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This does not apply to the DUAL ENG FAIL/STALL checklist
December 15, 2006
787 Flight Crew Operations Manual
Checklist Introduction -
Non-Normal Checklists
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary CI.2.5
After moving the control, the crewmember taking the action also states the
checklist response. Action is taken by the pilot flying and the pilot monitoring
based on the crewmember’s area of responsibility. With the airplane stationary on
the ground, action is taken by the captain as pilot flying and the first officer as pilot
monitoring based on preflight areas of responsibility.
Closed loop (sensed) checklist items change from white to green when the action
is taken. The pilot monitoring is responsible to “check off” any open loop (not
sensed) item and to verify that all closed loop items are green.
The pilot flying may also direct reference procedures to be done by recall if no
hazard is created by such action, or if the situation does not allow reference to a
checklist.
Checklists show lists of inoperative equipment only when knowledge of the
condition of such equipment is needed for planning the rest of the flight and the
condition is not shown on EICAS.
The pilot flying is to be made aware when there are deferred items. These items
may be delayed until the usual point during approach or landing.
Consequential EICAS alert messages can show as the result of a primary failure
condition (such as AUTO SPEEDBRAKE from HYD PRESS SYS C) or the result
of a non–normal checklist crew action (such as PACK L from SMOKE AIR
CONDITIONING). Consequential messages are shown for crew awareness with
icons automatically removed. The checklists for the consequential messages can
have procedural steps, notes, or other information. The crew does not do these
checklists. If consequential checklist steps, notes, and information are applicable
to the primary failure condition, then these are included in the primary checklist.
The statement “Do not accomplish the following checklists:” followed by a list of
the checklists, shows in the printed primary checklist to inform the crew of
consequential checklists. All consequential alert messages may not show while
doing the primary checklist, depending on operational circumstances. The
statement “Inhibited checklists:” followed by the list, shows in the electronic
checklist. The statement need not be read aloud when doing the electronic
checklist.
Following completion of the applicable non–normal checklist items, normal
checklists are used to verify that the configuration is correct for each phase of
flight.
Pilots must be aware that checklists cannot be made for all conceivable situations
and are not intended to replace good judgment. In some conditions, deviation from
checklists may, at the captain’s discretion, be needed.
The following symbol shows that the checklist is complete.
Each checklist has a checklist complete symbol at the end.
December 15, 2006
787 Flight Crew Operations Manual
Checklist Introduction -
Non-Normal Checklists
Copyright © The Boeing Company. See title page for details.
CI.2.6 D615Z003 Boeing Proprietary
The checklist complete symbol can also be in the body of the checklist. This
occurs only when a checklist divides into two or more paths. Each path can have
a checklist complete symbol. The checklist complete symbol shows the end of the
applicable path. The crew need not continue the checklist after that point.
Following completion of each non–normal checklist, the pilot monitoring states:
“_______ CHECKLIST COMPLETE.” When a non–normal checklist is
complete except for the deferred items, and the normal checklist to which the
items have been deferred has not yet been done, the pilot monitoring states:
“______ CHECKLIST COMPLETE EXCEPT FOR DEFERRED ITEMS.”
December 15, 2006
787 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Unannunciated Checklists Section 0
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary TOC.0.1
Table of Contents
NuNAC.B0 NOonR-NToErmDal CEhNecGkliIstNs-UEn aSnTnuAncRiatTed LCh,e Rck li.s t.s . . . . . . . . . . . . . . . . . . . . . . 0.1
u DITCHING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.2
u DUAL ENG FAIL/STALL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.5
u ENG IN–FLIGHT START L, R . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.6
u ENG LIM/SURGE/STALL L, R . . . . . . . . . . . . . . . . . . . . . . . . . . 0.6
　
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