6 Manual Number 9018233, Revision A
Mid-Continent Instruments and Avionics December 22, 2014
1.2 TECHNICAL SPECIFICATIONS
1.2.1 ELECTRICAL ATTRIBUTES
Characteristics:
Input Voltage: 10-32 VDC
Input Power: (nominal) 4 watts (0.12A @ 28VDC)
(maximum) 25 watts max (limited to initial startup)
Lighting Input: n/a
Input Data: ARINC 429 (see Table 1.5)
Output Data: ARINC 429 (see Table 1.5);
discrete valid signal to ground; invalid signal is open (pin 2)
TABLE 1.1
1.2.2 PHYSICAL ATTRIBUTES
Characteristics:
Weight: 1.3 pounds (0.73 kg)
Dimensions:
(without connectors, mates & knob) Bezel: 2.30” x 5.20” x 0.125” (HxWxD)
Chassis: 2.31” x 3.16” x 4.84” (HxWxD)
Mating Connectors: 15-pin D-Sub with Configuration Module, MCIA p/n 9017275
Pneumatic fittings, MCIA p/n 9017642
Mounting: Mount from front; uses (4) #6-32 cap screws
TABLE 1.2
1.2.3 PERFORMANCE LIMITS
Characteristics:
Attitude: Pitch Angle No limits (360°+)
Pitch Rate 300° per second max
Roll Angle No limits (360°+)
Roll Rate 300° per second max
Altitude: Range -1,500 to +55,000 feet (available in meters)
Barometer 28.00 to 31.00 inches of mercury (available in mbar)
Airspeed: Range 20 to 500 knots (available in mph or kph)
TABLE 1.3
1.2.4 QUALIFICATIONS
Specifications:
Certifications: FAA TSO-C2d (Type B), C3e, C4c, C10b, C106, C113a,
C179a
EASA ETSO-C2d, C3d, C4c, C10b, C106, C113, C179a
Environmental Qualification: RTCA DO-160G
(details listed in Section 5.2)
Software Qualification: RTCA DO-178B, Design Assurance Level A
Complex Hardware Qualification: RTCA DO-254, Design Assurance Level A
TABLE 1.4
