Description
🛫 Performance & Operational Data (Ilyushin Il‑62M)
📊 Weights, Fuel & Load
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Maximum Take‑Off Weight (MTOW): ~165,000 kg (364,000 lb)
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Operating Empty Weight: ~71,600–74,000 kg
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Fuel Capacity: ~105,300 L (≈84,000–84,240 kg fuel)
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Max Payload: ~23,000–25,000 kg
✈️ Engines & Flight Speeds
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Engines: 4 × Soloviev D‑30KU turbofans (~107.9–112.8 kN each)
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Cruise Speed (economic): ~850–880 km/h (~Mach 0.80–0.82)
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Maximum Cruise Speed: ~880 km/h
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Operating Ceiling: up to ~12,000 m (~39,000 ft)
🛫 Take‑Off / Landing
| Parameter | Estimate |
|---|---|
| Take‑off field length (typical) | ~3,100–3,300 m |
| Landing field length | ~2,500 m |
| Note: Actual distance varies with weight, runway, weather, and engine thrust settings. |
🏔️ Climb & Ceiling
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Service Ceiling: ~12,000 m (~39,000 ft)
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Climb to 10,000 m with max payload: ~11–12 minutes (calculated)
📏 Range (Typical)
Range varies a lot with payload and fuel configuration:
| Condition | Approx. Range |
|---|---|
| Max fuel, no payload (ferry) | ~11,600 km |
| Max fuel + reduced payload | ~10,000–10,800 km |
| Typical commercial load | ~8,000–9,770 km |
| Max payload with full fuel | ~7,700–8,900 km |
(Cargo, passenger seating, and reserves all affect useful range.)
🔎 Fuel Use (indicative)
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Typical cruise fuel burn around ≈6,500–7,000 kg/hour at economic cruise settings.
📊 Summary — Il‑62M at a Glance
| Feature | Value |
|---|---|
| Crew | 3–5 |
| Passenger Capacity | ~168–186 |
| Fuel Capacity | ~105,300 L (~84 t) |
| Take‑off Distance | ~3,100–3,300 m |
| Landing Distance | ~2,500 m |
| Cruise Speed | ~850–880 km/h |
| Range | ~7,700–11,600 km depending on load |
| Service Ceiling | ~12,000 m |
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