| - Complete
set of documentation on the production of single-engine turboprop
(eight places) business class aircraft GM-17 “VIPER”
1. Patent of ¹ 49694
for design and production of single-engine turboprop aircraft GM-17;
2. Patent for the industrial standard of multipurpose aircraft (two
versions); ¹ 56675,
3. License for the useful model of ¹ 21387, the aircraft GM-17
4. Complete description of aircraft;
5. The general forms of aircraft GM-17 with the engines of different
types;
6. Assembly diagram and the centering calculations of aircraft GM-17:
7. Drawings of the parts, necessary for the production of GM-17
aircraft;
8. Assembly drawings of aircraft GM-17;
9. Schematics of all systems of aircraft GM-17 (fuel system, oil
system, electrical system, the pressurized system and cooling of
air, the hydraulic exhaust system of chassis, schematic of radio,
navigation and flying equipment and so on);
10. Express- report on the results of aerodynamic model tests of
aircraft in the wind tunnel [ADT]-102 of TscAgi (Central Institute
of Aerohydrodynamics in. Zhukovskiy);
11. Scientific and technical report of the results of model tests
of light single-engine aircraft GM-17 in the wind tunnel [ADT] T
-102 and T -103 of TscAgi (Central Institute of Aerohydrodynamics
in. Zhukovskiy);
12. Model airplane GM-17, executed M 1:10 necessary for fulfilling
of the wind-tunnel tests and tests;
13. 4 model airplanes M 1:20 with different types of engine and
wing tips;
14. Calculations of the evaluation of the influence of the blowout
of propeller on the aerodynamic characteristics of aircraft GM-17;
15. Calculation of loads on the head part of the airframe of aircraft
GM-17;
16. Calculations of the structure diagram of the head part of the
aircraft GM-17;
17. Calculations of the required thickness of the heat insulation
of the pressurized cabin of aircraft GM-17;
18. Calculations of the installation of metallic fuel tanks to the
aircraft GM-17;
19. The calculated aerodynamic characteristics of aircraft GM-17;
20. Program and the report of the static tests of the airframe of
aircraft GM-17;
21. Program and the report of the flight tests of aircraft GM-17;
22. Management on the flight operations of aircraft GM-17;
23. Drawings of the ground equipment, necessary for operating the
aircraft GM-17;
24. Catalog with the indication of the numbers of all components
of the airframe of aircraft (catalog of spare parts);
25. Manual on maintenance and repairing the engine of aircraft GM-17;
26. Manual on maintenance and repairing the screw of aircraft GM-17;
27. Manual on maintenance and repairing the airframe of aircraft
GM-17;
28. Manuals on maintenance and repairing the radio navigation and
flying equipment, established on the aircraft GM-17;
- Preparation for the production of aircraft GM-17:
1. The flow chart of the preparation for the production of aircraft
GM-17;
2. The flow chart of the production of aircraft GM-17, including
description, photo and video are materials;
3. Enumeration of tools and equipment, necessary for the production
of aircraft;
4. Enumeration and the nomenclature of the materials, necessary
for the production of aircraft;
5. Enumeration and the catalog numbers component product, necessary
for the production of aircraft GM-17;
6. Calculations and the description of the necessary production
capacities;
7. Enumeration of specialists and personnel, necessary for the production
of aircraft GM-17;
8. Calculations of the necessary financing for the series production
of aircraft GM-17;
9. The preliminary design of the building of plant for the production
of aircraft in Switzerland;
10. Permission of the government of canton for the creation of aviation
production in Switzerland, including privileges on the taxation
for 10 years.
- Two flying aircraft GM-17 “VIPER”
1. GM-17 “Viper”, S/N 001, Demo of aircraft, Production
2003, TT of 203 hour
Engine Walter M -601E, TT of 203 hour
Propeller of 5 blades, the V -510, TT of 203 hour
Flight instrument will be double
Registered IFR
Location: Switzerland
more information........
2. GM-17 “Viper”, S/N 003, Demo of aircraft, Production
2004, TT of 106 hour
Engine Walter M -601E, TT of 106 hour
Propeller of 5 blades, the V -510, TT of 106 hour
Flight instrument will be double
Registered IFR
Location Switzerland
more information........
P.S.
1. Possibility of design and administrative tracking of project;
2. The purchase of this project will give the right to a foreign
citizen to obtain a work and residence permission in Switzerland.
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