Specification & Performance Overview:

The M601-B turboprop engine weighs 190kg's and provides a maximum power output of 760hp. As you would imagine, this powerplant provides excellent performance characteristics and delivers enough power to give great multi-surface STOL performance. The reverse link system further aids STOL by reversing the propeller pitch during the landing run.

Year of manufacture:

1980, TTSN 941 hrs

Total Time:

TTSN: 941 hrs

Engine Year & Type:

1979, Walter M601-B 760hp Turboprop (Czech. S.S.R)

Engine Weight:

190kg (418lbs)

Engine Time:

TTSN: 2,825 hrs

Engine SMOH:

0 hrs

Propeller Year & Type:

1986, V508-B (Czech. S.S.R)

Propeller Time:

2,183 hrs, Propeller SMOH: 0 hrs

Fuel Type:

TC-1 Diesel

Fuel capacity:

*320-480 litres

Crew/passengers:

2/4 (with flexible seating)

Category/Avionics:

Touring, IFR

Duration:

*3.5-6hrs + 45min reserve

Range (~80lph):

*1,000-1,900km,
560m-1,200m

Take-off run:

*250m, 820ft

Landing distance:

*250m, 820ft

Service ceiling:

4,000m

Commercial load:

780kg

Max. take-off mass:

1,900kg

Fuel mass:

390kg

Undercarriage Year of Manufacture:

New (made to order)

Undercarriage Type:

Alluminium, Plastic

Dimension L/S/H

9.2m/11.2m/3.4m

Additional Items:

Log books, tool box, covers, 2 headsets, 2 parachutes, 2 life jackets, Western manual