Esterline CMC Electronics 600 Dr. Frederik Philips Boulevard Ville Saint-Laurent, Quebec, Canada H4M 2S9
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OPERATOR'S MANUAL FLIGHT MANAGEMENT SYSTEM
CMA-9000 OPERATIONAL PROGRAM S/W 169-614876-056
Esterline CMC Electronics 600 Dr. Frederik Philips Boulevard Ville Saint-Laurent, Quebec, Canada H4M 2S9 Item No.: 930-600166-000
July 17, 2013
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
LIST OF EFFECTIVE PAGES NOTE The portion of the text affected by the latest change is indicated by a vertical line in the margin of the page. Changes to illustrations are indicated by miniature pointing hands or black vertical lines. Original ...................0 ..................July 17, 2013
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LIST OF EFFECTIVE PAGES SUBJECT
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LIST OF EFFECTIVE PAGES SUBJECT Appendix SSJ 100-A - CMA-9000 VNAV SUPERJET 100 Display Pages - Detailed Descriptions
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Appendix C - Navigation Displays
C-i C-ii C-1 C-2 C-3 C-4 C-5 C-6 C-7 C-8 C-9 C-10
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Appendix D - CMA-9000 FMS Display Pages Flow Diagrams
D-i D-ii D-1 D-2
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Appendix E - System Messages and Remote Annunciators
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Index
IND-1 IND-2 IND-3 IND-4 IND-5 IND-6
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RECORD OF REVISIONS ASSIGNED TO (JOB TITLE)
REV. NO.
REVISION DATE
0
July 17/13
INSERTION DATE
On receipt of revisions, insert pages and record date inserted and initial. LOCATION
BY
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REV. NO.
REVISION DATE
INSERTION DATE
BY
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PURPOSE OF OPERATOR'S MANUAL This Operator's Manual applies only to CMA-9000 Flight Management Systems (FMS) which incorporate the specific operational program(s) indicated on the cover page. This manual describes the capabilities, components, typical flight applications, and operating procedures for the CMA-9000 family of the Flight Management Systems (FMS). THIS MANUAL IS INTENDED TO BE A GENERIC MANUAL FOR ALL FMS APPLICATIONS. THE PROCEDURES DESCRIBED HEREIN INCLUDE ALL THE AVAILABLE DISPLAYS AND CONTROLS. When the CMA-9000 FMS is set up through the configuration procedures, as described in the installation manual, some of the features described herein may be disabled and not displayed. CAUTION THE INFORMATION CONTAINED IN NAVIGATION DATABASES IS NOT CERTIFIED BY A REGULATORY AUTHORITY; THEREFORE, THE USER IS ULTIMATELY RESPONSIBLE FOR ENSURING THAT DATA IS CORRECT PRIOR TO USE. ALL FMSs ARE CERTIFIED FOR IFR NAVIGATION UNDER THE CONDITION THAT ANY INFORMATION TAKEN FROM THE DATABASE BE VERIFIED AGAINST AN INDEPENDENT SOURCE PRIOR TO USE. IT IS ESSENTIAL THAT PILOTS COMPLY WITH THIS REQUIREMENT BY USING APPROACH, TERMINAL AND ENROUTE CHARTS TO CHECK FOR DISCREPANCIES IN FMS GENERATED NAVIGATION DATA. IF THERE ARE ANY DISCREPANCIES BETWEEN THE INFORMATION FROM THE FMS DATABASE AND THE OFFICIAL PUBLISHED HARD COPY, THE PILOTS MUST FOLLOW THE HARD COPY PROCEDURE, AND ADVISE THE FMS DATABASE SUPPLIER OF THE DISCREPANCY.
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OPERATIONAL APPROVAL AND LIMITATIONS OPERATIONAL APPROVAL Approval of the CMA-9000 FMS for VFR/IFR operation must be obtained from the Civil Aviation Authority of the country of registration of the aircraft. When operated with any of the external GPS equipment listed in Figure 5B Approved Installation Configurations with GPS Equipment of the Installation Flight Line Manual, the CMA-9000 FMS has been approved for VFR/IFR GPS supplemental navigation in en-route, terminal and non-precision approach. LIMITATIONS Limitations on the operation of the system and its particular installation, are outlined in the Airplane Flight Manual Supplement (AFMS). In particular the operational manual is affected by the way the equipment has been configured with respect to its installation. Instructions for installation and configuration are provided in the Installation Manual. It is expected that the installer takes into account the “Installation Considerations and Limitations” provided in Section 1.L. of the Installation Manual to plan the installation and operation of the aircraft and to obtain TC or STC approval.
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SECTION 1 - INTRODUCTION
CONTENTS Subject
Page
SYSTEM OVERVIEW ........................................................................................................................................1-1 COMPONENT DESCRIPTION ..........................................................................................................................1-2 A. Flight Management System (FMS) with Embedded Display Unit..........................................................1-2 B. External Global Positioning System (GPS) Receiver .............................................................................1-2 NAVIGATION MODES ......................................................................................................................................1-3 A. GPS..............................................................................................................................................................1-3 B. DME/DME ....................................................................................................................................................1-4 C. VOR/DME ....................................................................................................................................................1-4 D. Inertial .........................................................................................................................................................1-4 E. Dead Reckoning (DR) ................................................................................................................................1-4 WAYPOINT NAVIGATION ................................................................................................................................1-5 TERMINAL AREA OPERATIONS AND GPS INSTRUMENT APPROACHES................................................1-7 NAVIGATION DATABASE................................................................................................................................1-7 PHASES OF FLIGHT ........................................................................................................................................1-7 ACRONYMS AND ABBREVIATIONS ..............................................................................................................1-8
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SECTION 1 INTRODUCTION SYSTEM OVERVIEW The CMA-9000 Flight Management System (FMS) provides a complete Global Navigation System (GNS) and area navigation (RNAV) solution for world-wide four-dimensional aircraft navigation in the oceanic/remote, enroute, terminal and non-precision approach. It includes extensive flight management capabilities and a full range of navigation and flight planning features, together with simple route and flight plan creation and modification procedures. A world-wide subscription navigation database, stored in a non-volatile memory, provides the FMS with information on waypoints, navaids, airports, terminal area procedures, airways... In addition the database is capable of storing customer defined routes and waypoints. The CMA-9000 also integrates the functionality of Radio Management System (RMS) and Multi-Function Control Display Unit (MCDU) into a standalone, cockpit mounted enclosure. In dual/triple FMS installations, the synchronization is established automatically on power-up. Flight management capabilities include: • Multi-sensor navigation modes • Navigation performance monitoring and alerting • Flight planning • Standard Instrument Departure (SID) • Standard Terminal Arrival Routes (STAR) • Instrument approaches (RNAV, GPS, ILS, VOR, NDB, …) • LP/LPV approaches are supported when the FMS is used with the CMA-4024 GLSSU • Direct-to/intercept navigation, holding patterns, procedure turns, arcs and offset tracks • Lateral guidance along flight plan • Automatic waypoint sequencing, with and without turn anticipation • Navigation and communications radio tuning functions •
For some aircraft models: • Vertical flight planning and performance initialization • Performance predictions and vertical profile generation • Vertical guidance along computed profile
The FMS accepts data from the following navigation sensors, if installed: • Global Positioning System (GPS) • Distance Measuring Equipment (DME) • •
• • •
VHF Omni-directional Range (VOR) TACAN Inertial Reference System (IRS) Heading Source (AHRS) Air Data Computer
Information from these sensors is combined to determine aircraft position. This position is then used for navigating along a programmed flight plan created by selecting procedures/waypoints from the navigation database.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
COMPONENT DESCRIPTION A. Flight Management System (FMS) with Embedded Display Unit The CMA-9000 provides a color display of alphanumeric data. An alphanumeric keyboard allows data entry, data editing and system control of the flight management functions. The display is a sunlight readable color Active Matrix Liquid Crystal Display (AMLCD). Dedicated function keys and line select keys allow easy operator control of flight management functions. The keyboard panel is integrally lit from a panel light dimming bus. The front panel is illustrated in Section 2 along with an explanation of the keys and their function. For the control of the display brightness, two options are proposed. The first option consists in the combination of light sensors and manual brightness setting. Two light sensors on the FMS front panel sense any change in the cockpit ambient light level. This results in an increase or decrease in display brightness relative to a manual brightness setting. The second option consists in an external dimming bus. The Flight Management Unit (FMU) accepts data from external navigation sensors and performs all the signal processing and computations required to generate high performance navigation data. The FMU accepts operator’s commands from the alphanumeric keyboard, provides navigation, steering and status data on its own display and to the primary navigation flight displays. The FMU also provides suitably formatted outputs for the flight guidance system. B. External Global Positioning System (GPS) Receiver The external GPS Receiver receives signals transmitted by US DoD Global Positioning System satellites. It provides all the signal processing and computational capability required to determine aircraft position, velocity and time. The GPS sensor continuously monitors the integrity of the satellites using a SBAS satellite source (for TSO-C145a/C146 receivers) or an embedded high performance Receiver Autonomous Integrity Monitor (RAIM) (for TSO-C129a receivers).
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
NAVIGATION MODES The FMS follows a hierarchical navigation mode system using TSO-approved sensors characterized by the following decreasing priority order: Navigation modes
The FMS will use GPS data for navigation provided the GPS Horizontal Integrity Limit (HIL) meets the phase of flight requirement. Otherwise, the FMS will select the next best navigation mode meeting the TSO-C115b accuracy requirement (95% confidence factor) for the phase of flight, following the above priority order. This complies with TSO-C129a and TSO-C115b. The following navigation modes are supported: A. GPS GPS is the highest priority navigation mode of the FMS, and will be used when sufficient satellite coverage exists in the phases of flight for which it is approved. The GPS mode is selected for navigation by the FMS when the GPS receiver computes an Integrity value(HIL or HPL) which is less than the Required Accuracy or Error Limit for the current phase of flight being either approach, terminal or En-Route. The GPS receivers may derive the integrity(HPL) using SBAS uplink or will use RAIM (HIL) when there is no SBAS source available. GPS receivers approved for TSOC145/C146 are capable of using the SBAS signal. When the HIL or HPL exceeds the alert limit, or if the GPS loses its integrity capability, then: •
If GPS is the only sensor available for navigation: GPS will remain selected for navigation, but the GPS Integrity annunciator will illuminate and the “GPS POS UNCERTAIN” alert message will be displayed. If at any time GPS becomes unavailable for navigation, the FMS will revert to the Dead Reckoning (DR) mode of navigation, the GPS integrity annunciator will illuminate, and the “GPS NAV LOST” alert message will be displayed.
•
If additional sensors are available and approved for the phase of flight (DME/DME or VOR/DME): The FMS will continuously compute an ANP based on the difference of two positions (GPS and other sensor) and the accuracy of the other sensor. If this ANP exceeds the required accuracy, or if at any time the GPS sensor becomes unavailable for navigation, the FMS will revert to the next best IFR-approved navigation mode, the GPS Integrity annunciator will illuminate, and the “GPS NAV LOST” alert message will be displayed.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) B. DME/DME DME/DME is used in areas with sufficient DME and TACAN coverage, provided the appropriate navigation database is configured. In this mode the FMS automatically tunes the DME transceiver, acquiring distance information from up to six DME and TACAN (DME capable) ground stations. The DME distance is corrected for slant range error. Information on the DME facilities in use is displayed on the DME STATUS page, and individual stations can be inhibited from the navigation solution from the VHF NAV DESELECT page. C. VOR/DME VOR/DME navigation is used in areas with sparse DME coverage where there are less than three DME stations available. This mode combines co-located DME distance and VOR bearing to determine position. Tuned facility information is displayed on the VOR/DME STATUS page. Individual stations can be inhibited from the navigation solution from the VHF NAV DESELECT page. D. Inertial The FMS inertial navigation mode is based on the following parameters: • Present Position Latitude and Longitude; • North-South velocity; • East-West velocity. The FMS uses the raw Inertial position and velocities provided by the IRS. When the FMS is interfaced with 3 IRS, the resulting inertial navigation mode position will be a weighted average of the 3 IRS raw inertial positions. E. Dead Reckoning (DR) When the external sensor data inputs become insufficient to maintain the normal navigation modes, the FMS reverts to the dead reckoning mode of navigation. The FMS must then rely on the last known aircraft position, combined with heading and TAS inputs, and the last valid computed wind, for its aircraft position calculation. Prolonged DR operation will result in decreased position accuracy. Alerts are provided when the estimated position accuracy exceeds the requirements for each phase of flight. Refer to Section 12 for additional information on the various FMS navigation modes.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
WAYPOINT NAVIGATION The FMS navigates from waypoint to waypoint sequentially, automatically changing the legs, and displays all required navigation parameters, computed according to the relationships and direction sense illustrated in Figure 1-1. The FMS steering function anticipates the next leg prior to reaching the active waypoint so that the aircraft turns are smooth without any overshoot. Waypoints may be defined as either fly-by (with turn anticipation) or fly-over (no turn anticipation). For fly-over transition the aircraft is considered to have passed a given point when it has crossed the perpendicular to the desired track at that point (wayline). Thus, for leg sequencing to occur, the aircraft needs only to pass abeam the waypoint. For fly-by leg transition, leg switching, in most cases, occurs when the aircraft passes the bisector of the active leg and the next leg. After the last defined waypoint is overflown, or when a route discontinuity is active, the FMS will invalidate its roll steering to the autopilot/flight director (AP/FD) system, thus forcing the AP/FD to revert to a basic lateral mode. Angular inputs to the FMS may be referenced to either magnetic or true north. The input mode is installation dependent as defined in the Airplane Flight Manual Supplement. The reference used for the FMS angular displays and outputs to the flight instruments, can also be selected by the operator. NOTE: On certain installations only magnetic angular reference is supported, due to Display System limitations.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
NORTH
WIND DIRECTION (WD)
BEARING TO WAYPOINT (BRG)
WINDSPEED (WS)
A HE
DESIRED TRACK (DTK)
DRIFT ANGLE (DA) RIGHT
GROUND TRACK ANGLE (TK)
R HEADING AI (HDG) RUE T
SP
D EE
S) (TA
O GR
P DS UN
EE
D(
GS
S OS CR IND W
DW
D IN
ND WI E D E SP S) (W
TRACK ANGLE ERROR (TKE) LEFT
)
"TO" WAYPOINT
CROSS-TRACK DISTANCE (XTK) LEFT
INE S. SE L YPOINT A OUR E D C WE E N W IR S T DE E BE IRCL AT C GRE
0012033
Figure 1-1 Navigation Relationships
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
TERMINAL AREA OPERATIONS AND RNAV INSTRUMENT APPROACHES Standard Instrument Departures (SID), Airways, Standard Terminal Arrival Routes (STAR), STAR transitions, GPS and GPS overlay instrument approaches, and approach transitions, can be selected for the departure/arrival airports. These procedures may be modified on the LEGS pages. The implementation of the RNAV ( LPV, LNAV/VNAV and LNAV minima) instrument approach procedures is primarly based on TSO-C129a, TSO-C145a and TSO-C146.The transition from en-route through terminal to non-precision approach is effectively a seamless series of waypoints/legs with progressive increases in HSI lateral deviation display sensitivity (to reduce flight technical error), and reductions in Error Limit value for each phase of flight, and appropriately-timed alert or advisory messages
NAVIGATION DATABASE The navigation database includes most of the information that the operator would normally determine by referring to the navigation charts. The database may be tailored to specific customer needs and contains such data as en-route and terminal VHF, NDB navigation facilities, airports, waypoints, named intersections, and terminal area procedures. All ARINC 424 procedural legs are implemented. These leg types and their corresponding graphical representation are illustrated in Appendix B.
