1. LIMITED LIABILITY COMPANY ОSА SINGLE-ENGINE AMPHIBIAN AIRCRAFT
VOSTOKAVIAPROM
ОSА SINGLE-ENGINE AMPHIBIAN AIRCRAFT
PROGRAM

2. I. GENERAL AVIATION (GA) MARKET ANALYSIS

3. In 2005, the General Aviation (GA) World fleet numbered units of aircraft (A/C). Today the fleet’s main share is in the U.S. – units of A/C, about 70% of the World’s total GA.*
*Source: “General Aviation Manufacturing Association (GAMA), 2005”, “Analysis and forecast: Amphibian aircraft Be-103 in the Chinese market (AVIC II)”

4. Development of the U.S.’ GA and its structure by A/C types is illustrative of the GA World fleet in general.
Dynamic of the GA in the USA and its diversification by type of A/C is typical for the whole world’s GA fleet.
Structure of the GA fleet in the U.S. ( units) by type of A/C (units, % of the total) in 2005*.
*Source: “General Aviation Statistic Databook, General Aviation Manufacturing Association (GAMA), 2005”

5. Diversification by type of A/C (240.070 un.) in the USA
Structure of the U.S.’ GA fleet ( units) by A/C types (units, % of the total) based on forecast for 2016
Diversification by type of A/C ( un.) in the USA
(un., % of the total number) based on forecast for *
Projected increase in the GA fleet in the U.S. in the period from 2005 until 2016 inclusively reaches 9.2%, units of A/C.
Applying a 9% upward trend to the existing GA World fleet ( units of A/C in 2005), we will have units of A/C in the GA World fleet in 2016.
In 2005 the GA World fleet of piston-engine aircraft made 73% of the total GA fleet in the U.S. According to forecasts, in 2016 the total share of the GA fleet in the U.S. will make 69%.
Applying this percentage ratio to the GA World fleet, we will receive the following:
Estimated number of the GA World fleet of piston-engine aircraft in 2005 is units of A/C.
Estimate of the GA World fleet of piston-engine aircraft in 2016 is units of A/C.
In 2005, the GA World fleet of naval aircraft accounted for units of A/C (10% of the GA World fleet of piston engine aircraft). According to the forecast, keeping the proportion (10%), in 2016 it can total units of A/C.

6. The GA World fleet of seaplanes, 2005 (23 000 units of A/C)
Other
hydroplanes
20 700
90%
Amphibian
aircraft
2 300
10%
The GA World fleet of seaplanes, 2005 ( units of A/C)
The World fleet of hydroplanes is divided into four sections, according to the aircraft type:
1. Amphibian;
2. Boat planes;
3. Float-type landplanes;
4. Landing craft & и aerodynamic
ground-effect craft.
The World fleet of amphibian aircraft reaches 9-10% of the World fleet of seaplanes and numbered unites of A/C in 2005, according to the estimate.
Forecast of the GA World fleet of seaplanes in 2016 ( units of A/C)
Provided the existing rate of 10% to the GA World fleet of seaplanes, the amphibian world fleet can total 2400 units of A/C in 2016.

7. Range with 3 passengers onboard, km Price per aircraft, USD thous.
Significant part of the GA World fleet of amphibian aircraft has a substantial working lifespan. Aircraft that were developed years ago continue to operate today. Their share in the GA amphibian fleet accounts for 50% (1150 units of A/C). Therefore, we can expect their gradual phase-out in the coming few years, which will generate a need for replenishment of this part of the fleet. Demand of the GA World fleet in 2006 – 2016 accordingly can make about 1200 – 1300 NEW AMPHIBIAN AIRCRAFT.
Forecast of GA amphibian aircraft’s market structure (1300 units of A/C) in
Single-engine aircraft account for 90% of the GA World fleet and, compared to two-engine aircraft, have lower price and operating costs as well as higher load ratio.
Production of the OSA amphibian will allow Vostokaviaprom LLC to enter the world amphibian aircraft market and occupy not less than 30% of it.
In , JSC KnAAPO had designed, constructed and tested the experimental amphibian aircraft SA-20P that became the OSA amphibian aircraft’s prototype.
Others
350
27%
OSA
260
20%
Be-103
130
10%
Centavr
105 8%
Seawind
455
35%
1000
Range with 3 passengers onboard, km
660
670
Useful load, kg
480
Motor petrol
Usable fuel
100LL
800
Price per aircraft, USD thous.
1,250
OSA
Specification
Be-103

