AS 350

Crew: 1
Capacity: 5
Length: 10.93 m[40] (35 ft 10½ in)
Rotor diameter: 10.7 m (35 ft 1 in)
Height: 3.14 m (10 ft 3½ in)
Disc area: 89.75 m² (966.1 sq ft)
Empty weight: 1,174 kg (2,588 lb)
Max. takeoff weight: 2,250 kg (4,960 lb)
Powerplant: 1 × Turbomeca Arriel 2B turboshaft, 632 kW (847 shp)

Performance

Never exceed speed: 287 km/h (155 knots, 178 mph)
Cruise speed: 245 km/h (132 knots, 152 mph)
Range: 662 km (357 nmi, 411 mi)
Endurance: 4.1 hrs
Service ceiling: 4,600 m (15,100 ft)
Rate of climb: 8.5 m/s (1,675 ft/min)

SA 365

Crew: 1 or 2 pilots
Capacity: 11 passengers
Length: 13.73 m (45 ft 1 in)
Height: 4.06 m (13 ft 4 in)
Empty weight: 2,411 kg (5,315 lb)
Max takeoff weight: 4,300 kg (9,480 lb)
Powerplant: 2 × Turboméca Arriel 2C turboshaft, Take-off Power, 625 kW (838 hp) each
Main rotor diameter: 11.94 m (39 ft 2 in)
Main rotor area: 111.98 m2 (1,205.3 sq ft)

Performance

Maximum speed: 306 km/h (190 mph; 165 kn)
Ferry range: 827 km (514 mi; 447 nmi)
Service ceiling: 5,865 m (19,242 ft)
Rate of climb: 8.9 m/s (1,750 ft/min)

Robinson 44

Crew: one or two pilots
Capacity: four, including pilot
Payload: 748 lb (340 kg)
Length: 459" (11,65 m)
Rotor diameter: 33 ft (10.1 m)
Tail rotor diameter: 4 ft 10 in (1.5 m)
Height: 10 ft 9 in (3.3 m)
Empty weight: 1,450 lb (657.7 kg)
Loaded weight: 2,500 lb (1,134 kg)
Powerplant: 1 × Lycoming IO-540-AE1A5 6 cylinder, flat engine with fuel injection, 245 bhp (183 kW)
Fuel: 100 low lead (100LL) fuel or 100/130.

Performance

Maximum speed: 130 kn (240 km/h; 150 mph)
Cruise speed: 110 kn (200 km/h; 130 mph)
Range: 300 nmi (560 km; 350 mi)
Altitude restrictions: 14,000 ft (4,300 m) density altitude or 9,000 ft (2,700 m) above ground level in order to be able to reach ground within 5 minutes in case of fire.

AS 332

Crew: 2
Capacity: 19
Length: 16.29 m (53.44 ft)
Rotor diameter: 15.6 m (51.18 ft)
Height: 4.80 m (15.09 ft)
Empty weight: 4,500 kg (9,920 lb)
Useful load: 4,100 kg (9,040 lb)
Max. takeoff weight: 8,600 kg (18,960 lb)
Powerplant: 2 × Turbomeca Makila 1A1 turboshaft, 1,300 kW (1,742 shp) each

Performance

Never exceed speed: 278 km/h @ 8,600 kg gross (150 kt)
Maximum speed: 262 km/h @ 8,600 kg gross (141 kt)
Cruise speed: 252 km/h @ 8,600 kg gross (136 kt)
Range: 841 km @ 8,600 kg gross (454 nm)
Service ceiling: 6,100 m (20,000 ft)
Rate of climb: 8.2 m/s @ 70 kt & 8,600 kg gross (1,620 ft/m @ 70 kt)

S-92

Crew: 2 (pilot, co-pilot)
Capacity: 19 passengers
Length: 56 ft 2 in (17.10 m)
Rotor diameter: 56 ft 4 in (17.17 m)
Height: 15 ft 5 in (4.71 m)
Empty weight: 15,500 lb (7,030 kg)
Loaded weight: 26,500 lb (12,020 kg)
Max. takeoff weight: 26,500 lb (12,020 kg)
Powerplant: 2 × General Electric CT7-8A turboshaft, 2,520 shp (1,879 kW) each
Fuselage length: 56 ft 2 in (17.1 m)
Fuselage width: 17 ft 3 in (5.26 m)
Rotor systems: Main rotor has 4 blades. From the main gearbox a set of driveshafts connect to the tail gearbox to turn the 4-blade tail rotor.
Cabin dimensions: 20 ft long by 6.6 ft tall[80]

Performance

Maximum speed: 165 knots (190 mph, 306 km/h)
Cruise speed: 151 kn, 174 mph (280 km/h)
Range: 539 nmi (999 km)
Service ceiling: 14,000 ft (4,270 m)