PHASES OF FLIGHT The phases of flight are defined as follows: Approach:
When below 15,000 feet AGL and within 2 nm of the FAF, with all GPS instrument approach conditions satisfied.
Terminal:
For arrivals, when below 15,000 feet AGL and within 30 nm radial distance of the arrival airport, but not in approach phase of flight. For departures, when below 16,000 feet AGL and less than 33 nm radial distance from the departure airport.
En-route:
When in neither approach nor terminal phases of flight.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
ACRONYMS AND ABBREVIATIONS A AA AAIM AAR AC ACARS ACCUR ACID ACT ACMS ACQ ADC ADF ADIRS ADS ADx AF AFCS AFMS AFN AG AGC AGL AHRS ALT AMLCD ANP ANT AOC AP/FD APPR APU ARC ARINC ARPT ARR ATA ATC ATK ATT ATS
-
Above (altitude) Air-To-Air Aircraft Autonomous Integrity Monitoring Air-To-Air Refuelling Aircraft Aircraft Communications Addressing and Reporting System Accuracy Aircraft Identifier Active Aircraft Conditioning Monitoring System Acquisition mode Air Data Computer Automatic Direction Finder Air Data Inertial Reference System Automatic Dependent Surveillance Primary (AD1) or Secondary (AD2) ADF radio Initial Approach Fix Automatic Flight Control System Airplane Flight Manual Supplement ATS Facilities Notification Air-To-Ground Automatic Gain Control Above Ground Level Attitude Heading Reference System Altitude Active Matrix Liquid Crystal Display Actual Navigation Performance Antenna Airline Operational Communications Autopilot/Flight Director Approach Auxiliary Power Unit Arc to Fix/Radius to Fix Aeronautical Radio Incorporated Airport Arrival Actual Time of Arrival Air Traffic Control Along Track Distance Attitude Air Traffic Services
BARO BRT BRG BW
-
Barometric Brightness Bearing Back Course Marker
Cx CAP CARP
-
COM radio (primary : C1, secondary : C2) Capable Calculated Air Release Point
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) CDI CDU CF CFG CHK CLR CMx CMA CMD CMU COM COMMS CON CONC COORD CPDLC CPS CRP CRS CRZ CTR
-
Course Deviation Indicator Control Display Unit Final Approach Course to fix Configuration Checker Clear Primary (CM1) or Secondary (CM2) COM radio Canadian Marconi (Avionics) Command Communications Management Unit Communication Communication Radios Connection Concentrator Coordinates Controller Pilot Datalink Communication Compass Computed Air Release Point Course (desired track) of route leg or to waypoint Cruise Center
DA DEL DEP DES DESEL DEST DF DGNSS DIFF DISCON DIS DIST DLU DME DOD DOP DR DTG DTK DTO DTRA DTW
-
Drift Angle Delete Departure Destination Deselected Destination Direct To Fix Differential Global Navigation Satellite System Differential Route Discontinuity Distance Distance Data Loader Unit Distance Measurement Equipment Department Of Defense Dilution of Precision Dead Reckoning Distance To Go Desired Track Direct To Transition Distance Distance To Waypoint
E E/W EDT EFA EFIS EHE EHSI ENRT EQUIP ESC
-
East East/West Edit Estimated Fuel at Arrival Electronic Flight Instrumentation System Estimated Horizontal Error Electronic Horizontal Situation Indicator En-Route Equipment Escape Point
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) EST ESS ETA ETE EW EXEC
-
Estimated External Sub-System Estimated Time of Arrival Estimated Time Enroute Electronic Warfare Execute
FAF FDE FF FFK FIR FL FLT FMS FMU F/O FOM FPU FR FREQ FSD FT FTE
-
Final Approach Fix Failure Detection and Exclusion Final Approach Fix Front panel Function Key Flight Information Region Flight Level Flight Flight Management System Flight Management Unit First Officer Figure of Merit Floating Point Unit From Frequency Full Scale Deflection Feet Flight Technical Error
Guard Geometric Dilution of Precision GLONASS Global Navigation Satellite System (Russian) Greenwich Mean Time Global Navigation System Global Navigation System Sensor Unit GPS Position Integrity Alert Limit Global Positioning System Ground Speed Global Navigation System Sensor Module Gross Weight
/H HARP HAT HDG HDOP HF HFOM HIL HOR HR HSI HT HW HYB
-
Holding Pattern High Altitude Release Point Height Above Terrain Heading Horizontal Dilution of Precision High Frequency Horizontal Figure Of Merit Horizontal Integrity Limit Horizontal Hour Horizontal Situation Indicator Height Hardware Hybrid
IAF IAS
-
Initial Approach Fix Indicated Airspeed
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) IC ICAO ID IDENT IDT IF IFR in Hg ILS IM INBD INACT INIT INT INTC INS IP IRS ITU
-
Intercom International Civil Aviation Organization Identifier Identifier Identifier Intermediate Fix Instrument Flight Rules Inches of Mercury Instrument Landing System Innner Marker Inbound Inactive Initialize Integrity Intercept Course Inertial Navigation System Identification Point Inertial Reference System Telecommunication Union
KG KT
-
Kilogram Knot(s)
L LAT LB LDA LDR LIB LNAV LOC LOCB LONG LP LPV LRU LSK LVL
-
Left Latitude or Lateral Pound Landing distance available Light Detect Resistor Library Lateral Navigation mode of the autopilot/flight director system Localizer Localizer Backcourse approach Longitude Localizer Precision approach Localizer Precision with Vertical guidance approach Line Replaceable Unit Line Select Key Level
M MA MAG MAGVAR MAHP MAINT MAP MB MC MCDU MDA MDA-DA MEW MGRS MHz MID
-
Meter Missed Approach Point when not RW Magnetic Magnetic Variation Missed Approach Holding Point Maintenance Missed Approach Point Millibars (hectopascal) Mission Computer Multipurpose Control and Display Unit Minimum Descent Altitude Minimum Descent Altitude-Decision Altitude Mean Effective Wind Military Grid Reference System Mega Hertz Maritime Identification Digits
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) MIN MLS MM MOD MRK MSG MSLA MTBF
-
Minute Microwave Landing System Middle Marker Modified Mark Message Mean Sea Level Altitude Mean Time Between Failures
N Nx NAV NDB NDBD NM NOTAMS NP NPA NVx NVM VNAV NVIS
-
North NAV radio (primary : N1, secondary : N2) Navigation or Navaid Non-directional Beacon NDB approach with DME facility (GPS or NDB/(DME)) Nautical Mile Notices To Airmen Navigation Performance Non-Precision Approach Primary (NV1) or secondary (NV2) NAV radio Non-Volatile Memory Vertical Navigation Night Vision Imaging System
/O OAT OFST OM OP ORIG
-
Overfly Waypoint Outside Air Temperature Offset Outer Marker Operations (independent/synchronized) Origin
Place/Bearing/Distance Place/Bearing-Place/Bearing Position Estimation Error Performance Page Programmable Interrupt Timer Phase of Flight Position Present Aircraft Position Predefined Previous Pseudo Range Number Progress Procedure Turn Power
QFE QNH
-
Field Elevation Pressure Sea Level Pressure
/R R RAD RADALT RAIM RALT
-
Radial-To Right Radial Radar Altitude Receiver Autonomous Integrity Monitor Radio Altimeter
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Remote Control Unit Receive only Flight Recorder Reference Relative Reserve Reselect Radio Frequency Radio Interface Board Radio Management System Required Navigation Range Required Navigation Performance Required Time of Arrival Real Time Clock Route Runway Threshold
/S S/W S SAR SAT SATCOM SD SDF SEL SID SMS SP SPD SQK SSM SSR STAR STAT STBY STC STS SURF SYNC
-
Search Pattern Software South Search and Rescue Satellite Satellite Communication System Slowdown Point Simplified Directional Facility Selected Standard Instrument Departure Short Message Service Space Speed Squawk Sign Status Matrix Secondary Surveillance Radar Standard Terminal Arrival Routes Status Standby Supplemental Type Certificate Status Surface Synchronization
/T T TACAN TACT TAS TCN TD TE TEL TEMP TERM TF TGL
-
Tactical Direct-To Angle referenced to True North Tactical Air Navigation Tactical True Air Speed TACAN Touchdown Fix when not RW Trailing Edge Telephone Temperature Terminal Track To Fix Temporary Guidance Leaflet
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) TK TKE TOGA TP TPDR TR TRANS TRK TRG TSE TSO TTFF TTG TTS TX1 TX2
-
Track (Actual) Track Angle Error Take-Off/Go-Around Turn Point Transponder Transmit/Receive Transition Track Transmit on Guard Total System Error Technical Standard Order Time To First Fix Time To Go Time To Station V/UHF1 Transmitting V/UHF2 Transmitting
UF UHF UTC UTM
-
UHF radio Ultra High Frequency Universal Time Coordinates Universal Transverse Mercator
V VAL VDOP VECT VERT VFOM VFR VHF VNAV VUHF VIR VIS VOR VORD
-
Velocity (VX, VY, VZ) Value Vertical Dilution of Precision Vector Vertical Vertical Figure Of Merit Visual Flight Rules Very High (30-300 MHz) Frequency Vertical Navigation Very Ultra High Frequency VOR ILS Receiver Visible VHF Omni-directional Radio Range VOR/DME approach (GPS or VOR/DME)
W WD WPT WS WT WGS WGT WXR
-
West Wind Direction Waypoint Windspeed Weight World Geodetic System Weight Weather Radar
XFILL XPDR XMT XTE XTK
-
Cross FMS Fill Transponder Transmit Extended Trailing Edge Point Cross Track
Z
-
Zulu (UTC) time
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SECTION 2 - CONTROL AND DISPLAY
CONTENTS Subject
Page
GENERAL .......................................................................................................................................................2-1 FMCDU FRONT PANEL .................................................................................................................................2-1 GENERAL DISPLAY CONVENTIONS .........................................................................................................2-12 Standard Colour Convention......................................................................................................................2-13 Airbus Colour Convention ..........................................................................................................................2-14 Font Size .......................................................................................................................................................2-15 Special Symbols ..........................................................................................................................................2-15 SCRATCHPAD MESSAGES ........................................................................................................................2-17 WAYPOINT NAMES AND OTHER CONVENTIONS ...................................................................................2-19
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
This Page Intentionally Left Blank
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SECTION 2 CONTROL AND DISPLAY
GENERAL The CMA-9000 FMS is a Flight Management Computer (FMC) embedded within a Multipurpose Control Display Unit (MCDU), thus becoming an FMCDU. The MCDU function can be interfaced with up to seven other ARINC739 capable LRUs (ACARS, SATCOM, ACMS, etc.). The unit’s front panel presents a full alphanumeric keyboard, with special function keys. These special function keys are mostly dedicated to FMS operations (e.g. INIT/REF, RTE, DEP/ARR, etc.). There are six line select keys (LSK) on each side of the display area. The functions of the LSKs are specific to each screen page.
FMCDU FRONT PANEL A typical front panel arrangement of the FMCDU is illustrated in Figure 2-1 on next page. The display screen is approximately 3 x 4 inch colour Active Matrix Liquid Crystal Display (AMLCD) providing fourteen lines of twentyfour characters. The page format is divided in four areas: page title, left side, right side, and scratchpad.
Page Title:
This area is the top line of the display (line 1 of 14). It identifies the page in view and indicates how many pages of the same set are available.
Left Side:
This area is comprised of six pair of lines, up to twelve characters per line. A line pair comprises a field title line and a data line. The operator has access to the data line of each pair through a Line Select Key aligned on the left side. This area extends from the left side of the screen to the center.
Right Side:
This area is similar to the Left Side area. The operator has access to the data line of each pair through a Line Select Key aligned on the right side. This area extends from the right side of the screen to the center. On some pages a field is placed in the middle of a line. For these fields the user cannot enter or delete data through the line select keys. Scratchpad: This area is the bottom line of the display (line 14 of 14). Typed characters and FMS-generated messages are displayed on this line.
