SCOUT TECHNICAL INFORMATION SAFETY & STABILITY. Autorotation speed. Landing Gears, Absorb System

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SCOUT HELICOPTER TECHNICAL INFORMATION Seats Power plant 3 210-220 hp Gross Weight Empty Weight 1985 lbs (900 kg) 1169 lbs (530 kg) SAFETY & STABILITY Normal Cruise Max. IAS, Sea Level / Standard Day Autorotation Rate of Climb Hover Out Of Ground Effect (HOGE) (hot&high version) Hover in Ground Effect (HIGE) 111 mph (187 km/h) 124 mph (209 km/h) 1476,38 fpm (7,5 m/s) 1350 fpm (8 m/s) 12139 ft (3700 m) 13780 ft (4200 m) Service Ceiling 20300 ft (6190 m) Landing Gears, Absorb System Powered by legendary Lycoming family Engine (available engines: Lycoming IO-390, IOX-390LS) Autorotation speed 1476,38 fpm (7,5 m/s) Successful crash tests 2000 hours before TBO Max. Range of Flight Max. Fuel Cruise Main Rotor Diameter Tail Rotor Diameter Overall Length Height 357 miles (600 km) 3,2 h 26-¾ ft (8.16 m) 50-¼ ft (1.2 m) 30-⅔ ft (9 m) 103 in (2.6 m)

TECHNICAL I N F O R M AT I O N SCOUT HELICOPTER Seats Power plant 4.64 m 15.2 ft. 210-220 hp Gross Weight 1985 lbs (900 kg) Empty Weight 1169 lbs (530 kg) Normal Cruise 111 mph (187 km/h) 9.32 m 30.6 ft. Ø 8.14 m 26.7 ft. Max. IAS, Sea Level / Standard Day Autorotation 0.41 m 1.3 ft. 2.39 m 7.8 ft. TOP VIEW 2.58 m 8.5 ft. Ø 1.2 m 3.9 ft. 2.31 m 7.6 ft. FRONT VIEW 1.97 m 6.5 ft. SIDE VIEW 3 1.59 m 5.2 ft. 1.97 m 6.4 ft. 124 mph (209 km/h) 1476,38 fpm (7,5 m/s) Rate of Climb 1350 fpm (8 m/s) Hover Out Of Ground Effect (HOGE) (hot&high version) 12139 ft (3700 m) Hover in Ground Effect (HIGE) 13780 ft (4200 m) Service Ceiling 20300 ft (6190 m) Max. Range of Flight 357 miles (600 km) Max. Fuel Cruise Main Rotor Diameter Tail Rotor Diameter Overall Length Height 3,2 h 26-¾ ft (8.16 m) 50-¼ ft (1.2 m) 30-⅔ ft (9 m) 103 in (2.6 m)

SCOUT HELICOPTER Video of flights: https://youtu.be/-r7wiozi18k

SCOUT HELICOPTER Video of flights: https://youtu.be/-r7wiozi18k

FEATURES SAFETY & RELIABILITY HIGH PERFORMANCE ERGONOMIC DESIGN & COMFORT Autorotation speed 1476,38 fpm (7,5 m/s) Landing Gears Absorb System Successful crash tests Powered by legendary Lycoming family Engine (available engines: Lycoming IO-390, IOX-390LS) 2000 hours before TBO Normal Cruise 111 mph (187 km/h) Max. IAS, Sea Level / Standard Day 124 mph (209 km/h) Rate of Climb 1350 fpm (8 m/s) Hover Out Of Ground Effect (HOGE) 12139 ft (3700 m) (hot&high version) Useful Payload 772 lbs (350 kg) 3 SEATS Stylish modern design Real big and very comfortable cabin Ergonomic design of cabin

TECHNICAL I N F O R M AT I O N OPTIONS ENGINES Power (hp) HOGE(feet/meters)** max OAT (F/C) Engines (models)* IO-390 210 5577/1700 IOX-390LS 220 12139/3700 Ne, hp 95/35 Fuel 100LL 104/45 100LL/Mogas Мk, Nm 250 1000 Ps = 1450 milibar Ne, hp 225 900 200 800 175 700 Мk, Nm 150 600 125 500 100 400 75 300 50 200 25 100 0 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 0 2800 n, RPM Power/RPM for IOX-390LS with supercharger option *For all models governor is included **For useful payload @595lbs/270kg

IOX-390LS Governor TECHNICAL I N F O R M AT I O N SuperCharger MODEL IOX-390-LS POWER 220hp@2700rpm FUEL AVGAS,MOGAS Liquid Cooling Cylinder Electronic Ignition

IOX-390LS TECHNICAL I N F O R M AT I O N MODEL IOX-390-LS POWER 220hp@2700rpm FUEL AVGAS,MOGAS

IOX-390LS Ne, hp 250 Мk, Nm 1000 TECHNICAL INFORMATION 225 Ps= 1450 milibar Ne, hp 900 200 175 150 125 Мk, Nm 800 700 600 500 MODEL IOX-390-LS POWER 220hp 100 400 FUEL 75 300 AVGAS, MOGAS 50 200 25 100 0 0 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 n, RPM

