a gyroplane3, however, powered in flight only
by the
onrushing air, much like a windmill, will not stall because a reduction in
forward speed with the rotor blades in autorotation, will not result in any
sudden loss of lift. As speed decreases, a gyroplane will begin to
descend, right side up and controllable, as its rotating wing continues to
provide lift with the upward flow of air driving the rotor. This
provides the gyroplane with an important inherent safety advantage over a
conventional airplane for activities requiring low altitude and low speed
operations.
For
such
low, slow flying missions, a gyroplane has a similar safety advantage over
a
helicopter. The helicopter obtains its lift from its engine-powered
rotor blades pulling the air downwards, creating an upward force on the rotor,
enabling the helicopter to hover. This, however, also makes the
aircraft unstable, and difficult to fly, since a loss of power to a helicopter
rotor will cause an immediate loss of lift. Only with sufficient
forward speed or altitude will a skilled pilot have sufficient time to put
a
helicopter into autorotation, and thus make a controlled landing while operating
as a gyroplane, although without the benefit of rotor blades optimized for
gyroplane flight. A helicopter is also more mechanically complex than
a gyroplane, requiring additional safety-critical systems, notably a
transmission between engine and main rotor, and a tail rotor with its
transmission needed to offset the torque in the system created by the powering
of the rotor in flight. For these reasons, a gyroplane, not requiring
a tail rotor or complex transmission because its rotor is not driven by its
engine, is inherently safer, simpler, quieter and easier to operate
while much less expensive to maintain than a helicopter.
3 Gyroplane
is an official term now designated by the FAA to describe an aircraft that
gets
its lift from rotor blades and its thrust from an engine-driven propeller
either
in front, the tractor configuration, or at the rear, the pusher
configuration.
The
one material advantage of a
helicopter over a gyroplane is its ability to hover, which is necessary in
some
situations such as sea rescue, sling-load work, or landing in uneven
terrain. For air surveillance and point-to-point flying, the
inability to hover is not a disadvantage. Helicopters at low
altitude, out of ground effect, whenever possible, will avoid hovering because
of the danger inherent in doing so. In a low level surveillance roll,
such as law enforcement, border patrol, traffic control, etc., proper procedure
for all rotorcraft is to circle in a slow orbit, something the Hawk 4 and
SparrowHawk can do efficiently and safely.
In
summary, gyroplanes in flight, being
in constant autorotation, are much safer in low and slow flight than either
airplanes or helicopters. Airplanes flying low and slow risk a
stall/spin crash, which cannot happen in a gyroplane. If power fails
in a gyroplane, the autorotation continues and the aircraft can be guided
softly
to the ground from any altitude. When power fails in a helicopter,
the pilot must convert from powered flight to autorotative flight to keep
the
rotor blades turning. This is an unforgiving process, requiring a
skilled, practiced, accurate, and rapid reaction by the pilot, and it requires
a
minimum altitude and/or airspeed to be performed safely. If a power
failure occurs when a helicopter is operating with insufficient altitude
or
speed, specifically if operating within the “height-velocity” curve shown on
graphs in the helicopter’s flight manual (informally known as the “dead man’s
curve”), the pilot will not be able to avoid a crash landing.
The
gyrodyne is a derivative of the
gyroplane that, as the name implies, has a powered rotor that enables the
gyrodyne to hover and to takeoff and land vertically. Gyrodynes
differ from helicopters in that their rotors are powered, not by the main
engine, but by tipjets normally used only for takeoff, landing and
hovering. In forward flight the tipjets are turned off and the
aircraft operates as a gyroplane with the attendant advantages of safety,
reliability and economy. Since the rotor is not driven mechanically
by torque from the main engine located in the aircraft fuselage, a gyrodyne,
like a gyroplane does not require a tail rotor with its complexity and
maintenance requirements.
Interrupted
History of the Gyroplane
In
the 1920s and 1930s, following
the successful flights of the Spaniard, Juan de la Cierva, the originator
of the
autogiro or gyroplane, Harold Pitcairn and his colleague Walter
Kellett, under license from Cierva, designed and built a series of gyroplanes
in
America, which eventually made vertical takeoffs and landings. Their
efforts resulted in the autogiro concept proving commercially successful
in many
applications during the 1930s and early 1940s. An outstanding example
was its use by the U.S. Postal Service for nearly ten years to deliver mail
from
the roofs of post offices. Thousands of flights carrying mail were
performed by Kellett and Pitcairn gyroplanes flying in Camden, Philadelphia,
Chicago, New Orleans, Washington, D.C., and other cities.
