IC E
ANT I
W IN G
IC E
ANT I
W IN G
P SI
C D
R PACK
OVHT
ISOLATION
VALVE
L PACK
2APU
BLEED
1
TRIP
RECIRC FAN
TEST
RESET
OFFOFF
ON ON
OFF
AUTO
OPE N
AUTO
OFF
AUTO
HIGH HIGH
AUTO
OFF
RAM D O OR
FUL L O PENBLE ED
DUA L
ALTN M ANU AL
DES CEN T
OFF S CH E DAU T O
FAIL
TRIP OFF
PAC K
OVE RHE AT
W IN G-BOD Y
BLE ED
TRIP O FF
TRIP O FF
PAC K
OVE RHE AT
W IN G-BOD Y
BLE ED
TRIP O FF
RAM D O OR
FUL L O PEN
0
20
40
60
80
DUC T
PRE SS
a b
g gaa
a
a
a
a
a
a
b
ELEC 1ELEC 2 ENG 2
OFF
ON
BHYD PUMPS
OFF
ON
ENG 1
A
LO W
PRE SSU RE
LOW
PRE SSU RE
OVE R HE A T
LO W
PRE SSU RE
OVE RHE AT
LOW
PRE SSU R E
B
A
C
A B C
BLEED AIR CONTROL
MODULE
AC/DC POWER CONTROL
PANEL, P5-4
HYDRAULIC PUMPS
PANEL, P5-8
FLIGHT COMPARTMENT
DUAL DUCT
PRESSURE GAGE
BLEED AIR
CONTROL MODULE
HYDRAULIC PUMPS
PANEL, P5-8
AC/DC POWER CONTROL
PANEL, P5-4
2309325 S0000524777_V2
NGS - Flight Deck Control Panels
Figure 202/47-00-00-990-801 (Sheet 2 of 2)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
47-00-00
Page 221
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF 568, 569, 581, 583, 585, 588-590, 592-599, 601-603, 606, 607, 610-615, 620,
625-627, 691-699, 833-835, 838, 971, 980-999; ILF 101, 301, 304, 308, 310, 314,
315, 317-319, 323, 331-399, 406, 409, 410, 412, 424, 425, 427-429, 451, 501-504,
507, 512-514, 516, 518, 524, 531-533, 535, 537, 552-556, 560-562, 567, 804-807,
812, 821, 822, 831, 832, 836, 837, 841, 842, 851, 852, 857, 858, 947, 948 POST
SB 737-47-1003