8. CHINA’S GA MARKET DEMAND FOR NEW A/C, ACCORDING TO AREAS OF USE
Due to China’s rapid economic growth, Chinese GA market is dictating requirements that differ from global trends.
CHINA’S GA MARKET DEMAND FOR NEW A/C, ACCORDING TO AREAS OF USE
(8000 A/C, in )*
Considering multiple operating features of the light amphibian aircraft Be-103 and OSA, demand for these aircraft in China by the year 2020 can reach up to 250 units of A/C with the use in the following areas:
● Air tourism – 50 units; ● Maritime patrolling – 50 units;
● Military application – 50 units; ● Aerial survey – 20 units; ● Business – 20 units;
● Private use – 30 units; ● Training – 30 units.
*Source: “Analysis and forecast: amphibian aircraft Be-103 in the Chinese market (AVIC II)”

9. II. EXPERIMENTAL AMPHIBIAN AIRCRAFT
AS-20P

15. Power plant with engine М-14, new nacelle, feeder tank and pylon
PRINCIPAL DIFFERENCE OF THE SINGLE-ENGINE AMPHIBIAN AIRCRAFT SA-20P DESIGN FROM BE-103
Power plant with engine М-14, new nacelle, feeder tank and pylon
Canopy emergency release mechanism

16. Horizontal tail with expanded area and horn-balanced elevator
THE MAIN STRUCTURE DIFFERENCE OF THE SINGLE-ENGINE AMPHIBIAN AIRCRAFT SA-20P FROM BE-103
Horizontal tail with expanded area and
horn-balanced elevator
Spray deflector
Removable hydraulic rudder
Attachable arrow-type step

17. DEVELOPMENT OF THE SА-20P AMPHIBIAN AIRCRAFT (PROTOTYPE OF OSA) PROGRAM
2000
Start of the aircraft engineering design (Issue of the administrative order by JSC KnAAPO No.520 on ).
2001
Development of the design documentation and construction of the aircraft.
2002
Participation of the aircraft in an aquatic festival on 12th of June.
On 16th of October the first flight of the SА-20P (V km/h, H m).
Total flight hours for the first two flights under the first flight program – 1 hour 7 minutes, 11 landings on artificial runway.
2003
Flights with refined horizontal tail, take-offs from water and landing on water.
Performed: 21 flights, 45 take-off and landing operations on artificial runway, 17 takeoff and landing operations on water, three-time in-flight engine cut-off and ignition.
Total flight hours – 20 hours 31 minutes.
Registration of the aircraft with the Uniform Registry of Aircraft under the Federal Aviation Association with the number No.RA-3068К.

18. DEVELOPMENT OF THE SА-20P AMPHIBIAN AIRCRAFT PROGRAM (continued)
2004
Installation of hydraulic rudder, installation and testing of environmental monitoring system, stall flights.
Performed: 7 flights, 16 takeoff and landing operations on artificial runway, 7 takeoff and landing operations on water. Total flight hours – 5 hours 32 minutes.
Collaboration with the industry’s Technical council. Decision of the Council’s panel on implementation of the first stage of flight development tests.
2005
First stage of the flight development testing.
Performed: 3 flights, total flight hours – 1 hours 37 minutes.
Performed during 2002 and 2005: 33 flights (excluding taxing and runs). Total flight hours made 27 hours 10 minutes.
Installation of reduced glove mid-wing and small arms (PKT).
2006
Registration of the aircraft with the Uniform Registry of Aircraft under the Federal Aviation Association as experimental. Getting of the Certificate on the M9F engine. Continued flight development tests on the M9F engine including qualification flights under OSA’s certification, trial performance.

19. SА-20P PRODUCTION

20. DEVELOPMENT OF THE SА-20P AMPHIBIAN AIRCRAFT PROGRAM (continued)

21. III. SINGLE-ENGINE AMPHIBIAN AIRCRAFT (OSA)

22. GENERAL VIEW OF SINGLE-ENGINE AMPHIBIAN AIRCRAFT OSA & ITS MAIN CONSTRUCTION FEATURES VERSUS SA-20P
Modern Russian Flight Navigation System (PNK)
SA-20P
Power plant with increased takeoff power – engine M-9F (420 h.p.) with propeller Ø2,6 м
Nacelle with improved aerodynamic and operational performance
Shift of feeder tank to the strut, an increased fuel capacity by 26 kg (to 242 kg)
Trapezoidal horizontal tail
Reduced vertical tail