Funding
for development of aircraft for
the private market had collapsed in the years of the Great Depression and
in the
build up toward Word War II, the main source of investment in aviation came
from
the U.S. military. At the time, Igor Sikorsky, who was an important
designer of transport airplanes for the government, recognized the potential
of
a helicopter to the military. After licensing rotor technology from
Pitcairn, he convinced the U.S. military to invest in the helicopter as the
next
logical step in the evolution of rotorcraft, promising more versatility for
military purposes than the gyroplane. This commitment to the
helicopter effectively ended government funding for technical development
of the
gyroplane.
After
World War II, there was a brief and modest resurgence as investors enabled
three
private companies to develop two-seat commercial gyroplanes that were certified
by the FAA: the Umbaugh (later the Air & Space 18A), the Avian (a
Canadian design of that same period that reached FAA certification, but was
never produced), and the McCulloch J-2. In each case, as an expedient
to FAA certification, the designers adapted helicopter rotors and blades,
and
thus did not fully use the gyroplane technology created by their 1930s
predecessors. As a result, none of these civilian gyroplanes
performed well and their companies failed.
More
significantly, during the 1950s, Igor Bensen, who had been a principal in
General Electric’s rotary wing program after World War II, developed a
home-built open-frame gyroplane kit for amateurs, which he called the
“gyrocopter.” Stemming from this initiative, home-built kits, mostly
seating one person, became popular with enthusiasts and more than a dozen
small
manufacturers have produced and sold several thousand kits.
The
technical development of the
helicopter necessary to achieve the potential of helicopter flight was, however,
much more difficult and took far longer than the military
expected. Real utility was not fully attained until the middle of the
Vietnam War, and then only after billions of dollars had been spent developing
turbine-powered helicopters with sufficient payload to move large numbers
of
troops and equipment into and out of the jungle.
While
the
Vietnam War clearly demonstrated the versatility of vertical flight, it also
demonstrated that the helicopter was too expensive, both to purchase and
to
operate, for widespread civilian use. Large helicopter manufacturers
have thus found that the civilian side of helicopter with current production
technology has not been sufficiently profitable to encourage major investment.
Nevertheless, companies such as Boeing and Bell, that have committed large
capital outlays toward helicopter and tilt-rotor technology for military
applications, recognize vertical takeoff and landing has substantial commercial
potential. These companies continue to look for civilian use of that
technology as evidenced by their investment into the development of aircraft
targeted for commercial use, including a civilian tilt-rotor. This
indicates to the Company the correctness of its opinion that with the right
technology there is a substantial civilian market for a VTOL
aircraft.
Company
Products
GBA
Hawk 4 Gyroplane
The
first
pre-production piston-engine version of the four-seat Hawk 4 flew in September
1999, followed by the turbine-engine version in July 20004. This latter aircraft, powered by
a
Rolls-Royce Model 250 420shp turboprop engine, was developed to become the
Company’s first major production aircraft. It incorporates rotor
blades optimized for autorotative flight and the Company’s patented rotor head
with infinitely variable collective pitch control. This enables the
pilot to optimize the rotor blade pitch to the existing conditions and attain
a
smoothly controlled ultra-short ground roll for both take-off and
landing. The turbine engine further contributes to the reliability,
maintainability, payload and low operating cost characteristics of the
aircraft. The Company has flown the Hawk 4 in several hundred
incident-free sorties and hundreds of hours of flight time in its
pre-certification flight-test program.
4
The piston-powered
Hawk 4, although with space for a pilot and four passengers, was limited
by
payload to four occupants. The more powerful turbine version can
carry a pilot and four passengers.
