RAF2000 FI EJ2.2
MAX PERSONS
2 PERSONS
USEFUL LOAD
331kg
CRUISE SPEED
70-80mph
ENDURANCE
4.6 Hours
TAKE-OFF ROLL
0-75 feet

RAF2000 Specifications

RAF2000 FI EJ2.2 EXTERIOR

 

DIMENSIONS

 

 Lenght

 4.15 meter

 Height

 2.59 meter

 Width

 1.53 meter

 Aircraft Dry Weight

 358 Kg

 Payload

 331Kg

 Gross Weight can be set as high as Category Weight

 698.54 Kg

 

ENGINE

 

Manufacturer

 SUBARU

Displacement

2200 cc

Horsepower

130 hp

Cooling

Liquid Cooled

Ignition

Electronic, Computer Controlled, Single Spark Plug/Cylinder

 

REDUCTION DRIVE

 

Manufacturer

 RAF

 Type

 HTD COG BELT

 Ratio

 2.10 to 1

 

PROPELLER

 

 Manufacturer

 WARPDRIVE

 # of blades

 3

 Diameter

 172.72 cm / 68 inches

 Pitch

 Ground Adjustable

 

ROTOR BLADE

 

Manufacturer

 RAF

 Rotor Span

 9.14 M /30 FT

 Blade Cord

 21.56 CM / 8.5 Inches

 Materials

Composites, Aluminum Spar,  Foam Core

 

ACTUAL DISC LOADING

 

Take-off Weight when set at Category Weight 0.95 Kg / 2.18 LBS/sq.feet

 

 

FUEL CAPACITY

 

FUEL CAPACITY

 85 Litre / 25 US Gallons

 Endurance (1/2hr on reserve)

 4.6 Hours

 Fuel Consumption (80% or  4200 rpm)

 21.82 Litre per hour / 4.8 US Gallons

 Unusable Fuel

 2.27 Litre / 1/2 Gallon

 Approved Fuel

 Premium Auto Gas / Unleaded

 Grades

 91-93 Octane

 

PERFORMANCE

 

 PERFORMANCE

 2.2 FI

 Minimum Speed (Min Altitude 300 FT)

 20-25 mph

 Cruise Speed

 70-80 mph

 Recommended VNE

 100 mph

 Maximum Speed

 120 mph

 Stall Speed

 N/A

 Take-off Air Speed

 30-35 mph

 Take-off Roll (Single Occupant)

 0-75 feet

 Landing Roll

 0-10 feet

 Rate of Climb

 1200 RPM

 

RAF2000 FI EJ2.5 EXTERIOR

 

DIMENSIONS

 

 Lenght

 4.15 meter

 Height

 2.59 meter

 Width

 1.53 meter

 Aircraft Dry Weight

 367 Kg

 Payload

 349Kg

 Gross Weight can be set as high as Category Weight

 698.54 Kg

 

ENGINE

 

Manufacturer

 SUBARU

Displacement

2500 cc

Horsepower

165 hp

Cooling

Liquid Cooled

Ignition

Electronic, Computer Controlled, Single Spark Plug/Cylinder

 

REDUCTION DRIVE

 

Manufacturer

 RAF

 Type

 HTD COG BELT

 Ratio

 2.10 to 1

 

PROPELLER

 

 Manufacturer

 WARPDRIVE

 # of blades

 4

 Diameter

 167.64 cm / 66 inches

 Pitch

 Ground Adjustable

 

ROTOR BLADE

 

Manufacturer

 RAF

 Rotor Span

 9.14 M /30 FT

 Blade Cord

 21.56 CM / 8.5 Inches

 Materials

Composites, Aluminum Spar,  Foam Core

 

ACTUAL DISC LOADING

 

Take-off Weight when set at Category Weight 0.95 Kg / 2.18 LBS/sq.feet

 

 

FUEL CAPACITY

 

FUEL CAPACITY

 85 Litre / 25 US Gallons

 Endurance (1/2hr on reserve)

 3.3 Hours

 Fuel Consumption (80% or  4200 rpm)

25 Litre per hour / 6.5 US Gallons

 Unusable Fuel

 2.27 Litre / 1/2 Gallon

 Approved Fuel

 Premium Auto Gas / Unleaded

 Grades

 91-93 Octane

 

PERFORMANCE

 

 PERFORMANCE

 2.5 FI

 Minimum Speed (Min Altitude 300 FT)

 20-25 mph

 Cruise Speed

 90 mph

 Recommended VNE

 100 mph

 Maximum Speed

 140 mph

 Stall Speed

 N/A

 Take-off Air Speed

 30-35 mph

 Take-off Roll (Single Occupant)

 0-75 feet

 Landing Roll

 0-10 feet

 Rate of Climb

 1200 RPM

 

NOTES:

 

* Performance optimum at sea level and dependant on wind

* RAF 2000 Gyroplane requires flight instruction (min of 45hrs in-flight training)

* Prices and specs subject to change without prior notice

Contact Numbers

Phone: +27 54 331 3534
Fax: +27 54 332 3628
After Hrs + 27 78 459 2636/ + 27 83 282 8792

Physical Address

233B Diedericks Road,
GA Hanger 4
Upington International Airport
Upington, 8801
Republic of South Africa

Postal Address

PO Box 2071
Upington
8800
South Africa

Email Addresses