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Page 2-1 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
Figure 2-1 CMA-9000 FMS Front Panel, Hardware variation 045
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Page 2-2 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
Figure 2-2 FMS Front Panel, Hardware variation 445
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
VAR 060
VAR 460
Figure 2-3 Front Panel, Hardware variation 060/460
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
VAR 070
VAR 470/471
Figure 2-4 Front Panel, Hardware variation 070/470/471
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Page 2-5 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
Figure 2-5 Front Panel, Hardware variation 050
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Page 2-6 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
The item numbers 1 to 33 below refer to the front panel elements of Figure 2-1 and subsequent figures. Display Screen (Item 1): Provides 14 lines of 24 characters: • Line 1 displays the page title and page number; • Lines 2 to 13 are used for data display; • Line 14 (scratchpad) is for user data entry, and system display of alert/advisory messages. Alphanumeric Keyboard (Item 28) These keys allow typing alphanumeric characters into the scratchpad successively from left to right. Line Select Keys (LSK) (Item 10) There are twelve LSKs on the front panel, six on either side of the display, aligned with their corresponding data field. LSKs are identified by their location from top to bottom of the screen and as left or right (LSK1L, LSK2L, …LSK6R). Depending of the context of a given page, pressing a line select key may: • display a new page, • enter data from the scratchpad into the selected field, • copy data from the selected field to the scratchpad. Data Entry from Scratchpad Data entries are permitted only on lines adjacent to the LSKs. Entry of data from the scratchpad into the selected field is accomplished by pressing the adjacent LSK which moves the data from the scratchpad to the selected field. This action clears the scratchpad, unless an entry format error is made. Data Copy to Scratchpad When the scratchpad is empty, data can also be copied from a data field to the scratchpad by pressing the LSK adjacent to the desired data line. Slash (/) Key (Item 26) The slash key " / " is used to separate two items of data entered in the same data field (LSK) (such as wind direction and speed): • If a single entry is made without being preceded or followed by a slash, it will be entered into the field adjacent to the LSK (field closest to the edge of the screen). • Entering data into the field closest to the center of the screen always requires typing of a slash. Cancellation of Waypoint Attribute (/H, /O) – Some waypoints are displayed on the LEGS page with an attribute appended to the right of the identifier: • waypoint followed by a holding pattern (/H), • waypoint marked as a mandatory fly-over (/O), This waypoint attribute is identified using the slash symbol followed by a single letter. The attribute can be cancelled using the slash key alone without a letter and the appropriate LSK. NOTE:
Cancellation of the attribute does not delete the waypoint itself.
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Page 2-7 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) SP Key (Item 24) This key allows typing a blank space into the scratchpad. Plus-Minus [+/-] Key (Item 25) This key allows typing a "+" (plus) or "-" (minus) sign into the scratchpad. Pressing this key will first display a "-" (minus) sign in the scratchpad. Pressing it a second time will replace the minus sign with a "+" (plus) sign. Decimal (.) Key (Item 27) This key allows typing a decimal point into the scratchpad, for numeric data entries. CLR Key (Item 15) The CLR key is used to clear messages and data from the scratchpad or an individual data field. Clearing Data from Scratchpad One press clears the last entered character from the scratchpad. When pressed and held for more than 1 second, it clears the entire scratchpad. Acknowledging Alert and Advisory Messages The CLR key also acknowledges alert and advisory messages and clears them from the scratchpad. Delete Data from an Entry Field To delete an entry already made in a given data field: •
Pressing the CLR key with the scratchpad empty will display DELETE in the scratchpad.
•
This DELETE message can be cleared by another press of the CLR key if the latter was inadvertently pressed.
•
The deletion process is completed by pressing the LSK next to the data to be deleted.
Function Keys (qty 10) (Items 14, 16-23 & 33) Function keys are used for single-key access to certain FMS pages. The first row of function keys (INIT/REF, RTE, DEP/ARR, LEGS, PROG) is common to all hardware variations of the unit. •
INIT REF - provides access to pre-flight initialization pages and various reference data pages. NOTE : If the key is pressed for more than 1 second, the MESSAGE RECALL page will be displayed.
•
RTE - provides access to the ROUTE page for the definition of routes.
•
DEP ARR - provides access to the DEP/ARR page for the selection of departure and arrival procedures and runways.
•
LEGS - provides access to the LEGS pages containing detailed data concerning each leg of the route.
•
PROG - provides access to the PROGRESS pages for display of current flight and navigation status information.
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Page 2-8 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) For the second row, various variations of the unit support different combinations of function key labelling (see Figure 2-1 to 2-5 above, and Table 2-1 below). A given combination is selected by the operator depending of the type of operations of this aircraft. •
MSG - provides access to the MESSAGE RECALL page for display of System Alert messages.
•
HOLD - if no holding pattern exists in the route, brings LEGS page in view with “/H” in the scratchpad for line selection of the desired holding fix waypoint. If a holding pattern already exists in the route, accesses the HOLD page for the definition of holding pattern parameters at the designated waypoint or present position.
•
VNAV – o provides access to the VNAV Approach page when advisory (uncoupled) approach VNAV is enabled (see section 7). o provides access to the vertical navigation page associated to the current phase-of-flight when Performance VNAV is enabled (see section 18).
•
FMC COMM - provides access to company datalink (Airline Operational Communications) related pages.
•
RADIO - provides access to RADIO tuning functions.
•
ATC - provides access to ATC datalink related pages, or provides access to ATC Transponder control and display pages NOTE: On a given installation, the ATC key can be used only for one of these two purposes. If transponder control and display is required on an installation where ATC Datalink is also enabled, access to the transponder control pages is via the RADIO page.
•
FIX - provides access to FIX page for all fix and abeam waypoint functions.
•
TACT - provides access to tactical functions (not for airlines operations). See Section 11.
Front Panel Variation 045/445 050 060/460 070/470/471
Item 22
Item 20
Item 33
Item 17
Item 14
RADIO RADIO ATC RADIO
FMC COMM TACT FMC COMM ATC
VNAV VNAV VNAV VNAV
HOLD HOLD HOLD HOLD
FIX ATC FIX MSG
Table 2-1 Configurable Key layout per Front Panel Variation NEXT Key (Item 29) When multiple-page of a given set exist (as indicated in the page title line), pressing the NEXT key advances the display to the next page number, or wraps around to page 1 if presently on the last page. NOTE:
If the NEXT functionality is configured, additional press of the INIT/REF, RTE, DEP/ARR, LEGS, PROG, FREQ, FUEL and HOLD keys allow the access to the next page, as per the NEXT key.
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Page 2-9 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
PREV Key (Item 30) When multiple-page of a given set exist (as indicated in the page title line), pressing the PREV key moves backs the display to the previous page number, or wraps around to the last page if presently on page 1. EXEC Annunciator (Item 11) Illuminates when the active route is being edited. A modified (temporary) route is thus being created to allow editing and reviewing without affecting the current guidance being performed with the active route. When the EXEC annunciator is lit, all flight planning pages display: • MOD in reverse video in the column 2 of the title line, and • the ERASE prompt in field LSK6L o Pressing the ERASE prompt LSK erases all modifications and restores the display of the active route. Even if a modified route exists, the FMS continues to use the (unmodified) active route for navigation and guidance. EXEC Key (Item 12) Allows crew to accept modifications to the active route. When data entries have been made active (by pressing the EXEC key), the title MOD status will revert to ACT (active). Any modification can be erased (cancelled) prior to EXECution by pressing the ERASE prompt (LSK6L). System Annunciators (Items 2-8) Various hardware variations of the unit support different annunciator labelling. Conditions for illumination vary with hardware variation and software configuration options. Front Panel Variation 045/445 050 060/460 070/470/471
Item 2
Item 3
Item 4
Item 5
Item 6
Item 7
Item 8
FAIL FAIL FAIL FAIL
MSG MSG MSG MSG
RNP RNP RNP RNP
OFST OFST OFST OFST
IND IND IND IND
None None None None
ATC ATC ATC ATC
Table 2-2 Annnunciator layout per Front Panel Variation FAIL (Item 2) -
illuminates at maximum brightness with the display blank upon detection of a major unit failure (e.g. system is halted).
MSG (Item 3) - illuminates when a new alert message appears in the scratchpad. The annunciator stays lit as long as the condition causing the alert message remains, or until the message is acknowledged by pressing the CLR key, or until the message is viewed on the MESSAGE RECALL page. RNP (Item 4) -
illuminates when the FMS ANP exceeds the RNP.
POS (Item 4) -
illuminates when the FMS is in dead reckoning navigation mode.
OFST (Item 5) - illuminates during offset (parallel track) navigation IND (Item 6) -
illuminates when the FMS operates on INDEPENDENT mode.
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Page 2-10 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
BRT Key (Item 13) Controls the brightness of the screen and annunciators. After an elapsed time of 5 seconds, the first press of this key will always increase brightness, each depression of the BRT key alternately brightens or dims the display. NOTE1: When night and NVG mode selected and short power interruption occurs, the brightness of the display may require minor re-adjustments. NOTE2: When external dimming control is selected in the configuration, the brightness of the screen and annunciators can also be controlled by an external system providing a 0-5 VDC to the FMS. LDR Sensor (Item 9) Detects ambient light conditions in order to perform auto-brightness control of display screen and annunciators. MENU Key (Item 31) Provides access to the MCDU MENU 1/2 page, which allows access to other subsystems connected to the MCDU (e.g. ACARS, SATCOM, …). This key relates only to the ARINC 739 MCDU capabilities of the CMA9000. MENU Annunciator (Item 32) Illuminates when a sub-system, other than the one currently displaying pages, is requesting crew attention. • •
For example, if any of the installed subsystems that uses the FMCDU as control head (e.g. CMU, IFDMU, SATCOM, ACMS, DFDAU) is requesting crew attention while the MCDU function is connected to the FMS, the MENU light will be turned on. Conversely, if the MCDU function is connected to any of the above mentioned sub-systems and the FMS is requesting attention, the MENU annunciator will equally be turned on.
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Page 2-11 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
GENERAL DISPLAY CONVENTIONS
A typical screen page is illustrated below as an aid in describing the various page layouts, page prompts, and data entry rules.
ACT,MOD STATUS FIELD [CYAN] [LARGE]
MOD BOX DATA FIELD [GREEN] [LARGE]
PAGE NUMBER AND NUMBER OF PAGES [CYAN] [LARGE]
PAGE TITLE [CYAN] [LARGE]
RTE1 LEGS
299o
CAFTA
1/2 2.25N M
A
THEN
COMPUTED AND RECEIVED DATA [WHITE] [SMALL]
-- ROUTE DISCONTINUITY -
YZP01 299o DASH DATA FIELD [GREEN] [LARGE]
ERASE PROMPT [GREEN] [LARGE]
10.6N M
YZP02 ----
SCRATCHPAD [WHITE] [LARGE]
DATA FIELD UNIT [WHITE] [SMALL]
LEGS ETA>
PAGE PROMPT [BLUE [LARGE]
MESSAGES DISPLAYED IN THE SCRATCHPAD [AMBER] [LARGE]
Figure 2-6 Basic Display Format Page Title -
displayed in cyan on the top line of the screen.
Page Number -
when a display consists of several pages (as indicated in the upper right of the page), the additional pages may be displayed by pressing the NEXT or PREV keys. When the NEXT key configuration option is selected, the Front-panel Function Keys (FFKs) (elements 14 to 23 on Figure 2-1) can be used as a NEXT key as well.
Page Prompt -
pressing the LSK adjacent to a page prompt will bring in view the associated page.
Scratchpad -
This area is the bottom line of the display (line 14 of 14).
•
Keyboard entries are displayed in white large font in the scratchpad and then moved to the data field by pressing the appropriate Line Select Key (LSK). Error checking for invalid format or data type, or out of range values, is performed when the LSK is pressed.
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Page 2-12 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) •
Copying data from a data field into the scratchpad is accomplished by pressing the appropriate LSK when the scratchpad is empty. Data in the scratchpad remains there when a new page is selected, and can thus be carried over for entry into other pages.
Standard Colour Convention The colour convention used on the FMS pages is configurable in order to better blend with a given cockpit environment. The standard colour convention is as follows:
Figure 2-7 Standard Colour Convention Green
Fixed data fields, field titles and waypoint names (on LEGS page).
White
Computed (dynamic) data, data units, scratchpad data, data entry error, and advisory/maintenance messages.
Cyan
Page titles, page browsing prompts and inactive route related information.
Magenta
Depending on configuration, used in normal video, or reverse video, to identify the active waypoint on ACT RTE LEGS 1/X, and PROGRESS pages.
Amber
Used to display cautions and warnings, including alert conditions requesting immediate crew attention or action (e.g. alert scratchpad messages).
Red
Reserved for maintenance purposes only. Major change (e.g. confirmation of system reconfiguration).
Reverse Video Text can also be displayed in reverse video: Green
Temporary states prompting crew attention (such as CONFIRM and CANCEL). Navigation and guidance actions (e.g. missed approach initiation, manual waypoint sequence, hold exit initiation).
White
Pending active waypoint sequencing; activated mode/function; temperature compensated altitudes; waypoint attribute designators (e.g.: FAF, MAP).
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Page 2-13 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Cyan
Used for certain status advisories, such as modified route in title line.
Magenta
Depending on configuration, used in normal video, or reverse video, to identify the active waypoint on ACT RTE LEGS 1/X, and PROGRESS pages.
Amber
Unachievable temperature compensated altitudes constraints.
Red
Not used
Temperature Compensation All temperature compensated altitude constraints are displayed in reverse video. Thus altitude constraints can be displayed in reverse Green (constraints), or Amber (broken altitude constraints).
Airbus Colour Convention The Airbus colour convention diverts from the standard configuration as follows: •
the active waypoint is displayed in reverse video green on the LEGS/PROGRESS pages,
•
downpath waypoints are displayed in white on the LEGS/PROGRESS pages,
•
altitude, speed, and time constraints are displayed in magenta,
•
On LEGS pages, text in the title lines is displayed in green.
Figure 2-8 Airbus Colour Convention
NOTE:
In this document, the page examples will follow the standard convention. For page examples using the Airbus A300/310 standard, refer to section 18A Performance VNAV for A300/310 and appendix A300-A CMA-9000 VNAV A300/310 Display Pages – Detailed Descriptions.
