Features
- Attitude, altitude, airspeed, slip, and vertical trend indication
- Displayed heading via ARINC 429 input
- Five primary functions utilize modern solid-state MEMS gyro, accelerometer and pressure transducer technology
- Small 2.4” x 5.5” footprint
- Extremely lightweight — 1.6 lbs
- Self-contained, rechargeable Nanophosphate® lithium-ion emergency battery
- Smooth, high-definition graphics
- Unique, two-screen display with wide viewing angles and a user-friendly menu structure
- Selectable orientation — horizontal and vertical
- Aircraft-specific, programmable airspeed range markings
- Simple user interface — one knob configures the display and provides menu control
- 10–32 VDC power input
- External, automatic and manual dimming control settings
- Software configurable lighting curves
- Field-upgradable software via standard USB port
- FAA TSO certified to C2d, C3e, C4c, C10b, C106, C113a, C179a
- ANAC TSO certified to C2d, C3e, C4c, C10b, C106, C113a, C179a
- EASA ETSO certified to C2d, C3d (incomplete), C4c, C10b, C106, C113, C179a
- RTCA DO-178B and DO-254 Design Assurance Level (DAL) A
- RTCA DO-160 and RTCA DO-311 qualified
- Designed and built in Wichita, Kansas, USA
Operating Range
Attitude: 300° per second pitch, roll and yaw (max)
Altitude: -1,500 to +55,000 ft (-457 m to 16,764 m)
Airspeed: 20 to 500 knots (23 to 575 mph) (37 to 926 kph)
Specifications
Power Input: 10-32 VDC; 6W nominal, 25W max
Output: ARINC 429 (see manual for specific labels)
Vertical Trend: 6 second time frame
Lighting: 5, 14 or 28 VDC external input or internal photocell (Programmable dimming curve)
Weight: 1.6 lbs (0.73 kg)
Battery: Rechargeable, field-replaceable, internal battery (Nanophosphate® lithium-ion)
Battery run time: 60 minutes minimum when fully charged and properly maintained