Technical Data
ANG-01 Specifications
Complete technical data for the ANG aircraft across all major systems. Performance figures at TAS 7 000 m, ISA standard configuration.
Flight Performance
Built for speed, range, and efficiency
Key performance figures at TAS 7 000 m, ISA standard configuration. Actual values may vary with weight, configuration, and air density.
450 km/h
243 kts
Maximum speed (TAS)
370 km/h
200 kts
Cruise speed (TAS)
2 500 km
1 350 nm
Range
18.6
≈ 18 : 1
Glide ratio (L/D max)
Cruise speed (TAS)370 km/h (200 kts)
Maximum speed (TAS)450 km/h (243 kts)
Cruise 65% (TAS)350 km/h (189 kts)
Cruise 55% (TAS)335 km/h (180 kts)
Range2 500 km (1 350 nm)
Rate of climb7 m/s (1 378 ft/min)
Stall speed VS0 (flaps)≈ 90 km/h (48 kts)
Approach speed VREF75 km/h (41 kts)
Takeoff / landing roll240 m / 150 m
Glide ratio (L/D max)18.6 (≈ 18 : 1)
Weight & Loads
MTOW950 kg
Empty weight380 kg
Useful loadup to 570 kg
Fuel capacityup to 275 L (2 × 110 L + 55 L header tank)
Dimensions & Cabin
Wingspan9.6 m
Wing area10.8 m²
Fuselage width1.35 m
Cabin height1.20 m
Cabin width (shoulder)1.33 m
Cabin length (max)2.30 m
Baggage volume780 L
Overall length7.31 m
Overall height2.70 m
Engine & Propeller
EngineRotax 916 iS — 160 hp (turbo, EFI)
FuelA-95 MOGAS / Aviation fuel (90/10% blend)
Typical consumption28 L/h (economy cruise)
Propeller3-blade carbon, in-flight variable pitch
Pitch controlElectric governor in spinner; manual & auto modes
Avionics & Electrics
Glass cockpit2 × Garmin G3X Touch 10" + G5 backup + GMC 507
AutopilotIntegrated (via GMC 507)
Nav / ComVFR / IFR by configuration
Electrical systemDual-bus / redundant (by configuration)
Flight Control System
ActuatorsNo cables or springs: composite pushrods & bellcranks
BearingsSpherical bearings at all pivot points
Control surfacesSlotted, with horn & mass balance
ElevatorTwo-section with turbulators for enhanced efficiency
Elevator trimElectric on right section, stick-mounted control
Rudder trimAdjustable tab for cruise balance
FlapsFuselage servo actuator, electronic control unit
Landing Gear & Brakes
ConfigurationRetractable tricycle (nose + mains, single-strut damper)
Shock absorptionOleo-pneumatic on all struts
Nose-wheel steeringPedal-linked; ±30° turn
Wheels / tiresMitas 16 × 4 (4.00-8) 2PR B5 Super (all positions)
BrakesHydraulic disc on mains; differential from both seats
MaterialsCast wheels; composite nose fork & lever
Fuel System
Layout2 × 110 L wing-root tanks + 55 L header tank
Total capacityUp to 275 L (excl. unusable)
FeedGravity to header tank + two boost pumps
ConstructionSandwich wing tanks (AEROGLASS + Divinycell foam); antistatic PE header tank
Limitations
G-load−2.0 … +4.0 g (up to 20 s)
VS0 (flaps)90 km/h (48 kts)
V2min (takeoff)90 km/h (48 kts)
VREF (landing)75 km/h (41 kts)
VFE (full flaps)130 km/h (70 kts)
VLE (gear)130 km/h (70 kts)
Documentation
Essential manuals
Download the core manuals to get familiar with your ANG aircraft.
Ready to configure?
Build your ANG Crown with the online configurator or explore the aircraft models.