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Esterline CMA-9000 - Page 536

Esterline CMA-9000
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OPERATOR’S MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
If the aircraft is located before 50nm from the T/D, when an immediate descent in cruise is initiated by lowering
or:
or Modified route
count for the new cruise altitude.
manually changed before selecting a new FGCP altitude. However, the aircraft
ob is pushed.
altitude remains
ircraft remains level).
s the VNAV mode and the
GCP altitude selector, the autopilot engages the DES mode and the aircraft starts
descending;
e engages.
OUT alert message is raised
page and confirms
activation by pressing the EXEC key.
eed depending
ance to reserves are displayed.
The crew can manually de-activate engine-out by pressing the CANCEL E/O prompt in the engine-out cruise
page.
NOTES:
the FGCP-selected altitude and pushing the select
The aircraft will descend to the FGCP-selected altitude.
The CRZ page title automatically changes to CRZ DES.
The Cruise Altitude will automatically be updated to the FGCP altitude for the Active
(whichever is displayed).
The vertical profile will automatically be recomputed to ac
The CRZ ALT can also be
will not descend until the FGCP altitude is lowered and the FGCP pre-selected altitude kn
When this action is performed, the autopilot engages the DES mode.
If the aircraft is within 50nm of the T/D:
Lowering the FGCP altitude will preselect a new selected altitude (the current cruise
unchanged and the a
Pressing the VNAV push-button on the FGCP, arms the VNAV mode of the autopilot.
There are three operational options:
If the crew presses the DES NOW prompt on the MCDU, the autopilot engage
aircraft starts descending;
If the crew pushes the F
If the aircraft sequences the T/D, the airplane starts descending and the VNAV mod
1.7.4 Engine Out in Cruise
The engine-out detection and alerting is performed automatically; ENGINE
The crew manually activates engine-out by pressing the ENGINE OUT prompt in the cruise
the
During engine out cruise, the FMS provides speed guidance at either the Green-Dot or LRC sp
upon the crew selection.
Predictions of the estimated time enroute (ETE) and dist
The activation/de-activation of FMS E/O mode can be performed manually at any time while in Cruise
regardless of the automatic detection of an E/O condition.
The FMS ignores FGCP-selected speed if engine out is active.
Page F-29
August 17, 2010
DRAFT

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