Mid-Continent MD302 SAM

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