Garmin GNS 530W 사용 설명서 - 페이지 6

{카테고리_이름} Garmin GNS 530W에 대한 사용 설명서을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 530W 23 페이지. For continued airworthiness bell 206b
Garmin GNS 530W에 대해서도 마찬가지입니다: 파일럿 매뉴얼 부록 (24 페이지), 파일럿 매뉴얼 부록 (50 페이지), 파일럿 매뉴얼 부록 (50 페이지), 파일럿 매뉴얼 부록 (24 페이지), 보충 설명서 (12 페이지), 빠른 참조 (23 페이지), 빠른 참조 (25 페이지)

2.2 Description of Alteration

This STC upgrades existing avionics for the Bell 206B rotorcraft as summarized below.

The Garmin Model 500W Series GPS/WAAS Nav/Com unit is a 6 ¼ inch wide unit mounted in the center

pedestal of the Bell 206B. The 500W Series units combine a large number of easily accessible controls

to use the color multi-function display, Nav and Com transceiver, GPS/WAAS navigator in a single unit.

A GPS/WAAS antenna is installed on the top of the Bell 206B forward engine cowl. A monitored avionics

cooling fan is installed in the center pedestal with a fan fail fault annunciation located in the existing Bell

206B annunciator panel.

Installation of optional remote HTAWS annunciators, and optional cyclic stick switches for remote control

of COM and HTAWS functions are also covered under this STC.

The 500W Series unit can interface to the Garmin G500H system GDU 620 PFD/MFD for display of

navigation information and HTAWS annunciation.

Rotorcraft modified under this STC are restricted to VFR only, including rotorcraft that may not have

previously been restricted to VFR. To clarify this operation limitation, a placard with the text,

"APPROVED FOR DAY/NIGHT VFR" is required to be in the pilot's view.

The installed equipment is connected to an avionics bus that receives power as soon as the battery and

avionics master switches are turned on. Circuit breakers are installed on an overhead circuit breaker

panel as shown below. Note: dual navigator system installation as shown.

The installed 500W Series equipment can be accessed as described below:

500W Series

190-01226-03 Rev. 5

Instructions for Continued Airworthiness Bell 206B

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