Garmin GFC 600 매뉴얼 - 페이지 17

{카테고리_이름} Garmin GFC 600에 대한 매뉴얼을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GFC 600 46 페이지. Installed in piper pa46-310p/350p

Section 3A – Abnormal Procedures

(Red LED illuminated next to AP key, AP FAIL in Message Window on GMC 605 display)

Indicates the AFCS system failed the automatic Pre-Flight test. The autopilot, yaw damper (if installed),

ESP, and electric elevator trim are inoperative. Flight Director may still function.

(AIRDAT FAIL in Message Window on GMC 605 display)

If pressure altitude, indicated airspeed, or true airspeed is invalid or missing, AIRDAT FAIL is displayed in

the message window. This indicates that any mode dependent on air data may not be supported such

as ESP high speed, ESP low speed, OSP, USP, IAS, VS, or ALT modes.

If necessary, the autopilot may be manually disconnected using any one of the following methods.

1. AP DISC / TRIM INT Button ................................................................................. PRESS and RELEASE

2. AP Button (GMC 605 mode control panel) ................................................................................. PRESS

3. Pitch Trim Switch.................................................................... ACTIVATE either half of the split switch

4. AUTOPILOT Circuit Breaker .......................................................................................................... PULL

190-02011-11 Rev. 2

(Yaw damper remains engaged)

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

(Pilot's control wheel)

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