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29 Cards in this Set
- Front
- Back
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Standard Aircraft Empty Weight including unusable, fuel, oils and fluids:
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5,310 kg (11,707 lb)
6,000 kg ( 13,228 lb) |
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Maximum Gross-Weight at Takeoff (standard conditions)
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11,000 kg (24,251 lb)
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Corresponding Useful Load:
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5,690 kg (12,544 lb)
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Minimum Weight in Flight:
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6,600 kg (14,551 lb)
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Maximum Operating Weight with External Load (standard conditions):
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11,200 kg (24,690 lb)
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Maximum Sling Capacity:
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5,000 kg (11,023 lb)
4,500 kg (9,921 lb) |
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Overall Length with Rotor Spinning
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63.98 ft.
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Rotor Blade Diameter
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53.14 ft
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Distance between main wheels
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9.84 ft.
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Distance between nose wheel and main landing gear wheels:
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17.22 ft.
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Height at Main Rotor Beanie
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15.09 ft.
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Height of Tail Rotor Blade Tip
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16.30 ft.
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Width of Cabin
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6.56 ft.
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Tail Rotor Blade diameter
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10.33 ft.
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Type Engines
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2 Makila 2A1 free turbine turboshaft engines
Modular design - Electronic Governing system (FADEC) 1665 kW at max. contingency power rating |
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Main Rotor Hub type
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Speriflex
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Tail Rotor
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Consists of 4 composite rotor blades
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Main Rotor
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Consists of 5 rotor blades
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Type of Landing Gear
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Retractable Tricycle Landing Gear
oleopneumatic struts trailing arm mail landing gear automatic wheel centering and castoring lock on nose landing gear. |
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Wheel Brakes
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2 separate hydraullically controlled disk brakes
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Intermediate TGB provides
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140 degrees of direction change
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Tail Rotor Drive Shafts
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8 total, 7 horizontal, 1 inclined. The first two are steel(for heat), the rest are aluminum alloy
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Describe the Engine Modules.
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There are 4 modules
Module No 1 - Air Intake and accessory drive gearbox. Module No 2 - 3-Stage Axial Compressor Module No 3 - Centrifugal Compressor, Combustion Chamber and Gas Generator Turbine Module No 4 - 2-Stage Free Power Turbine |
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Makila 2A Engine Rating
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OEI HI Rating 1758 kw - 2358 shp
OEI LO Rating 1661 kw - 2228 shp OEI CT Rating 1573 kw - 2110 shp Max Takeoff Rating 1563 kw - 2097 shp Max Continuous Rating 1410 kw - 1892 shp |
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Makila 2A1 Rating
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OEI HI Rating 1776 kw - 2382 shp
OEI LO Rating 1667 kw - 2236 shp OEI CT Rating 1608 kw - 2156 shp Max Takeoff Rating 1567 kw - 2101 shp Max Continuous Rating 1418 kw - 1902 shp |
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What is the rotational velocity of the tail rotor?
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1287 rpm for NR=265 rpm
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Tail Rotor Head type?
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Speriflex
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What design of the landing gear protect the fuselage belly in a gear up landing?
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The Wheels do not fully retract. They extend some amount below the belly, even when retracted.
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Tail Rotor Guard and Skid
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Made of steel. Taped for tell tale sign of ground contact. 11 deg nose up at touchdown
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