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Page 2-14 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Font Size There are 2 types of fonts, small and large, on the pages. Each font supports upper and lower case alpha characters. Lower case alpha characters are used only for the display of units and unit acronyms. The data fields (line adjacent to LSK) are displayed in: • •
Large Small
Manual entries. Computed or system generated data.
Data on the field title line (above the data line) are displayed in small font. The page title line is displayed in large font.
Special Symbols The following special symbols are used to convey their respective meaning: Dash Data Field (-----) Box Data Field (
Optional data entry. ) Mandatory data entry.
Blank Fields
Data cannot be computed.
Triangle (>) Pointing inward
Toggle prompt or command prompt
Pointing outwards Page access prompt
Asterisk Fields (****)
Data exceeds the maximum value for that field, or the external source of data is failed.
Leading Zeros
Only required during data entry for: • angular data (bearing, course, wind direction, etc.) • latitude/longitude coordinates • runway identifiers
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Page 2-15 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
Summary of conventions:
Page Title Active waypoint
Display Elements
Font Large Large
Page prompt (with outward triangle) Legs page waypoint
Large Large
Fix caption Units Tuning in progress Active waypoint being sequenced (fly-by transition) Entered data Computed data Temporary states pilot attention requested Toggle option (with inward triangle) Command prompt (with inward triangle)
Small Small Large Large Large Small Large Large Large
This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.
Color Cyan Reverse video magenta Reverse video green (Airbus) Cyan Green White (Airbus) Green White Reverse video white Reverse video white White White Reverse video green Green triangle with White text Green triangle with Green text
Page 2-16 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SCRATCHPAD MESSAGES
The FMS can generate the following types of system messages: System Alerts
Require immediate pilot action or attention. Example:
Data Entry Advisories
Indicate that the user-entered data is incorrect. Example:
Status Advisories
Do not require immediate pilot action but require pilot awareness. Example:
Maintenance Advisories
Do not require immediate pilot action but indicate a particular external input failure condition. Example:
Maintenance Alerts
Indicate a particular FMCDU internal failure condition. Such messages never displayed in scratchpad.
Refer to Appendix E of this manual for additional information and the complete list of messages. Alert Messages A. System Alerts •
• • • •
Indicate: • a required pilot action, • a loss of functionality • or a degraded mode of operations. Displayed in amber in the scratchpad until acknowledged. Cause both the FMS front panel MSG annunciator and the remote MSG annunciator to illuminate until all new messages are cleared/acknowledged by the pilot. Displayed in amber in the MESSAGE RECALL page. Highest priority scratchpad messages: • cannot be typed over or overwritten by any other message type or data entry; • must be acknowledged by pressing the CLR key before data entry can take place.
B. Maintenance Alerts • • •
Indicate an internal FMCDU failure condition. Never displayed in the scratchpad as they are covered by the generic FMS FAILED (system alert) collector message. Displayed in amber on the MAINT MESSAGES page.
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Page 2-17 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Advisory Messages C. Data Entry Advisories • • • • • •
Immediate system response to data entries performed by the crew. Notifiy the crew that the entered data is incorrect. Identified in the scratchpad by a leading exclamation mark "!". Displayed in white in the scratchpad (until acknowledged) Never displayed on the MESSAGE RECALL or MAINT MESSAGES page Can be typed over and overwritten by system alerts only
D. Status Advisories • • • •
Do not require immediate pilot action but require pilot awareness Displayed in white in the scratchpad (until acknowledged). Never displayed on the MESSAGE RECALL or MAINT MESSAGES page. Second lowest scratchpad priority (can be typed over and overwritten by any message type except maintenance advisories).
E. Maintenance Advisories • Do not require immediate pilot action but indicate a particular external input failure condition, typically a loss of redundancy without loss of capability (e.g. DME 1 FAILED). • Displayed in white in the scratchpad unless an associated (system alert) collector message is active. • Displayed in white on the MAINT MESSAGES page, regardless of the presence of an associated (system alert) collector message. • Lowest priority scratchpad messages (can be typed over and overwritten by any other message type).
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Page 2-18 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
WAYPOINT NAMES AND OTHER CONVENTIONS Terminal Area Waypoints - where specific identifiers have not been assigned, the following two-character prefix codes are added to the runway identifier (number) to create terminal area and approach-related waypoints in the navigation database: AF CF FF IF MA SD RW OM MM IM BM TD
-
Initial Approach Fix Final Approach Course Fix Final Approach Fix Intermediate Fix Missed Approach Point when not RW Step-down Fix Runway Threshold Outer Marker Middle Marker Inner Marker Back Course Marker Touchdown Fix when not RW
Unnamed Turnpoints and Intersections - where no name has been assigned to a turnpoint or intersection, the waypoint name in the navigation database is created by adding the distance of the point from the nearest applicable navigation facility to the facility identifier, e.g. SEA77. Temporary Waypoints - place/bearing/distance (PBD), place/bearing-place/bearing (PBPB) and along track waypoints are automatically named by adding a sequence number to the first three characters of the reference waypoint, e.g. ANC01. Similarly, the names of waypoints entered in latitude/longitude are created by adding a sequence number to the prefix WPT. Alternatively, depending of configuration option, waypoints entered in latitude/longitude can be automatically named per the entered coordinates (e.g. N45W123). DME ARC Waypoints - the waypoint name in the navigation database is created by adding the radial from the DME station in degrees followed by the radius of the arc in nautical miles (represented by a letter: A = 1 nm, B = 2 nm, J = 10 nm, etc) to the prefix D, e.g. D173J. Conditional Waypoints - a conditional waypoint is used in the navigation database when a route leg does not terminate at a defined latitude and longitude. Such legs include radar vectors, intercepts, and course or heading legs, or a leg with a manual or an altitude termination. Conditional waypoint names are displayed in parentheses as shown below. Conditional waypoints cannot be used for direct-to navigation, nor as references for temporary waypoint creation, and cannot be copied into the scratchpad. (INTC)
-
Leg terminates at the interception of the next leg.
(3000)
-
Leg terminates automatically when climbing through the displayed altitude.
(VECT)
-
Leg is a radar vector. Operator action is required to sequence to the next leg.
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Page 2-19 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
Course Legends - courses may be displayed with the following legends depending on the leg type, as listed below: CRS
-
Indicates a course leg inbound to the next waypoint
FR FIX
-
Indicates a course outbound from the FIX
HDG
-
Indicates a heading leg
HOLD AT -
Replaces the active waypoint course on RTE LEGS 1/X and PROGRESS 1/4 pages when navigating a holding pattern
P-T
Appended to the courses of the outbound legs of the procedure turn
-
Course Prefixes - the required turn direction (L or R) is added as a prefix to the displayed course, and is most commonly used at the inbound turn of a procedure turn and in missed approaches.
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Page 2-20 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SECTION 3 - PREFLIGHT
CONTENTS Subject
Page
SECTION 3 - PREFLIGHT.........................................................................................................................................3-i CONDENSED PREFLIGHT PROCESS..........................................................................................................3-1 PREFLIGHT.....................................................................................................................................................3-2 START-UP AND INITIALIZATION..................................................................................................................3-3 ACTIVE DATABASE SELECTION.................................................................................................................3-4 FMS DISPLAY SETUP....................................................................................................................................3-5 SYSTEM POSITION, DATE AND TIME UPDATE..........................................................................................3-6 ANGULAR REFERENCES FOR NAVIGATION AND DISPLAY (POLAR AREA DEFINITION) ................3-7 ACTIVE ROUTE SELECTION USING THE COMPANY ROUTE NAME.......................................................3-8 ROUTE SELECTION FROM THE LIST OF COMPANY ROUTES ................................................................3-9 BUILDING A ROUTE BY WAYPOINT INSERTION .....................................................................................3-10 BUILDING A ROUTE BY AIRWAY INSERTION..........................................................................................3-11 VERIFYING ACTIVE ROUTE LEGS BY COURSE AND DISTANCE..........................................................3-12 INITIAL LEG ..................................................................................................................................................3-13 CANCELLING ANY PROCEDURE OR ROUTE MODIFICATION...............................................................3-13 ROUTE 2 OPTION ........................................................................................................................................3-13 ROUTES 2 & 3 OPTION ...............................................................................................................................3-17 ACCESSING INIT/REF INDEX PAGES........................................................................................................3-24 CRUISE PERFORMANCE PARAMETERS INITIALIZATION (if configured) ............................................3-25 FUEL PERFORMANCE PARAMETERS INITIALIZATION (if configured) ................................................3-26 FUEL AND WEIGHT PERFORMANCE PARAMETERS INITIALIZATION (if configured) ........................3-26 GPS SATELLITE DESELECTION (If configured).......................................................................................3-28 DUAL/TRIPLE FMS OPERATIONS .............................................................................................................3-28 SYNCHRONIZED OPERATIONS .................................................................................................................3-29 INDEPENDENT OPERATIONS ....................................................................................................................3-30 RADIO TUNING OPERATIONS – DUAL/TRIPLE FMS or FMS and RADIO HEAD ..................................3-30 EMBEDDED CALCULATOR/CONVERSION TOOL (if configured) ..........................................................3-30
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Page 3-i July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
This Page Intentionally Left Blank
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Page 3-ii July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SECTION 3 PREFLIGHT CONDENSED PREFLIGHT PROCESS This page sequence gives an overview of the Preflight operations of the FMS. The intent of each step is summarized on the next page.
FMS1 IDENT
1/2
NAV DATABASE ACTIVE K L M W W 0 6 9 7 OCT10-NOV06/03 S E C O N1/3 D POS INIT/REF -DEC04/96 K L MFWMWS0 6P9O7S NOV07 DR O P P R ON47 G R Ao26.28 M C F G o18.67 NO W122 ACT RTE 1 6 1 4R0E0F0 -W0A0Y5P O I N T 0 0 7 71/3 7 CKUBFI SOTROIMNG4ID7NAo 3 T1 A. B8 A0 SW E 1 2 2 oD1A8TD.EE0S0T E C -MKSEA ROTDEES T M A R 2 1 / 0PANC 2 UACT NDWAATYARTE O USSTA ERRNDBY B A S E1 LEGS DFALTTE N1/2 KL007 E C --U---D2T6E4SoT S E TM AIRN12S21./P80ON2SM CO ROUTE JOH /H
. . o 1D 1A 3T NE M 1/1 U T C2 6 2 FMS1 SETUP 280/1600A :04z OCT20/99 175D7173J DISPLAY o 6MAG 3ACT R ARTE R C A N1 C CO 1 0ROUTES> .6N M FUEL 1/2 1. GOR1600A T IMMAEX R A N G E FOFSSSE TW T 0>UTC 5736o0 NCMR S 1 0 . 0+5.0 N M9 7H 0 R0 SK G OFFSET ANC 2. RANCE FDUAETLU MW T C OEONRDDU/oFAF o 0>5LAT_ 5 .---.0 9 NWGS84< M1N4M0 0 K G 132 + 4CLONG 4R S RW06R F U E L/oFAF FLOW MILEAGE 3.
4.
100K G / N M 110K G / H R F U E LLEGS R E M A I N ILEGS N G A TETA> FIX ZCH 892K G UNIT
128.050 1524.5 V O R 1 115.80 116.30 V O R 2 AUTO116.70 109.30HOLD X P D R 7777 3A 1211 TCN
033 X 111 Y
6.
RADIO DETAILS>
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Page 3-1 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
PREFLIGHT 1. IDENT - check software version number. Check Configuration Number. Check active database date and interchange if necessary. 2. POS INIT/REF – If GPS is available, check aircraft present position, time and date. Otherwise, manually enter the system and/or IRS position (for alignment). 3. MOD, ACT RTE, DEPARTURES - enter route, confirm FMS flight plan matches clearance. 4. ACT RTE LEGS - check all course and distances between waypoints of the active route. 5. SETUP - check display reference (MAGNETIC, TRUE). 6. FUEL (only if configured) - if a fuel computer is not configured, enter fuel quantity and fuel flow, for computation of maximum range and endurance, and the fuel remaining over a desired waypoint. 7. GPS SAT DESELECT – (only if ARINC 743A GPS is configured): check that GPS satellites are not deselected or deselected according to NOTAMs. 8. VHF NAV DESELECT – deselect any applicable VHF navaids as per NOTAMs. 9. RADIO - check frequencies (if radios are used). 10. PERFORMANCE VNAV – Pre-flight initialization is significantly different when Performance VNAV is enabled. Please refer to Section 18 accordingly. A detailed description of each display page is contained in Appendix A. Radio display pages are detailed in Section 13.
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Page 3-2 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
START-UP AND INITIALIZATION 1. Verify that all relevant circuit breakers are on. 2. Upon initial power-up, the FMS will test all the annunciators. After these tests, it displays the IDENT 1/2 page as the default power-up page. NOTE: The RADIO page (Horizontal or Vertical format) can also be configured as the default power-up page.
FMS1 IDENT 1L 2L 3L 4L
1/2
NAV DATABASE ACTIVE K L M W W 0 6 9 7 OCT10-NOV06/03 SECOND KLMWW0697 NOV07-DEC04/03 OP PROGRAM CFG NO 614876-050F 00777 CUSTOM DATABASE DATE EC-RTEST MAR21/04
5L 6L
1R 2R 3R 4R 5R
POS INIT>
6R
3. Adjust the intensity of the FMS display by pressing and holding the BRT key until a comfortable viewing level is obtained. Each depression of the BRT key alternately brightens or dims the display. On initial power up, or when a time interval of more than 5 seconds has elapsed since the last time the [BRT] key was pressed, the first press of this key will always increase brightness. 4. Verify the OP PROGRAM (software version) and CFG NO. (system configuration) against the Aircraft Flight Manual Supplement. If either software or configuration numbers are incorrect, maintenance action is required. 5. Verify the date of the active database cycle. If all identification data is correct, system start up and initialization is complete.
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Page 3-3 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
ACTIVE DATABASE SELECTION CAUTION:
When the active database is changed, any existing active route is deleted.
