Garmin GFC 500, Руководство пользователя

Страница: 24 / 44

AFMS
– GFC 500 Autopilot in Textron 182 Series
190-02291-06 Rev. 2
Page 4
–4
GO AROUND
1. GO AROUND button ....................................................................... PRESS
– Verify GA / GA on G5
autopilot will not disengage
2. Autopilot (if engaged) ............... VERIFY airplane pitches up following flight director command bars
3. Throttle ...................................................................................................... APPLY Go Around power
4. GMC 507 Mode Panel .................................... PRESS NAV to couple to selected navigation source
OR
PRESS HDG to Fly ATC Assigned Missed Approach Heading
5. Altitude Preselect .................................................................................................................. VERIFY
Set to appropriate altitude.
NOTE
The pilot is responsible for initial missed approach guidance in accordance with published
procedure. When the GA button is pressed the Flight Director command bars will command go-
around pitch attitude and wings level. The pilot must select the CDI to the appropriate navigation
source and select the desired lateral and vertical flight director modes.
MANUAL PITCH TRIM WITH AUTOPILOT ENGAGED
(Amber TRIM UP or TRIM DOWN displayed on G5.)
NOTE
If the aircraft is not equipped with a pitch trim servo, the pilot must manually adjust the pitch trim
when airspeed and aircraft configuration changes are made.
A message will be displayed on the G5 display to indicate the pitch servo is holding sustained force, and the pilot
must manually trim the aircraft.
1. If TRIM UP message is displayed ........................................................... MANUALLY TRIM nose up
2. If TRIM DOWN message is displayed ............................................... MANUALLY TRIM nose down