The
Company believes that the safety,
reliability, maneuverability and low operating cost of the Hawk 4 will permit
it
to perform competitively with helicopters (and airplanes) for many missions
requiring low, slow flight, and the absence of a requirement for a runway
for
take-off or landing is a critical advantage. Potential customers
include the following:
|
|
1.
|
Law
enforcement (police, sheriff, border patrol, customs, and drug
interdiction).
|
|
|
2.
|
Public
service agencies (fire patrol, medical transport, wildlife and
land
management).
|
|
|
3.
|
Military
(courier, armed surveillance, VIP transport, forward artillery
control,
ground attack, unmanned aerial
vehicle).
|
|
|
4.
|
Commercial
(oil, gas, and power line patrol and inspection, land survey, aerial
photography, crop spraying, herd management, air taxi service,
corporate
transport, and flight training).
|
|
|
5.
|
Private
(commuting, sport flying,
training).
|
Although
certification of the Hawk 4 has not been completed, it has required significant
capital and will continue to require significant capital to complete
it. In consequence of the adverse affects on the venture capital
market of the spring 2000 decline of the stock market and the September 11,
2001
terrorist attacks, the Company cut back its operations very substantially
in
October 2001, and reoriented its immediate priorities toward offering the
Hawk 4
Gyroplane in its already well-tested form to the US government in roles similar
to those outlined above that would not require commercial
certification.
As
operation in the United States by Federal, State or Local Government agencies
is
exempted from commercial certification requirements under Public Use laws,
each
of these opportunities would give the Company the opportunity to begin receiving
revenues ahead of FAA certification. This would, as a result, reduce
the need for funding to permit the start of production of the Hawk
4. Consistent with this objective, the Company has continued to
present the case for the Hawk 4's utility in this role to members of Congress,
appropriate Federal Agencies, and to State and local agencies across the
nation,
and, importantly, with similar agencies of friendly foreign governments.
In this
context, the Company has had conversations with representatives of several
countries with respect to setting up a joint venture to certificate, manufacture
and sell the Hawk series of gyroplanes.
From
an
early stage of such discussions, it was recognized that the most serious
interest in this project was coming from Spain and that that country presented
an attractive combination of market potential, available skills and funding
sources, and favorable legal and political environment. As a result,
the Company has been diligently seeking to set up a JV through which the
Hawk 4
could be certified under FAA and European regulations. The objective,
in broad terms, is for GBA to provide the JV with its Hawk 4 technology and
oversee and participate in the certification program (on commercial terms),
while the other partners, governmental and industrial, would provide funding,
manufacturing, and other resources. GBA would be a significant
minority shareholder and the recipient of royalties on aircraft
sales.
As
early
as fiscal 2004, after favorable technical recommendations from a Spanish
due
diligence team, the Company believed that such an agreement with a mid-size
Spanish aerospace company as the industrial partner was close at
hand. At a late stage, however, that company decided that in the very
poor economic climate in the aerospace industry at that time, it would cease
investing in aerospace in favor of its more profitable non-aerospace
activities.
In
fiscal
2007, however, the Company obtained renewed interest from the government
of
Aragon, an Autonomous Community within Spain, and in December 2006 entered
into
a Memorandum of Understanding with Aragon to set up such a JV. Since
that time, the investment advisors for Aragon have been undertaking due
diligence on the project, presenting the project to potential industrial
partners and undertaking preliminary discussions with regard to funding with
the
Spanish government authorities. In early fiscal year 2008,
representatives of GBA and Aragon met with representatives of CDTI5, the investment arm of the central
Spanish
government’s Ministry of Industry, Tourism and Commerce. The Company
has been advised that the results of this meeting were favorable and that
CDTI
has asked Aragon and other potential partners to enter into the formal process
for funding requests. While the Company can give no assurance that
the JV will be established, or that if established it will be successful,
the
Company believes that the potential investors in the JV have the capability
to
fund such a project and, in the opinion of management, that they are likely
to
have access to a significant market for the Hawk 4. The Company
believes that the proposed JV offers a viable prospect for the Company to
profit
from its considerable investment in the Hawk 4 and gyroplane
technology.
SparrowHawk
Gyroplane and Derivatives
Starting
in fiscal 2003, AAI undertook the task of designing its own two-seat piston
engine powered gyroplane that it named the SparrowHawk. This
aircraft, incorporating safety features based on aerospace standards, offers
performance, stability and comfort standards that AAI believes are superior
to
any competitive kit-built gyroplane in its class. AAI finalized the
design of the SparrowHawk in the fiscal year ended June 30, 2004, and began
deliveries of kits for the home built market in the third quarter of that
fiscal
year. In addition, the Company developed and continues to sell, modification
kits designed to improve in-flight stability and safety for another
manufacturer’s kit gyroplane.
