Ilyushin IL-86 Aeroflot CCCP 86015 Under pushback at gate A16 terminal 1

 
   

Ilyushin IL-86 Aeroflot CCCP 86015 Under pushback at gate A16 terminal 1

 
     
 
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 643′, 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 [37,000 ft]), 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

 

 

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