| Specs
Integrations
Technical I. Design Considerations for EFIS Symbology and Hardware II. Design Concept III. Display Principles IV.
Hardware Human Factors and Environmental
Considerations |
IDU (Integrated Display Unit)
- Full-color, high-resolution, sunlight-readable (1,000 nit) LCD screen with fully adjustable brightness
- Black-anodized machined 6061-T6 aluminum bezel
- Integrated voice warning system
- Illuminated controls with tactile differentiation
- Recursively redundant system architecture
- Integrated illuminated slip indicator (PFD)
- Digital flight performance recording for last 21 flights
- SmartMedia data card reader
- Line replaceable components
- Upgradeable/expandable
Size: 6.25"w x 5.50"h x 4.5"d
Cutout: 6.27"w x 5.52"h
Weight: 4.0 lbs.
Electrical: 10 to 28 VDC, 4 amps @ 12 VDC
Operating temperature: -30 to 50 degrees C (internally cooled)
Mounting: Instrument panel
Primary Flight Display
- HUD symbology
- 3-D Highway-In-The-Sky navigation for waypoints and approaches
- Real-time 3-D terrain modeling
- Real-time 3-D towers, antennas and obstruction
- Conformal traffic display (with Ryan TCAD)
- Enhanced low-speed awareness cues
- Unusual attitude recovery mode
- Zoom / wide-angle modes
- Multiple declutter options
- ASI, ALT, VSI, AGL, CDI, trends, heading, timers, bugs and more
- On-screen full-function FMS
Multi-Function Display
- Vector-based moving map with Jeppesen NavData
- Full weather / traffic interface capability
- Class A / B / C TAWS
- Class A / B Helicopter TAWS
- Winds aloft / crosswind component
- Density altitude display
- True airspeed, groundspeed, OAT
- Dead-stick glide area (wind, terrain, and turn compensated)
- Conventional HSI / RMI display
- Towers, antennas, and obstructions
- Special-use airspace incursion symbology
- Horizontal projected path
- Waypoint information
- Multiple display options
- Multiple declutter options
- Fuel range and duration
- On-screen full-function FMS
AHRS (Attitude/Heading Reference System)
- Inertial AHRS with three solid-state angular sensors, three solid-state accelerometers and three magnetometers
- Non-tumbling, non-precessing
Size: 4.66"w x 4.863"h x 5.909"d
Weight: 4.6 lbs.
Electrical: 9 to 30 VCD, 0.14 amps max
Operating temperature: -40 to 70 degrees C
Storage temperature: -55 to 85 degrees C (non-condensing)
Mounting: Remote; near aircraft centerline
ADC (Air Data Computer)
- Shadin OAT
- Digital fuel flow
Size: 3.4"w x 3.5"h x 6.5"d (includes mounting rack)
Weight: 2.75 lbs.
Electrical: 14 to 28 VDC, 900 mA @ 14 VDC, 1300 mA @ 28 VDC
Operating temperature: -20 to 55 degrees C
Cooling: No cooling necessary
Mounting: Remote
GPS Receiver
- 12-channel, parallel tracking GPS/WAAS receiver
- Predictive RAIM and FDE
Size: 4.13"w x 1.6"h x 6.5"d (includes mounting flange)
Weight: 1.2 lbs.
Electrical: 14 or 28 VDC, 0.25 amps @ 28 VDC or 0.5 amps @ 14VDC
Operating temperature: -40 to 60 degrees C
Storage temperature: -70 to 95 degrees C (non-condensing)
Mounting: Remote
GPS Antenna
Size: 3.0"w x 0.6"h x 4.7"l
Weight: 0.375 lb.
Electrical: supplied by GPS Receiver
Operating temperature: -40 to 60 degrees C
Mounting: External
Certification Basis
- TSO-C2d
- TSO-C4c
- TSO-C6d
- TSO-C8d
- TSO-C10b
- TSO-C106
- TSO-C110a
- TSO-C113
- TSO-C145/146
- TSO-C147
- TSO-C151a
- RTCA/DO-160D
- RTCA/DO-178B, Level A
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