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Fleet

7 Ask-21 gliders

Two-seater glider with high technologies, with back T-tail and fixed landing gear, designed in fiberglass. 
Wingspan 17 m.
Wing area 17,9 m2
Maximum weight at take-off 600 Kg.
Weight when empty 360 Kg.
Maximum speed 280 Km./h
Stall speed 65 Km./h
Gliding coefficient 1:35
Use of School flights, Cross Country

7 Twin Astir gliders

Two-seater glider with high technologies, with back T-tail and fixed landing gear, designed in fiberglass.
Wingspan 17,5 m.
Wing area 17,8 m2
Maximum weight at take-off 580 Kg.
Empty weight 380 Kg.
Maximum speed 250 Km./h
Stall speed 70 Km./h
Gliding coefficient 1:37
Use of School flights, Cross Country

5 PW-5 gliders

Single-seater glider in fiberglass and fixed landing gear.

Wing span 13,44 m.
Wing area 10,16 m2
Maximum weight at take-off 300 Kg.
Weight when empty 190 Kg.
Maximum speed 213 Km./h
Stall speed 65 Km./h
Gliding coefficient 1:32
Use of training flights, Cross Country

1 Astir Club glider

Single-seater glider with back T-tail and fixed landing gear, designed in fiberglass.

Wingspan 15 m.
Wing area 12,4 m2
Maximum weight at take-off 380 Kg.
Empty Weight 260 Kg.
Maximum weight 250 Km./h
Stall speed 70Km./h
Gliding coefficient 1:37
Use of training flights, Cross Country

3 Rallye 180 aircraft

Single-engined aircraft with capacity for 4 seats, with fixed pitch blade and landing gear.

Wingspan 9,74 m.
Lycoming O-360-A3 engine

2 Robin DR-400 aircraft

Single-engined aircraft with capacity for 4 seats, with fixed pitch blade and landing gear.

Wingspan 9,44 m.
Lycoming O-360-A3A engine of 180 Hp
Maximum weight at take-off 1.000 Kg.
Weight when empty 560 Kg.
Maximum speed 308 Km./h
Cruising speed 200 Km./h
Glider towing use

3 Tobago TB-10 aircraft

Single-engined aircraft with capacity for four seats with fixed pitch blade and landing gear.

Wingspan 9,98 m.
Lycoming O-360-A1AD engine of 180Hp.
Maximum weight at take-off 1.150 Kg.
Weight when empty 700 Kg.
Maximum speed 320 Km./h
Cruising speed 235 Km./h
Use of School flights of Pilots and renting

1 single-engined Dimona H-36

Two-seater motorglider manufactured in fiberglass, with a T-type stabilizer and fixed landing gear with castoring tailwin.
Wingspan/ Wing Length./ Area.: 16m/ 6,85m/15,20m2
Limbach L2000 EB1/ 80Hp engine at 3400 rpm.
Hoffmann 160T blade with 3 positions available
Weight when empty 770/530 Kg.
Maximum stall speed 275/70 Km./h
Use of School flights and renting