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时间:2010-09-27 07:35来源:蓝天飞行翻译 作者:admin
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(5) CABIN PRESSURIZATION, MAN
ALT selector ................................................ As required to maintain cabin altitude at
8,000 feet, to minimize the
pressure differential across
the affected door.
NOTE
Set the selector to “UP” to increase cabin altitude; “DN” to
reduce cabin altitude.
(6) CABIN PRESSURIZATION, MAN
RATE switch................................................ As required commensurate with crew and
passenger comfort.
When reaching target cabin altitude:
(7) CABIN PRESSURIZATION, MAN
ALT selector ............................................................. Set to mid position/centre.
(8) Descent ............................................................... Initiate to 10,000 feet or lowest safe
altitude, whichever is higher.
(9) Land at the nearest suitable airport.
At 10,000 feet or lowest safe altitude:
(10) CABIN PRESSURIZATION, MAN
ALT selector ..............................................................DN to decrease cabin altitude to
landing field elevation.
(11) CABIN PRESSURIZATION, MAN
RATE switch................................................ As required commensurate with crew and
passenger comfort.
ABNORMAL PROCEDURES
Doors
05−08−5
REV 68, Apr 16/07

DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. DOORS (CONT'D)
C. Passenger Door − Not Latched (Cont’d)
When reaching target cabin altitude:
(12) CABIN PRESSURIZATION, MAN
ALT selector ............................................................. Set to mid position/centre.
END
ABNORMAL PROCEDURES
Doors
05−08−6
REV 68, Apr 16/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. DOORS (CONT'D)
D. Baggage Door − Not Closed/Locked
Indication: BAGGAGE DOOR caution message on.
(1) PASS SIGNS, SEAT BLTS switch .......................Select to ON.
(2) Cabin pressure .....................................................Check normal.
Cabin pressure is normal:
Yes
(3) No further action required.
− END −
No
Switch to manual pressurization control:
(3) CABIN PRESSURIZATION, MAN
ALT selector .........................................................Check set to mid position/centre.
(4) CABIN PRESSURIZATION,
PRESS CONT switch/light ...................................Select to manual mode.
Check PRESS CONT
MANUAL light on.
(5) CABIN PRESSURIZATION, MAN
ALT selector ................................................ As required to maintain cabin altitude at
8,000 feet, to minimize the
pressure differential across
the affected door.
NOTE
Set the selector to “UP” to increase cabin altitude; “DN” to
reduce cabin altitude.
(6) CABIN PRESSURIZATION, MAN
RATE switch................................................ As required commensurate with crew and
passenger comfort.
When reaching target cabin altitude:
(7) CABIN PRESSURIZATION, MAN
ALT selector ............................................................. Set to mid position/centre.
(8) Descent ............................................................... Initiate to 10,000 feet or lowest safe
altitude, whichever is higher.
(9) Land at the nearest suitable airport.
At 10,000 feet or lowest safe altitude:
(10) CABIN PRESSURIZATION, MAN
ALT switch.................................................................DN to decrease cabin altitude to
landing field elevation.
(11) CABIN PRESSURIZATION, MAN
RATE switch................................................ As required commensurate with crew and
passenger comfort.
ABNORMAL PROCEDURES
Doors
05−08−7
REV 68, Apr 16/07

DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. DOORS (CONT'D)
D. Baggage Door − Not Closed/Locked (Cont’d)
When reaching target cabin altitude:
(12) CABIN PRESSURIZATION, MAN
ALT selector ............................................................. Set to mid position/centre.
END
ABNORMAL PROCEDURES
Doors
05−08−8
REV 68, Apr 16/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ELECTRICAL
A. AC Bus 1 Transfer Failure
Indication: AC 1 AUTOXFER caution message and associated AUTO XFER FAIL light
on.
AC Bus 1 is powered:
Yes
(1) No further action required.
− END −
No
(1) Affected airplane systems .................................. Review
 
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