Automatic flight control system – Garmin G1000 Piper PA-46 Matrix User Manual

Page 440

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Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix

190-01108-00 Rev. B

426

AUTOMATIC FLIGHT CONTROL SYSTEM

SY

STEM

O

VER

VIEW

FLIGHT

INSTRUMENTS

EICAS

AUDIO P

ANEL

& CNS

FLIGHT

MANA

GEMENT

HAZARD

AV

OID

ANCE

AFCS

ADDITIONAL FEA

TURES

APPENDICES

INDEX

Once the following conditions have been met, the glidepath can be captured:

• The active waypoint is at or after the final approach fix (FAF).

• Vertical deviation is valid.

• The CDI is at less than full scale deviation

• Automatic sequencing of waypoints has not been suspended (no ‘SUSP’ annunciation on the HSI)

Command Bars Indicate

Descent on Glidepath

Figure 7-18 Glidepath Mode

Glidepath

Mode Active

GPS Approach

Mode Active

Glidepath

Indicator

LNAV/VNAV

Approach

Active

GPS is

Selected

Navigation

Source

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