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787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
1.6
1.6
Condition: Arcing, delamination, shattered, or cracked condition
of any flight deck window is observed.
If forward window arcing, shattered, or cracked:
FORWARD WINDOW HEAT
switch (Affected window). . . . . . . . . . . . . . . . . . . . . . . .OFF
[Removes electrical power to prevent arcing.]
BACKUP WINDOW HEAT switch (Affected side). . . . .OFF
Do not accomplish the following checklist:
WINDOW HEAT FWD
If damaged window deforms, or air leak is observed:
Plan to land at the nearest suitable airport.
If airplane altitude above 10,000 feet:
Descend to lowest safe altitude or 10,000 feet,
whichever is higher.
[Minimizes forces on the window. Outward cabin pressure
differential counters inward dynamic air load on the window.]
Sustained flight below 10,000 feet is not recommended
due to greater risk of bird strike.
U WINDOW DAMAGE L, R
December 15, 2006
787 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Air Systems Section 2
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary TOC.2.1
Table of Contents
[N]NCC.A2 NBoInN-N oArmLalT CIhTecUkliDstsE-A ir. S. y.s t.e m. .s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.1
[] CABIN ALTITUDE AUTO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2
CABIN TEMPERATURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2
[] CARGO A/C FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3
[] CARGO HEAT BULK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3
[] CARGO HEAT FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3
[] EQUIP CLG OVRD AFT, FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3
[] EQUIP COOLING AFT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3
[] EQUIP COOLING FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4
EQUIP OVBD VLV AFT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4
EQUIP OVRD VLV AFT, FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4
[] LANDING ALTITUDE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4
LIQUID CLG QTY L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.4
[] LIQUID COOLING L . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.5
[] LIQUID COOLING R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.5
[] OUTFLOW VALVE AFT, FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.6
[] PACK L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.6
[] PACK L+R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.8
[] PACK MODE L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10
RECIRC FAN LWR, UPR OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10
[] TRIM AIR L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10
VENTILATION ALTN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.10
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.2.2 D615Z003 Boeing Proprietary
Non-Normal Checklists -
Air Systems
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 2.1
2.1
NNC.2 Non-Normal Checklists-Air Systems
Condition: Cabin altitude is excessive.
# OXYGEN masks. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
# Crew communications. . . . . . . . . . . . . . . . . . . . . . Establish
# CABIN ALTITUDE and RATE. . . . . . . . . . . . . . . . . . . . Check
[Confirms pressurization problem.]
# If cabin altitude uncontrollable:
# Passenger OXYGEN switch. . . . . . . . . . . . . . . . . . . PUSH
Push and hold for 1 second.
[Backs up automatic activation of the passenger oxygen system.]
# Descent. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Accomplish
Without delay, close thrust levers, extend
speedbrakes, and descend at VMO/MMO. Level off at
lowest safe altitude or 10,000 feet, whichever is
higher. If structural integrity is in doubt, limit
airspeed and avoid high maneuvering loads.
[]CABIN ALTITUDE
December 15, 2006
787 Flight Crew Operations Manual
　
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