IL-96-400T Atlant-Soyuz Airlines "2005s" Colors. RA-96102 Enrute to the gate

 
 

 

IL-96-400T Atlant-Soyuz Airlines "2005s" Colors. RA-96102 Docking gate A12 Terminal 1

 
     
 
Measurement Il-96-300 Il-96M Il-96T Il-96-400
Length 55.3 m (181 ft 7 in) 64.7 m (212 ft 3 in) 63.939 m (209 ft 9.28 in)
Span 60.11 m (197 ft 3 in)
Wing area 350 m (3767.9 ft)
Wing sweep 30
Flaps/Slats I - 2/3 (275 KIAS), II - 3/25 (264 KIAS), III - 10/25 (243 KIAS),
IV - 25/25 (210 KIAS) for Takeoff, V - 40/25 (189 KIAS) for Landing
Cabin width 5.70 m (18.70 ft)
Fuselage Diameter 6.08 m (19.94 ft)
Height 15.7 m (57 ft 7 in)
Operating Empty Weight 120,400 kg (265,198 lb) 132,400 kg (291,630 lb) 116,400 kg (256,387 lb) 122,300 kg (269,383 lb)
Max. Zero Fuel Weight 180,000 kg (403,000 lb)   208,400 kg (459,030 lb)
Max. Landing Weight 183,000 kg (403,083 lb) 220,000 kg (484,581 lb) 220,000 kg (484,581 lb) 220,000 kg (484,581 lb)
Max. Take-off Weight 250,000 kg (551,000 lb) 270,000 kg (595,000 lb) 270,000 kg (594,713 lb) 265,000 kg (583,700 lb)
Max. Payload 40,000 kg (88,105 lb) 58,000 kg (127,753 lb) 92,000 kg (202,643 lb) 58,000 kg (127,753 lb)
Takeoff Run at MTOW 2,340 m (7,677 ft) 3,000 m (9,843 ft) 2,700 m (8,858 ft) 2,700 m (8,858 ft)
Landing Run 860 m (2,821 ft) 1,800 m (5,906 ft) 1,650 m (5,511 ft) 1,650 m (5,511 ft)
Cruising speed 0.78 to 0.84 Mach or 850 to 870 km/h TAS (459 to 469 KTAS)
Maximum speed (Vmo) 0.84 Mach or 900 km/h IAS (485 KIAS)
Service ceiling 13,100 m (43,000 Ft)
Cruise Altitude 9,000 to 12,000 m (29,527 to 39,370 Ft)
Range with max. payload 11,500 km (6,209 nmi) 12,800 km (6,907 nmi) 5,000 km (2,699 nmi) 10,000 km (5,400 nmi)
Range with max. fuel 13,500 km (7,289 nmi) 15,000 km (8,100 nmi) 12,000 km (6,479 nmi) 12,000 km (6,479 nmi)
Max. Fuel capacity 152,620 l (40,322 US gal)
Engines (x4) Aviadvigatel PS-90A Pratt & Whitney PW2000 Pratt & Whitney PW2337
or
Aviadvigatel PS-90A1
Aviadvigatel PS-90A1
Thrust (x4) PS-90A: 16,000 kg
(35,242 lb)
N2:10,425 RPM
17,030 kg
(37,511 lb)
N2:12,360 RPM
PW2337: 17,030 kg
(37,511 lb)
N2:12,360 RPM
PS-90A1: 17,400 kg
(38,326 lb)
Engine Dry Weight (x4) 2,950 kg
(6,497 lb)
3,314 kg
(7,300 lb)
PW2337: 3,314 kg
(7,300 lb)
2,950 kg
(6,497 lb)
Cockpit crew Three Two Two (op. Three)
3-class Seating capacity 237 307   315
2-class Seating capacity 263 340   386
1-class Seating capacity 300 420   436
Cargo Capacity F.H.1: 9,000 kg (Front)
F.H.2: 15,000 kg (Back)
F.H.3: 1,000 kg (Back)
6 LD3 (front)
10 LD3 (Rear)
  580m main deck
114m front lower deck
82m rear lower deck
18 LD3 (Front)
14 LD3 (Rear)
114m front lower deck
82m rear lower deck

18 LD3 (Front)
14 LD3 (Rear)

 

 

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