In
December 2005, the Company announced the introduction of its improved
SparrowHawk model, the SparrowHawk II. SparrowHawk II offered added
comfort and robustness, and reduced the time and effort, needed by the customer
to build the aircraft. The Company has continued to design
improvements for the SparrowHawk II during fiscal 2007 and in the first
half of fiscal 2008 will be introducing new version called the SparrowHawk
Quick Build. As the name implies, the primary objective for the
‘Quick Build’ is a significant further reduction of time and effort on the part
of the purchaser in building the aircraft, while maintaining conformity with
FAA
regulations. Careful attention has been paid to existing customer
input and to the needs of potential customers. Many of the latter
have the financial resources to purchase an aircraft, but have limited time
to
complete the build process. Through a thorough assessment of the
build process, changes in the design manufacture and product delivery, the
time
to assemble the kit by a typical purchaser is expected to be in the order
of 300
hours, cutting build time in half. Deliveries of the Quick Build kit
begin in October 2007. All future aircraft will be manufactured to
the SparrowHawk QB standard.
The
Company began deliveries of SparrowHawk kits during the third quarter of
its
fiscal year ended June 30, 2004, recording initial revenues from this aircraft
in the fourth quarter of fiscal year 2004. During the years ended
June 30, 2007 and 2006, the Company reported revenues from the sale of
SparrowHawk kits and parts of $562,000 and $667,000. The Company has
received advance payments from dealers and customers on SparrowHawk gyroplane
kit orders during the past several quarters, which have been recorded as
deferred revenue. Additional revenues have also been received from
the sale of modification kits, flight training and from contract manufacturing;
however, these revenue sources have not been, and are not projected to be,
significant to the Company.
During
fiscal year 2005, the FAA announced the establishment of a new category
of
aircraft, called Light Sport Aircraft (LSA), which permits manufacturers
to
produce and sell small, non-complex, fully assembled aircraft without the
necessity of fulfilling the requirements for an FAA
“Type-Certificate.” While helicopters have been excluded from the LSA
category as being too complex, gyroplanes are included, but in view of
the
limited experience of the FAA with gyroplanes, initially in a sub-category
defined as Experimental Light Sport Aircraft (E-LSA). The E-LSA
category for gyroplanes will end in 2008. The Company has petitioned
the FAA for a “deviation” from the regulation that would permit it to produce
and sell complete aircraft that meet the LSA standards, with the expectation
that the experience gained and demonstrated will justify full LSA authorization
for gyroplanes. The Experimental Aircraft Association (EAA) filed
with the FAA a “letter in support” of the Company’s petition for
deviation.
Management
believes a large market is likely to arise within the United States as
a result
of this FAA action. The Company believes that its technology will be
well suited to this market and be capable of conforming to the new
regulations. The Company has therefore initiated the design of a new
light gyroplane, called the SportHawk that would meet the LSA
regulations.
As
previously noted, the Company
identified an important untapped potential market for the Hawk 4 as a patrol
and
surveillance aircraft, both in the United States and
overseas. It has now become evident that as a derivative of its
SportHawk design, a smaller, professionally designed aircraft with low
purchase
and operating costs that can operate “off airport” and is easy to maintain and
fly, would also have important applications for patrol
surveillance. This is particularly the case in parts of the world
where skilled helicopter pilots and maintenance personnel are not readily
available. For this reason, the Company believes the SparrowHawk or
its derivatives sold as a fully assembled aircraft could be expected to
be
popular with law enforcement agencies around the world.
The
Company’s discussions with the Office of Domestic Preparedness (“ODP”) on
gyroplane usage have emphasized the merits of the SparrowHawk as a readily
available, ultra-low cost air surveillance vehicle. Similarly,
discussions have been held with the Department of Defense (“DOD”) for the use of
gyroplanes for mine and bomb detection to counter those threats in Iraq
and
elsewhere, emphasizing again its low cost and early availability in relation
to
other solutions. Sales representatives have also been appointed in
Korea and India to present the capabilities of small gyroplanes to government
agencies in those countries, and the Company has held meetings with several
agencies in China in relation to the use of the SparrowHawk in
China.
Consistent
with the design advances that are being incorporated into the SportHawk
for the
civilian market, and with the knowledge gained by these discussions with
potential customers, as mentioned above, the Company has initiated design
of a
corresponding SportHawk derivative directed toward government markets,
which it
is naming the ShadowHawk Gyroplane.
