Bombardier/Canadair CL-600 Challenger REFERENCE INFORMATION
Aircraft data
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Wing span over winglets: 19.61 m (64 ft 4 in)
Wing chord: at root 3.99 m (13 ft 1 in)
at tip 1.27 m (4 ft 2 in)
Wing aspect ratio (excl winglets): 8.0
Length overall: 20.85 m (68 ft 5 in)
Fuselage: Max diameter 2.69 m (8 ft 10 in)
Length: 18.77 m (61 ft 7 in)
Height overall: 6.30 m (20 ft 8 in)
Tailplane span: 6.20 m (20 ft 4 in)
Wheel track (c/l of shock-struts): 3.18 m (10 ft 5 in)
Wheelbase: 7.99 m (26 ft 2½ in)
Passenger door (port, fwd): Height 1.78 m (5 ft 10 in)
Width 0.94 m (3 ft 1 in)
Height to sill 1.63 m (5 ft 4 in)
Baggage door (port, rear): Height 0.84 m (2 ft 9 in)
Width 0.71 m (2 ft 4 in)
Height to sill 1.73 m (5 ft 8 in)
Overwing emergency exit (stbd): Height 0.91 m (3 ft 0 in)
Width 0.51 m (1 ft 8 in)
Dimensions, Internal
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Cabin: Length, incl galley, 8.66 m (28 ft 5 in)
toilet and baggage area,
excl flight deck:
Max width: 2.49 m (8 ft 2 in)
Width at floor level: 2.18 m (7 ft 2 in)
Max height: 1.85 m (6 ft 1 in)
Floor area: 18.8 m2 (202 sq ft)
Volume: 32.6 m3 (1,150 cu ft)
Weights and Loadings
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Manufacturer's weight empty: 9,806 kg (21,620 lb)
Operating weight empty: 12,079 kg (26,630 lb)
Max fuel: 9,072 kg (20,000 lb)
Max payload: 2,435 kg (5,370 lb)
Payload with max fuel: standard 485 kg (1,070 lb)
optional 757 kg (1,670 lb)
Max T-O weight: standard 21,591 kg (47,600 lb)
optional 21,863 kg (48,200 lb)
Max ramp weight: standard 21,636 kg (47,700 lb)
optional 21,908 kg (48,300 lb)
Max landing weight: 17,236 kg (38,000 lb)
Max zero-fuel weight: 14,515 kg (32,000 lb)
Max wing loading: standard 446.9 kg/m2 (91.54 lb/sq ft)
optional 452.6 kg/m2 (92.69 lb/sq ft)
Max power loading: standard 263 kg/kN (2.58 lb/lb st)
optional 267 kg/kN (2.61 lb/lb st)
Performance (at standard max T-O weight, except where indicated)
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Max cruising speed: M0.83 (476 kt; 882 km/h; 548 mph)
Normal cruising speed: M0.80 (459 kt; 851 km/h; 529 mph)
Long-range cruising speed: M0.74 (425 kt; 787 km/h; 489 mph)
Time to initial cruising altitude: 21 min
Initial cruising altitude: 11,280 m (37,000 ft)
Max certified altitude: 12,500 m (41,000 ft)
Service ceiling, OEI: at mid-cruise weight 17,373 kg (38,300 lb) 6,920 m (22,700 ft)
at max T-O weight 5,170 m (16,960 ft)
Balanced T-O field length (ISA at S/L): 1,737 m (5,700 ft)
Landing distance at S/L at max landing weight: 846 m (2,775 ft)
Range with max fuel and five passengers,
NBAA IFR reserves (200 n mile; 370 km; 230 mile alternate):
long-range cruising speed 4,077 n miles (7,550 km; 4,691 miles)
normal cruising speed 3,769 n miles
(6,980 km; 4,337 miles)
Design g limit: +2.5
