Jane's All the World's Aircraft, Том 64

aerobatic ailerons Air Force all-metal aluminium aspect ratio aspect ratio Length brakes cabin Cantilever climb at S/L DIMENSIONS door ELECTRONICS AND EQUIPMENT EXTERNAL ft 9 fuel tanks fuselage Height Width helicopter hp Lycoming hydraulic Imp gallons Israel Aircraft Industries Jane's kg/hp kg/m² km/h knots LANDING GEAR lb/hp lb/sq ft Length overall Height litres main rotor main wheels Max cruising speed Max level speed Max power loading max T-O weight Max wing loading miles Model monoplane NACA nosewheel optional overall Height overall passengers PERFORMANCE at max pilot POWER PLANT production prototype Range with max Rate of climb ratio Length overall rear Retractable rudder seats Service ceiling single-seat speed at S/L sq ft Stalling speed standard starboard STOL structure T-O run TAIL UNIT Tailplane trim tab two-blade two-seat tyres Weight empty WEIGHTS AND LOADINGS Wing aspect ratio Wing span Wing