Liberty Technologies, Inc.
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Liberty Technologies, Inc. |
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CUSTOM INTEGRATED IFR EFIS PACKAGE How to Enter a Flight Plan (Save the zip file to your hard drive, the instructions will unzip the file to view) How EFIS works (Save the zip file to your hard drive, the instructions will unzip the file to view)
Panel
Details .
The OP
Integrated navigation display consists of a full-color moving map which is
driven by the system’s approach certified WAAS/GPS receiver. Symbology used
for the moving map is similar to that of paper navigation charts so additional
training is not required to use it. The navigation
display also includes a terrain warning overlay which can to displayed for
additional situational awareness or suppressed to de-clutter the display.
Situational awareness can be further enhanced by displaying data received from
the Ryan TCAD or WSI In-Flight satellite weather receiver on the moving map.
Flight plans are entered and displayed on the navigation display, and
direct-to navigation and nearest search keys lower the heads-down time
required for flight planning.
System
Components
Turbine
Engine Features Chart
The Crossbow
NAV420 is a combined GPS Navigation and GPS-Aided Attitude & Heading
Reference system (AHRS) that utilizes both MEMS-based inertial sensors and GPS
technology to provide an unmatched value in terms of both price and performance.
Developed in response to years of extensive application experience in a wide
variety of airborne, marine and land applications, the NAV420 also incorporates
many new and enhanced design features including:
The NAV420
provides cons is tent performance over a wide temperature range in challenging
EMI environments across a broad range of input power conditions. It is designed
for use in a number of different applications including unmanned vehicle
control, land vehicle guidance, uncertified avionics and platform stabilization.
This high reliability, strap down inertial system provides attitude and heading
measurement with static and dynamic accuracies that exceed traditional spinning
mass vertical and directional gyros. With GPS integration, the NAV420 system
also provides GPS velocity data at up to 100 Hz. Velocity data includes aiding
from the inertial instruments to improve stability and reduce the latency
associated with stand-alone GPS measurements. Each NAV420 system comes with a
GPS antenna and User’s Manual Crossbow's NAV-VIEW software is also included to
assist users with system development, evaluation, and data acquisition.
The RAMI model
AV-GPS is a permanently mounted external aircraft antenna designed for use with
GPS receivers which provide +5 volts DC on their antenna connector. It is an
active (amplified) antenna providing an average of 26 dB gain over a passive
(non-amplified) antenna. The antenna is designed to operate at speeds up to 350
mph and altitudes up to 50,000 ft. It has a drag force of 0.18 lb @ 250 mph Antenna AV-GPS
Description
Features: Individual engine fuel flow (GPS calculates fuel remaining/used, fuel to destination, left/right engine used) TAS, winds aloft, wind component Mach, Indicated Air Speed, Instantaneous Vertical Speed, True Air Temperature, Rate of Turn, Outside Air Temperature, Pressure Altitude, Density Altitude, Magnetic Heading.
SANDIA Altitude Data System. The
SAE5-35 from SANDIA aerospace has set a new standard in providing accurate
altitude data. The SAE5-35 combines the features of three systems into a single
compact and reliable package. ALTITUDE ENCODING
…The SAE5-35 performs the functions of an Altitude Encoder by providing
Gillham Grey code to the aircraft’s mode C transponder. Innovative pressure
circuitry virtually eliminates the warm up time. DIGITAL ALITUDE
…The SAE5-35 provides two RS232 altitude data outputs in 10 foot increments
for use by GPS and Terrain Awareness Systems (TAWS). Each RS232 output is
totally independent so that a load on one output will not affect the other. And
because it provides altitude data from –1000 to 35,000 feet, it can be
installed on piston, turbine or jet aircraft. ALTITUDE IN-FLIGHT
MONITORING…(AIM) keeps a constant eye on your chosen altitude and lets you
know whenever you deviate more than 100 feet. SANDIA aerospace has given sight
to the "blind" encoder. .
