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520N STANDARD EQUIPMENT AND FEATURES
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Avionics New as of 2008
Miscellaneous
GNS-430W NAV/COM/GPS
Ground handling wheels
GTX-328 Mode A,C,S Transponder
Engine and airframe log books
SL-40 VHF COM
Engine maintenance manual
GAE-43 Altitude Encoder
Battery manual
GMA-347 Audio Panel
Flight manual
GI-106A CDI
Handbook of maintenance instructions
IVSI
Illustrated parts catalog
Attitude Indicator
Engine exhaust cover
GCF-328 Cooling Fan
Engine inlet cover
Artex C406-2HM ELT
Pitot tube cover
Avionics Master Switch
Main rotor blade tie-downs
Co-Pilots ICS Footswitch
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 temp warning light
Tail rotor transmission chip detector warning
light
STANDARD EQUIPMENT
STANDARD COCKPIT INTERIOR
STANDARD CABIN INTERIOR
WIRE STRIKE PROTECTION KIT
Installed weight = 15.4 lb. (7.0 kg)
Designed to provide an increased measure of protection for the helicopter’s frontal area in the event of inadvertent flight into horizontally strung wires. Includes a windshield deflector, and an upper and lower cutter/deflector. Each cutter has a high tensile steel cutting blade that can be easily replaced.
OPTIONAL EQUIPMENT
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INSTRUMENT CONSOLE SLANT PANEL
Installed weight = 3.0 lb. (1.4 kg)
Provides additional room for communication and navigation in the console between the pilot and co-pilot. Location allows moving communications equipment closer to pilot for ease of operation and tilts displays for improved readability.
DUAL FLIGHT CONTROLS
Installed weight = 10.4 lb. (4.7 kg).
Duplicates controls for copilot. Easily removed, even in the field, without tools. Allows aircraft to be used for training, dual-pilot VFR, or as a revenue generating passenger seat at the owner’s discretion. Left-hand command is standard.
RIGHT-HAND COMMAND
Installed weight = -0.0 lb. (0.0 kg)
For customers requiring right-hand command, controls and instrument panel are changed to right side. Available for single or dual controls on the MD 500E and the MD 530F only. Left hand command is standard.
OPTIONAL EQUIPMENT
33.5 GALLON AUXILIARY FUEL SYSTEM
Robertson Aviation, Inc.
Installed weight = 50.0 lb. (21.2 kg).
Provides extra flight time at speed for maximum endurance. Fully qualified crash-resistant design to FAA Part 27. Fits under rear seat. Includes fuel quantity gauge on tank. Compatible with business seat option.
21 GALLON AUXILIARY FUEL SYSTEM
-Fargo, Inc.
Installed weight = 44.5 lb. (20.2 kg).
Gravity feed to main tank. Fits behind rear seats.
AIRFRAME FUEL FILTER
Installed weight = 6.7 lb. (2.9 kg)
Designed to strip fuel of ice particles prior to entering the engine fuel system. Filter incorporates a filter unit mounted in series between the aircraft fuel system and engine fuel sys tem. Automatic illumination cockpit caution warning. When the filter becomes fully clogged, a bypass valve contained in the filter unit opens and fuel bypasses the filter element. Ice additives required for fuel temperatures below -12 °C.
250-C20R+ ENGINE
Rolls-Royce
Installed weight difference = 15.0 lb. (6.8 kg).
Provides engine rating to 450 shp. Available as option for MD 500E series.
COMFORT WINDOWS
Tech Tools, Inc.
Installed weight = 12.0 lb. (5.4 kg)
Two (2) in each cabin & two (2) in each cockpit with pop out vents. Bulged side windows increases elbow- room by up to 4 inches (10 cm).
AIR CONDITIONER R-134
W/ FORWARD EVAPORATOR
Integrated Flight Systems, Inc.
Installed weight 83.9 lb. (38.5 kg)
Compressor utilizes belt-drive from transmission with large condenser mounted above the cabin area. Evaporators are provided in the cockpit and cabin areas. Four outlets are used in the cockpit area and vents are provided in the cabin area. Separate fan controls are provided for cockpit and cabin.
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MD500 Series Options(4)