As
a result of the new FAA regulations
and the opportunities for government acquisition of fully assembled aircraft,
the SportHawk and ShadowHawk can be sold as complete aircraft, rather than
as
kits like the SparrowHawk. The Company believes that the production
of complete aircraft will enable it to maintain quality control over the
finished product, eliminate the delay between delivery and in-service dates,
and
overall enable the product and Company to be more effectively
branded.
Unmanned
Gyroplane Contract
The
relative mechanical simplicity and aerodynamic stability of the gyroplane
and
gyrodyne in comparison to a helicopter or other vertical lift aircraft allows
both aircraft to be potential candidates for unmanned as well as manned
applications. GBA has been approached separately by two aerospace
companies with proposals to assist them in the design of unmanned gyroplanes
for
two different US military applications.
The
Company has been engaged as a subcontractor to one of these companies
for a project called PAS (Precision Airdrop System) that is projected to produce
an unmanned gyroplane rotorcraft for military supply missions, missions
now
served with much less accuracy by parachutes. GBA has been engaged by
this major aerospace company to design, and ultimately manufacture, the
rotor
system and fuselage using their guidance system. A large-scale model
designed and built by GBA was successfully flown on a military test range
in
July of 2007, demonstrating the effectiveness of this technology. The
project is expected to proceed to full-scale demonstrator development beginning
in 2008. If successful, it is possible that the Company could receive
a significant order for full-scale production for these aircraft as early
as
2009.
The
Company’s DARPA “Heliplane” Gyrodyne Contract
The
Company’s technology is fully scalable and readily adaptable to the gyroplane’s
derivative form, the gyrodyne. As detailed earlier, the gyrodyne is a
rotary wing aircraft that uses “tipjets” for short duration power permitting
pure vertical takeoff and landing, providing the capability to
hover. During the en-route portion of the flight the tipjets are
turned off and the gyrodyne flies as a gyroplane in
autorotation. Such an aircraft is capable of both lifting substantial
payloads in gyrodyne mode and covering substantial range as a
gyroplane. The British Fairey Rotodyne aircraft demonstrated the
technical validity of this concept in the 1960's. With the
application of modern technology developed by the Company, the concept
is ready
to be turned into a highly utilitarian aircraft platform, with many diverse
applications.
In
recognition of these capabilities,
over the past three years the Company has been assessing military applications
of its gyrodyne technology to conceptual designs for a vertical takeoff
aircraft
with payload and range capabilities that no aerospace manufacturer has
been able
to offer and that would contribute to the military and security needs of
the
United States Government. As a consequence, the Company has been able
to respond to requests for proposals from government agencies and military
commands. These submissions have ranged from small UAV gyroplanes to
large vertical takeoff and landing (“VTOL”) freighters. Applications
have also been made in partnership with either a major aerospace company
or an
academic institution with preeminent aerospace credentials.
On
November 7, 2005, the Company
announced that the U.S. Defense Advanced Research Projects Agency (“DARPA”) had
selected a Company-led team to design a proof of concept high-speed, long
range
VTOL aircraft. This modern rotorcraft, named the “Heliplane” by
DARPA, is intended for use in combat search and rescue roles. It will
offer the VTOL capability of a helicopter, the fast forward flight of an
airplane, and the safety, simplicity and reliability of a GBA gyroplane and
is
designed to exploit the Company’s gyrodyne technology. DARPA is the
central research and development organization for the US Department of Defense
(DoD). It manages and directs select basic and applied research for
DoD, emphasizing technology development projects where payoff is high and
where
success may provide dramatic advances in the capabilities of this country’s
combat forces.
Phase
One
of this potential multi-year $55 million four-phase Heliplane program began
with
a 15-month $6.4 million award to develop the preliminary design and perform
key
technology demonstrations. On September 19, 2007, the DARPA contract
was modified, increasing the contract award from $6.4 million to $10.4
million,
and extending the term of Phase One from 15 to 23 months. Substantial
portions of Phase One payments are paid by the Company to subcontractors
and
consultants hired by the Company. Payments under this contract are
conditional upon the Company attaining several milestone objectives during
the
course of Phase One of the contract.
