ANG Aircraft — Full technical specs

ANG (Aircraft New Generation) – The most advanced aircraft in the world

The next-generation 5-seater: more space, more speed, more range.

First designed and built in 2019 by leading Ukrainian aeronautical engineers. Its full carbon structure makes it lighter and stiffer; its aerodynamic efficiency —with a unique 18.6 glide ratio— delivers high TAS speeds, low fuel burn, and long range. Proprietary technical solutions make it a world benchmark in its class.

Cabin 1.35 m Fuel burn 28 L/h Range 2,500 km Speed: cruise TAS 370 km/h · max TAS 450 km/h

Cruise (TAS)370 km/h (200 kt)

Max (TAS)450 km/h (243 kt)

Cruise 65% (TAS)350 km/h (189 kt)

Cruise 55% (TAS)335 km/h (180 kt)

Range2,500 km (1,350 nm)

Climb7 m/s (1,378 ft/min)

VS0 (flaps)~90 km/h (48 kt)

VREF75 km/h (41 kt)

STOL240 m / 150 m (takeoff/landing)

Performance

Cruise speed (TAS)	370 km/h (200 kt)
Maximum speed (TAS)	450 km/h (243 kt)
Cruise 65% (TAS)	350 km/h (189 kt)
Cruise 55% (TAS)	335 km/h (180 kt)
Range	2,500 km (1,350 nm)
Climb rate	7 m/s (1,378 ft/min)
Stall speed VS0 (flaps)	~90 km/h (48 kt)
Approach speed VREF	75 km/h (41 kt)
Takeoff / landing roll	240 m / 150 m
Aerodynamic efficiency (L/D max)	18.6 (≈ 18:1)

Data under TAS 7.000 m, ISA conditions and standard configuration; may vary with mass, configuration, and density altitude.

Weights & loads

MTOW (maximum takeoff weight)	950 kg
Empty weight	380 kg
Payload	up to 570 kg
Fuel capacity	up to 275 L (2×110 L + 55 L header tank)

Dimensions & cabin

Wingspan	9.6 m
Wing area	10.8 m²
Fuselage width	1.35 m
Cabin height	1.20 m
Cabin width (shoulder to shoulder)	1.33 m
Cabin length	2.30 m (max)
Baggage volume	780 L
Overall length	7.31 m
Overall height	2.70 m

Engine & propulsion

Engine	Rotax 916 iS — 160 hp (turbo, electronic injection)
Fuel	95/98 gasoline (MOGAS) and Avgas 100LL
Typical fuel burn	28 L/h (economy cruise)
Propeller	Three-blade carbon, in-flight variable pitch; electric governor in spinner. Cockpit control with manual and auto modes.

Avionics & electrical

Glass cockpit	2 × Garmin G3X Touch 10” + G5 (backup) + GMC 507; configurable.
Autopilot	Yes, integrated (controlled via GMC 507).
Nav/Com	VFR/IFR as configured
Electrical system	Dual bus / redundancies (as configured)

Flight control system

Transmission	No cables or springs: pushrods and bellcranks in composite materials.
Joints	Spherical bearings at all pivot points.
Surfaces	Slotted surfaces with aerodynamic balance (horn) and mass balance.
Elevator	Bi-section with turbulators for higher effectiveness.
Elevator trim	Electric on the right section, control on the stick.
Rudder trim	Adjustable tab for cruise balancing.
Flaps	Actuated by fuselage-mounted servo controlled by an electronic unit.

Landing gear & brakes

Configuration	Retractable tricycle (single-shock nose + mains).
Damping	Oleo-pneumatic on all legs.
Nose steering	Linked to pedals; ±30° turn.
Wheels / tires	Same size nose/mains: Mitas 16×4 (4.00-8) 2PR B5 Super.
Brakes	Hydraulic disc on mains; independent from both seats.
Materials	Casted rim; nose fork and trailing link in composite.

Fuel system

Layout	Two wing-root tanks (110 L each) + 55 L header tank in fuselage.
Total capacity	Up to 275 L (excluding non-drainable residual).
Feed	By gravity to header tank + two boost pumps.
Construction	Wing tanks sandwich (AEROGLASS + Divinycell foam), sealed with K-153 resin; header tank in anti-static polyethylene fuel-resistant.

Limitations

Load factor	−2.0 … +4.0 g (up to 20 s)
VS0 (flaps)	90 km/h (48 kt)
V2min (takeoff)	90 km/h (48 kt)
VREF (landing)	75 km/h (41 kt)
VFE (flaps full)	130 km/h (70 kt)
VLE (gear)	130 km/h (70 kt)