Garmin GFC 600 Руководство - Страница 27

Просмотреть онлайн или скачать pdf Руководство для Дисплей авионики Garmin GFC 600. Garmin GFC 600 46 страниц. Installed in piper pa46-310p/350p

TRANSITION to ILS APPROACH from VERTICAL NAVIGATION

(Optional Feature)

1. Navigation Source ................................................................................................. SELECT CDI to GPS

2. Approach Procedure ................................................................. LOAD into the GPS navigator flight plan

3. CDI.....................................................................................................VERIFY desired track

4. Altitude Preselect................................................ADJUST to desired altitude below current altitude

5. GMC 605 VNV Key....................................................................................................PRESS

6. Bold or subdued font VPTH annunciation............................................................. VERIFY on GMC 605

7. GMC 605 APR Key....................................................................................................PRESS

8. Bold or subdued font LOC and GS annunciations................................................... VERIFY on GMC 605

9. Airspeed..........................................................................MAINTAIN 90 KIAS or greater (recommended)

If the altitude preselect is not set at least 75 FT below the current aircraft altitude, the

autopilot will not capture the vertical navigation path.

The autopilot can capture the vertical navigation path from above or below.

Under certain display conditions, VPTH and GS armed modes are combined into a single

"GS/V" annunciation.

If the Course Deviation Indicator (CDI) is greater than half-scale deflection, the autopilot

will arm the LOC mode. The pilot must ensure that the current heading will result in a

capture of the selected course. If the CDI is within half scale deflection, the autopilot will

enter the capture mode when the APR key is pressed.

When the selected navigation source is an ILS, glideslope coupling is automatically

armed when the APR key is pressed. The glideslope cannot be captured until the

localizer is captured. The autopilot can capture the glideslope from above or below the

glideslope.

190-02011-11 Rev. 2

(VERIFY aircraft flight path will intercept the vertical navigation profile)

NOTE

GFC 600 Autopilot Installed in Piper PA-46-310P/350P

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