The
Company recognizes revenue on this contract as each defined milestone is
completed and the requisite meetings are held and technical data submitted
and
accepted by DARPA. At that time, DARPA will instruct the Company to
submit an invoice for payment for the respective milestone at the amounts
specified in the contract. Through December 31, 2006,
contract-related expenses incurred by the Company for each milestone of
the
contract, including its own labor, travel, supplies and other costs, and
the
costs of subcontractors and consultants, were deferred and expensed to
cost of
sales as the contract revenue for the milestone was recognized. The
Company is currently experiencing a negative profit margin on the DARPA
contract; therefore, all contract-related costs and expenses incurred subsequent
to December 31, 2006 have been expensed as incurred. Through June 30,
2007, the Company completed the first four milestones and substantially
all of
the fifth milestone of Phase One of the DARPA contract, and recognized
revenues
totaling $4,790,000, $2,350,000 recognized in the fiscal year ended June
30,
2006 and $2,440,000 recognized in the current fiscal year ended June 30,
2007.
The
Heliplane gyrodyne represents the
possible model for the next generation rotor wing aircraft, meeting economy
and
performance goals not considered achievable by any other type of VTOL
aircraft. As the Company’s gyrodyne technology is scalable to much
larger aircraft, it has potential applications for both heavy lift, high
speed
VTOL military aircraft and for runway independent commercial
airliners. The Company has been actively engaged in discussions with
government agencies and potential aerospace strategic partners in this
country
with respect to military and commercial gyrodyne and gyroplane applications,
and
in Europe, India, and China with respect to commercial gyroplane
applications.
Future
Company Gyrodyne Aircraft
The
Heliplane gyrodyne represents the
possible model for the next generation rotor wing aircraft, meeting economy
and
performance goals not considered achievable by any other type of VTOL
aircraft. As the Company’s gyrodyne technology is scalable to much
larger aircraft, it has potential applications for both heavy lift, high
speed
VTOL military aircraft. The Company has been actively engaged in discussions
with government agencies and potential aerospace strategic partners in this
country with respect to military applications, both manned and
unmanned.
The
gyrodyne technology developed for the Heliplane also has direct application
to
the design of short-range vertical take off and landing (“VTOL”) commercial
airliners that are runway independent. Growth in the economy can
produce heavy demand for aircraft that do not require the use of increasingly
congested runways and are not limited by air traffic control constraints,
and
the Company anticipates an opportunity to develop such an
aircraft. By using the airframe of an existing type-certificated
production airplane and adding the Company’s rotor system, gyrodyne airliners
can be delivered for substantially less investment and in less time than
would
normally be required to bring a new airliner to market. The Company’s
longer-range plans have identified opportunities for large (18-60 seat)
gyrodynes to provide commercial passenger service in short and medium-range
markets.
The
proposals that the Company has
presented, or participated in presenting, have been well received and helped
generate credibility for the value of the Company’s technology among key
segments of the aerospace industry. The Company will continue to seek
opportunities to obtain government research and development contracts for
use of
its technology in both military and civilian agency fields where it believes
that it can offer meaningful advantages in performance or cost over competing
technologies.
Market
Management
believes that it is in the national interest that the Company’s unique gyroplane
technology is developed. The terrorist actions of September 11, 2001
and later, have triggered important new opportunities to use the Company’s
technology in new counter-terrorism markets. The new circumstance of
our country, as well as other countries, is requiring sharply increased levels
of vigilance by many branches of government to protect critical national
assets
against terrorist attack. Public use regulations would permit the
Hawk 4 to be utilized as a highly efficient, safe, and inexpensive means
of
providing needed surveillance by government agencies for such roles. These
include border patrol as well as protection of pipelines, nuclear power plants
and key transportation infrastructures for which the Hawk 4 is particularly
well
suited, performing such missions far more effectively, and often at far lower
cost, than other air or ground vehicles.
The
attempted shooting down of an
Israeli commercial aircraft approaching Mombassa airport in Kenya by Al Qaeda
terrorists using surface-to-air “SAM” man-portable missiles has made the
protection of commercial aircraft from such missile attacks an extremely
important issue. Several proposals have been made to fit military
missile defense systems to commercial aircraft, but research undertaken under
Homeland Defense contracts has indicated that these approaches are extremely
expensive, and would take years to develop and
install. Significantly, however, the Kenya incident precisely fits
the scenario presented by the Company as a serious risk to the Salt Lake
City
2002 Winter Olympics, which resulted in the Hawk 4 demonstrating its capacity
to
guard against such an attack. The subsequent arrest in New York of
individuals attempting to import Russian SAM missiles into the United States
heightened concerns about this threat.
