OPERATOR’S
MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
Page
3-19
November 19, 2009
CRUISE PERFORMANCE PARAMETERS INITIALIZATION (if configured)
When a modification is made to the origin airport or associated departure procedure, the TRANS ALT field will
be update to show the navigation database extracted value, if one exists, otherwise the configured FMS default
value will be displayed.
When a modification is made to the destination airport or associated arrival procedure, the TRANS LVL field will
be update to show the navigation database extracted value, if one exists, otherwise the configured FMS default
value will be displayed.
The Transition Altitude and Transition Level are user modifiable.
Additional details on the TRANS ALT and TRANS LVL fields can be seen on the PLAN DATA page in Appendix
A.
For flight planning calculations while on ground, the CMA-9000 FMS will provide user modifiable Cruise TAS
and Cruise Wind values.
Upon a warm or cold start, the CMA-9000 FMS will keep the Cruise TAS value prior to the power down. Upon a
change in configuration, the CMA-9000 FMS will set the Cruise TAS value in accordance with the aircraft type:
ROTOR:
CRZ_TAS:
130KTS
FIX:
CRZ_TAS:
480KTS
The CMA-9000 FMS will reset the Cruise Wind value to zero after a cold start on ground. Upon a warm start or
cold start in air, the CMA-9000 FMS will keep the Cruise Wind value prior to the power down.
Display the INIT/REF INDEX 1/2 page by pressing [INIT REF].
1. Display the PLAN DATA 1/1 page by pressing [INIT REF], [NEXT] and <PLAN DATA> (LSK 4L).
2. To modify the TRANS ALT and/or TRANS LVL field(s), key in the transition altitude (e.g.: "18000" in feet or
"180" in flight level) and move it into the either the TRANS ALT or TRANS LVL field by pressing LSK 1L or
2L, respectively.
1 R
2 R
3 R
4 R
5 R
6 R
PLAN DATA 1/1
T R A N S A L T C R Z W I N D
18000
F T
300
T
/
90
K T
T R A N S L V L C R Z T A S
F L
180
360
K T
<
INIT/REF
1 L
2 L
3 L
4 L
5 L
6 L
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and must not be retained for reference
