OPERATOR’S MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
B.
• The crew manually entered the speed schedule .800/290 at LSK 2L.
• The field title at LSK 2L displays MAN SPD
• The descent mode is active (the target speed is displayed in reverse video – ACT is displayed in the
page title).
• The active target speed is Mach .800 in reverse video white.
• The aircraft is 50 feet below the FMS-computed descent path.
• An altitude-constrained descent waypoint (NOLLA) is ahead of the aircraft. The FMS displays the
computed ETA and DTG to the descent waypoint.
• The "FPA" field displays the currently flown aircraft descent angle "γ", which can be expressed as the
aircraft pitch attitude (θ) minus the angle of attack (α).
• The Vertical Bearing (V/B) and Vertical Speed (V/S) are calculated from the present position to the
waypoint position and altitude constraint defined in 3R
C. In the following example:
• The crew entered a speed schedule at LSK 2L;
• The descent mode is active (the active target speed is displayed in reverse video and ACT is displayed
in the page title).
• The airplane is below the crossover altitude and above the speed restriction altitude; the active target
speed is 290kts.
• There is a FAF in the active flight plan, hence the E/D data field shows the following:
• The E/D speed (manual entry of 180); AND
• E/D location: DTG (8 nm) to the FAF.
• The crew has manually entered the waypoint “HOAGI” in LSK [3R] data field that has an altitude
constraint of 15500ft. V/B and V/S are calculated from the present position to "HOAGI".
ACT MANUAL
ES 3/5
E/D(KT/NM) AT NOLLA
180 / 8 220/11000A
MAN SPD TO NOLLA
.800/290 2032.1z/52.NM
SPD REST WPT / ALT
250/10000 HOAGI/15500<
V/B V/S
2.7 2000
FPA VDEV
<SCHED
2.6 -50
PROFILE>
ACT MANUAL DES 3/5
E/D(KT/NM/FT) AT NOLLA
195/15/3000 220/ 11000A
MAN SPD TO NOLLA
.800/290 2022.1z/25.3NM
SPD REST WPT / ALT
250/10000 NOLLA/11200<
V/B V/S
2.2 1200
FPA VDEV
<SCHED 2.1 -50
PROFILE>
Page RRJ-A-21
August 17, 2010
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