Overview

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 Input: 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)
• Battery run time will vary depending on total power load for all other installations

Documents

• Installation Manual
• Technical Drawing