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Reversible Bench Seat, aft cabin
Cockpit Utility Light
Cabin Convenience Light
Instrument Lighting
Cargo Tie-Down Fittings
STANDARD EQUIPMENT
19
4.3 Engine & Electrical
Rolls-Royce 250-C47M Engine, 808 shp (603 kw)
Automatic Engine Reignition
Engine Wash kit, MD 600 series
Engine Compressor Anti-Ice
Engine Compartment Fire Detection System
115 Gallon (435 L) Fuel System
Heavy Duty Starter/Generator – 200 amp
Filter Assembly for Fuel and Engine Scavenge Oil
External Power Receptacle
4.4 Rotor and Controls
Flight Controls – dual, left hand command*
Yaw Stabilization Augmentation System (YSAS)*
4.5 Flight and Engine Instruments
Collective Hobbs Meter *
Dual Tachometer, NR and N2
Engine Oil Pressure Indicator
Engine Torque Meter
N1 Tachometer
Hobbs Engine Running Time Meter
Fuel Quantity Indicator
Digital Chronometer
Airspeed Indicator
Barometric Altimeter
Digital Volt and Ammeter
Outside Air Temperature Indicator
Magnetic Compass
Digital/Analog Turbine Outlet Temperature Indicator
Engine Oil Temperature Indicator
4.6 Avionics New for 2008
GNS-430W NAV/COM/GPS*
GTX-330 Transponder Mode A,C,S with TIS*
GNC-420 COMM/GPS*
GAE-43 Altitude Encoder*
GMA-347 Audio Panel*
GI-106A CDI*
IVSI*
Attitude Indicator*
GCF-328 Cooling fan*
Avionics Master Switch*
Co-Pilots ICS Footswitch*
Artex C406-2HM ELT*
STANDARD EQUIPMENT
20
4.7 Annunciator Panel
Battery Overtemp Warning Light
Engine Chip Detector Warning Light
Engine Out Warning Light
Fan Transmission Chip Detector 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 Temp Warning Light
FADEC and ECU Caution Lights
Voice Warning Audio System
4.8 Miscellaneous
Ground Handling Wheels
Engine and Airframe Log Books
Engine Maintenance Manual
Battery Manual
Flight Log Book
Handbook of Maintenance Instructions
Illustrated Parts Catalog
Engine Exhaust Cover
Engine Inlet Cover
Pitot Tube Cover
Main Rotor Blade Tie-Downs
NOTAR® Inlet, Thruster and Tailboom Cover
STANDARD EQUIPMENT
21
4.9 Airframe Features
Semi-Monocoque Aluminum Fuselage
Composite Tailboom and Empennage
Extended Tubular Skid Landing Gear
Hydraulic Landing Gear Dampers
4.10 Interior Features
6-Foot, Flat Cabin Cargo Floor
Flow-Through Positive Ventilation System
4.11 Engine and Electrical Features
Full Authority Digital Engine Control (FADEC)
Hydro-Mechanical Backup Engine Control
Engine Driven Fuel Pump
28-Volt DC Electrical System
4.12 Rotor and Controls Features
Fully Articulated, 6-Bladed Main Rotor System
Static and Rotating Main Rotor Mast System
600 shp (447 kw) Drive-Train System
NOTAR Anti-Torque System
Mechanical Flight Control System
PERFORMANCE SPECIFICATIONS
22
5.0 PERFORMANCE SPECIFICATIONS.
3,100 lb
3,600 lb
4,100 lb
Maximum Cruise Speed
KTAS Sea Level ISA
KTAS 5,000 ft. ISA
144 148
139 143
134 kt (154 mph) 134 kt (154 mph)
Maximum Permitted Speed
Vne (KCAS) at Sea Level
152 (175)
152 (175)
135 kt (155 mph)
Maximum Range
Sea Level ISA
5,000 ft. ISA
347 (430) 423 (487)
357 (411) 401 (461)
257 (296) 293 (337)
Maximum Endurance
Sea Level ISA
5,000 ft. ISA
3.9 4.4
3.8 4.1
3.6 hr 3.9 hr
Maximum Rate-of-Climb
Sea Level Standard ISA
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MD600 TechDescription Feb09(8)
