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􀂃 Engine Torque Meter
􀂃 Engine Oil Temp Indicator
􀂃 N1 Tachometer
􀂃 Fuel Quantity Indicator
􀂃 Digital Chronometer
􀂃 Airspeed Indicator
􀂃 Barometric Altimeter
􀂃 DC Ammeter
􀂃 Outside Air Temperature Indicator
􀂃 Magnetic Compass
􀂃 Turbine Outlet Temp Indicator
Avionics New for 2008
􀂃 GNS-430W NAV/COM/GPS*
􀂃 GTX-330 Transponder Mode A,C,S with TIS*
􀂃 GNC-420 VHF COM*
􀂃 GAE-43 Altitude Encoder*
􀂃 GMA-347 Audio Panel*
􀂃 GI-106A CDI*
􀂃 IVSI*
􀂃 Attitude Indicator*
􀂃 GCF-328 Cooling Fan*
􀂃 Artex C406-2HM ELT*
􀂃 Avionics Master Switch*
􀂃 Co-Pilots ICS Footswitch*
STANDARD EQUIPMENT
35
Annuciator Panel
􀂃 Battery Overtemp Warning Light
􀂃 Engine Chip Detector Warning Light
􀂃 Engine Out Warning Light
􀂃 Fuel Filter Obstruction Warning Light
􀂃 Fuel Low Warning Light
􀂃 Generator Out Warning Light
􀂃 Low Rotor rpm Warning Light
􀂃 Main Transmission Chip Detector Warning Light
􀂃 Main Transmission Oil Pressure Warning Light
􀂃 Main Transmission Oil Temperature Warning Light
􀂃 Tail Rotor Transmission Chip Detector Warning Light
Miscellaneous
􀂃 Ground handling wheels
􀂃 Engine and airframe log books
􀂃 Engine maintenance manual
􀂃 Battery logbook
􀂃 Flight manual
􀂃 Handbook of maintenance instructions
􀂃 Illustrated parts catalog
􀂃 Engine exhaust cover
􀂃 Engine inlet cover
􀂃 Pitot Tube Cover
􀂃 Main Rotor Blade Tie-Downs
PERFORMANCE SPECIFICATIONS
36
8.0 Performance Specifications
Characteristics at
Design Gross Weight
Metric
1406 kg
Imperial
3,100 lb
Maximum Cruise Speed Sea Level
1524 m (5,000 ft)
248 km/hr
249 km/hr
134 kt (154 mph)
135 kt (155 mph)
Speed for Best Range 1524 m (5,000 ft) 243 km/hr 118 kt (219 mph)
Maximum Permitted
Speed
VNE at sea level 282 km/hr 152 kt (175 mph)
Maximum Range Sea Level
1524 m (5,000 ft)
2.2 hrs
430 km
2.2 hrs (237 m)
232 nm (267 m)
Maximum Endurance Sea Level 381 km 206 nm (237 m)
Maximum Rate of Climb Sea Level, Standard Day
ISA +20° C Day
10.5 m/sec
105 m/sec
2069 fpm
2061 fpm
Maximum Operating
Altitude
Density Altitude 6096 m 20,000 ft
Service Ceiling ISA 5700 m 18,700 ft
Maximum Hook
Capacity
907 kg 2,000 lb
Hovering Performance (No wind)
In-ground effect Standard Day
ISA +20° C Day
4877 m
4359 m
16,000 ft
14,300 ft
Out-of-ground effect Standard Day
ISA +20° C Day
4389 m
3536 m
14,400 ft
11,600 ft
WEIGHTS
Characteristics Metric Imperial
Maximum Gross Weight Normal Capacity
External Load Operations
1406 kg
1701 kg
3,100 lb
3,750 lb
Empty Weight Standard Configuration 722 kg 1,591 lb
Useful Load Normal Capacity 684 kg 1,509 lb
External Load
Operations
979 kg 2,159 lb
Usable Fuel Capacity 242 l (64 gal) 183 kg 403 lb
POWER PLANT
Characteristics Metric Imperial
Rolls-Royce 250-C30
gas turbine
Rated Power 485 kw 650 shp
Derated for reliability
and safety to
Takeoff Power
Max Continuous Power
317 kw
280 kw
425 shp
375 shp
PERFORMANCE SPECIFICATIONS
37
8.1 Hover-In-Ground-Effect
PERFORMANCE SPECIFICATIONS
38
8.2 Hover-Out of-Ground-Effect
PERFORMANCE SPECIFICATIONS
39
8.3 Takeoff Gross Weight Worksheet
Example Mission #1 Mission #2
Empty Weight 1,591 lb
(722 kg)
Pilot 170 lb
(77 kg)
Fuel 403 lb
(183 kg)
Payload 936 lb
(424 kg)
Takeoff GW 3,100 lb
(1406 kg)
PERFORMANCE SPECIFICATIONS
40
8.4 Payload vs Range (5000’, ISA)
PERFORMANCE SPECIFICATIONS
41
8.5 Speed for Best Range
PERFORMANCE SPECIFICATIONS
42
8.6 Speed for Best Endurance
PERFORMANCE SPECIFICATIONS
43
8.7 Fuel Flow, Sea Level, ISA (15°C)
Note: Use for Estimates Only. Not FAA Approved. Based on clean aircraft, level flight performance, minimum
specification engine, particle separator and 10 ampere electrical load.
PERFORMANCE SPECIFICATIONS
　
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本文鏈接地址：MD500 Series TechDescription Feb09(10)