The
Company asserts that the most
practical and effective deterrent to missile attacks remains intensive
patrolling of airport approach and departure paths by safe Hawk 4 and/or
SparrowHawk Gyroplanes, which could perform this role more economically and
effectively than fixed-wing airplanes or helicopters. The Company has
therefore approached principal government agencies, including the Transportation
Security Administration (TSA) of the Department of Homeland Security, the
Office
of Domestic Preparedness (ODP) of the Department of Justice (DOJ), as well
as
representatives of airport authorities, to present the case for both the
Hawk 4
and the SparrowHawk in this role.
The
Company is also seeking orders from foreign governments with intensive border
patrol needs. The small, ultra low cost SparrowHawk, mechanically
very simple, although sophisticated in design, is well suited for areas where
substantial coverage is needed, but resources and skills are very
limited. The easy maintainability of the Hawk 4 also enables it to
excel in operating where infrastructure is relatively undeveloped and where
the
cost and complexity of acquiring and operating helicopters in adequate numbers
is infeasible. Given the potential for sales in foreign countries,
the Company has evaluated the efficiency of assembling Hawk 4 and SparrowHawk
Gyroplanes in strategic overseas locations, and has had discussions with
different foreign entities on possible sites.
Government
Regulation
The
nature of aviation products has resulted in their manufacture being regulated
by
governments for public safety, national defense, and economic and/or political
purposes. Such regulations vary widely by country, by product type
and by usage. The Company’s products and intended products are
principally impacted by United States laws and regulations, but also by
requirements in its export markets. As its products can be used for
private, commercial, public agency or military purposes, their sale and
operation are governed by regulations appropriate to each
category. Developmental flight testing of the Company’s aircraft is
carried out under exemption rules covering experimental aircraft. The
following section reviews the principal regulations applicable to each category
of the Company’s activities in the United States.
GBA
Hawk 4 Series Gyroplanes
Commercial
or Private Use: FAA certification is the process by
which the United States government ensures that aircraft sold into the US
civil
market meet appropriate standards for all civil users. FAA
certification is not required by military aircraft and by many aircraft in
“Public Use,” roles operated by Federal, State or local
agencies. Civil aircraft operated outside the United States are
regulated by the authorities of those countries and may be required to obtain
additional certification. The analysis and testing leading to a US
certificate is, however, currently acceptable in most foreign countries as
the
basis for granting certification in those countries.
FAA
certification has two related components. The first, Aircraft Type
Certification assesses the integrity of the design and associated
engineering through analysis and testing of components and complete aircraft
to
insure that the aircraft can achieve its performance standards
safely. The second, Aircraft Production Certification,
assesses the manufacturing organization to insure that its processes and
procedures will result in the production of aircraft that fully conform to
the
standards of the aircraft type certificate.
The
regulations pertaining to aircraft certification are contained in Title 14
of
the United States Code, the “Federal Aviation Regulations”
(FAR). Aircraft in the category of the Company’s Hawk 4 aircraft, to
be operated commercially or privately, must receive a Type Certificate under
Part 27 (normal category rotorcraft weighing less than 6,000 lbs) of the
FAR,
while the Production Certificate must be obtained under Part 21 of the
FAR.
Public
Use: The Company’s efforts to sell its Hawk 4 to government
agencies in the United States is based on the specific exemption for operation
of aircraft used by government agencies as authorized by Federal Public Law
103-411, which defines what is a “public aircraft operation.” This
law permits training and flights in “public aircraft” for performance of the
following governmental functions:
Flights
in response to fire fighting;
Flights
in response to search and rescue;
Flights
in response to law enforcement activities; and
Flights
in support of aeronautical research or biological or geological resource
management.
In
this
context, ''public aircraft'' means an aircraft:
(i)
used
only for the United States Government;
(ii)
owned by the United States Government and operated by any person for purposes
related to crew training, equipment development, or demonstration;
or
(iii)
owned and operated (except for commercial purposes), or exclusively leased
for
at least 90 continuous days, by a government (except the United States
Government), including a State, the District of Columbia, or a territory
or
possession of the United States, or political subdivision of that
government;
It
does
not include a government-owned aircraft:
(i)
transporting property for commercial purposes; or
(ii)
transporting passengers other than –
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|
(I)
|
transporting
(for other than commercial purposes) crewmembers or other persons
aboard
the aircraft whose presence is required to perform, or is associated
with
the performance of, a governmental function such as firefighting,
search
and rescue, law enforcement, aeronautical research, or biological
or
geological resource management; or
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|
|
(II)
|
transporting
(for other than commercial purposes) persons aboard the aircraft
if the
aircraft is operated by the Armed Forces or an intelligence agency
of the
United States.
