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FLEET
For our 6 types of flight services, we offer a truly complete and competitive fleet. Planes of different sizes serve you best, even on unthinkable itineraries.
LET 410 / 410 NG MICRO RANGE - 1500 NMI
Length 14.42 m
Wingspan 19.48 m
Height 5.83 m
Wing surface area 35.18 m²
Empty weight 3,725 kg
Load weight 5,800 kg
Max take-off weight 6,400 kg Passengers 19
Capacity 1,710 kg of goods
Engine Two turboprops Walter M601E GE Aviation Н80-200
Power 560 kW
Max speed 410S 388 km/h (210 kn) 410NG 440 km/h (238 kn)
Cruising speed: 410S 311 km/h (168 kn), 410NG 390 km/h (221 kn)
Rate of climb 468 m/min (1,535 ft/min)
Range 410S 1,040 km (562 nmi), 410NG 2,000 km (1,079 nmi)
Service altitude 7,000 m (22,966 ft)
See LET 410 in our livery
See the seating configuration
DASH Q8 100/200 MICRO AND SHORT RANGE - 800 NMI
Length 22.25 m
Wingspan 25.91 m
Fuselage diameter 2.69 m
Height 7.49 m
Wing surface area 54.4 m²
Empty weight 10,250 kg
Max take-off weight 15,650 kg
Passengers 36
Pratt & Whitney Canada PW 120A turboprop 2 engine with four-bladed propeller
Power 2 000 shp (1 490 kW) each
Max speed 490 km/h (265 kt)
Cruising speed 440 km/h (237 kt)
Rate of climb 1,560 ft/min
Range 1,520 km (0,8 nmi)
Service altitude approx. 8 000 m
Tangency approx. 10 000 m
Notes The dimensions, load capacities and motors vary depending on the versions.
See DASH Q8 100/200 in our livery
See the seating configuration
DASH Q8 300 MICRO AND SHORT RANGE - 800 NMI
Length 25.68 m
Wingspan 25.91 m
Fuselage diameter 2.69 m
Height 7.49 m
Wing surface area 54.4 m²
Empty weight 10,250 kg
Max take-off weight 15,650 kg
Passengers 50
Pratt & Whitney Canada PW 120A turboprop 2 engine with four-bladed propeller
Power 2 000 shp (1 490 kW) each
Max speed 490 km/h (265 kt)
Cruising speed 440 km/h (237 kt)
Rate of climb 1,560 ft/min
Range 1,520 km (0,8 nmi)
Service altitude approx. 8 000 m
Tangency approx. 10 000 m
See DASH Q8 300 in our livery
See the seating configuration
DASH Q8 400/400NG SHORT RANGE - 1300 NMI
Length 32,80 m
Wingspan 28.41 m
Fuselage diameter 2.69 m
Height 8.40 m
Wing surface area 64.2 m²
Empty weight 17,885 kg
Max take-off weight 30,481 kg
Passengers 78
Pratt & Whitney Canada PW 150 turboprop 2 engine with four-bladed propeller
Power 5071 shp (3 800kW) each
Max speed 667 km/h (360 kt)
Cruising speed 600 km/h (324 kt)
Rate of climb 1,200 ft/min
Range 2,040 km (1,300 nmi)
Service altitude approx. 8 300 m
Tangency approx. 10 000 m
See DASH Q8 400/400NG in our livery
See the seating configuration
AIRBUS A318 MEDIUM-LONG RANGE - 3,100 NMI
Length 31.45 m
Wingspan 34.10 m
Fuselage diameter 4.14 m
Wing arrow 25°
Height 12.89 m
Wing surface area 122.4 m²
Empty weight 39,500 kg
Load weight 61 900 kg
Max take-off weight 61,500 kg
Passengers 137
Fuel capacity 23 859 L Turbofan engine 2:CFM56-5B
Thrust 85-104 kN
Max speed 0.82 Mach (1 012.54 km/h)
Cruising speed 0.78 Mach (963 km/h)
Range 5,750 km (3,100 nmi)
Tangency 12 131 m (39 800 ft)
See Airbus A318 in our livery
See the seating configuration
AIRBUS A319 MEDIUM-LONG RANGE - 3,100 NMI
Length 33.84 m
Wingspan 34.10 m
Fuselage diameter 4.14 m
Wing arrow 25°
Height 12.11 m
Wing surface area 124.0 m²
Empty weight 40,800 kg
Load weight 70 400 kg
Max take-off weight 70,000 kg
Passengers Up to 143
Fuel capacity 23 859 L Turbofan engine 2:CFM56-5B
Thrust 90-120 kN
Max speed 0.82 Mach (1 012.54 km/h)
Cruising speed 0.78 Mach (963 km/h)
Range 6,950 km (3,750 nmi)
