Description
General aviation battery designed for a two battery, two bus, two alternator / generator system to satisfy the requirement for a secondary system to support FADEC and / or Glass Panel installations. Designed to run in parallel only when cranking. These are the only batteries required in the aircraft.
Full Authority Digital Engine Control (FADEC)
Electronic Engine Control (EEC)
Electronic Flight Instrument System (EFIS) and / or
Electronic Ignition Systems
Two light weight 8.5 AH batteries buss tied in parallel produce more starting power than one large 17 AH battery.Recombinant Gas – The RG® Series are low resistance, valve regulated lead acid (VRLA) batteries.
Superior starting power
Reliable essential power in the event of a generator failure
Low impedance design
Maintenance free
Constructed with non removable vent valves – no addition of electrolyte or water required
Aerobatic: Non spillable at any altitude or attitude
Factory tested to assure airworthiness
Manufactured with absorbed glass mat separators (AGM)
NOTE: This aircraft battery is not designed or intended for turbine aircraft engine starting applications. Warranty coverage applies to reciprocating aircraft engine starting, and standby / essential power installations.
SpecificationsPrimary Aircraft Purpose: General Aviation AGM Aircraft BatteryVoltage :24vRated Capacity: C1 = 1 hr.rate in ampere hours: 8.50Max Weight: 22.00 lb / 10.0 kg
Documents  FAA-PMA Installation Eligibility List  Limited Warranty   Warranty Card  RG Series Aircraft Battery Owner/Operator Manual  Storage and Boost Charge Recommendations  Valve Regulated (RG® Series) Lead Acid SDS  Concorde Battery AS9100 Certificate of Registration
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