Ilyushin Il-62 - Specifications (Il-62M)

Specifications (Il-62M)

Data from Jane's All The World's Aircraft 1988–89

General characteristics

• Crew: 5; 3 to 5 (a captain, a first officer, and a flight engineer, plus optionally a navigator and a radio officer on long overwater and/or VIP services to operator specification) plus a four to eight-person cabin crew to operator specifications
• Capacity: 168-186 passengers
• Length: 53.12 m (174 ft 3½ in)
• Wingspan: 43.20 m (141 ft 9 in)
• Height: 12.35 m (40 ft 6¼ in)
• Wing area: 279.55 m² (3,009 sq ft)
• Empty weight: 71,600 kg (157,848 lb)
• Max. takeoff weight: 165,000 kg (363,760 lb)
• Powerplant: 4 × Soloviev D-30KU turbofans, 107.9 kN (24,250 lbf) each
• Fuel: 105,300 L (27,817 US Gallons)

Performance

• Maximum speed: 900 km/h (486 knots, 560 mph)
• Range: 10,000 km (5,400 nmi, 6,215 mi) with 10,000 kg (22,000 lb) payload
• Service ceiling: 12,000 m (39,400 ft) (maximum cruising height)
• Rate of climb: 18 m/s (3,540 ft/min) (Il-62)