Tangency 11,918 m (39,100 ft)
See Airbus A319 in our livery
See the seating configuration
AIRBUS A320 MEDIUM-LONG RANGE - 3350 NM
Length 37.57 m
Wingspan 34.10 m
Fuselage diameter 4.14 m
Wing arrow 25°
Height 12.11 m
Wing surface area 124.0 m²
Empty weight 40,800 kg
Load weight 70 400 kg
Max take-off weight 70,000 kg
Passengers Up to 186
Fuel capacity 23 859 L Turbofan engine 2:CFM56-5B
Thrust 90-120 kN
Max speed 0.82 Mach (1 012.54 km/h)
Cruising speed 0.78 Mach (963 km/h)
Range 6,200 km (3,350 nmi)
Tangency 11,918 m (39,100 ft)
See Airbus A320 in our livery
See the seating configuration
AIRBUS A321 MEDIUM-LONG RANGE - 3200 NM
Length 44.51 m
Wingspan 34.10 m
Fuselage diameter 4.14 m
Wing arrow 25°
Height 12.11 m
Wing surface area 128.0 m²
Empty weight 48,500 kg
Load weight 83 400 kg
Max take-off weight 83,000 kg
Passengers 223
Fuel capacity 23 700 L Turbofan engine 2:CFM56-5B
Thrust 129-142 kN
Max speed 0.82 Mach (1 012.54 km/h)
Cruising speed 0.78 Mach (963 km/h)
Range 5,950 km (3,200 nmi)
Tangency 11,918 m (39,100 ft)
See Airbus A321 in our livery
See the seating configuration
AIRBUS A340 300/500/600 LONG RANGE
Length 63.69 m (300), 67.93 m (500), 75.36 m (600)
Wingspan 60.30 m
Fuselage diameter 5.64 m
Wing arrow 31°
Height 16.99 m
Wing area 361.6 m² (300), 437.3 m² (500/600)
Empty weight 131 000 kg (300), 168 000 kg (500), 174 000 kg (600)
Load weight 257 900 kg (300), 369 200 kg (500), 381 200 kg (600)
Max take-off weight 257 900 kg (300), 369 200 kg (500), 381 200 kg (600)
Passengers 279 (300), 240 (500), 306 (600)
Fuel capacity 140 640 L (300), 214 808 L (500), 198 139 L (600)
4 CFM56-5C turbofan engine
Thrust 126-151 kN
Max speed 0.86 Mach (1 061.93 km/h)
Cruising speed 0.82 Mach (1 012.54 km/h)
Range 13 500 km (7 300 nmi) (300), 9 000 nmi 16 670 km (500), 7 800 nmi 14 450 km (600)
Tangency 12,527 m (41,100 ft)
See AIRBUS A340/ 300 in our livery
See the configuration A340/300
See the configuration A340/500
See the configuration A340/600
See the seating configuration
AIRBUS A 380 LONG RANGE
Length 72.57 m
Wingspan 79.75 m
Fuselage diameter 7.14 m
Wing arrow 33.5°
Height 24.27 m
Wing surface area 845.0 m²
Empty weight 277 000 kg
Load weight 512 000 kg
Max take-off weight 510,000 kg
Passengers 466
Fuel capacity 323 546 L
Turbofan engine 4: EA GP7200
Thrust 327-357 kN
Max speed 0.89 Mach (1 098.72 km/h)
Cruising speed 0.85 Mach (1 049.58 km/h)
Range 15,200 km (8,200 nmi)
Tangency 13,136 m (43,000 ft)
See AIRBUS A380 in our livery
See the configuration
A380 will be in the fleet from the beginning of the 2026 season
BRITTEN NORMAN BN2 ISLANDER TAXI MICRO RANGE
Length 10.86 m (35 ft 8 in)
Wingspan 14.94 m (49 ft 0 in)
Height 4.18 m (13 ft 9 in)
Wing area 30.2 m² (325 ft²)
Wing loading 9.78 kg/m² (20 lb/ft²)
Empty weight 1,667 kg (3,675 lb)
Max takeoff weight 2,994 kg (6,600 lb) Passengers 9
2 Lycoming O-540-E4C engines
Power 260 hp (195 kW)
Max speed 273 km/h (170 mph)
Cruising speed 257 km/h (160 mph)
Rate of climb 295 m/min (970 ft/min)
Range 1,400 km (874 mi)
Tangency 4,024 m (13,200 ft)
See the BN2 Islander in our TwitAir (AviaROMA group) livery
See the seating configuration
AGUSTA WESTLAND AW 109E GRAND ELICOPTER TAXI
Length 13.04 m
Wingspan 3.5 m
Rotor diameter 11.0 m
Empty weight 1,576 kg
Max take-off weight 3,000 kg
Capacity 2 094 kg
2 Pratt & Whitney Canada 206C turbine engine Power 423 kW (567 shp) each
Max speed 285 km/h (154 kt)
Autonomy 859 km
Tangency 5,974 m (19,600 ft)
See AW109 in our livery