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Noorduyn Norseman Civil Aircraft Model Details

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General Information of Noorduyn Norseman
Designer : Robert B.C. Noorduyn

First Flight : November 14, 1935

Manufacturer : Noorduyn Aircraft Ltd

Number Built : 904, including prototypes

Primary Users : Bush plane operators worldwide

Role : General aviation aircraft

Status : 42 registered in Canada, unknown worldwide

General characteristics of Noorduyn Norseman
Airfoil : NACA 2412

Capacity : 10

Crew : 1

Empty Weight : 4,240 lb (1,923 kg)

Fuel Capacity : 242

Height : 10 ft 1 in (3.07 m)

Length : 32 ft 4 in (9.86 m)

Max Takeoff Weight : 7,400 lb (3,357 kg) 7,540 with floats

Powerplant : 1 × Pratt & Whitney R-1340-AN1 9 cyl.air cooled radial piston engine, 600 hp (450 kW) Power Loading 12.3 lb/hp

Propellers : 3-bladed Hamilton Standard, 9 ft 0.75 in (2.7623 m) diameterPower Loading 12.3 lb/hp

Wing Area : 325 sq ft (30.2 m2)

Wingspan : 51 ft 6 in (15.70 m)

Performance of Noorduyn Norseman
Cruise Speed : 150mph; 241km/h (130kn) KTAS @ 10,000ft

Range : 932mi; 1,500km (810nmi) @ 10,000ft

Rate Of Climb : 591ft/min (3.00m/s)

Service Ceiling : 17,000ft (5,182m)

Stall Speed : 68mph; 109km/h (59kn)

Wing Loading : 22.8lb/sqft (111kg/m2); Best rate of climb (Vy) 87 knots (161km/h); Maximum - Flaps extended (Vfe) 94 knots (174km/h); Maximum - operating (Vmo) 130 knots (241km/h)/141mph (wheels), 138mph (skis), 134mph (floats), Stall, clean (Vs1) 65 knots (120km/h); Stall, landing configuration (Vso)

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