Restricted in France at 472.5 kg MTOW, the A32L can be equipped with a USH 52 S cell parachute, certified for a mass of 520.00 kg.
Its fuel supply is provided by two tanks with a total capacity of 89 liters consumables, which feed that feed by gravity the engine fuel pump. This AEROPRAKT is equipped with two power controls (one per cockpit), a flap control, a carburettor reheat control and a park brake control (optional).
This ULM is standinf firmly on its tricycle landing gear thanks to the hydraulic damper of the front wheel which is also conjugated, and by its main gear aluminum alloy spring blade. The A32L is equipped as standard with 600 * 6 wheels: it can easily get out of rough terrain! The wheels of the main gear are also equipped with hydraulic brake discs.
Wing span: 9.55 m
Empty weight: 289.0 kg
(in its basic configuration)
MTOW: 472.5 kg
Useful load: 183.5 kg
• Rotax 912 UL 80 HP
• Rotax 912 ULS 100HP
• Rotax 912 iS 100HP
The basic model of the A32L is powered by a Rotax 912ULS engine, with three-bladed tractive propeller with adjustable pitch. In 100 hp version, this reputable and economical engine offers a low operating cost compared to the performance of this ultralight. The A32L is equipped with the excellent prop Kiev Prop, which can be changed for a three-blade E-PROP propeller.
On the engine side, you can opt for the DIGI EMS engine monitoring / indication system offered by Kanardia. In addition to having a direct reading of the engine data, the DIGI EMS also displays the intake pressure, the amount of fuel contained in the tanks, the battery voltage, the OAT, … according to the sensors installed.
In terms of avionics, the A32L is equipped with a VHF, a two-way intercom system with independent squelch / volume adjustment, a VHF Trig TY 91 (8.33kHz) and a TRANSPONDER mode S Trig TT21. Also optional: the equipment of the manufacturer Dynon including the SkyView system (PFD, MFD and autopilot), or those of the manufacturer Kanardia (NESIS III system for the PFD part, but also traditional instruments and artificial horizon).
PERFORMANCE (ROTAX 912 ULS 100HP)
Take off distance: +/- 105 m
Landing distance: +/- 135 m
Stall speed flaps up (Vs): 63 km/h IAS (ISA and MTOW)
Stall speed full flaps (Vs0): 52 km/h IAS (ISA and MTOW)
Cruising speed: 160 km/h to 200 km/h
Climb rate: 790 ft/min to 1500 ft/min
Endurance: 5 to 6h (with 1h reserve)
R Range: 850 km to 1000 km (with 1h reserve)
Cross wind: 14 kts
Load factors: + 4.0 / -2.0
Never exceed speed (Vne): 216 km/h IAS
Never exceed speed with flaps (Vfe): 112 km/h IAS