Specifications
| 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 m² (3767.9 ft²) | |||
| 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 |
|||
| 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) |
580m³ main deck 114m³ front lower deck 82m³ rear lower deck 18 LD3 (Front) 14 LD3 (Rear) |
114m³ front lower deck 82m³ rear lower deck 18 LD3 (Front) 14 LD3 (Rear) |
|
Data from Ilyushin Aviation Complex, FAA Certification Document A54NM and Il-96-300 Pilot Manual
Read more about this topic: Ilyushin Il-96
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