Specifications
| Powerplant | four Kuznetsov NK-86 two-spool turbofan engines, up to 127.5 kN (13,000 kgf, 28,665 lbf); thrust-to-weight ratio at maximum takeoff weight 0.242; VSU-10 APU |
| Overall dimensions | span 48.06 m (157 ft 8 in), length 60.21 m (197 ft 7 in), nominal height 15.68 m (51 ft 5 in) |
| Wing | area 300 m² (3,229 ft²), sweep 35° at quarter chord, mean aerodynamic chord 7.57 m (24 ft 10 in), aspect ratio 7, dihedral 6°43’, incidence 3° root, -1° tip, loading at maximum takeoff weight 672 kg/m² (133.15 lb/ft²) |
| Undercarriage | track 9.9 m (32 ft 5.5 in), wheelbase 21.05 m (69 ft) to outboard gear; 22.32 m (73 ft 3 in) to centre gear, ground turning circle 22 m (72 ft 2 in) minimum pavement width, 36 m (119 ft) typical pavement width |
| Crew | flightdeck three (four in USSR and Russian service due to industrial practices), cabin 11 (service-typical) |
| Accommodation | all-economy 350 passengers, 9-abreast (3-3-3), 84 cm (34 in) seat pitch, mixed-class 320 passengers: 18 first, 56 business; 246 economy, freight capacity 16,000 cubic metres/565,035 cubic feet, three compartments |
| Weights | maximum ramp 216,950 kg (478,290 lb), maximum takeoff (MTOW) 215,000 kg (458,560 lb), maximum landing 175,000 kg (385,800 lb), maximum fuel 86,000 kg (189,630 lb), maximum payload 40,000 kg (88,185 lb) early, 42,000 kg (92,594 lb) developed, operational empty 117,500 kg (259,043 lb) early, 115,000 kg (253,531 lb) late |
| Field lengths | takeoff balanced field length in ISA conditions 2,800 m (9,190 ft), landing in ISA conditions 1,200 m (3,940 ft) |
| Sea-level rate of climb | 15 m/s (2,950 ft/min) at 210,000 kg (463,000 lb); service-typical between 5 m/s (1,000 ft/min) and 10 m/s (2,000 ft/min) |
| Speeds | typical safe climb-out (V2) 295 km/h (159 kt), initial climb 550 km/h (297 kt), climb 510 km/h (275 kt), cruise (VNO) maximum 0.88 Mach at 11,000 m (36,000 ft) to 12,000 m (40,000 ft)(best cruise altitude 11,400 m ), 0.82 M to 0.805 M on under-210-minute sectors service-typical, 0.782 M long-range, never-exceed (VNE) 670 km/h (362 kt, 416 mph) indicated air speed (IAS) to 8,200 m (27,000 ft) or 750 km/h (416 kt, 466 mph) IAS above that altitude, approach 410 km/h (254 kt), typical runway threshold (VAT) 270 km/h (146 kt at 175,000 kg (385,800 lb), stall 330 km/h (178 kt) clean configuration at 210 t; 250 km/h (135 kt) with 25° flap, 210 t; 234 km/h (126 kt) 40° flap, 210 t |
| Practical air ranges (full ICAO fuel reserves; MTOW) | maximum payload 3,400 km (1,835 nmi, 2,113 mi), full passenger load and full tanks 4,000 km (2,160 nmi, 2,485 mi), 300 passengers and full tanks 5,000 km (2,700 nmi, 3,106 mi), maximum still air (ferry) 8,200 km (4,428 nm, 5,095 mi) |
| Typical fuel consumption | 14,000 kg (30,865 lb) first hour, 12,000 kg (26,455 lb) per hour thereafter |
Sources:
Read more about this topic: Ilyushin Il-86
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