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MD302 Standby Altitude Module, Grey, NiMH Battery

MD302 Standby Altitude Module, Grey, NiMH Battery

Description: SAM Standby Attitude Module, Digital, 10–32 VDC, Attitude, Altitude, Airspeed, Slip, Internal battery (NiMH), Gray bezel.

Tags: Avionics,Instruments & Clocks,Standby,EFIS,EACH,SAM,Mid-Continent

SKU: 6420302-8

Description

Maximize your panel space. SAM® is the only 2-inch digital Standby Attitube Module that can be installed horizontally and vertically. It provides attitude, altitude, airspeed, slip, vertical trend and heading. This unit’s nickel metal hydride battery keeps you flying in the event of electrical failure. The SAM 6420302-8 unit features a self-contained design, flexible configuration, dual-screen display and gray bezel.

Benefits
  • Attitude, altitude, airspeed, slip, and vertical trend indication
  • Heading via MD32 Magnetometer (optional) or aircraft system
  • 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, field-replaceable 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
  • Configurable for static source error correction (SSEC)
  • 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
  • Night Vision Imaging System (NVIS) compatible (available)
  • FAA / EASA / ANAC TSO certified to C2d, C3e, C4c, C6e, C10b, C106, C113a, 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
  • Two-year or 2,000-hour warranty
Specifications

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 m 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
Configurable: -90° to +90° pitch

Panel Roll
Configurable: -5° to +5° roll

Lighting
5, 14 or 28 VDC external input or internal photocell
Programmable dimming curve

Pilot Interface
16-detent, push and turn knob

Weight
1.6 lbs (0.73 kg)

Bezel
Gray

Battery
Rechargeable, field-replaceable, internal battery
Technology: Nickel metal hydride
Run time: 60 minutes minimum when fully charged and properly maintained

Mounting
Front panel mounted

Mating Connectors
Mid-Continent P/N 9017646 kit contains custom DB15 connector with configuration module, pitot and static connectors

Certification
FAA TSO certified to C2d, C3e, C4c, C6e (incomplete), 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

Rights
U.S. Patent 9,739,611

Power Input
10-32 VDC; 6 W nominal, 40 W max