General characteristics
Crew: five (two pilots, navigator, flight engineer, loadmaster)
Capacity: 200 passengers or 110,000 lb (50,000 kg)
Length: 154 ft 3 in (47.01 m)
Wingspan: 179 ft 9 in (54.78 m)
Height: 48 ft 3 in (14.7 m)
Wing area: 2,673 sq ft (248.3 m2)
Empty weight: 120,263 lb (54,550 kg)
Gross weight: 275,000 lb (124,738 kg)
Max takeoff weight: 286,000 lb (129,727 kg)
Powerplant: 4 × Pratt & Whitney T34-P-9W turboprop engines, 7,500 hp (5,600 kW) each with water injection
Propellers: 3-bladed Curtiss Electric fully feathering, reversible-pitch propellers.
Performance
Maximum speed: 312 kn (359 mph, 578 km/h) at 8,700 ft (2,700 m)
Cruise speed: 281 kn (323 mph, 520 km/h)
Range: 3,560 nmi (4,100 mi, 6,590 km) with 52,000 lb (24,000 kg) payload
Service ceiling: 29,950 ft (9,130 m) service ceiling
Rate of climb: 1,280 ft/min (6.5 m/s)
Wing loading: 102.9 lb/sq ft (502 kg/m2)
Power/mass: 0.1087 hp/lb (0.1787 kW/kg)
My reasoning for suggesting this aircraft
It looks unique in my opinion, mainly because it has a distinct appearance of having a long fuselage, and looking like a brother to the XC-99 and the father to the C-130.