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ROC SEL HI = 600 ft/min -----------------
LOW = 750 ft/min
ROD SEL 2 See table below
MASTERID HI - Not master controller ------
LOW = master controller
QFE SEL HI = QFE not selected -----------
LOW = QFE selected
SLAVE ID HI = Not slave controller -------
LOW = slave controller
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CONFIGURATION ITEM MESSAGE
OFV CONN HI = OFV not connected ----------
LOW = OFV connected
IBIT IN HI = Other controller not in test
LOW = Other controller in test
CARGO HT Indicates position of overboard exhaust
valve actuator.
CONFIGURATION ITEM MESSAGE
MANUAL IN HI = Manual not selected. -------
LOW = Manual selected.
L A/G HI = Air mode -------------------
LOW = Ground mode.
R A/G HI = Air mode -------------------
LOW = Ground mode.
SHOP MODE HI = Not shop mode. -------------
LOW = Shop mode.
L PACK VLV HI = Left pack on. --------------
LOW = Left pack off.
R PACK VLV HI = Right pack on. -------------
LOW = Right pack off.
41K SEL HI = 41K altitude option not selected,
LOW = 41K altitude option selected.
AUTO CTL IN HI = Other controller in control.
LOW = Other controller not in control.
PNL OK HI = Selector Pnl not failed. ---
LOW = Selector Pnl failed.
This table shows the inputs for ROD SEL 1 and 2.
INPUT INPUT STATE
ROD SEL 2 LO HI LO HI
ROD SEL 1 LO LO HI HI
Descent Rate: -750 -350 -500 -350
Training Information Point
Cargo heat valve refers to the overboard exhaust valve in
equipment cooling. See the equipment cooling section for more
information on the overboard exhaust valve (SECTION 21-27).
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21-30-00-129
AIR CONDITIONING - PRESSURIZATION CONTROL - CPC - BITE - SYSTEM STATUS MENU
AIR CONDITIONING - PRESSURIZATION CONTROL - CPC - BITE - SYSTEM STATUS MENU
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
21-30-00-129
SYSTEM TEST AND CLEAR
SYSTEM TEST AND CLEAR prepares the controller for a
system test and to automatically clear the fault history.
When you push the YES button, the controller does a check to
find if the system is in the auto mode. If the system is not in auto
mode, the display shows SYS IN MANUAL for two seconds.
Then the display shows SELECT AUTO.
If you push the YES button when the system is in the auto mode,
the controller does a check to find if the other controller is in
BITE. If the other controller is in BITE, the display shows these
things:
* BOTH SYS IN IBIT for two seconds
* IBIT ABORTED for two seconds
* SYS TEST AND CLR.
For each of these questions, you must push the YES or NO
button. If you push the YES button after each question, the
display shows the next question. If you push the YES button
after the last question, the display shows TESTING. Each of the
8 lower digits come on for 12 seconds, one digit at a time. This
takes approximately 100 seconds.
If there is no fault while in test, the display shows SYSTEM OK
for 2 seconds. Then the display shows SYS TEST AND CLR.
If there is a fault during TESTING, the display shows nn EXIST
FAULTS for 2 seconds. Then the display shows EXISTING
FAULTS menu.
Training Information Point
The acronym DADC refers to the air data inertial reference unit.
The acronym SMC refers to the stall management yaw
dampener computer.
AIR CONDITIONING - PRESSURIZATION CONTROL - CPC - BITE - SYSTEM TEST AND CLEAR
EFFECTIVITY
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D633A101-GUN Jun 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
21-30-00-130
AIR CONDITIONING - PRESSURIZATION CONTROL - CPC - BITE - SYSTEM TEST AND CLEAR
AIR CONDITIONING - PRESSURIZATION CONTROL - CPC - BITE - SYSTEM TEST AND CLEAR
EFFECTIVITY
GUN ALL 21-30-00
Page 41
D633A101-GUN Jun 10/2005
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
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