Span 114 ft 0 in Chord 16 ft Length (overall) 76 ft 8 in Hull Length 48 ft 0 in Height (overall) 23 ft 10 in Angle of Incidence 2-1/2 deg Diehedral 1-1/2 deg Airfoil GS-1 Wing Area (incl ailerons and struts) 1875 sq ft Ailerons 100 sq ft Fin 49.5 sq ft Rudder 57.5 sq ft Stabilizers 149 sq ft Elevators 104.5 sq ft Gross Weight 34,000 lb Empty Weight 24,748 lb Useful Load 9,252 lb Payload 5,902 lb Seats 44 Wing Loading 14.4 lb/sq ft Power Loading 14.76 lb/hp High Speed 134.7 mph Cruise Speed 115.0 mph Landing Speed 65.0 mph Ceiling 13,000 ft Climb (at S.L.) 712 fpm Range 875 sm Powerplant 4x P&W Hornet (575 hp * 1900 rpm each) Fuel Capacity 1040 gals Oil Capacity 80 gals Certification ATC 454 Year of Introduction 1931 Production 3 (NC80V, NC81V, NC752V) Cost $139,000 Manufactured by Sikorsky, Bridgeport, CT Wing Construction: Dural Spars, channel ribs, fabric covered Hull Construction: Dural, Alclad covered Landing gear: Retractable, Sikorsky Brakes, Oleo-spring shock absorbers. S-40 Names: NC80V "American Clipper" NC81V "Caribbean Clipper" NC752V "Southern Clipper"
Useful Load 10,813 lb Span 114 ft 0 in Length (overall) 76 ft 8 in Hull Length 48 ft 0 in High Speed 140 mph Cruise Speed 120 mph Landing Speed 65 mph Range 900 sm Powerplant 4x P&W Supercharged Hornet (660 hp each) Certification ATC 562 Year of Introduction 1935 Production None Conversions 3 (NC80V, NC81V, NC752V)