321 FAETA NG – FEATURES & PERFORMANCE

Main features

Thanks to the combination of its ROTAX engine and FITI propeller, the new 321 FAETA NG is one of the fastest ultralights with exceptional performance and low fuel consumption. Like the other ATEC aircraft, the new “NG” can be equipped with different types of features. Thus, the Glass cockpit and advanced analog instruments may vary depending on the wishes of each customer. The cockpit offers enough space and comfort during long flights since it is ventilated and heated. The demisting function of the canopy helps to keep good visibility, for greater safety. The seats and pedals are adjustable in all directions and can be adapted and customized according to the size of the driver. The new luggage trunk provides ample space for bags up to 5 kg.

schema-atec-001

FEATURES

Wing span: 6.2m
Height: 2.0m
Lengh: 6.25m

WEIGHT

Empty weight: 297.0 kg
(in its basic configuration)
MTOW: 472.5 kg
Useful load: 175.5 kg

ENGINE

Rotax 912 ULS or iS 100HP

PERFORMANCE OF THE 321 FAETA NG

Thanks to its flight characteristics, the 321 FAETA NG does not currently meet any competitor in its category. It is more manageable, but also more stable with immediate reactions to control. This aircraft is exceptional in its speed, up to 290 km/h, and its stall speed is only 54 km/h. It is specially designed for comfortable flights and daily use.

The control of the aircraft is carried out thanks to a doubled control lever. The front wheel can be steered using the low turning radius pedals. The lift flaps are electrically controlled: when they are in motion, the aircraft adjusts automatically, without the pilot noticing a change.

The propulsion unit is essential to the dynamics of FAETA NG. This is why the engines used are Rotax 912 ULS ou iS 100HP.

TWIN / TRIPAL PROPELLERS

logo-fiti-design

FITI Design is a company engaged in the design, technology and production of composite products for ultra-light aircraft and sports flying equipment. Its main activity is the production of fixed composite propellers, adjustable on the ground and in flight, for ultra-light aircraft. By choosing the 321 FAETA NG with a ROTAX 912 ULS 100 HP engine, this implies to opt for a FITI propeller to three or two blades. The engine mount is welded with premium CrMo thin wall steel tubes. The combination of this engine and propeller makes this FAETA NG one of the fastest low-altitude aircraft of its generation.

PERFORMANCES (Rotax 912 ULS 100HP)

Take off distance: /
Landing distance: /
Stall speed flaps up (Vs): 73 km/h IAS (ISA and MTOW)
Stall speed full flaps (Vs0): 54 km/h IAS (ISA and MTOW)
Cruising speed: 245 km/h to 220 km/h
Climb rate: 1200 ft/min
Autonomy: 5 to 10h (with 1h reserve)
R Range: 1225 km to 1800 km (with 1h reserve)

LIMITATIONS

Cross wind: 11 kts
Load factors: + 5.05 / -3.05
Never exceed speed (Vne): 290 km/h IAS
Never exceed speed with flaps (Vfe): 130 km/h IAS