23. OSA DESIGN DESCRIPTION
AIRFRAME Аaerodynamic design of OSA – a monoplane with low-stab displacing wings provided with root extensions. Traditional hydrodynamic configuration in combination with low-stab wings ensures highest hydro-aerodynamic efficiency during the water takeoff run, while absence of flops increases the aircraft’s aerodynamic performance.
WINGS are detachable and consist of a mid-wing and two outer wings. High-strength fasteners connect the wing components. Fuel tanks are located between the front spar, leading edge, medium and hatch-end ribs of the mid-wing. There are hatch removable covers in the fuel tanks and assembling and inspection hatches in leading and trailing wing edges.
EMPENNAGE The amphibian horizontal tail plane is supplied with an elevator mounted in the area of propeller blowing. The empennage consists of the stabilizer, elevator with trimmer, fin, dorsal fin and rudder with trimmer. The design provides for removable covers for the rudder control system assembling. In the rudder’s lower part a hydraulic rudder is installed, due to which the amphibian’s turning radius on water against the aircraft’s center of gravity does not exceed 0.5 of wing span.
LANDING GEAR of the aircraft is of a tricycle type with nose wheel. The main struts are mounted on the wing ribs and retracted forward into the wing bay. The nose landing gear with castor is fastened to a frame of the nose part of the boat and retracted forward into the nose wheel bay. Retraction and extension of landing gear are performed by hydraulic system securing extension of gears and their downlock. An emergency landing gear extension is carried out manually with the help of control cable by releasing the landing gear. The downlock is carried out under the weight and ram air pressure. The undercarriage doors drive is made by kinematical connection with the corresponding strut.

24. POWER PLANT OF OSA SINGLE-ENGINE
AMPHIBIAN AIRCRAFT
Power plant consists of the engine М-9F, manufactured by Voronezh Mechanical Plant (Russia), with MTV-9 type propeller, a subframe, exhaust collector, gears for the engine and units control, and cooling, starting, fuel and oil systems as well.
Engine М9F
Specification:
Cooling system ________________________________ air
Number of cylinders ______________________________9
Power, h.p. ___________________________________420
Cruise consumption, g/HP-h _____________________220
Crankshaft speed, rpm _________________________2950
Basic overhaul time, h _________________________1000
Weight, kg _____________________________________220
Usable fuel: B91/115 GOST , 100/100LL, motor petrol of with octane level not lower 85.
MTV-9/Hartzell propeller
Type of propeller: controllable pitch, tractor.
Specification:
Diameter, m _____________________ 2,6
Number of blades _________________3
Weight, kg ______________________44
М9F engine is installed in the aircrafts SU-26, SU-29, SU-31, SU-31М, SU-49 and in other GA airplanes.

25. CARGO & PASSENGER CABIN VERSIONS OF OSA AMPHIBIAN
In the cabin passenger seats are located in 6 in a row: 2 seats alongside with the path = 200 mm and spacing 1220 mm and 860 mm); interior volume: 4.6 m3.
1.75 m
CARGO
PASSENGER

26. MAIN INSTRUMENT PANEL
Installed equipment permits to carry out daylight flights under Visual Flight Rules (VFR) by one pilot according to the aviation regulations JAR-23

27. PATROLLING VERSION OF OSA, ARRANGEMENT & USE1 2 3 4 5 5 6
Patrolling version of the amphibian can be equipped with environmental monitoring data system (EMS) and small arms (PKT) and carry out the following mission:
Patrolling of forestland, sea, river and plain borders;
Environmental monitoring;
Search-and-rescue and antiterrorist operations;
Prevention of illegal activities and defeating personnel from the aircraft.
1 – Kalashnikov tank machine gun (PKT)
2 – ammunition chest
3 – storage stand for special equipment
4 – collimating sight
5 – TV and thermal control system
6 – airborne radar

28. PRINCIPLE OF EMS OPERATION
Environmental monitoring data system supplies a consumer with operational information on environmental condition and critical environmentally fragile facilities, examines territory to get Remote-Sensed Data (RSD) by carrying out special surveys.
PRINCIPLE OF EMS OPERATION
GPS NAVSTAR
INMARSAT
Information
transfer
EMS STRUCTURE
The GPS satellite system positions the aircraft and together with GIS locates measured environmental data on electronic map. Real-time information is transferred to any remote access point.
Air carrier (OSA type);
Inboard measuring complex;
Telemetry complex;
GIS inboard navigation satellite system;
GIS of ground control station;
Data processing system.

29. ACTIVITIES PERFORMED WITH THE USE OF ENVIRONENTAL MONITORING DATA SYSTEM
Condition monitoring of waste disposal facilities
Land use monitoring
Monitoring of mineral resources development
Soil landscape monitoring
Forecast & identification of wild fire
Infrared survey of heating mains
Radar mapping

30. TRIAL INSTALLATION OF LIGHT ARMS ON BOARD OF SINGLE-ENGINE AMPHIBIAN AIRCRAFT SA-20P
Installing of light arms is a necessary attribute of the OSA amphibian’s patrolling version.
Weapon type:
Kalashnikov PKT tank machine gun with electric solenoid trigger, in service of the Defense Ministry of the Russian Federation.
Military characteristics of PKT:
Calibre___________________7.62 mm
Rate of fire___________800 round/min
Accuracy range_____________1000 m
Ammunition ____________800 rounds
Firing is controlled from the control panel on the instrument panel and by the trigger switch on the aircraft control stick. The machine gun is unmovably fixed and targeting is effected by the aircraft by means of movable collimating sight.

