AMS 2000 does not act as an auto pilot, or control the aircraft in any way. Think of it as an assistant to you, the pilot, which keeps track of minor details and frees you to fly the aircraft.
The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements. The AMS 2000 should be installed in accordance with the standards established by the customer’s installing agency and existing conditions, as to unit location and type of installation.
Page 2-2 P/N 8900 Electrical Installation The AMS 2000 will operate with an input range from 14 to 28VDC. Refer to the attached interconnect drawing 4089-023. The installing facility will supply and fabricate all external cables. The required connectors are included in the install kit. The length and routing of external cables must be carefully measured and planned before the actual installation is attempted.
Rev M Page 2-3 P/N 8900 The AMS 2000 can be selected to receive Gray code or serial data input. Use Jumper S3 to select serial or Gray code input as indicated (See figure 2-1). Serial option - In Serial mode Pin 14 is the RX, RS-232 communication line that is used to receive serial data from the encoder (8800-X) or Serializer (9200-X).
IN8900A Shadin Avionics File: IN8900AMG.doc Directory: 8900 INSTALLATION MANUAL AMS 2000, ALTITUDE ALERT SYSTEM Rev M Page 2-4 P/N 8900 Post Installation Test Procedure 1. Verify proper jumper selection per drawing 4089-024. 2. Aircraft power on. 3. Refer to Operation Guide to verify operation of 30 second self test.
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