1. Copy the SECOND cycle date into the scratchpad, by pressing LSK 2R. 2. Move the cycle date into the ACTIVE field by pressing LSK 1R. The active database cycle is replaced by the second database cycle, as shown by the interchange of cycle dates. The active database cycle is displayed in large font. The active database can only be changed on the ground. Display the IDENT 2/2 page by pressing [INIT REF], and [NEXT].
FMS1 IDENT 1L 2L
2/2 1R
MAGVAR MODEL 2010 (DEF)
2R
3L
3R
4L
4R
5L
5R
6L
POS INIT>
6R
Field 2L displays the in-use 5-year cycle of the Magnetic Variation Table Model. (DEF) indicates that the default 5-year cycle beginning in 2010 is in use. It is valid until the end of 2015. (DEF) blanks when the default Magnetic Variation Table Model is replaced with a new cycle (e.g. 2015) loaded from an external media, via Service Bulletin. NOTE: Other parameters such as aircraft model, engines model, performance database, policy file, weight units, decel factor and fuel flow factor are also displayed when Performance VNAV is enabled. Refer to Section 18.
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Page 3-4 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
FMS DISPLAY SETUP From the IDENT 1/2 page, go to DISPLAY 1/1 page, by pressing [INIT REF], [NEXT] and (LSK 1R).
DISPLAY 1L
1/1
1R
2L
2R
3L
3R
4L
4R
5L
5R
6L
6R
1. Press LSK 1L and adjust display PARALLAX for proper viewing angle. 2. Press [INIT/REF]. 3. Press to return to the IDENT 1/2 page.
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Page 3-5 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SYSTEM POSITION, DATE AND TIME UPDATE From the IDENT 1/2 page go to POS INIT/REF 1/3 page by pressing (LSK 6R).
POS INIT/REF
1/3
FMS POS DR 1L 2L 3L 4L
N47o26.28 W122o18.67
REF WAYPOINT KBFI N 4 7 o3 1 . 8 0 W 1 2 2 o1 8 . 0 0 GATE N47o32.30W122o18.70 BF1 SET IRS POS
N47o32.30W122o18.70
UTC
5L
1757:04
6L
DATE
1R 2R 3R 4R
OCT20/04
5R
ROUTE>
6R
NOTE: Position/time/date cannot be updated if the NAV mode is GPS. At power up the system position is the last calculated position prior to shutdown, or the current GPS position, if available. Initialization of position, date and time is not normally required. If GPS is available, the FMS internal clock is updated to GPS-based UTC and date. Unless an IRS is configured and the GPS position is available, a manual initialization of position, date, and time is not normally required except during an initial aircraft installation, or possibly after a maintenance action. In this case, if GPS position is unavailable, the alert message “SET IRS POS” appears. If the navigation mode is not GPS: 1. Enter the new time into the scratchpad, e.g. 175704. 2. Move the new time to UTC field by pressing LSK 5L. and/or 3. Enter the new date to the scratchpad, e.g. OCT20/04. 4. Move the new date to the DATE field by pressing LSK 5R.
To initialize the position use the POS INIT/REF 1/3 page: 1. Enter the airport identifier into the scratchpad. 2. Move the airport identifier to the REF WAYPOINT field by pressing LSK 2L. REF WAYPOINT and IRS mode fields blank on aircraft lift-off.
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Page 3-6 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 3. Line select airport or IRS position into the scratchpad (by pressing LSK 2R or LSK 4R, or enter any other desired position into the scratchpad (e.g. N472628W1221867). 4. Move the new position to the POSITION field by pressing LSK 1R.
ANGULAR REFERENCES FOR NAVIGATION AND DISPLAY (POLAR AREA DEFINITION) Display the SETUP 1/1 by pressing on the INIT/REF INDEX.
FMS1 SETUP
1/1
DISPLAY
1L
>MAG
1R
2L
2R
3L
3R
4L
4R
FMS OPERATION
5L
>SYNCHRONIZED
6L
5R
ROUTE>
6R
The default angular reference of all navigation displays (heading, course, actual track, and bearing) is Magnetic North (degree symbol following each angle display), and that of wind direction is True North (T symbol following each angle display). Select the angle display reference to TRUE or MAGNETIC by pressing LSK 1L. In some installations, the angle display reference can only be controlled via an external true/mag cockpit switch. In this case the MAG/TRUE selection prompt (at LSK 1L) is removed; only the current state is displayed. Upon entering the polar area (by default above N73 and below S60), the angular reference automatically reverts to true north and the reference toggling is inhibited. The FMS invalidates all its magnetic angles in those regions. If the angular reference was magnetic previous to entering the polar area, the USING TRUE REF advisory scratchpad message is displayed to inform the crew of the change from magnetic to true north. Upon the airplane leaving the polar area, the system behaviour depends upon the aircraft installation: • If interfaced with a true/mag cockpit switch, then the FMS uses the switch state to determine the angular display reference. • Otherwise, the angular reference display is maintained to True and the True/Mag toggling capability is restored. The CHECK TRUE/MAG REF advisory scratchpad message prompts the crew to check/select the angular reference. NOTE:
It is possible to configure the FMS to change the definition of the polar area, in order to provide better availability of magnetic angles. The purpose of this feature is to enable operations in some airports charted in magnetic angles and located marginally within the default polar area. Special care should be taken at the aircraft level when enabling this feature given that the magnetic data becomes less reliable when approaching the poles.
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Page 3-7 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) CAUTION: FMS operations above latitude N85 and below latitude S85 are expected to be limited to flying fixto-fix legs (great circle tracks), including fly-by leg transitions. Procedures using angular references are therefore not intended to be conducted in these areas.
ACTIVE ROUTE SELECTION USING THE COMPANY ROUTE NAME Display the RTE 1/X page by pressing the [RTE] function key.
MOD
RTE 1
1/3
ORIGIN
DEST
RUNWAY
FLT NO
1L
KSEA
2L
-----
PANC
KL007
ROUTE
1R 2R
3L
KSEAPANC1
3R
4L
CO RTES>
4R
5L 6L
5R
DEPARTURES>
6R
1. Key in the company route identifier into the scratchpad, e.g.: KSEAPANC1. 2. Move the company route name to the CO RTES field by pressing LSK 3R. "MOD" status is displayed in the title line. 3. Verify the ORIGIN and DEST identifiers. 4. Enter flight number into the scratchpad. Move to the FLT NO field by pressing LSK 2R. The entered flight number will also be displayed on the PROGRESS pages titles.. 5. Accept the new active route by pressing [EXEC]. "MOD" status in the title line changes to "ACT". The selected route is now active. NOTE: When loading a company route in flight, the FMS will append a "+" to the company route identifier on the RTE page thus indicating that the company route has been appended to the end of the current flight plan. When a company route is inversed, the route name is preceded by the prefix INV in reverse video.
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Page 3-8 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
ROUTE SELECTION FROM THE LIST OF COMPANY ROUTES With the ACT or MOD RTE 1/X page displayed: Display the company routes by pressing (LSK 4R).
SELECT CO ROUTE 1L
KSEAPANC
2L
KSEAPANC2
1/1
KSEAPANC1
3L 4L
1R 2R 3R
LOAD
4R
5L
>DIRECT
5R
6L
6R
Company routes are displayed left to right, sorted by origin identifier. NOTE: If the display of the CO ROUTE is configured to ORIG_DEST, the entry of an ORIGIN or both ORIGIN and DEST identifiers on RTE x 1/X page will reduce the company routes list, when on ground, to those specified in the ORIGIN or ORIGIN and DEST fields. When airborne, all company routes are displayed. If CO ROUTE is configured to ALL, every CO ROUTE in the company database will be displayed. 1. Display the desired route by pressing [NEXT] or [PREV] as often as required. 2. Select route identifier by pressing the appropriate LSK. 3. Select the direction in which the route is loaded by toggling DIRECT/INVERSE using LSK 5L. 4. The RTE 1/X page is re-displayed. Verify the ORIGIN and DEST identifiers. 5. Accept the new active route by pressing [EXEC]. When airborne, selecting a company route will replace the destination with the selected company route destination and will insert a discontinuity after the active waypoint followed by the selected company route waypoints. If a procedure (for e.g. STAR or Approach) is part of the flight plan, the whole procedure is replaced by the selected company route.
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Page 3-9 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
BUILDING A ROUTE BY WAYPOINT INSERTION When no company route is available, a route can be created by first defining the origin and destination airports on the ROUTE page, followed by entry of the individual waypoints on the RTE x LEGS page. Display the ACT or MOD RTE x 1/X page by pressing [RTE].
ACT
RTE 1
1/3
ORIGIN
DEST
RUNWAY
FLT NO
1L
KSEA
2L
-----
PANC
KL007
ROUTE
1R 2R
3L
KSEAPANC1
3R
4L
CO RTES>
4R
5L 6L
5R
DEPARTURES>
6R
1. Key the departure airport identifier into the scratchpad and move it to the ORIGIN field by pressing LSK 1L. "MOD" status is displayed in the title line. 2. Key the destination airport identifier into the scratchpad and move it to the DEST field by pressing LSK 1R. 3. Display the MOD RTE x LEGS 1/1 page by pressing [LEGS]. The active waypoint identifier field contains boxes. 4. Key the identifier of the first waypoint into the scratchpad and move it to the active waypoint location by pressing LSK 1L. The direct course and distance from present position to the active waypoint is computed and displayed, and the INTC CRS prompt is displayed at the LSK 6R location with dashes ("---") in the intercept course field. NOTE: The minimum route comprises of the origin and destination airports and a single waypoint. If desired, direct-to navigation from the present position to the first waypoint of the route can be initiated at this time as described in Section 9 (Direct-To/Intercept). 5. Key in all subsequent waypoint identifiers in turn, inserting them into the route by pressing the appropriate left hand LSK. Press [NEXT] as required to display a new RTE x LEGS page. 6. Additional temporary waypoints can be inserted into the route as described in Section 5.
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Page 3-10 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
BUILDING A ROUTE BY AIRWAY INSERTION When no company route is available, a route can be created by first defining the origin and destination airports on the ROUTE page, followed by entry of the individual airway identifier on the ROUTE page. 1. Key the departure airport identifier into the scratchpad and move it to the ORIGIN field by pressing LSK 1L. "MOD" status is displayed in the title line. The "ERASE" prompt is displayed at LSK 6L and the EXEC annunciator illuminates. 2. Key the destination airport identifier into the scratchpad and move it to the DEST field by pressing LSK 1R. 3. Display the RTE x 2/X page by pressing [NEXT].
MOD VIA
1L
LACRE3
RTE 1
2/3 TO
HUMPP
-- ROUTE DISCONTINUITY -
2L
1R 2R
3L
J20
OCS
3R
4L
J154
RAMMS
4R
5L
DIRECT
GWENS
5R
6L
ARRIVALS>
6R
4. Key the identifier of the first waypoint into the scratchpad and move it to the TO location by pressing LSK 1R. DIRECT is displayed below VIA, indicating that the first flight leg will be from Present Position direct to the first waypoint of the desired airway. 5. Key in the airway identifier and move it to the airway field by pressing LSK 2L, a box data field appears against LSK 2R. 6. Key in the next airway identifier and move it to the airway field by pressing LSK 3L, the waypoint at the junction of the two airways appears in the box data field against LSK 2R and a box data field appears against LSK 3R. 7. Key in all subsequent airway identifiers in turn, inserting them into the route by pressing the appropriate left hand LSK. Press NEXT as required to display a new ROUTE page.
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Page 3-11 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
NOTE: The route can be modified by defining the waypoint identifier at which the desired airway segment is terminated and repeating the procedure for entering the following airways. If a departure or an arrival is selected on the DEP/ARR page, the procedure and the transition name will be displayed in the VIA and TO fields. If a waypoint is inserted immediately before an already inserted waypoint, a DIRECT TO the entered waypoint will be created followed by a route discontinuity and a DIRECT TO the already inserted waypoint. The route can also be modified by adding and/or erasing waypoints on the selected RTE x LEGS page. 8. Display the first leg by pressing [LEGS] and [PREV] or [NEXT] as required. 9. Close-up any route discontinuity as described in Section 5. 10. Verify the course, distance, altitude/speed advisory of each airway leg in turn by pressing [NEXT] as required to display all legs. 11. Make the selected route active by pressing [EXEC].
VERIFYING ACTIVE ROUTE LEGS BY COURSE AND DISTANCE Display the MOD RTE x LEGS 1/X page by pressing [LEGS].
MOD
RTE 1 LEGS
2/4
299o
39.6N M
298o
154N M
307o
86.7N M
306o
165N M
282o
197N M
1L
CAFTA
2L
YZP
3L
MOCA1
4L
BKA
5L
KILLA
6L
1R 2R 3R 4R 5R
LEGS ETA>
6R
1. Verify the course and distance of all route legs. 2. Display all route legs in sequence by pressing [NEXT] as often as required. 3. Return to the MOD RTE x LEGS 1/X page by pressing [LEGS] or [PREV] as required. 4. Make the route active by pressing [EXEC].
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Page 3-12 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) The "MOD" status in the title line changes to "ACT", the ERASE prompt disappears and the EXEC annunciator extinguishes.
INITIAL LEG Following the waypoint of a route, navigation and guidance is computed initially for the leg from present position direct to the first waypoint. On takeoff, the FMS automatically re-computes a Direct-To to the first waypoint. If a runway and SID are selected and the first leg is not a Direct-To leg, navigation and guidance is computed initially from the runway threshold to the first waypoint. On take-off, the FMS automatically re-computes the initial leg using the present position as the start of the leg.
CANCELLING ANY PROCEDURE OR ROUTE MODIFICATION During any procedure which involves a modification to the active route, an ERASE prompt is displayed at LSK 6L. Prior to EXECuting the procedure, it can be cancelled and all route modifications deleted by pressing (LSK 6L).