31. INSTRUMENT PANEL OF THE AIRCRAFT’S PATROLLING VERSION
Attitude indicator AGB-96R
Radio compass ARK-35
Installed equipment makes possible daylight and night flights in easy and adverse weather conditions (VFR-IFR) by one or two pilots according to JAR-23.
Magnetic direction indicator MKB-80
Altitude indicator VR-10
Normal load factor indicator AK-9S
HF Radio “Kristall”
Airspeed indicator USBS-350
VHF Radio “Yurok”
First pilot’ and co-pilot’s navigation system indicators
Aircraft transponder SO-94-R
Aircraft wireless intercom SPU-34М (2 pcs.)
Power supply check indicator VA-3
Aircraft navigation system includes: weather locator and satellite navigator based on MRK-22 with attitude indicator and aviation clock functions. Any iformation received from the navigation system is displayed on left instrument subpanel. Display on the right subpanel duplicates possibilities of the first pilot’s display and can show data received from other systems of the aircraft during such tasks as patrolling, monitoring and management in the air of various activity types.

32. COMPARATIVE ANALYSIS OF OSA & BE-103 PERFORMANCES
Specification
BE-103
OSA
Engine, producer country
TCM IO-360ES, USA
M-9F, Russia
Quantity and engine (power)
2 x 210 h.p.
1 x 420 h.p.
Usable fuel
Aviation gasoline 100LL
Motor petrol AI-92, AI-95
Maximum take-off weight, kg
2330
Empty weight, kg
1850
1660
Useful load, kg
480
670
Maximum fuel capacity, kg
245
242
Stalling speed, km/h
112
Maximum cruising speed, km/h
240
Economic speed, km/h
190
201
Seating capacity, persons
1+4
1+5
Maximum range (with emergency reserve for 30 min), km
1100
1035
Range (3 passengers onboard), km
650
980
Range (5 passengers onboard), km -
745
Maximum wave height, m
0.4
0.5
Fuel cost per one flight hour, USD
100.6
29.6

33. DISTANCE – PAYLOAD CHART
Be-103
OSA
L, km

34. IV. COMPARISON OF OSA WITH AIRCRAFT WITH AMPHIBIOUS FLOATS

35. CESSNA CE-206H
CESSNA CE-182S

36. Fuel cost per flight hour, USD
Price of basic configuration aircraft, USD thous.
One passenger seat price, USD thous.
Fuel consumption, kg/h
Fuel cost per flight hour, USD

37. Maximal range, km
Number of passengers
Maximal range, km
Medium speed, km/h

38. OSA COMPARISON VERSUS AIRCARFT WITH AMPHIBIOUS FLOATS
Cessna Skylane
CE-182S
Cessna Stationair
CE-206H
OSA
Take-off engine power
h.p.
230
300
420
Cruising speed
km/h
207
212
201
Weight: maximum take-off kg
1406
1633
2330
empty
1162
1264
1660
including floats
280
265 -
useful load (crew, pass., fuel)
244
369
670
Ferry range (pilot, maximum fuel load and reserve for 30 min.)
Maximum fuel weight
167
237
242
Fuel weight excluding emergency reserve
147
211
Cruise consumption
kg/h 27 35 40
Maximum range km
1128
1279
1035
Full passenger load range (pilot, passengers, reserve for 30 min.)
Seating capacity (pilot + passengers)
person
1 + 1
1 +3
1+ 5
Load weight (pilot + passengers)
159
313
468
Maximum fuel capacity 85 56
202 65 26
173
Range
487
154
745
Price of aircraft with standard specification (2005)
USD
incl. floats
89 230
One passenger seat price
USD/pass.
Usable fuel price
USD/kg
2.34
0.74
Fuel cost per one flight hour
USD/h
63.2
81.9
29.6
Cabin size (height * length * width m
1.23*2.52*1.07
1.26*2.80*1.12
1.26*3.34*1.23
Max. wave height while takeoff/landing
0.4
0.5

39. THANK YOU FOR YOUR ATTENTION
VOSTOKAVIAPROM LLC
THANK YOU FOR YOUR ATTENTION
VOSTOKAVIAPROM LLC
23 Liteinaya Str., Komsomolsk-on-Amur, , Russia
Telephone: +7 (4217)
Fax: +7 (4217)