Embraer 175 - Page 246

EMERGENCY &
ABNORMAL
PROCEDURES
AIRPLANE
F
LIGHT
MANUAL
4-18 ANAC APPROVED
Page 2 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
AFM
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1385
CAUTION
CREW WARNING SYSTEM FAULT .................................4-18..........07
DISPLAY CONTROL FAILURE .........................................4-18..........07
DISPLAY CONTROL FAULT.............................................4-18..........08
EICAS FAULT....................................................................4-18..........08
EICAS OVERHEAT............................................................4-18..........08
FMS POSITION DISAGREE..............................................4-18..........08
FMS 1(2)-GPS POSITION DISAGREE .............................4-18..........08
GROUND PROXIMITY FAILURE......................................4-18 ..........08
IRS EXCESSIVE MOTION ................................................4-18..........08
IRS 1 (2) FAILURE.............................................................4-18..........08
MCDU 1 (2) OVERHEAT
(PRE-MOD. SB 170-31-0017) ......................................4-18..........08
MFD 1 (2) FAULT...............................................................4-18..........09
MFD 1 (2) OVERHEAT ......................................................4-18 ..........09
NAVCOM 1 (2) FAILURE...................................................4-18..........09
NAVCOM 1 (2) OVERHEAT ..............................................4-18..........09
PFD 1 (2) FAULT ...............................................................4-18..........09
PFD 1 (2) OVERHEAT.......................................................4-18..........10
SYSTEM CONFIGURATION FAILURE.............................4-18..........10
TERRAIN FAILURE ...........................................................4-18 ..........10
VALIDATE CONFIGURATION ..........................................4-18..........10
VHF 3 FAILURE.................................................................4-18..........10
VHF 1 (2) (3) OVERHEAT .................................................4-18..........10
WINDSHEAR FAILURE.....................................................4-18..........10
ADVISORY
ADS PROBE 1 (2) (3) (4) FAILURE...................................4-18 ..........11