ROUTE 2 OPTION NOTE: If RTE 3 option is enabled, ignore this sub-section and go to next sub-section (ROUTE 3 OPTION). When configured with RTE 2 option, two independent routes (RTE 1 and RTE 2) may reside in the FMS at the same time. The FMS allows activation of one route as the active flight plan. The other flight plan is stored as the inactive route. The default route at power-up, with both routes empty, is RTE 1. The inactive route may be manually created or selected from the stored company routes. It may also be copied from the active route. The procedures to create, select, and/or edit the inactive route are identical to those of the active route. 1. Display the ACT RTE x 1/X page by pressing [RTE] (a route has been previously entered and executed).
ACT
RTE 1
1/2
ORIGIN
DEST
RUNWAY
FLT NO
1L
KSEA
2L
23R
PANC
AS007
ROUTE
1R 2R
3L
KSEAPANC1
3R
4L
CO RTES>
4R
5L 6L
5R
OFFSET
R0.0N M
This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.
6R
Page 3-13 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 2. Access the inactive route by pressing LSK 6L (e.g. RTE 2). NOTE: The inactive route pages are displayed in monochrome cyan to distinguish them from the active route pages.
RTE 2 ORIGIN 1L 2L
1R
RUNWAY
-----
ROUTE
3L 4L
1/2 DEST
----------
3R
CO RTES>
4R
5L 6L
2R
5R
6R
A. INACTIVE ROUTE MANIPULATIONS (SUMMARY) 1. Using the procedures outlined in Section 3, enter the origin, destination, and waypoints, or select a stored company route as the inactive route. Next, press , (LSK 6R) to save the modifications or (LSK 6L) to delete them. NOTE: In the case of a dual/triple FMS installation, the inactive route modification is cross-talked to the off-side FMS upon pressing the prompt. The EFIS typically displays the inactive flight plan in cyan when an inactive route page is displayed on the FMS. 2. The inactive route is edited directly on the ROUTE, LEGS, DEP/ARR and HOLD pages. Both active and inactive routes have their own independent set of ROUTE, LEGS, DEP/ARR and HOLD pages. 3. To ACTIVATE the inactive route, press LSK 6R on the inactive RTE page, followed by pressing the [EXEC] key. NOTE: The following COPY RTE procedures highlight the basic steps required to select, then activate a second route.
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Page 3-14 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) B. INACTIVE ROUTE MANIPULATIONS (DETAILED STEPS) 1. To copy the active route, e.g. RTE 1, to the inactive route, press LSK 4L of the inactive RTE page. RTE 1 remains active and continues to be used for navigation.
RTE 2
1/2
ORIGIN
1L
KSEA
2L
RW34R
DEST
PANC
RUNWAY ROUTE
3L 4L
2R
KSEAPANC1
3R
CO RTES>
4R
5L 6L
1R
5R
CONFIRM>
SAVE?
6R
2. Press LSK 6R to CONFIRM copying of the route. NOTE: The copied route contains the active and subsequent waypoints. Overflown waypoints are not copied. In the case of a dual/triple FMS installation, the inactive route is crosstalked to other FMU's upon each CONFIRM of flight plan changes. 3. Press [LEGS] to display the RTE 2 waypoints. Modify the RTE x LEGS page as required to build a new flight plan based on the current active route.
RTE 2 LEGS
1/5
299o
39.6N M
298o
154N M
307o
86.7N M
306o
165N M
282o
197N M
1L
CAFTA
2L
YZP
3L
MOCA1
4L
BKA
5L
KILLA
6L
1R 2R 3R 4R 5R
LEGS ETA>
6R
4. Access the RTE x LEGS ETA and FUEL pages to perform predictions as for the inactive route. Predictions are based on the aircraft’s present position direct to the first waypoint in the inactive route. NOTE: There are no predictions made on the inactive route when Performance VNAV is configured.
This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.
Page 3-15 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 5. When changes are completed, press the [RTE] key to access the RTE 2 page.
RTE 2
1/2
ORIGIN
1L
KSEA
2L
RW34R
PANC
RUNWAY ROUTE
3L 4L
DEST
2R
KSEAPANC1
3R
CO RTES>
4R
5L 6L
1R
5R
RTE 2
ACTIVATE>
6R
6. Press (LSK 6R) to the inactive route. 7. The RTE 2 LEGS page is displayed. Press the [EXEC] key to confirm activation of RTE 2.
MOD
RTE 2 LEGS
2/4
299o
39.6N M
298o
154N M
307o
86.7N M
306o
165N M
282o
197N M
1L
CAFTA
2L
YZP
3L
MOCA1
4L
BKA
5L
KILLA
6L
1R 2R 3R 4R 5R
LEGS ETA>
6R
8.
Prior to pressing [EXEC], (LSK 6L), may be used to cancel activation.
9.
The LEGS page title legend changes from MOD to ACT. The former inactive route, now active, is displayed in multiple colors.
10. The previous active route is now inactive route (displayed in cyan).
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Page 3-16 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
ROUTES 2 & 3 OPTION When configured with for ROUTES 2 & 3 option, up to three independent routes (RTE 1, and RTE 2, and RTE 3) may reside in the FMS at the same time. The FMS allows activation of one route as the active flight plan. The other flight plans are stored as inactive routes. The default route at power-up, with all routes empty, is RTE 1. The inactive routes may be manually created or selected from the stored company routes. They may also be copied from the active route. The procedures to create, select, and/or edit the inactive route are identical similar to those of the active route with the addition of the VIA feature (which is available only when the Performance VNAV function is enabled). Without use of the VIA feature (described below in dedicated sub-section), when an inactive route is made active, the FMS will fly direct-to the first waypoint of the new active route. 1. Display the ACT RTE x 1/X page by pressing [RTE] (a route has been previously entered and executed).
ACT
RTE 1
1/3
ORIGIN
DEST
RUNWAY
FLT NO
1L
KSEA
2L
RW34R
PANC
-------ROUTE
1R 2R
3L
----------
3R
4L
CO RTES>
4R
5L
6L
5R
DEPARTURES>
This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.
6R
Page 3-17 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 2. Access an inactive route by pressing LSK 6L (e.g. RTE 2) or LSK 5L (RTE 3). NOTE: The inactive route pages are displayed in monochrome cyan to distinguish them from the active route pages.
RTE 2 ORIGIN 1L 2L
1/2 DEST 1R
RUNWAY
-----
ROUTE
3L
2R
----------
3R
CO RTES>
4R
4L
5L
5R
6L
6R
A. INACTIVE ROUTE MANIPULATIONS (SUMMARY) 1. Using the procedures outlined in Section 3, enter the origin, destination, and waypoints, or select a stored company route as the inactive route. Next, press , (LSK 6R) to save the modifications or (LSK 6L) to delete them. NOTE: In the case of a dual/triple FMS installation, the inactive route modification is cross-talked to the off-side FMS upon pressing the prompt. The EFIS typically displays the inactive flight plan in cyan when an inactive route page is displayed on the FMS. 2. The inactive route is edited directly on the ROUTE, LEGS, DEP/ARR, and HOLD pages. Both active and inactive routes have their own independent set of ROUTE, LEGS, DEP/ARR, FUEL and HOLD pages. 3. To ACTIVATE the inactive route, press LSK 6R on the inactive RTE page, followed by pressing the [EXEC] key. The LEGS page will display RTE 2 or RTE 3 waypoints, depending on which RTE page was being previously viewed. NOTE: The following COPY RTE procedures highlight the basic steps required to select, and then activate a second or third route.
This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.
Page 3-18 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) B. COPYING THE ACTIVE ROUTE TO THE INACTIVE ROUTE MANIPULATIONS (DETAILED STEPS) 1. To copy the active route, e.g. RTE 1, to the inactive route, select the inactive route from the active route page (press LSK 5L for RTE 3, or 6L for RTE 2), and then press LSK 4L of the inactive RTE page. RTE 1 remains active and continues to be used for navigation.
RTE 2
1/3
ORIGIN
1L
KSEA
2L
RW34R
DEST
PANC
RUNWAY ROUTE
3L 4L
2R
----------
3R
CO RTES>
4R
5L 6L
1R
5R
CONFIRM>
SAVE?
6R
2. Press LSK 6R to CONFIRM copying of the route. NOTE: The copied route contains the active and subsequent waypoints. Overflown waypoints are not copied. In the case of a dual/triple FMS installation, the inactive route is crosstalked to other FMU's upon each CONFIRM of flight plan changes and upon synchronization. 3. Press [LEGS] to display the RTE 2 waypoints. Modify the RTE x LEGS page as required to build a new flight plan based on the current active route. NOTE: ETE/ETA and EFA are not displayed for the inactive route when Performance VNAV is configured.
RTE 2 LEGS
1/5
299o
39.6N M
298o
154N M
307o
86.7N M
306o
165N M
282o
197N M
1L
CAFTA
2L
YZP
3L
MOCA1
4L
BKA
5L
KILLA
6L
1R 2R 3R 4R 5R
LEGS ETA>
6R
4. Access the INACTIVE RTE x LEGS ETA and RTE x FUEL pages to perform display predictions for the inactive route. Predictions are based on the aircraft’s present position direct to the first waypoint in the inactive route.
This document includes Proprietary Information and shall not be reproduced or communicated to third party without prior written permission by CMC Electronics Inc.
Page 3-19 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
5. When changes are completed, press the [RTE] key to access the RTE 2 page.
RTE 2
1/2
ORIGIN 1L
KSEA
2L
RW34R
DEST
PANC
RUNWAY ROUTE
3L 4L
5L
6L
1R 2R
----------
3R
CO RTES>
4R 5R
RTE 2
ACTIVATE>
6R
6. Press (LSK 6R) to the activate the inactive route. 7. The RTE 2 LEGS page is displayed. Press the [EXEC] key to confirm activation of RTE 2.
MOD
RTE 2 LEGS
299o
1L
CAFTA
2L
YZP
3L
MOCA1
4L
BKA
5L
KILLA
6L
1/5 39.6 N M
298o
154.0
307o
86.7
306o
165. 0
282o
197. 0
1R 2R 3R 4R 5R
LEGS ETA>
6R
8. Prior to pressing [EXEC], (LSK 6L), may be used to cancel activation. 9. The LEGS page title legend changes from MOD to ACT. The former inactive route, now active, is displayed in multiple colors. 10. The previously active route now forms one of two inactive routes (displayed in cyan). C. SWITCHING FROM RTE 1 to RTE 2 or RTE 3 WITHOUT THE VIA FUNCTION Activation of an Inactive route while in-flight or on ground results in a modified route consisting of the waypoints of the Inactive route, starting at the Top waypoint location on the MOD RTE x LEGS page. The previously active route becomes the inactive route but retains its route number. Any one route at a time, RTE 1, RTE 2 or RTE 3 may be active, while the other two are inactive.
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Page 3-20 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
D. USING THE VIA FUNCTION (available only when Performance VNAV is enabled) The VIA function can be used to append waypoints from the active route to the beginning of the inactive route upon its activation, in order to plan a diversion point from the original active route. Typically this function is used to plan the diversion to an alternate airport. The VIA waypoint is a waypoint from the active route from which the diversion to the inactive route will be initiated. The VIA prompt is available at LSK 2R of the inactive RTE page, provided that this route does not contain a departure runway/SID (the FMS does not allow departing the active route to string a SID of the inactive route). Once a VIA waypoint is entered, no departure selection is possible on the inactive route. In the following example, an alternate airport (PAFA) is to be entered on RTE 2, to be flown to after being diverted from PANC, the destination of the active route. 1. On the inactive RTE 2 page, enter the destination PANC at (LSK 1L). Enter the new destination PAFA at (LSK 1R). When the inactive route origin coincides with the active route destination, then this inactive route is considered an alternate, and the VIA waypoint field is automatically pre-filled with the last waypoint of the active route (typically the missed approach holding point). In the example below, NAPTO being the missed approach holding point of the active route (PANC) is automatically copied to (LSK 2R) field.
RTE 2 ORIGIN
1L
PANC
2L
-----
PAFA
RUNWAY
VIA RTE 1 NAPTO ROUTE
3L 4L
1/2 DEST
2R
----------
3R
CO RTES>
4R
5L 6L
1R
5R
CONFIRM>
SAVE?
6R
2. The VIA waypoint can be modified if required (e.g. KILLA) to provide an earlier diversion point from the current active route.
RTE 2
DEST
RUNWAY
VIA RTE 1
1L
PANC
2L
-----
PAFA
KILLA
ROUTE
3L 4L
1/2
ORIGIN
2R
----------
3R
CO RTES>
4R
5L 6L
1R
5R
SAVE?
CONFIRM>
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6R
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
3. Via the DEP/ARR INDEX page, select an approach for PAFA ARRIVALS.
PAFA ARRIVALS 1L 2L
1/1
STARS RTE 2 APPROACHES -NONE- VOR19R TRANS D040S
1R 2R
3L
3R
4L
4R
5L
5R
6L
CONFIRM>
SAVE?
26
4. Press [LEGS] to display the RTE 2 waypoints. Modify the RTE x LEGS page as required. NOTE: ETE/ETA and EFA are not displayed for the inactive route.
RTE 2 LEGS
1/2
RTE 1 KILLA
92.0 N M
004o
65.4
000o
113. 0
108o
5.6
198o
2.8
1L
PEE
2L
UMM
3L
CEPLA
4L
ELACA
5L
ROPEE
6L
4900A 4600
SAVE?
CONFIRM>
1R 2R 3R 4R 5R 26
5. Access the INACTIVE RTE x FUEL pages to display predictions for the inactive route. Predictions for the inactive route with VIA function are based on the active route up to the VIA waypoint and then direct to the first waypoint of the inactive route. 6. When all changes are complete, press (LSK 6R) to confirm RTE 2. 7. Prior to pressing , (LSK 6L) may be used to cancel RTE 2 changes. NOTE: In the case of a dual/triple FMS installation, the inactive route is crosstalked to other FMU's upon each CONFIRM of flight plan changes and upon synchronization.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
8. To activate RTE 2 route to alternate destination PAFA, press the [RTE] key to access the RTE 2 page.
RTE 2
1/2
ORIGIN 1L
PANC
2L
-----
DEST
PAFA
RUNWAY
VIA RTE 1 NAPTO ROUTE
3L 4L
5L
6L
1R 2R
----------
3R
CO RTES>
4R 5R
RTE 2
ACTIVATE>
6R
9. Press < ACTIVATE> (LSK 6R) to activate RTE 2 route. 10. The RTE 2 LEGS page is displayed in MOD state. NOTE: The modified route contains the current active route waypoints downpath to the VIA waypoint, followed by the RTE 2 waypoints.
