FAA Approved Airplane Flight Manual Supplement

190-00716-02 Rev. 3 Hawker Beechcraft King Air 300/300LW

FAA APPROVED Page 99 of 167

If Flying Full Approach Including Transition:

3. Airplane cleared to an initial approach fix

a. ACTIVATE THE APPROACH from the PROC page,

ACTIVATE a DIRECT TO ( D ) the IAF

b. HSI CDI ...................................................................................... SELECT GPS Nav Source

c. Mode Control Panel .............................. PRESS APR, Verify GPS mode active, GP armed

d. Pathways ......................................................................................................... AS DESIRED

e. VERIFY ................................................................. Course pointer slews to the front course

4. Established inbound on Final Approach Course

a. VERIFY ................................................ Course Pointer is set to the final approach course

b. VERIFY ............................................................ LPV or L/VNAV is annunciated on the HSI

c. VERIFY ............................................................................................ GP Indicator Displays

d. VERIFY ............................................................................... SUSP is not displayed on HSI

e. SET ........................................................... Missed Approach Altitude In Altitude Preselect

5. Airspeed ................................................. MAINTAIN 120 KIAS OR GREATER (Recommended)

6. VERIFY ...................................................... Airplane Captures and Tracks GPS Course and GP

7. At Decision Altitude (DA):

a. A/P Y/D DISC TRIM INTRPT Switch ........................................................................ PRESS

Continue visually for a normal landing

b. GO AROUND button

(on left power lever) ............................................... PRESS, Execute Go Around Procedure

NOTE

If SBAS is unavailable before conducting an LNAV/VNAV approach, the G1000 will revert to

baro VNAV operation with automatic temperature compensation on the final approach

segment. The baro VNAV glidepath may be intercepted and flown in the same manner as

an SBAS generated glidepath. Refer to the G1000 Pilot’s Guide, 190-01343-01 Revision A

or later, for additional information on manually applying temperature compensation to other

segments of an approach and approach minima.