Embraer 175 - AMS CONTROLLER FAILURE; BLEED APU LEAKAGE; BLEED 1 (2) FAILURE; BLEED 1 (2) LEAKAGE

ABNORMAL
PROCEDURES
AIRPLANE
F
LIGHT
MANUAL
4-04 ANAC APPROVED
Page 4 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
AFM
-
1385
AMS CONTROLLER FAILURE
Exit and avoid icing conditions and limit the altitude to 10000 ft or MEA
(whichever is higher) maximum. At 10000 ft, push the pressurization
dump button in.
NOTE: - Assisted crossbleed start is not available.
- Pneumatic assisted engine start APU is not available.
BLEED APU LEAKAGE
Turn off APU bleed and wait 3 minutes.
If the message BLEED APU LEAK persists, press the APU emergency
stop button to turn the APU off.
If the message BLEED APU LEAK still persists, turn bleed 1 and the
crossbleed off and verify BLEED 1 OFF and XBLEED SW OFF
messages are displayed on EICAS.
BLEED 1 (2) FAILURE
Turn off the affected bleed and wait 1 minute.
If
the BLEED 1 (2) FAIL message extinguishes, turn the affected bleed
on.
If the BLEED 1 (2) FAIL message persists, limit the altitude to 31000 ft
maximum.
If both engine bleeds are inoperative and APU bleed is available, limit
the altitude to 15000 ft maximum.
BLEED 1 (2) LEAKAGE
Push the affected bleed button and the crossbleed button out. For
Bleed 1 Leak, push also the APU bleed out. Exit and avoid icing
conditions. Limit the altitude to 31000 ft maximum and wait 3 minutes.
If the BLEED 1 (2) LEAK message persists, push the opposite side
bleed button out, the APU bleed button out and limit the altitude to
10000 ft or MEA (whichever is higher). At 10000 ft push the
pressurization dump button in.