MOD 1L 2L 3L 4L
RTE 2 LEGS
R167o TUVUJ 211o
NAPTO
/H
2/4
7.10N M 240/ 7663 22.7N M
200/
3000A
THEN — ROUTE DISCONTINUITY PEE 240/ 7115 004o 65.4N M
5L
UMM
6L
240/
6802
LEGS ETA>
1R 2R 3R 4R 5R 6R
11. Press the [EXEC] key to confirm activation of RTE 2. 12. Prior to pressing [EXEC], (LSK6L), may be used to cancel the activation. 13. The LEGS page title legend changes from MOD to ACT. The former inactive route, now active, is displayed in the active route color scheme. 14. The previously active route (RTE 1 in this example) becomes inactive and is displayed in monochrome cyan. Activation of an Inactive route with a VIA from the original destination airport to an alternate airport results in a modified route consisting of the current active waypoint and remaining waypoints, up to and including any missed approach and hold, followed by a discontinuity, then the waypoints of the Inactive route.
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Page 3-23 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) Activation of an Inactive route with a VIA from an en-route waypoint results in a modified route consisting of the current active waypoint up to the VIA waypoint, followed by a discontinuity, then the waypoints of the Inactive route. The previously active route becomes an inactive route but retains its route number.
ACCESSING INIT/REF INDEX PAGES Display the INIT/REF INDEX 1/2 page by pressing [INIT REF].
FMS1 INIT/REF INDEX 1/2 1L
2L
3L
4L
5L
6L
NAV DATA>
1R
WPT LISTS>
2R
NEAREST>
3R
FUEL>
4R
NAV STATUS>
5R 6R
Display the INIT/REF INDEX 2/2 page by pressing [NEXT] or [PREV].
FMS1 INIT/REF INDEX 2/2 1L
DISPLAY> RTE DISCON>
2L
1R 2R
3L
3R
4L
4R
5L
DATA LOAD>
5R
6L
MAINT>
6R
NOTE: All prompts displayed on the INIT/REF INDEX pages are configurable and the page layouts illustrated above are provided as examples only. In this particular example, LSK 1L, LSK 4L, LSK 1R, LSK 2L and LSK 4R are installation dependent, and thus may not appear as shown above. appears only when the aircraft is on ground for maintenance database loading. appears only when the aircraft is on ground for maintenance operations.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
NOTE : The PLAN DATA page is mutually exclusive with the Performance VNAV functions. Refer to Section 18 for performance initialization and vertical flight planning when Performance VNAV is enabled. 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 FMS will provide user modifiable Cruise TAS and Cruise Wind values. The cruise TAS and cruise wind will only appear airborne if the system TAS is failed. Upon a warm or cold start, the FMS will keep the Cruise TAS value prior to the power down. Upon a change in configuration, the FMS will set the Cruise TAS value to 480 kts. The 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 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 TRANS ALT
1L 2L
18000F T
TRANS LVL F L 180
1/1
CRZ WIND 300T / 90K T CRZ TAS
360K T
1R 2R
3L
3R
4L
4R
5L
5R
6L
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6R
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
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. 3. Key in the cruise wind (e.g. 300/90) and move it into the CRZ WIND field by pressing LSK 1R. 4. Key in the planned cruise true airspeed (e.g. 360) and move it into the CRZ TAS field by pressing LSK 2R.
FUEL PERFORMANCE PARAMETERS INITIALIZATION (if configured) These are not mandatory entries. Refer to Section 14, Performance functions. NOTE :
Section 14 referred above is mutually exclusive with the Performance VNAV functions. Refer to section 18 for performance initialization and vertical flight planning when Performance VNAV is enabled.
FUEL AND WEIGHT PERFORMANCE PARAMETERS INITIALIZATION (if configured)
NOTE :
The FUEL page described below is mutually exclusive with the Performance VNAV functions. Refer to section 18 for performance initialization and vertical flight planning when Performance VNAV is enabled.
If the FUEL+WEIGHTS option is configured for the FUEL pages, the FMS provides on the RTE x FUEL 2/2 page several fields used by the operator to enter the empty weight, optional equipment weight, crew weight, cargo weight and total fuel weight including reserve. These values are used by the FMS to calculate the initial Gross-Weight (GWT) estimate, displayed on the RTE x FUEL 1/2 page. Once the initial GWT is accepted by the FMS, the Gross Weight will be continuously estimated by subtracting the fuel consumption based on the average fuel flow. The display of the GWT units will match the display of the fuel flow units that is, if the fuel flow is displayed in Kg/Hr or Lb/Hr, then the GWT will also be displayed in Kg or Lb respectively. CAUTION: The unit selection on the FUEL 1/2 and FUEL 2/2 pages has to be consistent with other fuel indicators configured in the cockpit. Verify units on the FUEL pages and on other fuel indicators. Display the INIT/REF INDEX 2/2 page by pressing [INIT REF], [PREV] or [NEXT].
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
Display the RTE x FUEL 1/2 page by pressing (can be configured on any LSK) on the INIT/REF INDEX 2/2 page or the [FUEL] functional key (if configured).
ACT RTE 1 FUEL 1L 2L 3L 4L
1/2
MAX RANGE 760N M ENDURANCE 01+21 FUEL FLOW
GROSS WT 9700K G FUEL WT 1400K G MILEAGE 110K G / H R 100K G / N M FUEL REMAINING AT FIX ZCH 892K G UNIT
KG<
5L 6L
1R 2R 3R 4R 5R 6R
1. Key in the current fuel weight (e.g. 9700) and move it into the FUEL WT field by pressing LSK 2R. 2. Key in the current fuel flow (e.g. 110) and move it into the FUEL FLOW field by pressing LSK 3L. 3. UNIT at LSK 5R toggles between LB and KG. Maximum range and endurance are calculated based on entered fuel quantity and fuel flow rate. The maximum range is computed along the track to the FIX waypoint (if the FIX is defined) or with the current track, given current or estimated fuel weight (excluding the reserve), fuel flow, and ground speed (if the FIX is not defined). The endurance is computed using the given current or estimated fuel weight (excluding the reserve) and fuel flow. CAUTION: On power interruptions, the fuel units will revert to the configured units (from maintenance page). Verify units when reading or entering values. Display the RTEx FUEL 2/2 page by pressing [NEXT] or [PREV].
ACT RTE 1 FUEL
EMPTY WT
RESERVE
EQUIP WT
1L
1700K G
2L
300K G
5000K G 700K G
CREW WT
300K G
3L
CARGO WT
2000K G
4L
UNIT KG<
5L 6L
2/2
FUEL+RES
1R 2R 3R 4R 5R 6R
4. Key in the fuel weight including reserve (e.g. 1700) and move it into the FUEL+RES field by pressing LSK 1L. 5. Key in the fuel reserve weight (e.g. 300) and move it into the RESERVE field by pressing LSK 2L.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
6. Key in the aircraft empty weight (e.g. 5000) and move it into the EMPTY WT field by pressing LSK 1R. 7. Key in the optional equipment weight (e.g. 700) and move it into the EQUIP WT field by pressing LSK 2R. 8. Key in the total crew weight (e.g. 300) and move it into the CREW WT field by pressing LSK 3R. 9. Key in the total cargo weight (e.g. 2000) and move it into the CARGO WT field by pressing LSK 4R. 10. UNIT at LSK 6R toggles between LB and KG.
GPS SATELLITE DESELECTION (If configured) If required by NOTAM deselect the indicated satellite(s). Refer to Appendix A, GPS SAT DESELECT 1/1 page for the deselection commands. Otherwise ensure that no satellites are deselected.
DUAL/TRIPLE FMS OPERATIONS In dual/triple FMS installations, the operator can set the FMS to operate in either synchronized or independent mode from the SETUP 1/1 page. The operating mode can be configured to automatically startup in either synchronized or independent mode. From the INIT/REF INDEX 1/2 page, display the SETUP 1/1 page by pressing .
FMS1 SETUP
1/1
DISPLAY
1L
>MAG
1R
2L
2R
3L
3R
4L
4R
FMS OPERATION
5L
>SYNCHRONIZED
6L
5R
ROUTE>
6R
1. Select either INDEPENDENT or SYNCHRONIZED mode of operation. NOTE: When the XFMS synchronization option of the FMS is configured to ALWAYS, manual selection of independent mode is inhibited. When the XFMS synchronization option of the FMS is configured to NO (e.g. independent) manual selection of the independent and synchronized modes are inhibited.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
2. Press LSK 5L, confirm by pressing LSK 6R or cancel by pressing LSK 6L. After confirming change to independent mode, the alert scratchpad message “FMS INDEPENDENT OP” is displayed by all FMSs and the IND annunciator is illuminated on all CDUs. NOTE: Selection from independent to synchronized mode is prevented with the display of the alert message “UNABLE FMS-FMS SYNC” when: • communication between the FMSs has been lost, • on-side FMS is in a holding pattern, • on-side FMS is in a GPS approach, • any FMS in a missed approach procedure, • a conflicting operational s/w part number, • FMSs have a different active navigation database, • performance database (when used, refer to section 18) are different, • user databases (when used, refer to Section 11) are different. NOTE: On synchronization, the flight plan is transferred from the FMS where the synchronization was initiated to the other FMSs, overriding any existing flight plan.
SYNCHRONIZED OPERATIONS NOTE: To operate correctly in the synchronized mode the FMSs must contain the same databases. Furthermore the active database must be the same in all FMSs. In the synchronized mode of operation, the following items are automatically synchronized between all FMSs: • • • • • • •
FMS settings (e.g. UTC/Date entry, TRUE/MAG selection, etc). Flight-Plan related information (e.g. flight plan entries or changes) Navigation-related information (e.g. system position, RNP, etc.) Guidance-related information (e.g. Missed approach request, Hold exit request, etc.) Alert messages and their fault sources Radio-related information (e.g. self-test commands, tuning data, etc.) Etc.
Only one FMS can change an active flight plan at any time. If one FMS is already in MOD status (route modifications in progress), any attempt to change the flight plan of another FMS will bring in view the “ !CDU ENTRY CONFLICT” message in the scratchpad. In synchronized mode, both FMS will use the best system sensor for navigation and guidance computations (unless deselected on the DESELECT 1/1 page). Therefore, FMS present position, track and ground speed are synchronized. NOTE: In synchronized mode of operation, the GPS integrity annunciator will illuminate only if the GPS integrity is lost on all GPS sensors. When synchronized, an FMS will change to independent mode if its Phase of Flight is different from the other FMS(s) for more than 5 seconds.
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Page 3-29 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
INDEPENDENT OPERATIONS In the independent mode of operation, all entries made on either FMS are not reflected on the other FMS. The alert message FMS-FMS POS DISAGREE is displayed in the scratchpad if the estimated position is significantly different between different FMS. NOTE: Due to slight variations in the position computation made by each FMS, leg sequencing may not occur at exactly the same time on all FMSs while in independent operations.
RADIO TUNING OPERATIONS – DUAL/TRIPLE FMS or FMS and RADIO HEAD The radio tuning feature may not use FMS cross talk to establish synchronization. Depending of the installation, it may use burst tuning and the radios’ feedback to establish synchronization. Its operations will not be affected by the selection of synchronized or independent mode of operations. In a dual/triple FMS architecture, when the standby frequency is entered, it is cross talked to the cross-side FMS (both FMS always display the same standby frequency of the same radio).
EMBEDDED CALCULATOR/CONVERSION TOOL (if configured) If any mathematical calculations are required, use the CALC/CONV 1/2 page. Conversions from one unit to another (e.g.: Meters to Feet) can be performed using the CALC/CONV 2/2 page. Refer to Appendix A for specific details.
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Page 3-30 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SECTION 4 - DEPARTURES
CONTENTS Subject
Page
SECTION 4 - DEPARTURES ....................................................................................................................................4-i INTRODUCTION .............................................................................................................................................4-1 SID SELECTION WHILE IN FLIGHT..............................................................................................................4-3 CONDENSED SID AND SID TRANSITION PROCESS .................................................................................4-3 STANDARD INSTRUMENT DEPARTURE (SID) SELECTION .....................................................................4-4
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Page 4-i July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
This Page Intentionally Left Blank
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Page 4-ii July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
SECTION 4 DEPARTURES CAUTION: In case of disagreement between the published SID information and FMS displayed information, the operator MUST follow the published SID directives.
INTRODUCTION The complete departure procedure, including Standard Instrument Departure (SID) and SID transition, can be loaded into the route at the same time or in segments, depending on the ATC clearance received. The segments are selected from lists of named procedures extracted from the navigation database for the specified origin airport. When a SID is selected, the waypoints and procedural legs are extracted from the navigation database, procedural leg types are decoded, and all resulting waypoints are inserted into the route. SID transitions are appended to the route after the SID and are usually separated from it by a route discontinuity, unless the last waypoint of the SID and the first waypoint of the en-route portion of the route are identical. Figure 4-1 shows a typical SID and SID transition. The SID transition is linked to the appropriate waypoint of the en-route portion, and enroute waypoints preceding the intersecting waypoints are deleted. If there is no SID transition, the SID is separated from the en-route portion by a route discontinuity. For certain types of SID and transition, the waypoints may not be loaded into the route until the runway is selected. ATC clearances which modify the selected SID procedures can be incorporated by selection of the new procedure while the aircraft is still on ground. This results in the automatic deletion of the waypoints associated with the cancelled procedure.
