FAA Approved Airplane Flight Manual Supplement

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

Page 96 of 167 FAA APPROVED

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

For TAWS-A equipped aircraft: When executing a missed approach from an ILS approach,

occasional Glideslope Deviation cautions may be received while establishing the missed

approach climb, even if the aircraft is not below the ILS glideslope. This is caused by

transitioning through ILS glideslope side lobe signals. If the Glideslope Deviation alert

annunciates during the initial portion of the go-around, continue to execute the go-around

procedure and fly the appropriate missed approach procedure.

ILS GLIDE SLOPE INOPERATIVE

1. Load the approach into the Active Flight Plan .................................... VERIFY the G1000 tunes

the proper ILS frequency

2. Approach Minimums ................................................ SET on TMR/REF page (if not already set)

If Flying Vectors-To-Final:

3. Airplane on Vectors-To-Final

a. Mode Control Panel .................................................. PRESS HDG to fly ATC radar vectors

b. PROC button on PFDs or GCU ......................SELECT ‘ACTIVATE VECTORS-TO-FINAL’

NOTE

SUSP may annunciate on the HSI when Vectors-To-Final is selected. The flight plan will

automatically un-suspend when the airplane intercepts and turns inbound on the final

approach course. When automatic flight plan waypoint sequencing resumes, SUSP will

extinguish.

c. HSI CDI ......................................................... VERIFY CDI automatically changes to LOC

Course pointer slews to the front course

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

e. Mode Control Panel ........................................................... PRESS NAV, verify LOC armed

Pressing the NAV button will arm the autopilot / flight director to capture Localizer and

prevent Glideslope from arming or capturing if the glideslope is inoperative or out of

service.