The AP 100 is the
solution for the customer who wants the convenience of a quality audio panel but
not all the extras.
The RT-3209 transceiver
systems enable pilots and installation technicians to customize the VHF
communication system in any aircraft. High 20 Watt output power and low cost
provides the best in value and installation flexibility for every aircraft and
mission profile. The system is ideally suited for installations where minimum
panel space is to be used. Special
functions accessible via the front panel allow full control customization. The
lightweight AR-3209 remote transceiver unit is mated with this control head, to
complete the system. It can be installed at any convenient place in the
aircraft. Both active and preset frequencies are displayed and can be
transferred by a single stroke of the "Flip-Flop" button. Up to 20
preset frequencies memories can be easily entered in channel mode from the front
panel. When power is turned on, the "BITE" system automatically checks
and monitors the full system to insure proper operation at all times. All
systems will be JTSO certified for either VFR or IFR use in all types of fixed
wing and rotary wing aircraft and comply with the stringent ICAO requirements
Annex 10 for FM immunity. For truly compact installations, this transceiver can
be combined with matching Becker NAV-VOR/ILS, ADF, and Transponder systems. The
remote receiver unit can be controlled by many other CDU or FMS devices and is
perfect for use as a COMM in flight management systems.
Single
VOR/LOC/GS Receiver RN3320 The
RN 3320 VOR/ILS lightweight
remote receivers with VOR/LOC/GS capabilities are mated with this control unit
to complete a system. These receivers can be installed at any convenient place
in the aircraft. Both active and preset frequencies are displayed and can be
transferred by a single stroke of the "Flip-Flop" button. Up to 20
preset memory frequencies can be easily entered. Parallel/serial outputs are
provided for automatic DME channeling. The steering signals and flag drive
outputs are compatible with most commonly used CDI, HSI, Flight Director and
Autopilot systems. All systems will be JTSO certified for either VFR or IFR use
in all types of fixed wing and rotary wing aircraft and comply with the
stringent ICAO requirements of Annex 10, FM immunity. For truly compact
installations, the RN 3320 receiver systems can be combined with other equipment
including a VHF-COM, ADF and ATC transponder which have matching control units.
The remote receiver units can be controlled by other types of CDU or FMS devices
and are ideally suited for use with flight management systems.
The ATC4401 has been designed as a part for all aircraft and helicopters where small dimensions and light weight are essential. It has the same look and similar size as the successful transceiver AR 4201. The mounting behind the panel is as simple as for the AR 4201. Outstanding performance combined with low power consumption is provided. The ATC 4401-175 with min.175 Watt transmit power. The ATC4401 is state of the art designs with fully transistorized transmitters and compliant with the current, most stringent operating standards.
This is furnished for each modular component of the integrated system. FTC LTI’s Force Trim Control is a new servo design with improved dampening cyclic input control developed for non hydraulic rotorcraft systems. Older rotorcraft systems were controlled by the use of trim springs to center the cyclic stick giving it a no-force position. The FTC home switch gives the servo’s its new home position. This new FTC system can have additional trim input by making small servo adjustments using the cooly-hat switches for adjusting the trim servo positions to change cyclic’s physical position. The cooly-hat switch is comprised of four (4) individual switches, each for controlling one of the 90 degree directions relative to the line of flight. When a cyclic stick is moved by the pilot to a new position resetting the home switch for the new cyclic position will recenter home and only need slight input trim corrections to continue the rotorcrafts new course. All forces are removed by re-setting a new home position. After using the switches controlled by the cooly-hat to achieve proper adjustment, the pilot may then stop applying force to the cyclic stick and yet maintain the present control orientation on the helicopter. The cooly-hat switch is thus used by the pilots to reduce the amount of effort needed to control the helicopter. This system is designed for all three axis pitch, roll and yaw.
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Engine Interface Unit (EIU)
EDM950
Dual Communication Transceivers
(RT3209) 2 ea
