PUMA SA-330 Spec

MANUFACTURE : AEROSPATIALE 1974 POWER PLANT Power Plant :2 (two) Turmo IV.C Turbomeca 1558 Hp Each Take Off Power :1494 SHP Max. Contingengy Power :1262 SHP SPECIFICATIONS Seating Capacity :3 Cockpit + 17 Seat (airline), 18 Seat (troop) Litter Capacity :6 Each Avarage Cruise Speed :120 Kts Speed with Slung Load :40 -100 Kts Max. Speed (VNE) :167 Kts Fuel Consumption :660 Ltr/hr Fuel Capacity :Internal Tank : 1550 Ltr :External Tank : 700 Ltr :Ferry Tank (1) : 475 Ltr Max. Range (15'''''''' Reserve) :379 Nm / 703 Km Ceiling (T/O & Landing) :13000 ft Ceiling (Inflight) :16500 ft Max. Rate of Climb :1200 ft/min DIMENSION Rotor Blades :4 Fully Artriculated Fuselage Length :14.82 M Overall Length :18.2 M Fuselage Width :3.0 M Overall Height :5.14 M Main Rotor Diameter :15.09 M Tail Rotor Clearance :1.83 M Cabin Doors Dimension :1.35 M x 1.35 M LOADING INFORMATION Max. Gross Weight :7400 Kg / 16300 Lb Empty Weight - Std :4240 Kg / 9346 Lb Usefuel Load - Int :3160 Kg / 6964 Lb Usefuel Load - Ext :3260 Kg / 7185 Lb HELIPAD SIZE Size :20 x 20 M (Fato : 27.3 x 27.3 M ) Minimum Strenght :11.100 Kg

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