dscn0202

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1.1.  Structure

All-composite sandwich structure (Carbon / Aramide / Glass)

One-piece, fully-cantilevered wing

Non-pressurized

1.2.     Undercarriage

Single-beam composite main landing gear

Main wheel size 6.00 – 6’’, nose wheel 4.00 – 6’’

Hydraulic disc brakes

Directly steerable nose wheel

1.3.     Propulsion

1.3.1.      Engine(s)

AVGAS Engine (Continental IO-360-AF :

Fuel injected avgas engine; naturally aspirated; approx. 180 hp

13.8 gal/hr (52 l/hr) @ max power; 10.4 gal/hr (39 l/hr) @ 75% power

DIESEL Engine

Turbocharged; 155 hp @ 2300 rpm

7.9 gal/hr (30 l/hr) @ max power; 5.9 gal/hr (22.5 l/hr) @ 75% power

Single-Lever Operation

1.3.2.      Propeller

Three-blade, constant speed propeller; natural composite propeller blades

1.4.     Cabin

Front seats individually adjustable in length / height (coupled), entire seat can be inclined

Rear seat as bench with two individually shaped seat cushions. Rear seatback folds forward for access to baggage area

Rear seat with ISOFIX child seat attachments

Cabin doors left / right front seats (hinged front, opening forward), plus left-side rear cabin door (hinged aft, opening rearward), creating an unobstructed, large opening on left side of cabin

Access to luggage compartment through rear seat bench, or through luggage door in right side of fuselage

1.5.     Instrumentation / Cockpit

Glass Cockpit – Standard):

-          Flight Design Vision Touch By Garmin  

-          Autopilot

-          Traffic, Terrain & Weather Depiction/Avoidance

1.6.     Optional Equipment

Glider / banner towing system

Float option possible in future

Icing protection under consideration (details in planning)

1.7.     Safety

Three-point safety belts with inertia reel on each seat

“Safety Cell” 

Seat belts with airbags optional

Airframe Emergency Parachute installed as standard equipment

2.       Performance Data

2.1.     Masses and Capacities:

Empty mass                                           1320 lb (600 kg) typical

MTOM                                                     2640 lb (1200 kg)

Seating Capacity                                    max. 287 lb (130 kg) per seat

Baggage                                                 max. 165 lb (75 kg)

Fuel                                                         70 gal (265 l) total in both wings

2.1.1.      Loading Examples:

Average Cabin Loading Max Fuel Loading High cabin loading AVGAS High cabin loading Diesel Low weight ops (towing)
Empty Aircraft Weight 1320 lb (600 kg) 1320 lb (600 kg) 1320 lb (600 kg) 1320 lb (600 kg) 1320 lb (600 kg)
Occupant Weight 792 lb(4 x 198 lb) 792 lb(4 x 198 lb) 1056lb(4 x 264 lb) 1144 lb(4 x 286 lb) 198lb (1 x 198 lb)
Luggage Weight 132 lb 165 lb 165 lb
Fuel Weight 66 gal AVGAS = 396 lb 70 gal Diesel = 490 lb 16.5 gal AVGAS = 99 lb 14.3 gal Diesel = 99 lb 13 gal Diesel = 92 lb
Endurance 6:25 hrs @ 75% power 11:45 hrs
@ 75% power
(13:35 @ 65% power)
1:35 hrs
@ 75% power
2:25 hrs
@ 75% power
2:00 hrs
@ towing cycle
Operating Weight 2640lb (1200 kg) 2640lb (1200 kg) 2640lb (1200 kg) 2640lb (1200 kg) 1610lb (732 kg)

2.2.     Speeds

Stall speed full flaps V0 (MTOM)50 kts

Max cruise speed Vh 160 kts

Never exceed speed Vne 195 kts

Maximum Range and Endurance

AVGAS Engine:

Maximum range                                      1200 NM  @ 65% power; 8.4 gal/hr  145 kt

Maximum endurance                              10:00 hrs                   @ 55% power; 7.0 gal/hr

Diesel Engine:

Maximum range                                      1700 NM  @ 75% power; 5.9 gal/hr 145 kt

Maximum endurance                              13:35 hrs                   @ 65% power; 5.1 gal/hr

2.2.1.      Climb rate

at MTOW, MP, ISA 0m                           984 ft/min

2.2.2.      Takeoff @ ISA 0, hard surface

Takeoff roll                                              1312 ft

Takeoff distance                                     2132 ft to clear 50 ft  obstacle

2.3.     Operational Limitations

VFR and IFR operation

2.4.     Noise Level

ICAO Annex 16 Chapter 10                    less than 79.9 dB(A)

… complies with Landeplatz Lärmschutzverordnung (enhanced noise limits).

2.5.     Certification

Initial certification by EASA (application filed in Q1 2011)

FAA certification by reciprocity of EASA certification

 

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