Airplane Flight Manual Supplement

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C

Page 64 of 95

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..........................................................................................................................GPS

c. Mode Control Panel .................................................................... PRESS NAV (GPS Mode)

NOTE

Ensure groundspeed is less than 200 KTS within 1 minute of the IAF

d. When Established Inbound to the FAF ................................................. PRESS CDI softkey

until LOC navigation source to be used for the approach displays

(Autopilot / Flight Director Mode will automatically change to ROL)

e. VERIFY ............................................................. Course Pointer is set to the Front Course

f. Mode Control Panel ............................................................................................PRESS BC

BC Mode, Armed or Active

4. Established inbound on Final Approach Course

a. VERIFY Course Pointer is set to the front course

b. VERIFY LOC is annunciated on the HSI

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 110 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

Recommend descending 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 alerts. If a TAWS

WARNING is issued, immediately follow the TAWS WARNING procedure in the

EMERGENCY PROCEDURES Section of this AFMS.

7. AFTER LEVELING AT MDA......................SET Missed Approach Altitude In Altitude Preselect