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Boeing 787-8
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787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Air Systems -
Controls and Indicators
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC 2.10.7
Pressurization System
Pressurization Panel
AUTO – outflow valve controlled automatically.
MAN (manual) illuminated (amber) –
outflow valve is controlled manually
bypasses automatic outflow valve control and cabin altitude limiter
AUTO extinguished
OPEN – moves the outflow valve toward open.
CLOSE – moves the outflow valve toward closed.
Pull ON, then rotate –
sets landing altitude manually
landing altitude followed by MAN displayed on EICAS
when turned slowly, landing altitude display changes in 100 foot
increments. When turned quickly, display changes in 500 foot increments
Push –
landing altitude set automatically from FMS (Approach
, Ch. 11, Sec. 43)
landing altitude followed by AUTO displayed on primary EICAS
1
OUTFLOW VALVE (FWD / AFT) Switches
2
OUTFLOW VALVE MANUAL Switches
3
Landing Altitude (LDG ALT) Selector
MAN MAN
PRESSURIZATION
FWD AFT
OUTFLOW
VALVE
OPEN
OPEN
CLOSE CLOSE
PULL ON
MANUAL
LDG ALT
TAKEOFF & LDG
AUTOAUTO
MAX P .11 PSI
OVERHEAD PANEL
1
2
3
October 31, 2007

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