Embraer 175 - Electrical

AIRPLANE
FLIGHT
MANUAL
EMERGENCY &
ABNORMAL
PROCEDURES
ANAC APPROVED 4-10
REVISION 15 code 01 Page 1
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
ELECTRICAL
TABLE OF CONTENTS
Block Page
WARNING
BATTERY DISCHARGING................................................4-10.......... 03
BATTERY 1 (2) OVERTEMPERATURE ...........................4-10.......... 03
BATTERY 1-2 OFF............................................................4-10.......... 03
ELECTRICAL EMERGENCY.............................................4-10.......... 04
CAUTION
AC BUS 1 OFF ..................................................................4-10.......... 05
AC BUS 2 OFF ..................................................................4-10.......... 05
AC ESSENTIAL BUS OFF ................................................4-10.......... 05
AC STANDBY BUS OFF ...................................................4-10.......... 06
APU GENERATOR OFF BUS...........................................4-10.......... 06
BATTERY 1 (2) DISCHARGING .......................................4-10.......... 06
BATTERY 1 OFF...............................................................4-10.......... 06
BATTERY 2 OFF...............................................................4-10.......... 06
DC BUS 1 OFF..................................................................4-10.......... 07
DC BUS 2 OFF..................................................................4-10.......... 07
DC ESSENTIAL BUS 1 OFF .............................................4-10.......... 07
DC ESSENTIAL BUS 2 OFF .............................................4-10.......... 09
DC ESSENTIAL BUS 3 OFF .............................................4-10.......... 10
GPU CONNECTED ...........................................................4-10.......... 10
IDG 1 (2) OFF BUS ...........................................................4-10.......... 10
IDG 1 (2) OIL .....................................................................4-10.......... 10
TRU 1 (2) FAILURE...........................................................4-10.......... 10
TRU ESSENTIAL FAILURE ..............................................4-10.......... 10