OPERATOR’S MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
A transition to E/O Cruise mode occurs as soon as the CRUISE altitude is captured during the LRC E/O Drift-
lly changes to E/O CRZ.
is above the engine-out LRC ceiling, the aircraft may not be able to
speed.
ulating cruise trip predictions, while assuming the crew
• Sequencing the next speed-constrained waypoint, or
• Switching to Descent, o
• Entering or exiting a ho hold.
NOTES:
• The target speed displayed in reverse video remains derived from the FMS.
• For accurate profile calculation over long cruise segments, select a new FMS cruise speed or
use MACH cruise speed segments instead of using FCGP Speed intervention.
Down.
The VNAV page title automatica
• The FMS commands LRC speed.
CAUTION: If the FCP-selected altitude
maintain this altitude at LRC
1.7.5 FGCP Speed Intervention in Cruise
The FMS uses the FGCP selected CAS or MACH for calc
will revert to FMS-computed speed when:
r
ld other than an altitude-constrained
ACT MIN FUEL CRZ 2/5
CRZ ALT MAX
FL350 FL400
MFUEL SPD
.790
{SCHED
{DES FORECAST PROFILE}
Page F-34
August 17, 2010