Embraer EMB145 - Page 307

AIRPLANE
OPERATIONS
MANUAL
SUPPLEMENTARY
PROCEDURES
NAVIGATION
REVISION 36
1-02-80
Page
3
Code
01
AOM-145/1114
TRANSITION FROM FMS TO AUTOPILOT ILS APPROACH
ILS Frequency .............................................................. SELECT AS
REQUIRED
Radio Altitude ............................................................... SELECT AS
REQUIRED
HDG Mode (Flight Guidance Controller) ...................... SELECT
Before selection, set the desired interception course on heading
bug.
Navigation Source ........................................................ SELECT
Select the NAV source on the Display Control Panel (LOC course
selected on the PFD).
Autopilot/Flight Director ................................................ AS REQUIRED
When cleared for Approach:
APR Mode (Flight Guidance Controller).................. SELECT
ARC DME APPROACH USING FMS
Pilot Not-flying............................................................... CHECK DME
During Arc DME approach using FMS the pilot not-flying must check
DME Raw Data.
MISSED APPROACH
CAUTION:
ONLY PERMITTED FOR AIRPLANES WITH SOFTWARE
NZ4.8 MOD C OR NZ5.2 MOD B OR LATER SOFTWARE
VERSION INSTALLED.
Go-Around Button......................................................... PRESS
Thrust Levers................................................................ MAX
Verify that airplane rotates to 10° nose up wings level (Pitch Mode)
and changes to Speed Hold Mode after 20 seconds.
Flaps ............................................................................. 9°
With positive rate of climb:
Landing Gear........................................................... UP
Airspeed................................................................... APPROACH
CLIMB SPEED
OR ABOVE
NOTE: During the GO-AROUND procedure, the DON’T SINK aural
warning may sound. In this case monitor the sink rate and
follow the GO-AROUND guidance.