Standby Attitude Module (SAM)

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R143,846.17 - R165,914.21 excl. VAT

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SKU: N/A Category: Standby Instruments Tags: backup, md302

Description

Entirely self-contained, SAM® is a solid-state instrument that displays attitude, altitude, airspeed, slip, vertical trend, and heading information to the pilot during normal or standby operation in the event of primary instrument failure.

SAM’s small size and selectable orientation (horizontal and vertical) allows for flexible cockpit design and installation.

Five primary functions

Attitude, altitude, airspeed, slip and vertical trend indication

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Compact design

2.4” x 5.5” footprint

Airspeed range markings

Fully customizable to meet aircraft specifications

Extremely lightweight

Weighs just 1.6 lbs (0.73 kg)

Upgradeable software

Field-upgradeable software via standard USB port

Heading

Displayed heading via ARINC 429 input

Easy installation

One knob configures the display and provides menu
control to the pilot

Technology

Five primary functions utilize modern solid-state MEMS gyro, accelerometer and pressure transducer technology

FAA TSO certified

C2d, C3e, C4c, C10b, C106, C113a, C179a

Lithium-ion emergency battery

Self-contained, rechargeable Nanophosphate® lithium-ion emergency battery

ANAC TSO certified

C2d, C3e, C4c, C10b, C106, C113a, C179a

Selectable orientation

Horizontal and vertical

EASA ETSO certified

C2d, C3d (incomplete), C4c, C10b, C106, C113, C179a

Two-screen display

Smooth, high-definition graphics with extra-wide viewing angles and a user-friendly menu structure

RTCA qualified

RTCA DO-178B and DO-254 DAL A
RTCA DO-160 and RTCA DO-311 qualified

Adjustable lighting

External, automatic and manual dimming control settings and software configurable lighting curves

Warranty

Two-year or 2,000-hour warranty

Power input

10-32 VDC

Made in the USA

Designed and built in Wichita, Kansas

Static source error correction (SSEC)

Air data corrections configurable via standard USB port

Specifications

Model Number

MD302

Power Input

10-32 VDC; 6W nominal, 25W max

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

Displayed via ARINC 429 input (external interface dependant)

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 and 28 VDC external input or internal photocell
Programmable dimming curve

Pilot Interface

16-detent, push and turn knob

Dimensions

2.4″ x 5.5″

Weight

1.6 lbs (0.73 kg)

Battery

Rechargeable, field-replaceable, internal battery
Technology	Nanophosphate® lithium-ion
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 C2d, C3e, C4c, 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