737 Flight Crew Operations Manual
1.27
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
1.27
16 Maintain a cabin differential pressure of 0 psi by
limiting flight altitude to 9000 feet.
►►Go to step 24
17 Descend to the minimum safe altitude.
PT804 - PT817
18 CAB ALT indicator . . . . . . .Select a higher altitude
(maximum 13,000 feet) to
maintain a cabin differential
pressure of 0 psi
PM398 - PQ976, PT826 - PT832
19 LAND ALT indicator . . . . . .Select a higher altitude
(maximum 13,000 feet) to
maintain a cabin differential
pressure of 0 psi
►►Go to step 24
20 Descend to the minimum safe altitude.
PT804 - PT817
21 Pressurization mode selector . . . . . . . . . MAN DC
PM398 - PQ976, PT826 - PT832
22 Pressurization mode selector . . . . . . . . . . . . MAN
▼
Continued on next page
▼
▼Window Damage - Unheated Side (L3, R3) continued▼
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE light (as installed) will illuminate at
a cabin altitude of approximately 10,000
feet.
March 24, 2017
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