Features

■  Simultaneously provides one primary power output and three lighting power outputs.

■  Pitot/Static ports or optional electrical input provides ability to work in automatic mode without pilot intervention: 

    •  Arms at beginning of flight.

    •  Activates instantly upon power loss.

    •  Recharges during flight.

    •  Turns off after flight.

■  Utilizes sealed lead-acid cells for reliability and cold weather performance.

■  Lighting outputs can power LED or incandescent lighting at 5, 14 or 28 VDC.

■  Remote, mini-annunciation switch (with automatic dimming) controls test and manual operations.

■  Quality Mil-Spec connectors included.

■  Field replaceable battery module(s).

■  Designed to operate Mid-Continent Instruments' standby attitude indicator for one hour after primary power loss.

■  Amp-hours of power at 18V: 1.0 Ah.

■  Total system weight: 3.2 lbs..

■  Designed and built in Wichita, Kansas, USA.

■  One year limited warranty.

Specifications

Power Inputa	10-32 VDC; 0.25A nominal, 4.0A max (14V) 2.0A max (28V)
Power Output	18 VDC nominal
Battery Capacity	1.0 Ah (0.05C) at 25°C
Certification	FAA TSO-C4c and RTCA DO-160E
Weight	3.2 lbs.
Mating Connector	25-pin female D-Sub (MD25F20JVL0 or equivalent)  9-pin female D-Sub (MD9F20JVL0 or equivalent)
Annunciator Lighting	LED backlighting, automatic internal dimming
Battery Charging	Automatic recharging when main power is present
Compatibility	Provides 60 minutes minimum (when fully charged) of backup power to  Mid-Continent's Electric Attitude Indicator Model 4200 or 4300 and lighting  power to two additional instruments (5, 14 or 28V)