FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 2
Page 90 of 135 FAA APPROVED
NOTE
If the Course Deviation Indicator (CDI) is greater than one dot from center, the autopilot
will arm the BC mode and indicate BC in white on the PFD. The pilot must ensure that
the current heading will result in a capture of the selected course. If the CDI is one dot or
less from center, the autopilot will enter the capture mode when the APR button is
pressed and annunciate BC in green on the PFD.
5. Airspeed ................................................. MAINTAIN 120 KIAS OR GREATER (Recommended)
6. At the FAF ..................................Use desired vertical mode to fly the approach’s vertical profile
Use Altitude Preselect to level off at intermediate altitudes and at the MDA
NOTE
It is recommended to descend at 1000 ft/min or less. Descending at a higher rate or
reaching MDA too far before the Visual Descent Point (VDP) could cause TAWS or GPWS
alerts. If a TAWS or GPWS WARNING is issued, immediately follow the TAWS OR GPWS
WARNING procedure in the EMERGENCY PROCEDURES Section of this AFMS.
7. AFTER LEVELING AT MDA ...................... SET Missed Approach Altitude In Altitude Preselect
GO AROUND (GA)
1. Control Wheel ................................................................................................... GRASP FIRMLY
2. GO AROUND button (left power lever) .................................. PUSH – Verify GA / / GA on PFD
in lateral and vertical mode fields
3. Rotate to Go Around attitude ........................................... Follow Flight Director Command Bars
4. Balked Landing ........................................................................................................... EXECUTE
5. Mode Control Panel ....................... PRESS NAV to Fly Published Missed Approach Procedure
PRESS HDG to Fly ATC Assigned Missed Approach Heading
NOTE
The pilot is responsible for initial missed approach guidance in accordance with published
procedure. The G1000 may not provide correct guidance until the aircraft is established
on a defined leg of the procedure.
6. Altitude Preselect .................................................................. VERIFY Set to appropriate altitude
At An Appropriate Safe Altitude:
7. Mode Control Panel ................................................................................ AP to Engage Autopilot