Airplane Flight Manual Supplement

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air
Page 59 of 95
NOTE
Ensure groundspeed is less than 200 KTS within 1 minute of the IAF
Airplane will navigate in GPS mode throughout the intermediate portion of the approach
procedure. When the airplane is inbound towards the final approach course, the CDI
will automatically switch from GPS/SBAS navigation to LOC navigation.
d. VERIFY ................................................................. Course pointer slews to the front course
4. Established inbound on Final Approach Course (FAF Active Waypoint)
a. VERIFY Course Pointer is set to the final approach course
b. VERIFY LOC is annunciated on the HSI
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
RNAV (GPS) (LPV or LNAV/VNAV)
1. Load the approach into the Active Flight Plan
2. Approach Minimums............................................................................ SET ON TMR/REF page
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 MFD...................... SELECT ‘ACTIVATE VECTORS-TO-FINAL’
NOTE
SUSP may annunciate on the HSI when Vectors-To-Final is selected. The flight plan will
automatically unsuspend when the airplane intercepts and turns inbound on the final
approach course. When automatic flight plan waypoint sequencing resumes, SUSP will
extinguish.
c. VERIFY ................................................................. Course pointer slews to the front course
d. Mode Control Panel .............................................PRESS APR, Verify GPS and GP armed