| 1 | A | B | C | D | E |
| --- | --- | --- | --- | --- | --- |
| 2 | Ilyushin Il-96 - Specifications |  |  |  |  |
| 3 | Measurement | Il-96-300 | Il-96M | Il-96T | Il-96-400 |
| 4 | Length | 55.3 m (181 ft 7 in) | 64.7 m (212 ft 3 in) | 63.939 m (209 ft 9.28 in) | 63.939 m (209 ft 9.28 in) |
| 5 | Span | 60.11 m (197 ft 3 in) | 60.11 m (197 ft 3 in) | 60.11 m (197 ft 3 in) | 60.11 m (197 ft 3 in) |
| 6 | Wing area | 350 m² (3767.9 ft²) | 350 m² (3767.9 ft²) | 350 m² (3767.9 ft²) | 350 m² (3767.9 ft²) |
| 7 | Wing sweep | 30° | 30° | 30° | 30° |
| 8 | 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 | 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 | 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 | 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 |
| 9 | Cabin width | 5.70 m (18.70 ft) | 5.70 m (18.70 ft) | 5.70 m (18.70 ft) | 5.70 m (18.70 ft) |
| 10 | Fuselage Diameter | 6.08 m (19.94 ft) | 6.08 m (19.94 ft) | 6.08 m (19.94 ft) | 6.08 m (19.94 ft) |
| 11 | Height | 15.7 m (57 ft 7 in) | 15.7 m (57 ft 7 in) | 15.7 m (57 ft 7 in) | 15.7 m (57 ft 7 in) |
| 12 | 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) |
| 13 | Max. Zero Fuel Weight | 180,000 kg (403,000 lb) | - | 208,400 kg (459,030 lb) | - |
| 14 | 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) |
| 15 | 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) |
| 16 | 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) |
| 17 | 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) |
| 18 | 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) |
| 19 | Cruising speed | 0.78 to 0.84 Mach or 850 to 870 km/h TAS (459 to 469 KTAS) | 0.78 to 0.84 Mach or 850 to 870 km/h TAS (459 to 469 KTAS) | 0.78 to 0.84 Mach or 850 to 870 km/h TAS (459 to 469 KTAS) | 0.78 to 0.84 Mach or 850 to 870 km/h TAS (459 to 469 KTAS) |
| 20 | Maximum speed (Vmo) | 0.84 Mach or 900 km/h IAS (485 KIAS) | 0.84 Mach or 900 km/h IAS (485 KIAS) | 0.84 Mach or 900 km/h IAS (485 KIAS) | 0.84 Mach or 900 km/h IAS (485 KIAS) |
| 21 | Service ceiling | 13,100 m (43,000 Ft) | 13,100 m (43,000 Ft) | 13,100 m (43,000 Ft) | 13,100 m (43,000 Ft) |
| 22 | Cruise Altitude | 9,000 to 12,000 m (29,527 to 39,370 Ft) | 9,000 to 12,000 m (29,527 to 39,370 Ft) | 9,000 to 12,000 m (29,527 to 39,370 Ft) | 9,000 to 12,000 m (29,527 to 39,370 Ft) |
| 23 | 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) |
| 24 | 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) |
| 25 | Max. Fuel capacity | 152,620 l (40,322 US gal) | 152,620 l (40,322 US gal) | 152,620 l (40,322 US gal) | 152,620 l (40,322 US gal) |
| 26 | Engines (x4) | Aviadvigatel PS-90A | Pratt & Whitney PW2037 | Pratt & Whitney PW2337 or Aviadvigatel PS-90A1 | Aviadvigatel PS-90A1 |
| 27 | Thrust (x4) | PS-90A: 156.9 kN (35,242 lb) N2:10,425 RPM | 170.1 kN (38,250 lb) N2:12,360 RPM | PW2337: 166.8 kN (37,500 lb) N2:12,360 RPM | PS-90A1: 170.7 kN (38,326 lb) |
| 28 | 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) |
| 29 | Cockpit crew | Three | Two | Two | Two (op. Three) |
| 30 | 3-class Seating capacity | 237 | 307 | - | 315 |
| 31 | 2-class Seating capacity | 263 | 340 | - | 386 |
| 32 | 1-class Seating capacity | 300 | 420 | - | 436 |
| 33 | 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) | - | 580 m³ main deck 114 m³ front lower deck 82 m³ rear lower deck 18 LD3 (Front) 14 LD3 (Rear) | 114 m³ front lower deck 82 m³ rear lower deck 18 LD3 (Front) 14 LD3 (Rear) |

Question: What kind of engines and first-class seating are found on the Ilyushin Il-96 400?
Answer: Ilyushin Il-96 400 is powered by four Aviadvigatel PS-90A1 and can carry up to 436 first class passengers.