Embraer EMB145, Operation Manual

Page: 225 / 2662

NORMAL PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-02-17
Page
10
Code
02 REVISION 37
AOM
-145/
111
4
Standby Instruments ..................................................... SET
Conventional Standby Instruments:
Uncage the STANDBY ATTITUDE indicator, if it is caged, and
observe that the red flag is removed and the horizon is steady.
Compare its indication with the main attitude indicators. Set the
QNH and compare its readout with one of the main altitude
tapes.
Integrated Standby Instrument System:
Ensure airplane is not moved until ISIS is initialized. Initialization
occurs within 90 seconds after airplane power-up.
Compare its indication with the main attitude indicators. Set the
QNH and compare its readout with the main altitude tapes.
Check no ALT or SPD flags displayed.
MFD SYS Pages ........................................................... CHECK
RMU .............................................................................. SET
The PF assigned for the flight must set the COMM and NAV
frequencies as appropriate for the expected SID or departure
procedure.
The use of the VHF COMM sets must follow the arrangement
described below:
COMM 1: ATC
COMM 2: Company frequency, ATIS, VOLMET, etc.
COMM 3 (if available): Distress (121.5) and air-to-air broadcast.
Verify if the ATC/TCAS window is in SBY. Select the ABOVE
function.
Test the TCAS by placing the yellow cursor box over the code.
Press the RMU test button for 5 to 7 seconds until the test OK
message on the RMU and “TCAS TEST, PASSED” aural
annunciation is heard.
Enter the flight number or CALL SIGN on the appropriated window
into the RMU.
Verify that BACK-UP TUNING is set to NORMAL and is copying
RMU2.
Flight Control DISCONNECT Handles ......................... CHECK
Speed Brake Lever ....................................................... CLOSED