787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Flight Management, Navigation -
FMC Takeoff and Climb
Copyright © The Boeing Company. See title page for details.
11.41.6 D615Z003-TBC
Manually change transition altitude here or on DESCENT FORECAST page.
Valid entries are XXX, XXXX, XXXXX, or FLXXX.
CDU altitude data change from altitudes to flight levels above the transition
altitude.
Displays maximum angle of climb speed.
Push – displays speed in the scratchpad for pilot selection to the speed line.
Push (below speed transition or restriction altitude) –
• displays MOD EO CLB page
• deletes climb speed transition or restriction data
Push (below engine-out maximum altitude) – displays MOD EO CLB page.
Push (above engine-out maximum altitude) –
• displays MOD EO D/D or MOD EO LRC D/D page
• cruise altitude (1L) lowered to engine-out maximum altitude if that altitude
is less than the active cruise altitude
Shaded white until the modification executed. Upon execution, thrust reference
limit becomes CON in all cases above.
Displays when climb altitude constraint exists between current altitude and FMC
cruise altitude.
Push – deletes all waypoint altitude constraints between the airplane altitude and
the MCP altitude or FMC cruise altitude, whichever is lower. FMC cruise altitude
is not affected.
10
Maximum Angle (MAX ANGLE)
11
Engine Out (ENG OUT)
12
Climb Direct (CLB DIR)
August 14, 2009
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