Generator Control Panels

Hitek, Inc. introduces the concept of the Totally Integrated Primary Electrical System for light aircraft.

This concept embraces an engineered and proven system that includes various combinations of the following features:

Primary Electric Power Distribution
Electric Power Control and Protection
Multiple Distribution Feeder Outputs with Wire Protection
Electric Starting with Automatic Control (Two(2) Step Starting)
Dual Engine Driven Electric Power Sources for Single Engine Aircraft (S/G + Aux Alt.)
Electric Air Conditioner Control with Auto Load Shed per FAA AC43.13-1B
Status Reporting and Metering Functions
Generator and Alternator Load Current
Generator Fail and Alternator Fail Annunciation
Low Voltage Warning

Battery State of Charge (SOC)

The real value in what all this means to the Aircraft Builder, whether Certified or Experimental, is best understood when you consider what you do not have to buy from other vendors, or fab in house such as:

GCU's (Generator Control Units)

ACU's (Alternator Control Units)

Primary Bus Bars and Cabling

Current Shunts (or other protective monitoring such as Hall Effect or CT's)

Primary Distribution Feeder Protection devices

Primary Junction Box

Another significant advantage is realized in assembly labor savings.
Additionally, you get the clean appearance of a well engineered installation.

Choose from one of the available models listed below, or contact us for a one on one consultation regarding your Electrical System Requirements.

5-11-0003F Mechanical and Electrical Specifications,   Typical Installation Diagram,
5-11-0004C Mechanical and Electrical Specifications,   Typical Installation Diagram,
5-11-0007   Mechanical and Electrical Specifications,   Typical Installation Diagram
5-11-0009   Mechanical and Electrical Specifications,   Typical Installation Diagram,