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􀂃 CRASH RESISTANT, HIGH CAPACITY FUEL SYSTEM
To accommodate longer range requirements and increased safety, the MD 600N™ now incorporates a 115 gal (435 l) crash-resistant fuel system. The system utilizes puncture resistant fuel bladders and self-sealing tank fittings meeting the requirements of FAR Part 27
􀂃 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 tobe used for training, dual-pilot VFR, or as a revenue generating passenger seat at the owner’s discretion. Left-hand command is standard.
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STANDARD EQUIPMENT
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􀂃 LARGE, WIDE CABIN DOORS
To enhance loading and unloading of the MD 600N’s large cabin flat floor, double center-opening doors have been incorporated into the standard design. These doors allow a full 62 inch (157 cm) opening and feature double locking mechanisms to ensure secure closing. All doors are equipped with gas-struts to provide open holding operation during loading/unloading.
􀂃 ENGINE INLET PARTICLE SEPARATOR
Installed weight = 13.2 lb. (6.0 kg).
Centrifugal-vortex air flow cover for the engine efficiently traps sand and dust (FOD) which might otherwise damage the engine compressors. It has been demonstrated to be 92% efficient down to 3 microns of particulates. A bleed air ejector expels contaminants overboard.
􀂃 QUICK-RELEASE DOOR HINGES
Meeker Aviation
Installed weight = 7.0 lb. (3.2 kg)
Reinforced hinges offer push-pin release allowing quick removal and replacement of doors. Available for crew, cabin and engine cowl doors.
STANDARD EQUIPMENT
􀂃 AIR CONDITIONER
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.
􀂃 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.
􀂃 INDIVIDUAL CABIN SEATING
Standard seating for the MD 600N® includes a forward, aft cabin bench seat that is reversible, allowing forward or aft facing seating. Shown to the right are individual forward seats that are also reversible.
􀂃 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. - 5 -
OPTIONAL EQUIPMENT
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􀂃 33.5 GALLON AUXILIARY FUEL SYSTEM
Robertson Aviation, Inc.
Installed weight = 50.0 lb. (21.2 kg).
Provides extra hour of 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.
􀂃 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 system. Automatic illumination cockpit caution warning. When the filter becomes fully clogged, a bypass valve contained in the filter unit opens and fuel by-passes the filter element. Ice additives required for fuel temperatures below -12 °C.
􀂃 HEATER TRANSPORT, SINGLE LITTER KIT
Installed weight = 30.0 est. lb. (13.6 kg) est.
Right-side litter kit providing capability to transport a single patient. Requires removal of cabin 3-place bench seat.
OPTIONAL EQUIPMENT
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􀂃 ROTOR BRAKE
Installed weight = 6.7 lb. (3.0 kg)
Rotor brake enhances safe shutdown in high winds, during shipboard operations at busy heliports and job sites. Requires less than one minute to stop rotor. Hydraulically actuated caliper- type disc brake is operated by pilot. Left or right-hand command side installation.
􀂃 FLAT PANEL MONITOR MOUNTS
Installed weight = 5.2 lb. (3.3 kg)
Lightweight mounting platforms for cockpit and cabin areas. Offer adjustments for tilting and rotating panels. Simple thumb-screw and knobs allow easy installation and removal.
􀂃 SEAT EQUIPMENT RACK
Installed weight = 7.6 lb. (3.5 kg)
3 pins secure a universal equipment rack that replaces the standard rear seat. Consists of mounting rails which accept standard seat floor fittings that can be attached to equipment frame. Allows quick removal and replacement of standard seat.
　
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