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PSP 604-15
AIR-CONDITIONING AND
PRESSURIZATION
L (R) PACK NOT OFF
L PACK NOT OFF
or
R PACK NOT OFF
(1) Affected PACK ....................................................................... ON
(2) Affected PACK ..................................................................... OFF
L (R) PACK NOT OFF caution message persists:
Yes
(3) Affected 10TH STAGE bleed.................................CLOSED
(4) 10TH STAGE ISOL ................................................. CLOSE
APU operating and L PACK NOT OFF caution message on:
Yes
(5) APU LCV..........................................CHECK CLOSED
− END −
No
(3) No further action required.
END
CABIN ALT
CABIN ALT
(1) 10TH STAGE bleeds............................................CHECK OPEN
(2) PACKs.......................................................................CHECK ON
(3) Thrust ........................................................................ INCREASE
(4) EMER DEPRESS....................................................CHECK OFF
(5) MAN ALT.......................................................MID POS/CENTRE
Automatic pressurization is restored:
Yes
(6) No further action required.
− END −
No
(6) Manual Cabin Pressurization
Control Procedure ................................................ACCOMPLISH
(See Page ABNORM 2–6)
END
ABNORM 2-4
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AIR-CONDITIONING AND
PRESSURIZATION
LANDING ALT HI
LANDING ALT HI
(1) LDG ALT .........................................................................CHECK
On airplanes 5301 to 5366 without SB 604−21−004:
NOTE
If destination field elevation is greater than 8,000 ft,
select 6,000 ft and reset destination field elevation at
the beginning of the descent.
If in flight:
(1) Cabin altitude ..............................................................MONITOR
END
Unpressurized Flight
(1) Altitude ...........................................................MAX 10,000 FEET
or lowest safe altitude.
(2) RAM-AIR ........................................................................... OPEN
(3) EMER DEPRESS................................................................... ON
(4) Airspeed ....................................................................... 250 KIAS
recommended during cruise to provide sufficient airflow to
cabin.
END
ABNORM 2-5
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AIR-CONDITIONING AND
PRESSURIZATION
Manual Cabin Pressurization Control
(1) MAN ALT.......................................................MID POS/CENTRE
(2) PRESS CONT...............................................................MANUAL
To increase cabin altitude:
(3) MAN ALT.................................................................................UP
(4) MAN RATE..........................................................AS REQUIRED
To decrease cabin altitude:
(3) MAN ALT................................................................................ DN
(4) MAN RATE..........................................................AS REQUIRED
To maintain cabin altitude:
When reaching target cabin altitude as per the table below:
(5) MAN ALT.......................................................MID POS/CENTRE
CRUISE FL 180 200 220 240 260 280 290
TGT CABIN ALT 1700 2000 2400 2800 3200 3700 4100
CRUISE FL 310 330 350 370 390 410
TGT CABIN ALT 4600 5300 6000 6700 7400 8000
Before landing:
Differential pressure exists after landing:
Yes
(6) MAN ALT.........................................................................UP
(7) MAN RATE.........................................................MAX INCR
NOTE
Do not set cabin altitude below destination field
elevation.
− END −
No
(6) No further action required.
END
ABNORM 2-6
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AIR-CONDITIONING AND
PRESSURIZATION
CPAM FAIL
CPAM FAIL
NOTE
EICAS pressurization system readouts (e.g., cabin altitude,
rate of change, and differential pressure) are not available.
EICAS cabin pressure warning and caution messages are
also not available.
(1) Standby cabin altimeter...............................................MONITOR
END
Display Overtemperature
..........DISPLAY TEMP annunciation on affected CRT
..........Raster image is removed from the affected CRT
EICAS display is affected:
　
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