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ZLIN Z 143 LSi GENIUS

ZLIN Z 143 LSi GENIUS

SMART, INDESTRUCTIBLE, ALL-PURPOSE.

ZLIN Z 143 LSi GENIUS

All-metal, aluminum structure of the aircraft

ZLIN Z 143 LSi GENIUS

High performance and easy control

ZLIN Z 143 LSi GENIUS

Easy maintenance at minimum cost

ZLIN Z 143 LSi GENIUS

With additional fuel tanks, it enables up to 14-hour flight endurance.

ZLIN Z 143 LSi GENIUS

Monitoring the safe-life of the aircraft

ZLIN Z 143 LSi GENIUS

SMART, INDESTRUCTIBLE, ALL-PURPOSE.

The all-metal ZLIN Z 143 LSi GENIUS is a multi-purpose training and courier airplane. With its capabilities it is superior to all other similar competitors. It allows full and safe use of its exceptional technical and flight capabilities. Designed for continued flight training, night and IFR training flights, air patrolling, rescue flights and courier service.

AIRCRAFT STRUCTURE

Unique all-metal riveted body. The main beam of the central wing is furnished with nitrogen overpressure control. The landing gear is also designed to operate on unpaved runways. The aircraft can be fitted with a digital system according to customers’ requirements.

1350 kg – Max. take-off weight
1100 km – Max. range
+3,8/-1,5 – Load factor

Videos Z 143 LSi GENIUS 1 2

The low-wing airplane concept and canopy construction allow unlimited and excellent visibility thanks to non-replicable construction solutions. It is an advantage during flight operations, when landing, taxiing, and in the event of an emergency exit from the cockpit.

The safe-life system is used to monitor and evaluate the lifetime of the airplane. This exceeds 20,000 flight hours.

ENGINE

The American Textron Lycoming injection engine, coupled with a constant speed propeller, excellent airplane flight characteristics, and precise and responsive control, allows for various training activities and maneuvers to be executed.

The powerful engine allows for all requirements to be met, particularly when training new pilots. Engine operating time at maximum revolutions is unlimited.

The MTV-9-B /195-45 three-blade composite propeller is hydraulically adjustable with constant speed.

235 HP at 2400rpm
35 litres per hour in economical mode

GARMIN AVIONICS

The Garmin G500 multifunctional avionics modified for the ZLIN Z 143 LSi GENIUS integrates all essential flight and engine instruments into digital screens.

The 3D terrain viewing feature is an invaluable tool. The system, coupled with autopilot, is set for maximum use and intuitive control. It allows pilots to gain a unique view of the situation and thus increase crew safety.

Complex data is collected in real-time and displayed on two adjustable, large, high-resolution screens.

OPTOELECTRONIC DEVICES

Upon request, we can install a FLIR camera or other digital suspension system on the ZLIN Z 143 LSi GENIUS for aerial monitoring, search and rescue missions.

AIRCRAFT INTERIOR

The spatially exceptional design of the all-glass canopy allows a perfect overview of what is happening around the aircraft. The canopy opens reliably in all situations in a simple forward motion. It is equipped with a stopping mechanism and an emergency jettison system.

The layout of the control elements and instruments contributes to the comfort of the crew. The training aircraft can be controlled from both pilot seats independently.

Ergonomically precisely shaped and adjustable seats are a must component of a ZLIN aircraft today.

The interior layout allows easy reconfiguration from a four-seater to two-seater with an additional fuel tank. Sufficient luggage space is also available..

RECONNAISSANCE AIRPLANE? NO PROBLEM!

Upon request, we can install a FLIR camera or other digital suspension system for aerial monitoring, search and rescue missions on the ZLIN Z 143 LSi GENIUS.

Key features of ZLIN Z 134 LSi GENIUS

Easy conversion from 4-seater to 2-seater
All aluminium structure
Both sides stick flight control
Easy controllability
High manoeuvrability
Simple and easy maintenance
Category N/U
Night and IFR training

Technical details - ZLIN Z 143 LSi GENIUS

Category	Utility		Normal
	▼ Metric	▼ Imperial	▼ Metric	▼ Imperial
Empty weight	855 kg	1885 lbs	855 kg	1885 lbs
Max. take-off weight	1350 kg	2976 lbs	1080 kg	2380 lbs
Load factor (g)	+3,8 / -1,5	+3,8 / -1,5	+4,4 / -1,8	+4,4 / -1,8
Takeoff distance (ground roll)	295 m	968 ft	170 m	558 ft
Takeoff distance (over 50 ft obstacle)	640 m	2100 ft	450 m	1476 ft
Max. rate of climb - sea level	4,9 m/s	965 ft/min	7,4 m/s	1457 ft/min
Max speed (IAS) - sea level	259 km/h	140 knots	259 km/h	140 knots

Main tanks capacity	2 × 61 litres	2 × 16,1 gals	2 × 61 litres	2 × 16,1 gals
Auxiliary tanks capacity	2 × 51 litres	2 × 13,4 gals
Range (2200 RPM, 10000 ft, max. fuel capacity)	1100 km	599 NM	460 km	248 NM

Basic dimensions
	▼ Metric	▼ Imperial
Wing span	10,14 m	33,25 ft
Length	7,58 m	24,86 ft
Height	2,91 m	9,55 ft

Engine
Manufacturer		TEXTRON Lycoming, USA
Type		IO-540-C4D5
Max. power (2400 RPM)		235 HP
Max. cruising power (2200 RPM)		175 HP
Economy cruising power (2000 RPM)		140 HP

Propeller (constant speed)
Manufacturer		MT Propeller, Germany
Type		MTV-9-B/195-45a (three-blade)

Utility	Metric	Imperial
Empty weight	855 kg	1885 lbs
Max. take-off weight	1350 kg	2976 lbs
Load factor (g)	+3,8 / -1,5	+3,8 / -1,5
Take-off distance (ground roll)	295 m	968 ft
Take-off distance (over 50 ft obstacle)	640 m	2100 ft
Max. rate of climb (sea level)	4,9 m/s	965 ft/min
Max speed (IAS) (sea level)	259 km/h	140 knots
Main tanks capacity	2 × 61 litrů	2 × 16,1 gals
Range (2200 RPM, 10000 ft, max. fuel capacity)	1100 km	599 NM

Normal	Metric	Imperial
Empty weight	855 kg	1885 lbs
Max. take-off weight	1080 kg	2250 lbs
Load factor (g)	+4,4 / -1,8	+4,4 / -1,8
Take-off distance (ground roll)	170 m	558 ft
Take-off distance (over 50 ft obstacle)	450 m	1476 ft
Max. rate of climb (sea level)	7,4 m/s	1457 ft/min
Max speed (IAS) (sea level)	259 km/h	140 knots
Main tanks capacity	2 × 61 litrů	2 × 16,1 gals
Range (2200 RPM, 10000 ft, max. fuel capacity)	460 km	248 NM