Specifications (NC.211)
Data from French Postwar Transport Aircraft
General characteristics
- Crew: 5
- Capacity: 12,000 kg (26,455 lb) payload, 76 paratroops, 60 stretchers or 100-150 passengers (civil)
- Length: 30.5 m (100 ft 1 in)
- Wingspan: 44 m (144 ft 4 in)
- Height: 10.7 m (35 ft 1 in)
- Wing area: 200 m2 (2,200 sq ft)
- Empty weight: 25,625 kg (56,493 lb)
- Gross weight: 42,250 kg (93,145 lb)
- Powerplant: 4 × SNECMA 14R 14-cyl. two-row air-cooled radial piston engines, 1,200 kW (1,600 hp) each at 2,600 rpm with 47.2 in (1,199 mm) Hg / +8.6 psi (59,295 Pa) boost for take-off
- Propellers: 3-bladed, 4 m (13 ft 1 in) diameter
Performance
- Maximum speed: 390 km/h (242 mph; 211 kn) at 3,000 m (9,843 ft)
- Cruising speed: 288 km/h (179 mph; 156 kn) at 3,000 m (9,843 ft)
- Range: 1,000 km (621 mi; 540 nmi) with full payload
- Range with 9,600 kg (21,164 lb) payload: 2,000 km (1,243 mi; 1,080 nmi)
- Service ceiling: 8,000 m (26,247 ft)
- Wing loading: 210 kg/m² (43 lb/sq ft)
- Power/mass: 0.0284 kW/kg (0.0369 hp/lb)
Read more about this topic: SNCAC NC 211