Overview
The Bombardier Challenger 605 entered service in the mid-2000s as an updated development of the Challenger 604. Designed to improve avionics, cabin comfort, and operational efficiency, it remained within the large-cabin segment. The aircraft continued the long-running Challenger lineage.
Live Fleet Activity (CL60)
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Specifications
Units
- Engine
- 2 × General Electric CF34-3B
- Engine type
- Turbofan
- Thrust
- 2 × 9,140 lbf · 41 kN
- Avionics
- Rockwell Collins Pro Line 21
- Wing tips
- Blended tips
- Seats
- 12
- Crew
- —
- Cabin width
- 8 ft 2 in · 2.49 m
- Cabin height
- 6 ft 1 in · 1.85 m
- Cabin length
- 28 ft 5 in · 8.66 m
- Exterior length
- 68 ft 5 in · 20.86 m
- Tail height
- 20 ft 8 in · 6.30 m
- Fuselage diameter
- 8 ft 10 in · 2.69 m
- Wing span
- 64 ft 4 in · 19.61 m
- Baggage volume
- 115 ft³ · 3.3 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 48,200 lb · 21,900 kg
- Max landing weight
- 38,000 lb · 17,200 kg
- Max payload
- 4,850 lb · 2,200 kg
- Fuel capacity
- 3,000 gal · 11,300 L · 9,000 kg (Jet A)
- Max cruise speed
- 470 kt · 541 mph · 870 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 4,045 nm · 4,650 mi · 7,490 km
- Fuel burn
- 1.36 nm/gal · 0.67 km/L
- Ceiling
- 41,000 ft · 12,500 m
- Rate of climb
- 4,450 ft/min · 23 m/s
- Takeoff distance
- 5,850 ft · 1,780 m
- Landing distance
- 2,800 ft · 850 m
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