OPERATOR’S MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
CAUTIO with ATC altitude
oint altitude constraints. The FGCP altitude must
the vertical path containing speed restrictions, the flight crew must
comply with the altitude constraints using the FGCP pre-selected altitude as the airplane may not
es the following VNAV-related information for display on the PFD:
and digital readout
• Vertical Track Deviation (VDEV)
-of-Descent, End-of-Descent, Pseudo-waypoints and Deceleration symbols
(refer to Table 1-1 for details).
d alerts are generated when the FMS detects vertical profile anomalies or performance
problems. A scratchpad alert message may also cause the display of an associated message on the PFD (e.g.
1.2 Preflight
1.2.1 Aircraft Performance Status Check
Confirm that the Aircraft, Policy and Engine type displayed on the IDENT 2/2 page are correct.
CAUTION: If there is a discrepancy between the displayed and actual aircraft and/or engine type, do not
initialize VNAV and advise maintenance.
N: In climb, the flight crew remain responsible at all times for compliance
clearances and instructions and wayp
be set appropriately to ensure compliance.
In descent operations above
converge quickly to the descent path.
PFD displays: The FMS provid
• Target speed: speed bug
• V1, speed bug and digital readout
• VR, speed bug
ND displays: Top-of-Climb, Top
1.1.3 VNAV Advisories & Alerts
Scratchpad advisories an
Drag Required).
FMS1 IDENT 2/2
AIRCRAFT ENGINES
SSJ100 SaM-146 G
MAGVAR MODEL POLICY
2005 (DEF) SSJ100 POL
{SETUP POS INIT}
Page F-9
August 17, 2010
To Next Page
Loading...