Ilyushin Il-96
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)
63.939 m (209 ft 9.28 in)
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)
Wing area
350 m² (3767.9 ft²)
350 m² (3767.9 ft²)
350 m² (3767.9 ft²)
350 m² (3767.9 ft²)
Wing sweep
30°
30°
30°
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
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
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)
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)
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)
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)
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)
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)
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)
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)
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)
152,620 l (40,322 US gal)
152,620 l (40,322 US gal)
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
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)

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.