Garmin SR02232LA Manual de Instruções descarregar pdf (Página 12)

400W Series Rotorcraft 190-00356-21 Rev. C

Instructions for Continued Airworthiness Page 12 of 15

Table 4: 400W Series Power Input

14 VDC 28 VDC

Input Connector Mode

Typical Max Typical Max

GPS 400W

Main power P4001 -- 760mA 1.4A 410mA 700mA

GNC 420W

Main power P4001 -- 1.12A 2.5A 560mA 1.2A

COM power P4002 RX 4mA 15mA 8mA 15mA

TX 3.25A 6.0A 1.6A 3.0A

GNC 420AW

Main power P4001 -- 1.12A 2.5A 560mA 1.2A

COM power P4002 RX N/A N/A 3mA 15mA

TX N/A N/A 1.6A 3.0A

GNS 430W

Main power P4001 -- 1.60A 2.5A 800mA 1.2A

COM power P4002 RX 4mA 15mA 8mA 15mA

TX 3.25A 6.0A 1.60A 3.0A

GNS 430AW

Main power P4001 -- 1.60A 2.5A 800mA 1.2A

COM power P4002 RX N/A N/A 3mA 15mA

TX N/A N/A 1.6A 3.0A

Circuits should be protected in accordance with the approved data in this document (see Table 5) and

the guidelines in AC 43.13-1B, chapter 11 Section 4. For rotorcraft with multiple power busses, it is

recommended that for each 400W Series unit, all power inputs be connected to the same power bus. For

power interconnect drawings, refer to ‘Appendix H STC Approved Installation Diagrams’ in the 400W

Series Installation Manual (P/N 190-00356-02), listed under reference documentation in paragraph 2.1 of

this document.

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Garmin SR02232LA Manual de Instruções Página 12