EC 120

Crew: 1 or 2 pilots
Capacity: 4 passengers
Length: 9.6 m (31 ft 5 in)
Rotor diameter: 10.0 m (32 ft 8 in)
Height: 3.4 m (11 ft 2 in)
Empty weight: 991 kg (2,185 lb)
Useful load: 724 kg (1,596 lb)
Max. takeoff weight: 1,715 kg (3,781 lb)
Powerplant: 1 × Turbomeca Arrius 2F turboshaft, 376 kW (504 shp)

Performance

Never exceed speed: 278 km/h (150 knots, 172 mph)
Cruise speed: 223 km/h (120 knots, 138 mph)
Range: 710 km (383 nm, 440 mi)
Service ceiling: 5,182 m (17,000 ft)
Rate of climb: 5.84 m/s (1,150 ft/min)

AW109

Crew: 1 or 2
Capacity: 6 or 7 passengers
Length: 11.448 m (37 ft 7 in) fuselage
Width: 2.88 m (9 ft 5 in)
Height: 3.50 m (11 ft 6 in)
Empty weight: 1,590 kg (3,505 lb)
Max takeoff weight: 2,850 kg (6,283 lb)
Powerplant: 2 × Pratt & Whitney Canada PW206C Turboshaft engine, 418 kW (561 hp) each
Main rotor diameter: 11.00 m (36 ft 1 in)

Performance

Maximum speed: 285 km/h (177 mph; 154 kn)
Ferry range: 932 km (579 mi; 503 nmi)
Rate of climb: 9.8 m/s (1,930 ft/min)

Bell 214

Crew: 2
Capacity: 3,880 lb including 14 troops, or 6 stretchers, or equivalent cargo
Length: 48 ft 0 in (14.63 m))
Rotor diameter: 50 ft 0 in (15.24 m)
Height: 12 ft 10 in (3.90 m)
Empty weight: 7,588 lb (3,442 kg)
Loaded weight: 13,800 lb (6,260 kg)
Max. takeoff weight: 15,000 lb with slung load (6,805 kg)
Powerplant: 1 × Lycoming LTC4B-8D turboshaft, 2,930 shp (2,185 kW)

Performance

Cruise speed: 140 knots (260 km/h, 161.5 mph)
Range: 255 mi (475 km)
Service ceiling: 16,400 ft density altitude (5,000 m)

EC 135

Crew: 1 pilot
Capacity: up to seven passengers or two crew and two patients (Air Ambulance variant) or 1,455 kg (3,208 lb) payload
Length: 12.16 m (39 ft 11 in)
Height: 3.51 m (11 ft 6 in)
Empty weight: 1,455 kg (3,208 lb)
Max takeoff weight: 2,910 kg (6,415 lb)
Powerplant: 2 × Turboméca Arrius 2B2 turboshaft engines, 472 kW (633 hp) each
or 2 x Pratt & Whitney Canada PW206B turboshaft engines rated at 463 kW (621 hp) (take-off power)
Main rotor diameter: 10.2 m (33 ft 6 in)
Main rotor area: 81.7 m2 (879 sq ft)

Performance

Cruising speed: 254 km/h (158 mph; 137 kn)
Never exceed speed: 287 km/h (178 mph; 155 kn)
Range: 635 km (395 mi; 343 nmi)
Service ceiling: 6,096 m (20,000 ft)
Rate of climb: 7.62 m/s (1,500 ft/min)

EC 130

Crew: 1 (pilot in left seat)
Capacity: 6 passengers (2 at front and four at back) can be modified to take 7 passengers (3 at front and four at back)
Length: 10.68 m (35 ft)
Rotor diameter: 10.69 m (35 ft 1in)
Height: 3.34 m (10 ft 11 in)
Empty weight: 1,377 kg (3,036 lbs)
Useful load: 1,050 kg (2,315 lbs)
Max. takeoff weight: 2,427 kg (5,351 lbs)
Powerplant: 1 × Turbomeca Arriel 2B1 turboshaft, 632 kW (847 shp)

Performance

Never exceed speed: 287 km/h (155 knots, 178 mph)
Cruise speed: 240 km/h (130 knots, 150 mph)
Range: 610 km (329 nm, 378 mi)
Service ceiling: : 4,770 m (15,655 ft)
Rate of climb: 9.0 m/s (1,770 ft/min)

AS 355

Crew: 1
Capacity: 6
Length: 12.94 m (42 ft 5½ in)
Rotor diameter: 10.69 m (35 ft 0¾ in)
Height: 3.14 m (10 ft 3½ in)
Disc area: 89.75 m² (966 sq ft)
Empty weight: 1,305 kg (2,877 lbs)
Max. takeoff weight: 2,540 kg[27] (5,732 lbs)
Powerplant: 2 × Allison 250-C20F turboshaft, 313 kW (420 shp) each

Performance

Never exceed speed: 278 km/h (150 knots, 172 mph)
Cruise speed: 224 km/h (121 knots, 139 mph)
Range: 703 km (380 nm, 437 mi)
Service ceiling: 3,400 m (11,150 ft)
Rate of climb: 6.5 m/s (1,280 ft/min)