C-64A Norseman

C-64A Norseman / Noorduyn Norseman merupakan kapal terbang belukar berkipas enjin tunggal Kanada yang direka bagi berlepas dari permukaan tidak diratakan. Kapal terbang Norseman diketahui didaftarkan dan/atau beroperasi di 68 negara diseluruh dunia dan juga telah ditempatkan dan diterbangkan di benua Artik dan Antartika.

 Pengguna tentera 

 Tentera Udara DiRaja Australian - 14 kapal terbang berkhidmat dengan RAAF dari 1943 hingga 1946.
 No. 1 Communications Unit RAAF
 No. 3 Communications Unit RAAF
 No. 4 Communications Unit RAAF
 No. 5 Communications Unit RAAF
 No. 7 Communications Unit RAAF

 Tentera Udara DiRaja Kanada

 Tentera Udara Israeli

 Royal Netherlands East Indies Army Air Force

 Tentera Udara DiRaja Norwegian

 Tentera Udara Swedish

 Tentera Udara DiRaja

 Tentera Udara Amerika Syarikat

 Spesifikasi 
+ Norseman Mark V General Specifications  Length (wheels)   Height   Cabin Length   Cabin Width  4.21 ft (max) Cabin Height  4.46 ft (max) Seats  Up to 10   Wingspan   Wing Area  Wing Loading  22.8 lb/sq ftStandard Empty Weight  4,240 lbMax Takeoff Weight (wheels)  7,400 lbMax Takeoff Weight (floats)  7,540 lbAverage Useful Load  3,160 lbPayload with Full Fuel  1,825 lb  Fuel Capacity, Standard  242 gal / 1452 lbOil Capacity  23 gal / 172.5 lb  +  Powerplant  Type  Radial piston engine Make & Model  Pratt & Whitney R-1340-AN1 Power Developed  600 hp @ 2250 rpm Power Loading  12.3 lb/hp  +  Propeller  Type  Constant-speed, 3 blade Make  Hamilton Standard Diameter  108.75 inches  +  Performance  Takeoff Distance Over 50' Obstacle   Rate of Climb, Sea Level  591 ft/min Max Cruise Speed (10,000 ft)  130 KTAS Range, max (10,000 ft)  810 nm Service Ceiling    Landing Distance over 50' obstacle (no reverse)    +  Speeds  Knots Indicated Airspeed (KIAS) Best rate of climb (Vy)   Maximum - Flaps extended (Vfe)   Maximum - operating (Vmo)  /141 mph (wheels), 138 mph (skis), 134 mph (floats) Stall, clean (Vs1)   Stall, landing configuration (Vso)    + Norseman Mark V and VI Dimensions General   Span (incl Navigation Lights)  51 ft 8 inches Length (overall)  32 ft 4 inches Height  13 ft 9 inches Height (tail wheel on ground)  10 ft 1 inch  Fuselage  Including stubs, unless otherwise noted   Width (max without stubs)  53 inches Width (max with stubs)  99 inches Height (max without radio mast)  90 inches Height (max with radio mast)  108.5 inches Length (without engine mount)  307 inches Length (with engine mount)  321 inches  Wings  Airfoil Section at root  NACA 2412Airfoil Section at tip  NACA 2412Chord at root  87 inchesChord near tip  87 inchesAngle of Incidence  +3°Dihedral (measured along front spar)  2.5°Sweepback Angle  0° Wing Area (less ailerons)  296.3 sq ft Aileron Area (total)  28.70 sq ft Flap Area (total)  30.80 sq ft  Tail   Horizontal Stabilizer Span  13 ft 10 7/8 inches Horizontal Stabilizer Chord  2 ft 3 5/8 inches Horizontal Stabilizer Area (including elevators)  60.06 sq ft Elevator Area (including trim tabs)  31.56 sq ft Elevator Trim Tabs Area (total)  1.39 sq ft Vertical Stabilizer Area  14.68 sq ft Rudder Area (including trim tab)  19.04 sq ft Rudder Trim Tab Area  0.125 sq ft

 Rujukan 
Notes

Bibliography

 Grant, Robert S. Noorduyn Norseman: Red Lake, Ontario, Canada, Norseman Capital of the World. Red Lake, Ontario: Norseman Floatplane Festival, 2007. (booklet)
 Mathisrud, Nils. Norwegian Wings #1: Noorduyn Norseman Mk. IV & Mk. VI. Oslo: FlyGloster Publishing, 2007. ISBN 978-82-92822-00-5.
 Milberry, Larry. Aviation in Canada. Toronto: McGraw-Hill Ryerson, 1979. ISBN 0-07-082778-8.
 Munson, Kenneth. Bombers, Patrol and Transport Aircraft 1939-1945. London: Blandford Press, 1969. ISBN 0-7537-0919-8.

 Pautan luar 
 Official Noorduyn Norseman web site
 Unofficial Noorduyn Norseman web site

Kategori:Kapal terbang enjin tunggal
Kategori:Kapal terbang berkipas