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􀂃 RDR-2000 WEATHER RADAR
Installed weight = 27.3 lb. (12.4 kg)
Incorporating an all-new design, this unit provides all of the capabilities and features expected in a traditional two-dimensional digital radar system, but also adds something exclusive - the Vertical Profile Display™ which provides a “three dimensional” view of the storm cells. A simple switch allows you to also see how fast a storm is building, or to check the angle of the storm’s leading edge to see if it is to- ward or away from your position.
􀂃 HEATED PITOT TUBE
Installed weight = 0.3 lb. (0.1 kg)
This option helps to reduce the possibility of inadvertent ice or freezing rain from clogging up the static pitot system which provides airspeed and altitude information. (NOTE: This option is included when single pilot IFR suite is selected.)
􀂃 DUAL HEATED PITOT TUBES
Installed weight = 2.4 lb. (1.1 kg)
Provides an additional source for ram air pressure differential, further reducing the possibility of losing airspeed and altitude information while flying in inadvertent icing conditions.
(NOTE: This option is required when the single-pilot IFR suite with electromechanical or EFIS co-pilot instruments is selected.)
OPTIONAL EQUIPMENT
15
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􀂃 ENGINE PARTICLE SEPARATOR
Installed weight = 28.0 lb. (12.7 kg).
This is a Donaldson centrifugal-vortex air flow cover for the engines which efficiently traps sand and dust (FOD) which might otherwise damage the engine compressors. It has been demonstrated to be 95% efficient down to 3 microns of particulates. A bleed air ejector expels contaminants overboard. In the event one of the covers becomes clogged with debris, a differential pressure-controlled, solenoid-operated by-pass door automatically opens for each engine. Above 47 knots, an actuator automatically opens the NACA inlet.
􀂃 AUXILIARY FUEL TANK (FARGO)
53-gal. installed weight, empty = 104.6 lb. (47.4 kg) 28-gal. installed weight, empty = 70.2 lb. (31.8 kg)
Either tank is installed in the aft baggage compartment, attaching to existing hardware. They are filled from the outside of the fuselage, and are gravity-fed into the main fuel cell. The pilot has a control cable knob in the cockpit, and an additional fuel quantity gauge on the instrument panel. Space is still available in the baggage compartment for a reduced amount of cargo.
􀂃 SIX PLACE CABIN INTERCOM
Installed weight = 3.3 lb. (1.5kg).
Provides outlet jacks (no headsets provided) for all six passengers in the main cabin. When combined with customer-furnished headsets, the passenger and crew can communicate.
OPTIONAL EQUIPMENT
16
􀂃 FLEXCOM II WITH C-5000 CONTROL HEAD.
Installed weight = 31.4 lb. (14.2 kg)
This frequency-agile radio system provides the crew with access to every discrete AM or FM channel assigned to Public Safety, Industrial, Forestry, Business, Military, Air Traffic Control or Federal Agency operation (29.7 MHz to 960.0 MHz). The high-speed scanning receiver features a two-level priority and multiple high performance pre-selector filters. Voicscrambling or encryption
􀂃 BENDIX/KING KR-87 AUTOMATIC IRECTION FINDER (ADF) WITH KI-227 INDICATOR
Installed weight = 7.5 lb. (3.4 kg).
This provides selection, storage and simultaneous display of two frequencies, with a “standby” and “active” flip-flop capability. Selection of this option requires that you first select the Enhanced VFR Suite.
􀂃 BENDIX/KING KLN-90 GLOBAL POSITIONING
Installed weight = 9.1 lb. (4.1 kg)
Capable of tracking nine satellites at once, this instrument provides world-wide coverage, giving the operator a bird’s eye view of the helicopter’s present position and route of flight in relation to near-by navigation aids and airports. A work-saving feature is the moving map display graphics, enhanced witsupplementary information, such as airport services. Database updates are available 13, 6 or 4 times per year.
􀂃 ARTEX-100HM EMERGENCY LOCATOR TRANSMITTER.
Installed weight = 6.9 lb. (3.1 kg)
Activated manually or by high impact loads, this device transmits a homing beacon on the emergency channels, allowing rescue teams the ability to easily track and locate the landing site.
􀂃 “T” INSTRUMENT PANEL.
Installed weight = 4.5 lb. (2.0 kg)
Provides extra space for optional co-pilot instruments, a FLIR monitor, or other customer modifications.
OPTIONAL EQUIPMENT
17
􀂃 STANDARD INTERIOR
Six individual “stroking” (energy absorbing) seats are mounted to the ceiling and the floor. The seats are interchangeable and can be folded up for additional cargo storage or removed or installed without tools in about three minutes.
􀂃 BUSINESS INTERIOR.
Installed weight = 51.6 lb. (23.4 kg)
　
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