Display and HSI-415 RMI-301 Horizontal Magnetic Indicator Situation Indicator The Model 301 Radio Magnetic Indicators With over 35 years of experience The HSI-415 is a panel are full function, dual switched pointer, in cockpit displays, avionics and mounted, internally rotating azimuth display instruments, instrumentation, Moog is a prime lighted Horizontal Situation Indicator compatible with ARINC-429 equipment. contributor to the success of numerous (HSI) capable of providing display of aerospace platforms. We offer total in- aircraft heading, bearing course, course • Display of ARINC 429 heading and house engineering capabilities for design, deviation, VOR to / from and glidescope bearing information manufacture and test of a full range of information. This instrument is ideally • Internally lighted by an anti-reflection products. As the supplier of choice for suited for “third system” standby operation coated glass wedge major OEMs in the fixed wing and rotary through the use of an internal VOR-LOC • Modular electronics packaging wing communities, we serve both the composite video converter. facilitates rapid service and repair military marketplace and commercial • Self-contained, state-of-the-art aviation. • Unique Radio Magnetic Indicator mode electronics to enhance reliability and

of operation accuracy

• Display of either XYZ or DC SIN / COS • Meets rigid environmental requirements bearing information for most aircraft installations

General Aviation • Internal VOR-LOC converter available for use when required by a specific RMI-3100 BDI-302 installation Radio Magnetic Indicator Digital Bearing Distance Indicator HSI-423 Model 3100 Series Radio Magnetic Indicator Horizontal is designed for use with remote mounted The BDI-302 Digital Situation Indicator avionics in both fixed wing and rotary wing Bearing Distance aircraft. A servo driven compass azimuth Indicators are full function, The HSI-423 family of dial operating against a fixed lubber line dual switched pointer, rotating azimuth dual servo-bearing pointer, 4 inch, presents aircraft heading information to display instruments with a dual DME Horizontal Situation Indicators (HSI) the pilot. Each of two pointers provide distance display. The modular design are designed for helicopter and fixed bearing information for a selected ADF allows for configurations which can wing aircraft applications. All critical or VOR station. accept a variety of different signal information concerning the aircraft’s formats, including, but not limited to, position relative to ground-based RMI-3337 ARINC 429, ARINC 407 (XYZ), CSDB navigational aids is presented in one Radio Magnetic and SIN / COS. convenient display. Indicator • Display of a variety of digital and / or • Dual servo-bearing pointer display analog signal formats • Dedicated autopilot outputs The Model 3337 • Dual switchable bearing pointers • Isolated bootstrap Radio Magnetic Indicator is • Warning flags indicate VOR / ADF and • Available with side mounted D-sub designed for installations utilizing remote HEADING information connection or rear-mounted MS mounted avionics in both fixed wing and • Meets environmental requirements for circular style rotary wing aircraft. The unit presents many aircraft installations • Also available in U.S. Night Vision aircraft magnetic heading on a standard Goggle (NVG) compatible azimuth dial rotating under a fixed lubber line.

• Interfaces directly with most all navigational receivers • Internally lighted display

2 Moog • www.moog.com Displays and Avionics

• Black or gray bezel • No moving parts to wear out - advanced data • FAA / CAA approved microprocessor circuitry and liquid • Manually actuated selected heading crystal technologies for extremely low marker maintenance and long life • Digital distance display Signal Data Conversion • Easy replacement of electromechanical • Digital selected course display indicators - new solid state design uses • Accepts data in ARINC 582 and ARINC Whatever your signal the same envelope of your old, unreliable 407 formats for operation in TACAN, conditioning unit VOR, Inertial Reference Systems and needs, we lead • Exceptional design flexibility for interface Localizer modes the way with and dial format adaptability - easily • Master / Slave Mode Selection to a multitude matched to the current configuration display student’s course selection of signal conversion • Outstanding performance in all on instructor’s HSI for tandem trainer devices that provide interface to and from conditions - readable, lightweight, and configurations such as the Alpha-Jet navigation and avionics systems. reliable across temperature ranges and aircraft. other tough environments • Bearing pointer #1 processes and Typical examples would include synchro- • Built-in-Test (BIT) Displays all segments displays navigation data selected from to-digital and digital-to-synchro converters of the digital display and bargraph are either of two independent sensors. that are compatible with MIL-STD-1553 readable for the first three seconds Selection is accomplished using an B Data and a variety of other custom during power-up external mode-switch or hard wired where signals. • Exceedance monitoring of engine dual inputs are not required. One digital conditions. Instruments record magnitude input (ARINC 582) and one analog synchro Typical Signals and duration of exceedance of engine input (ARINC 407) are provided to Our platform experience includes major ratings accomodate a variety of equipment commercial and military programs: configurations ARINC 407, ARINC 429, ARINC 461, • Bearing pointer #2 processes and displays Trainer Aircraft ARINC 568, ARINC 575, ARINC 582, digital navigation data conforming to CSDB, VOR SIN / COS, VOR ARINC 582 COMPOSITE VIDEO, MIL-STD-1553 HSI-323A • Deviation from the selected course is A/B, ADF DC SIN / COS, RS232, RS485, Horizontal Situation calculated within the HSI and displayed SYNCHRO, RESOLVER, ANALOG, Indicator using data from any of the three possible DIGITAL BIT PARALLEL bearing inputs. Selection of the data The HSI-323A is a source is accomplished using an external 3ATI panel-mounted, mode-switch or hard wired where multiple

LCD Displays internally lighted Horizontal Situation inputs are not required Indicator (HSI) that provides a pictoral • Localizer mode (ILS Energize) provides High-Tech display of the horizontal navigation access to drive the lateral deviation bar Presentation Plus situation, plus manual controls for course and warning flag from the unit’s rear and heading selection. connector, using standard DC analog Improved Reliability signals • Servo-driven heading display card with Our solid state indicators provide an warning flag for invalid heading data economical upgrade to your instrument • Two servo-driven bearing pointers, with panel with today’s digital look. The LCD a parking feature for invalid bearing indicators are designed, developed data and produced by Moog. With extensive • Selected course pointer that supports experience in avionics, you can be servo-driven and manually actuated confident of the highest quality product, modes of operation service and support. • Lateral deviation bar, TO-FROM pointer Specifications and information are subject to change without prior notice. © 2009 Moog Inc. MS1061 rev. 5 06/18 and warning flag for invalid navigation KAI T-50 photo courtesy of KAI Korea Aerospace Industries, LTD. Bell 407 helicopter photo courtesy of Bell Helicopter Textron Inc. Moog • www.moog.com 3 Americas Asia-Pacific Europe 1213 North Main Street Yokohama Nishiguchi KN Bldg. 10F 30 Suttons Business Park Blacksburg, VA 24060 2-8-4 Kitasaiwai, Nishi-ku Reading, Berkshire RG6 1AW United States Yokohama, Kanagawa 220-0004 United Kingdom Japan www.moog.com Tel: +1 540-552-3011 Tel: +81 45-328-1803 Tel: +44 (0) 118-966-6044 Fax: +1 540-557-6400 Fax: +81 45-328-1801 Fax: +44 (0) 118-966-6524 Email: [email protected]

Moog • www.moog.com