IL-76

General characteristics

Crew: five

Payload: 42 tonnes (Il-76M), 48 tonnes (Il-76MD), 60 tonnes (Il-76MD-90A) ()

Length: 46.59 m (152 ft 10 in)

Wingspan: 50.5 m (165 ft 8 in)

Height: 14.76 m (48 ft 5 in)

Empty weight: 92,500 kg (Il-76TD-90)[nb 1] (203,962 lb)

Max. takeoff weight: 195,000 kg (Il-76)[nb 2] (429,975 lb (Il-76TD-90))

Powerplant: 4 × Aviadvigatel PS-90-76 turbofans

 

Performance

Maximum speed: 900 km/h

Range: 5,000 km (2,700 nmi)

Service ceiling: 13,000 m (42,700 ft)

Wing loading: 566.7 kg/m² (Il-76M/T)

Thrust/weight: (Il-76)

minimal landing run: 450 m with thrust reversal

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IL-96

General Characteristics

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Wingspan 147.3ft (44.9m)

Length 134.5ft (41.0m)

Height 41.2ft (12.6m)

Empty Weight 86,587lbs (39,275kg)

Loaded Weight 303,333lbs (137,590kg)

 

Performance

Power/Weight Ratio 0.889

Wing Loading 117.6lbs/ft2 (574.1kg/m2)

Wing Area 2,579.9ft2 (239.7m2)

Drag Points 51376

TU-204

General characteristics

Crew: 2 (3 on -120CE Freighter, Captain, First Officer and Flight Engineer)

Capacity: Tu-204-100/Tu-214: 212 in single class,

Tu-204-300: 166 in single class

Length: 46.10 m (151 ft 3 in)

Wingspan: 41.80 m (137 ft 2 in)

Height: 13.90 m (45 ft 7 in)

Wing area: 182.4 m² (1963 ft²)

Empty weight: Tu-204-100: 58,300 kg (128,530 lb)

Max takeoff weight: Tu-204-100: 107,500 kg

Powerplant: 2× Tu-204-100: Aviadvigatel PS-90A turbofans

 

Performance

Maximum speed: 900 km/h (560 mph)

Cruise speed: 810 to 850 km/h (500 to 530 mph)

Range: (Tu-204-100) 6,500 km (Tu-204-120) 6,300 km (Tu-214)

6,700 km (Tu-204-300) 8,500 km ()

 

 

An-32

General characteristics

Crew: 4

Capacity: 42 paratroopers/50 passengers/24 Casualties on stretcher with three medical personnel

Length: 23.78 m (78 ft 0¾ in)

Wingspan: 29.20 m (95 ft 9½ in)

Height: 8.75m (28 ft 8½ in)

Wing area: 75 m² (807 ft²)

Empty weight: 16,800 kg (37,038 lb)

Max. takeoff weight: 27,000 kg (59,400 lb)

Powerplant: 2 × ZMKB Progress AI-20DM turboprop, 3,812 kW (5,112 ehp) each

 

Performance

Maximum speed: 530 km/h (286 knots, 329 mph)

Cruise speed: 470 km/h (254 knots, 292 mph) (econ cruise)

Range: 2,500 km (1,350 nmi, 1,553 mi)

Service ceiling: 9,500 m (31,165 ft)

An-124

General characteristics

Crew: 4–6 (pilot, copilot, navigator, senior flight engineer

 

Capacity

88 passengers or the hold can take an additional

350 on a palletised seating system

Payload: 150,000 kg (330,000 lb)

Length: 68.96 m (226 ft 3 in)

Wingspan: 73.3 m (240 ft 5 in)

Height: 20.78 m (68 ft 2 in)

Wing area: 628 m² (6,760 sqft)

Empty weight: 175,000 kg (385,000 lb)

Loaded weight: 405,000 kg (893,000 lb)

Powerplant: 4 × Progress D-18T turbofans, 229.5 kN (51,600 lbf) each

 

 

Performance

Maximum speed: 865 km/h (467 kn (537 mph))

Cruise speed: 800–850 km/h (430 kn (490 mph))

Range: 5,200 km (2,808 nm, 3231 mi)

Service ceiling: 12,000 m (39,370 ft)

Wing loading: 365 kg/m² (74.7 lb/sqft)

An-140

General characteristics

Crew: two

Capacity: 52 passengers

Length: 22.60 m (74 ft 2 in)

Wingspan: 24.505 m (80 ft 5 in)

Height: 8.23 m (27 ft 0 in)

Wing area: 51 m² (549 ft²)

Empty weight: 12,810 kg (28,240 lb)

Max. takeoff weight: 21,500 kg (47,350 lb)

Powerplant: 2 × Klimov TV3-117VMA-SBM1 turboprops

Alternate power plant: Pratt & Whitney Canada PW127A turboprops, 1,900 kW (2,500 shp) each

 

Performance

Maximum speed: 575 km/h (310 knots, 357 mph)

Cruise speed: 460 km/h (250 knots, 290 mi)

Range: 1380 km / 2420 km (745 nm, 860 mi / 1307 nm, 1504 mi) [32]

Ferry range: 3,680 km (1,990 nm, 2,290 mi)

Service ceiling: 7600 m (25,000 ft)

Rate of climb: 6.83 m/s (1,345 ft/min)

 

 

Be-200

General characteristics

Crew: 2

Length: 32.0 m (105 ft 0 in)

Wingspan: 32.8 m (107 ft 7 in)

Height: 8.9 m (29 ft 2 in)

Wing area: 117.4 m² (1,264 ft²)

Empty weight: 27,600 kg (60,850 lb)

Max Take Off Weight (Land): 41,000 kg (90,390 lb)

Max Take Off Weight (Water): 37,900 kg (83,550 lb)

Max Capacity (Water or Retardant): 12,000 kg (26,450 lb)

Max Capacity (Cargo): 7,500 kg (16,530 lb)

Max Capacity (Passengers): 44 (Be-200ES) 72 (Be-210)

Powerplant: 2 × Progress D-436TP turbofans, 7,500 kgf (16,534 lbf) each

 

Performance

Maximum speed: 700 km/h (435 mph)

Cruise speed: 560 km/h (348 mph)

Economy speed: 550 km/h (342 mph)

Landing speed: 200 km/h (124 mph)

Takeoff speed: 220 km/h (137 mph)

Minimum speed (Flaps 38°): 157 km/h (98 mph)

Range: 2,100 km (1,305 mi)

L-410

General Characteristics

Capacity: 19 passengers or 1,615 kg (3,560 lb) of cargo

Length: 14.42 m (47 ft 4 in)

Wingspan: 19.48 m[45] (63 ft 11 in)

Height: 5.83 m (19 ft 1½ in)

Wing area: 34.86 m² (375.2 ft²)

Empty weight: 3,985 kg (8,785 lb)

Max. takeoff weight: 6,400 kg (14,110 lb)

Powerplant: 2 × Walter M601E turboprop engines

 

Performance

Maximum speed: 380 km/h (205 knots, 236 mph) at 4,200 m (13,800 ft) (max cruise)

Cruise speed: 365 km/h (197 knots, 227 mph) (econ cruise)

Range: 1,380 km (744 nm, 857 mi) (max fuel)

Service ceiling: 6,320 m (20,725 ft)

Rate of climb: 7.4 m/s (1,455 ft/min)

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Fax: +7 495 660 08 58

 

Russia, Moscow region,

city district Khimki, md. Klyazma, d. 1B,

Industrial Park "Sheremetyevo"