The MD302 Standby Altitude Module or SAM™features a unique two-screen display that provides attitude, altitude, airspeed, slip, vertical trend, and heading information to the pilot during normal or standby operation in the event of primary instrument failure. This self-contained, solid-state instrument features a selectable orientation, horizontal or vertical, which allows flexible cockpit design and installation. The MD302 is also equipped with a rechargeable Nanophosphate® lithium-ion battery that provides up to one hour of emergency operation when fully charged.
规格：
Weight:
1.6 lb (0.73 kg)
Dimensions:
5.50 x 2.37 x 5.17 in
Power Input:
10 VDC — 32 VDC, 6 watt (nominal), 40 watt (maximum)
Output:
ARINC 429 (high or low speed, see manual for specific labels)
Operating Range:
Attitude: 300° per second pitch, roll and yaw (max)
Altitude; -1,500 to 55,000 ft (-457 to 16,764 m)
Airspeed: 20 to 500 knots (23 to 575 mph) (37 to 926 kph)
Vertical Trend:
6 second time frame
Heading:
Within ±2° up to 55°N or 45°S
Units of Measure:
Altitude: Feet or meters
Barometric Setting: Inches of mercury, millibars
Airspeed: Knots, miles per hour or kilometers per hour
Panel Tilt:
-90° to +90° pitch, configurable
Panel Roll:
-5° to +5° roll, configurable
Lighting:
5 VDC, 14 VDC, and 28 VDC external input or internal photocell
Programmable dimming curve
Pilot Interface:
16-detent, push and turn knob
Mounting:
Front Panel Mount
Mating Connectors:
Mid-Continent P/N 9017646 kit contains custom DB15 connector with configuration module, pitot and static connectors
Certification:
FAA TSO certified C2d, C3e, C4c, C6e (incomplete), C10b, C106, C113a, C179a
ANAC TSO certified C2d, C3e, C4c, C10b, C106, C113a, C179a
EASA ETSO certified 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
特征：
This MD302 Standby Altitude Module(EDMO# MD302-2):
Black bezel
Features:
Attitude, altitude, airspeed, slip, and vertical trend indication
Optional Heading via the MD32 Magnetometer or aircraft system
Five primary functions utilize modern solid-state MEMS gyro, accelerometer and pressure
transducer technology
Compact footprint — only 2.4 x 5.5 inch
Lightweight — Only 1.6 lb
Self-contained, rechargeable, field-replaceable emergency battery
Smooth, high-definition graphics
Unique two-screen display with wide viewing angles and a user-friendly menu structure
Selectable horizontal and vertical orientations
Aircraft-specific, programmable airspeed range markings
Configurable for static source error correction (SSEC)
Simple user interface — one knob configures the display and provides menu control
External, automatic and manual dimming control settings
Software configurable lighting curves
Field-upgradable software via standard USB port
Designed and built in Wichita, Kansas, USA
