Ilyushin Il-96
Specifications

Ilyushin Il-96

Section Title: Specifications
Table Section Text: None

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

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 PW2037	Pratt & Whitney PW2337 or Aviadvigatel PS-90A1	Aviadvigatel PS-90A1

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)

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)	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)

Sentence(s)

Ilyushin Il-96 is powered by four Pratt & Whitney PW2337 engines with a thrust (37,000 lbf).

final_sentence: Ilyushin Il-96 is powered by four Pratt & Whitney PW2337 engines with a thrust (37,000 lbf).