|
AirFrame
|
|
|
Fusulage Construction
|
Semimonocoque Molded Construction |
|
Airframe Material
|
Carbon Fiber Composite |
|
Number of Doors
|
2 |
|
Wing
|
|
|
Wing Location
|
Bottom Wing |
|
Wing Construction
|
Front & Rear Spar |
|
Wing Rib Material
|
GFRP/CFRP Sandwich Construction |
|
Wing Skin Material
|
Composite |
|
--Aileron
|
|
Aileron Type
|
Conventional |
Aileron Trim
|
None |
Aileron Control System
|
Control Rods |
--Flap
|
|
Flap Type
|
Plain |
|
Wing Flap Actuation
|
Electric |
|
Empennage
|
|
|
Empennage Type
|
T Tail |
|
Empennage Rib Material
|
GFRP/CFRP Sandwich Construction |
|
Empennage Skin Material
|
Composite |
|
Rudder Trim
|
Cable Link Trim Tab |
|
Yaw Trim Actuator
|
Manual |
|
Yaw Control System
|
Cable and Pully |
|
Pitch Trim
|
Cable Link Trim Tab |
|
Pitch Control System
|
Control Rods |
|
Pitch Trim Actuator
|
Electric |
|
Landing Gear
|
|
|
Landing Gear Type
|
Tricycle |
|
Retractable
|
Yes |
|
Retraction System
|
Hydralic/Electric |
|
Emergency Extension
|
Gravity Downlock |
|
Ground Steering
|
Rudder Pedals |
|
Shock Absorbtion Main Gear
|
Oil/Air Strut |
|
Shock Absorbtion Other Gear
|
Nosewheel Air/Oil Strut |
|
Brake Type
|
Hydraulic Actuated Brake Disc |
|
Brake Controls
|
Toe Brakes |
|
Cabin
|
|
|
Instrument Panel
|
IFR Glass |
|
Flight Control
|
Joystick |
|
Number of Seats
|
4 |
|
Heating
|
Engine Exhaust Shroud |
|
Window Defrost
|
Ducted Hot Air |
|
Cooling
|
Ducted Ram Air |
|
Profiles
|
|
|
Normal Climb Profile Speed (KIAS)
|
85 |
|
Maximum Climb Profile Speed (KIAS)
|
79 |
|
|
Engine
|
|
|
Number of Engines
|
2 |
|
Engine Manufacturer
|
Thielert |
|
Engine Model
|
TAE125 |
|
Engine Type
|
Turbo Normalized Diesel |
|
Geared
|
Geared |
|
Cooled
|
Liquid Cooled |
|
Fuel/Air Mechanism
|
Fuel Injected |
|
Number of Cylinders
|
4 |
|
Max HP
|
135 Per Side |
|
Starter System
|
Electronic Ignition |
|
Propeller
|
|
|
Propeller Manufacturer
|
MT |
|
Propeller Model
|
MTV-6-A-C-F/CF187-129 |
|
Number of Blades
|
3 |
|
Minimum Diameter
|
74 |
|
Maximum Diameter
|
74 |
|
Propeller Type
|
ECU Pitch Control |
|
Propeller Governor
|
Oil Pressure |
|
Fuel System
|
|
|
Fuel System Type
|
Fuel Pump |
|
Approved Fuel Type 1
|
Jet Fuel |
|
Approved Fuel Type 2
|
Diesel |
|
Approved Fuel Type 3
|
|
|
Fuel Capacity (G)
|
79 |
|
Tank Type 1 Location
|
Wing |
|
Tank Type 1 Capacity (G)
|
26 |
|
Tank Type 2 Location
|
Auxillary Tank/Engine Nacelle |
|
Tank Type 2 Capacity (G)
|
13.7 |
|
Usable Fuel (G)
|
76.4 |
|
Oil Capacity (Quarts)
|
6 |
|
Electrical System
|
|
|
Power Source
|
Engine Driven Alternator |
|
Power Storage
|
Battery |
|
System Voltage
|
28 |
|
Alternator Amp
|
60 Per Side |
|
Battery Voltage
|
24 |
|
Battery Amp/Hour
|
10 |
|
Limitations
|
|
|
Maximum T/O Weight (lbs)
|
3935 |
|
Maximum LDG Weight (lbs)
|
3748 |
|
Standard Empty Weight (lbs)
|
2756 |
|
Useful Load (lbs)
|
1179 |
|
Station 1 Baggage Location
|
Nose |
|
Max Weight Station 1 (lbs)
|
66 |
|
Station 2 Baggage Location
|
Behind Rear Seats |
|
Max Weight Station 2(lbs)
|
100 |
|
Station 3 Baggage Location
|
Behind rear Baggage Compartment |
|
Max Weight Station 3(lbs)
|
40 |
|
Wing Loading (lbs/sq.ft)
|
22.5 |
|
Vne (KCAS)
|
194 |
|
Vno (KCAS)
|
155 |
|
Va(Max Gross) (KCAS)
|
126 |
|
