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Esterline CMA-9000 - Page 490

Esterline CMA-9000
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OPERATOR’S MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
STATUS ADVISORY
MESSAGE
DESCRIPTION ACTION
DRAG REQUIRED
While on descent, the FMS detects one of
the following conditions:
1.The current indicated Mach/airspeed
exceeds the Mach/IAS descent speed
target by more than the DRAG LIMIT
defined in the PDB; or
2. The current indicated Mach/airspeed
approaches the MMO/VMO by more than
0.01M/5 knots; or
NOTE: During deceleration path, the
predicted speed at the end of the path is
used.
Take appropriate action to slow the aircraft
down by reducing the current:
MACH/IAS below MMO/VMO by at
least 0.02M/10 knots, OR
MACH/IAS to within half of the DRAG
LIMIT parameter in the PDB of the
required descent target speed.
EMERGENCY
ENGAGED
Emergency Tuning switch has been
engaged.
NOTE: The radios are set to emergency
frequencies.
Acknowledge emergency status.
END OF OFFSET
End of offset navigation. Acknowledge the end of the offset.
F/O MAP CONTROL IN
USE
Capt and F/O are using the same FMS to
drive their EFIS map.
NOTE: Selected FMS is using F/O EFIS
panel selections. Capt EFIS control
panel selections are ignored.
Capt or F/O to select another FMS if
individual map displays are required.
FMS NAV IN DR
The FMS is receiving insufficient navigation
information from other sensors.
NOTE: The FMS is in dead reckoning
navigation mode using heading and
speed inputs and last computed
value of wind.
Take appropriate measure to fly in manual
mode. Verify sensors power status and
self-test status.
GPS INTEGRITY VALID
GPS sensor has just acquired integrity that
satisfies the limit requirement for the phase
of flight.
Acknowledge GPS navigation mode.
GPS NAV
DESELECTED
GPS sensor has been de-selected by the
pilot.
Ensure GPS navigation mode should be
deselected.
HOLD EXIT TYPE
CHANGED
A modified route that contains a holding
pattern for which the exit type has been
changed is executed.
Acknowledge the message and monitor
the lateral guidance to be consistent with
the newly entered exit type.
HSI SCALES
CHANGING
The FMS is commanding an HSI lateral
scale sensitivity increase when entering
terminal area and/or when adopting a new
RNP value.
Acknowledge HSI scale change.
HSI SCALES TO
CHANGE
At 3 nm inbound to the FAF, GPS approach
is enabled (armed).
The HSI lateral deviation sensitivity will
change from 1 nm to 0.3 nm full scale at 2
nm to the FAF waypoint.
Acknowledge HSI scale change.
ILS RECEIVER ACTIVE
ILS changed Status from STANDBY to
ACTIVE.
Acknowledge the status change.
IN INERTIAL MODE
Reversion to Inertial navigation mode.
Acknowledge Inertial navigation mode.
Verify GPS integrity by monitoring the
NAV STATUS page.
Page E-15
August 17, 2010
DRAFT

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