|
An
aircraft described in the preceding sentence shall, notwithstanding any
limitation relating to use of the aircraft for commercial purposes, be
considered to be a public aircraft for the purposes of this part without
regard
to whether the aircraft is operated by a unit of government on behalf of
another
unit of government, pursuant to a cost reimbursement agreement between such
units of government, if the unit of government on whose behalf the operation
is
conducted certifies to the Administrator of the Federal Aviation Administration
that the operation was necessary to respond to a significant and imminent
threat
to life or property (including natural resources) and that no service by
a
private operator was reasonably available to meet the threat.
Military
Use: Aircraft sold to the US military are not required to
meet FAA regulations, but must conform to military specifications that serve
a
similar purpose. The Company has not attempted to sell its Hawk 4 to
the United States Armed Forces and is thus not familiar with the detailed
requirements that would have to be met. It believes, however, that
should a military application for the Hawk 4 be needed by the US Armed Forces,
a
version of the Hawk 4 could be designed to meet military
specifications.
GBA
SparrowHawk Gyroplanes
Homebuilt
Kit Aircraft: While it might be possible to design and
manufacture a gyroplane in the size and performance class of the SparrowHawk
to
meet the FAA FAR Parts 21 and 27 regulations that the Hawk 4 is designed
to
meet, the Company has not chosen to do this. The Company’s entry to
the SparrowHawk market has been through the alternative path of producing
homebuilt aircraft kits for which there is an established
market. Homebuilt aircraft kits are permitted by the FAA under its
FAR Part 21 regulations governing the certification and operation of
amateur-built aircraft. Such kits, however, require that the majority
portion of the kit be built by an amateur (the “51% rule”), limiting the
manufacturer’s portion to 49%.
Light
Sport Aircraft: The FAA issued new regulations in
2004 defining a new classification of aircraft called Light Sport Aircraft
(“LSA”) and regulated in two categories, namely Special Light Sport Aircraft
(“SLSA”) and Experimental Light Sport Aircraft (“E-LSA”). These
regulations define an LSA by specific detailed limits upon size, weight,
speed,
and complexity. The LSA regulations specifically exclude helicopters
and other aircraft types considered to be overly complex for the LSA
classification. Such aircraft are not limited by the 51% rule, with
the manufacturer permitted to fully build the aircraft.
Aircraft
conforming to the SLSA category, must in addition to the basic LSA limitations,
be designed and manufactured to certain defined standards that include
requirements such as, for example, the need for engines that are either
FAA-certified or have parts traceability.
Unlike
helicopters, gyroplanes are not specifically excluded from the LSA
classification, but in view of the FAA’s relative unfamiliarity with the type,
are eligible for a subcategory defined as Experimental or
E-LSA. E-LSA aircraft must meet the LSA size, weight and other limits
and can be sold as fully assembled aircraft, but are not required to meet
the
SLSA manufacturing standards. Manufacture of E-LSA aircraft is,
however, limited to the period ending January 31, 2008.
Public
Use Aircraft: The Company is offering SparrowHawk aircraft fully
built to US government agencies for Public Use, for which the regulations
and
limitations are covered by the same regulation, Public Law 103-411, that
governs
Public use for the Hawk 4, as described above.
Research
and Development Aircraft Flown under Government Contract
Any
aircraft developed and flown under
government contracts that the Company may be granted, such as the DARPA
Heliplane contract, will be tested and flown under FAA regulations governing
experimental aircraft.
Distribution
and Marketing
It
has
been the Company’s plan to market the Hawk 4 through a dealer network, both in
the United States and the rest of the world. A GBA Authorized Dealer network
with 14 United States dealers, 3 International dealers and over 60 national
sales representatives was established and these dealers placed firm orders
with
deposits for 145 Hawk 4 gyroplanes. As of June 30, 2007, dealer
deposits totaled $2,145,000, which amount has been reported as a long-term
liability in the accompanying consolidated financial statements. The
deposit guarantees a delivery sequence number and represents a percentage
of the
total estimated purchase price. The Company has also issued common
stock to dealers as partial consideration for the delay in the certification
of
the Hawk 4 Gyroplane. These costs have been c