IOX-390LS Power, Hp 230 Altitude characteristic Lycoming IO-390, Liqued Cooling Supercharger IOX-390LS TECHNICAL INFORMATION 220 210 200 190 MODEL IOX-390-LS 180 170 160 150 140 130 120 110 100 90 IOS-390LS IO-390 POWER 220hp FUEL AVGAS, MOGAS 80 0 1000 2000 3000 4000 5000 6000 7000 Altitude, m

225 OPTIONS 220 215 TECHNICAL INFORMATION 210 205 200 195 190 185 hp 180 175 170 165 160 155 150 145 140 0 500 1000 1500 2000 2500 3000 3500 4000 H, m

BASE CONFIGURATIONS TECHNICAL INFORMATION Engine Governor (automatic rotor rpm correction) Avionics and instruments Radio HOT&HIGH Engine Kit 3 Seats with leather cover 3 Inertial seat belts Base interior External Paint PRICE (EXW Kiev, Ukraine) ISA IO-390 InstrumentsEMS Garmin GTX-225 - $195 000 HOT&HIGH IOX-390LS InstrumentsEMS Garmin GTX-225 $215 000

OPERATING COST TECHNICAL INFORMATION ISA CONFIGURATION (AIR COOLING LYCOMING IO-390) Hours Unit Cost Cost per Hour RESERVE FOR OVERHAUL $34,50 2000 Hour Engine Overhaul ($24,000 include labor) 2000 $29 000 $14,50 2000 Hour Aircraft Overhaul Parts Kit ($28,000) (Includes new bearings, seals, belts, etc., and life-limited components with less than 2000 hours remaining.) 2000 $28 000 $14,00 500 rotor head torsion strip kit($3,000) 500 $3 000 $6,00 DIRECT OPERATING COST $55,78 Fuel @ $5.76 per gallon and 9,24 gph for average use (ISA) $53,22 Oil $0,63 Unscheduled Maintenance, Parts and Labor @ $35 per hour $1,93 TOTAL $90,28 OPERATING COST-PER-ROAD MILE $0,90 CONFIGURATION ISA POWER IO-390 FUEL AVGAS@$5,76 PG TOTAL $90,28 per hour

OPERATING COST TECHNICAL INFORMATION HOT&HIGH CONFIGURATION (LIQUID COOLING LYCOMING IOX-390LS) Hours Unit Cost Cost per Hour RESERVE FOR OVERHAUL $34,50 2000 Hour Engine Overhaul ($24,000 include labor) 2000 $29 000 $14,50 2000 Hour Aircraft Overhaul Parts Kit ($28,000) (Includes new bearings, seals, belts, etc., and life-limited components with less than 2000 hours remaining.) 2000 $28 000 $14,00 500 rotor head torsion strip kit($3,000) 500 $3 000 $6,00 CONFIGURATION HOT&HIGH POWER IOX-390LS DIRECT OPERATING COST $61,10 Fuel @ $5.76 per gallon and 10,16 gph for average use (HOT&HIGH) $58,54 Oil $0,63 Unscheduled Maintenance, Parts and Labor @ $35 per hour $1,93 TOTAL $95,60 OPERATING COST-PER-ROAD MILE $0,96 FUEL AVGAS@$5,76 PG TOTAL $95,60 per hour

OPERATING COST TECHNICAL INFORMATION HOT&HIGH CONFIGURATION (LIQUID COOLING LYCOMING IOX-390LS) Hours Unit Cost Cost per Hour RESERVE FOR OVERHAUL $34,50 2000 Hour Engine Overhaul ($24,000 include labor) 2000 $29 000 $14,50 2000 Hour Aircraft Overhaul Parts Kit ($28,000) (Includes new bearings, seals, belts, etc., and life-limited components with less than 2000 hours remaining.) 2000 $28 000 $14,00 500 rotor head torsion strip kit($3,000) 500 $3 000 $6,00 CONFIGURATION HOT&HIGH POWER IOX-390LS DIRECT OPERATING COST $40,66 Fuel @ $3.75 per gallon and 10,16 gph for average use (HOT&HIGH) $38,10 Oil $0,63 Unscheduled Maintenance, Parts and Labor @ $35 per hour $1,93 TOTAL $75,16 OPERATING COST-PER-ROAD MILE $0,75 FUEL MOGAS@$3,75 PG TOTAL $75,16 per hour

OPTIONS TECHNICAL INFORMATION Second control SET Outdoor Cover Transport Wheels Cabin Cover Main Rotor Head Cover Main Rotor Blades Cover Tail Rotor Hub Cover Tail Rotor Blades Cover $2900 $2600 $750

OPTIONS TECHNICAL INFORMATION Available soon Heater system $800 External cargo box $1500 Climate control system $4500

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