曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
MD500 Series TechDescription Feb09(10)