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Page 4-1 July 17, 2013
R1 0
9°
21
6
SA (C N M HA A V2 TY2. RCUS 5 R 60 - 18 ZS) 0
N34 30.6 W119 46.3
RZS
SAN MARCUS
D (H) 114.9
1 0 600
31 1
D16
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VTU
°
N34 06.9 W119 03.0
D (L)108.2
D20
N33 56.0 W118 25.9
3 23
LOS ANGELES INTL 126
070° hdg
dg °h
7 DM
LAX
LOS ANGELES D (H)113.6
0 04
TAKE-OFF Runways 6L/R: Climb via a 040° heading for vector to V-23. Thence via (transition or FILLMORE assigned route). D (L)112.5 FIM Runways 7L/R: Climb via a 070° heading for vector to V-23. Thence via (transition or N34 21.4 W118 52.9 assigned route). HENER 28 HENER N34 19.9 Transitions: 9° D R) NE HE 2. (CHATY 0° 25 D27 W119 13.7 R San Marcus (CHATY2. RZS): From Chaty Int 86 097 V1 27 ° V27- 186 6000 V 1 7° N34 15.5 to RZS VOR: Via V-23, and FIM R-097 to FIM D 6000 W118 35.4 VOR, then FIM R-250 to Deano Int then RZS DEANO 17 V 5 86 9 10 N34 19.0 D22 R-109 to RZS VOR. Cross Charty Int at or 600 7 0 2 1 89 W119 25.0 above 5400'. 16 D 00° ° 16 Direct distance from Los Angeles Intl to: Chaty Int 20 NM CHATY N34 14.5 W118 35.0 AT OR ABOVE 5400' VENTURA
Expect clearance to filed altitude 3 minutes after departure.
(RWYS 6L/R AND 7L/R)(DME REQUIRED)
CHATY TWO DEPARTURE (CHATU2.CHATY)
CHATY TWO DEPARTURE (CHARTY2.CHARTY) (PILOT NAV) 9812020
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
E
°
V23
Figure 4-1 Typical Standard Instrument Departure with Transition Procedure
Page 4-2 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
NOTE: When stringing a SID procedure to an Enroute Transition or Enroute segment at their common waypoint, if speed and/or altitude constraints exist for this waypoint in both procedures, the constraint(s) from the SID procedure are retained. The SID altitude/airspeed constraint(s) will probably be lower/slower than the Enroute Transition or Enroute constraints. CAUTION: During Standard Instrument Departures, the FMS does not support the low speed flight regime of aircraft in which the bank angle is limited by the autopilot to 15 degrees as a function of airspeed and aircraft flap/slat configuration. Where required by the magnitude of the track angle change, the FMS may use up to a maximum of 30 degree bank angle in computing the roll steering command to the autopilot. Crews should therefore exercise caution when engaging LNAV in this flight regime and may wish to use the heading select mode until sufficient airspeed is allowing bank angles larger than 15 degrees. No difficulties are anticipated for engaging LNAV when track angle changes are less than 15 degrees.
SID SELECTION WHILE IN FLIGHT The FMS allows the activation in flight of an inactive route containing a SID, subject to the selection of the inactive runway. The FMS prefixes an inactive SID sequence with the corresponding inactive runway waypoint on activation in flight.
CONDENSED SID AND SID TRANSITION PROCESS This section provides an overview of the process of selecting the SID and SID transition procedures. The intent of each step is summarized on the next page. 1. MOD, ACT ROUTE - Select departure/arrival index page. 2. DEP/ARR INDEX - Select departure. 3. DEPARTURES - Select SID, SID transition,and/or runway. 4. MOD, ACT LEGS - Confirm the SID, SID transition and/or runway procedure agrees with the clearance, then execute the modified route. A detailed description of each FMS page is contained in Appendix A.
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Page 4-3 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
STANDARD INSTRUMENT DEPARTURE (SID) SELECTION This procedure is based on the SID and SID transition depicted in Figure 4-1 and assumes that only these portions of the departure are to be loaded at this time. CAUTION: When operating with departure published in TRUE heading reference, a runway must be selected otherwise unexpected CHECK TRUE/MAG REF alert could be generated. Display the DEP/ARR INDEX 1/1 page by pressing: • [DEP/ARR] (if on ground). • [DEP/ARR] (if airborne and midway point of active route not reached yet). • From ARRIVALS 1/1 page. • From DEPARTURES 1/1. NOTE: If the FMS is configured for two routes (RTE 1 and RTE 2), the origin and destination of the inactive route are also displayed. The active route information is displayed in white text. The inactive route origin and destination airport codes are displayed in cyan. Example of the DEP/ARR INDEX page when configured for two routes.
DEP/ARR INDEX ACT 1L
2L
1/1
RTE 1
KSEA
ARR>
PANC
ARR>
2R
KSEA
ARR>
3R
PANC
ARR>
4R
1R
RTE 2 3L
4L 5L
5R
6L
6R
Example of the DEP/ARR INDEX page when configured for three routes.
DEP/ARR INDEX ACT 1L
1/1
RTE 1
PANC ARR>
2L
1R 2R
RTE 2 3L
PANC ARR>
4L
3R 4R
RTE 3 5L
CYVR ARR>
6L
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5R 6R
Page 4-4 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 1. Display the DEPARTURES 1/X page by pressing the DEP prompt at LSK 1L or from RTE page when on ground and no departure selected. The DEPARTURES 1/X page is displayed, with the origin airport ICAO code included in the title line. Lists of SIDs and runways for that airport are displayed
KBFI DEPARTURES 1/1 SIDS
RTE 1
RUNWAYS
1L
LACRES
13R
2L
QUIET1
31L
1R 2R
3L
3R
4L
4R
5L
5R
6L
RTE VIA>
6R
2. Display the desired RUNWAY by pressing the PREV or NEXT key as required, and select the RUNWAY by pressing the appropriate right hand LSK. NOTE: Once a runway is selected, then only those SIDs applicable to that runway will be displayed. 3. Display the desired SID by pressing the PREV or NEXT key as required, and select the SID by pressing the appropriate left hand LSK. The SID list is replaced by the selected SID, with the legend "" beside the name. Transitions available for the selected SID are listed below the SID, under the heading "TRANS". If no transitions are available, the word "-NONE-" is displayed. If no runway was selected, a list of runways applicable to the selected SID appears on the right hand side of the page.
KBFI DEPARTURES 1/1 SIDS 1L
RTE 1
LACRES< S E L >
RUNWAYS 13R
TRANS
1R
2L
HUMPPS
2R
3L
ORTIN
3R
4L
VAMPS
4R
5L 6L
5R
RTE VIA>
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6R
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
4. Display the desired SID transition by pressing the PREV or NEXT key as required, and select the transition by pressing the corresponding left hand LSK.
KBFI DEPARTURES 1/1 SIDS 1L
RTE 1
LACRES< A C T >
RUNWAYS 13R
TRANS 2L
VAMPS
1R 2R
3L
3R
4L
4R
5L
5R
6L
RTE VIA>
6R
The list of transitions is replaced by the selected transition, with the legend "" beside the name. NOTE: Any selected element can be changed by pressing the appropriate left/right hand LSK to re-display the desired list (toggles the selection). 5. Display the first SID leg by pressing LEGS and PREV or NEXT as required. NOTE: For certain types of SID and SID transition, the selection of the runway may also be required before the SID waypoints are loaded into the route from the navigation database. The message “!SELECT TRANS/RUNWAY” is then displayed in the scratchpad. 6. Close-up any route discontinuity as described in Section 5. 7. Verify the course, distance, altitude/speed advisory, and procedural leg type information of each SID leg in turn by pressing NEXT as required to display all legs. NOTE: Pressing ERASE (LSK 6L) at any time during this procedure will cause all selections made up to that time to be deleted. 8. Make the selected SID and SID transition active by pressing EXEC. NOTE: On DEPARTURES page, the active SID and SID transition are now shown with the legend "" beside the name(s).
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SECTION 5 - ENROUTE
CONTENTS Subject
Page
CONDENSED EN-ROUTE PROCESS ...........................................................................................................5-1 LEAVING THE TERMINAL AREA..................................................................................................................5-3 DISPLAYING THE LEGS OF THE ROUTE....................................................................................................5-3 INSERTING WAYPOINTS ..............................................................................................................................5-4 A. PLACE/BEARING/DISTANCE WAYPOINTS .........................................................................................5-4 B. PLACE/BEARING-PLACE/BEARING WAYPOINTS ..............................................................................5-4 C. ALONG-TRACK WAYPOINTS ................................................................................................................5-5 D. LATITUDE/LONGITUDE WAYPOINTS ...................................................................................................5-5 E. NAVIGATION DATABASE WAYPOINTS ...............................................................................................5-6 ROUTE DISCONTINUITIES............................................................................................................................5-6 ROUTE DISCONTINUITY CLOSE-UP ...........................................................................................................5-7 WAYPOINT DELETION ..................................................................................................................................5-7 A. BY CLOSE-UP METHOD ........................................................................................................................5-7 B. BY CLEAR KEY .......................................................................................................................................5-8 FLY-OVER AND FLY-BY WAYPOINTS.........................................................................................................5-8 A. TO CONVERT TO FLY-OVER FROM FLY-BY .......................................................................................5-8 B. TO CONVERT TO FLY-BY FROM FLY-OVER .......................................................................................5-9 LEG SEQUENCING ........................................................................................................................................5-9 A. FLY-BY WAYPOINTS ..............................................................................................................................5-9 B. LARGE COURSE CHANGES..................................................................................................................5-9 C. FLY-OVER WAYPOINTS.......................................................................................................................5-10 ETA AND EFA...............................................................................................................................................5-12 WAYPOINT WIND ENTRY AND ETA ..........................................................................................................5-13 4-LEVEL WIND OPTION...............................................................................................................................5-15 WAYPOINT LATITUDE/LONGITUDE DISPLAY..........................................................................................5-18 PROGRESS ALONG THE ROUTE (DISTANCE-TO-GO, ETA) ..................................................................5-19 REQUIRED TIME OF ARRIVAL COMPUTATION .......................................................................................5-20 WIND COMPONENTS, NAVIGATION ANGLES AND AIR DATA ..............................................................5-21 OFFSET TRACK INITIATION .......................................................................................................................5-21 OFFSET TRACK CANCELLATION .............................................................................................................5-22 AIRWAY INTERCEPT...................................................................................................................................5-23 POSITION FIX INFO DISPLAY.....................................................................................................................5-23 DOWNTRACK FIX CREATION ....................................................................................................................5-24 CURRENT NAVIGATION MODE STATUS ..................................................................................................5-26 GPS SENSOR AND SATELLITE STATUS ..................................................................................................5-26 PREDICTIVE RAIM REQUESTS ..................................................................................................................5-27 PREDICTIVE RAIM SATELLITE DESELECTION........................................................................................5-28 WAYPOINT INFORMATION FROM THE NAVIGATION DATABASE ........................................................5-29 DUPLICATE IDENTIFIER SELECTION .......................................................................................................5-29 RNP MODIFICATION....................................................................................................................................5-31 NEAREST......................................................................................................................................................5-32 TIMER (If configured) ..................................................................................................................................5-34
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This Page Intentionally Left Blank
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SECTION 5 ENROUTE CAUTION: FMS operations above latitude N85 and below latitude S85 are expected to be limited to flying fixto-fix legs (great circle tracks), including fly-by leg transitions. Procedures using angular references are therefore not intended to be conducted in these areas. CONDENSED EN-ROUTE PROCESS This page sequence gives an overview of the main FMS pages used enroute. The intent of each step is summarized on the next page.
ACT
RTE 1 LEGS
299o
1/2
39.6N M
CAFTA ACT RTE 1 LEGS ETA 1/2 298o 154N M ETA WIND YZP FL350B CAFTA 1 9 1 6 . 4 Z4 5 3. 00 0N TM/ 9 0 320o ACT RTE 1 LEGS POS 1/2 YZP01 YZP 1950.2Z 300T/ 90 THEN CAFTA PROGRESS 1/4 MOCA1 D I S22C08O00N0TT1.I87NTZU IY3TQ0YD03TT-6/G4N39M0 8 7 3E2T A - - R O U T EYZP CAFTA1 8 T Y Q 3 25T 2. 42 0 6 6 71 28 1 7 < KILLA 90 BKA 228004T 4 . 5 Z 3 0 0 /PROGRESS 2/4 MOCA1 TOU LEGS 8 8 . 3 N M 1830.5Z ATA FTR OYMPOS> 1 9 Q 2 T 2 2 2 A8L7T3F2T 2 1 2 7 . 0WZI N3D0 0 / 9 0 T K / G S KILLA SEA 1300 1803 BKA TRUE T >020T1/9TT45 T 28 / 2 2 8 K TE T E 1. O YKQ D1 T8G7 3 6 4 3 3 2 ACT RTA PROGRESS 3/4 T2 K NE M/ X 0 T0 K+ 1 7 . 9 < ARRIE__ . KILLA R T A W1P7 RTA TT TQ R3060403 /8L703.20 0 N M 1 9NTE XY CAFTA 1938.0Z 2. R N P / TOU ANP H S. I 7 NS MC A 0 LPROGRESS E+ 3 0 . 5 4/4 0 DIS 3.
1 . 0 0 / 0 D. E0 S5TN M H E A D W1I.N0DN M CROSSWIND 288N M 248K T N A V PANC MODE 027 K9TN M 0 5 + 4 7 . 2 R44K T 1 2 7 RTA WIND
5. ALT(CORR) 3424F T
6. 7.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
NOTE: Progress pages can be in a set of 3 or 4 (depending on configuration). 1. LEGS - displays each route leg and waypoint. Waypoints may be modified or created, and directto/intercept, fly-over or holding procedures performed on these pages. 2. LEGS ETA - displays ETA for each waypoint on the corresponding LEGS page. 3. LEGS POS - displays latitude-longitude coordinates of each leg termination. Also displays RNP value for the leg, if any is defined in the Navigational Database. 4. PROGRESS 1/4 - displays current active waypoint, distance to go (DTG), course, estimated time of arrival (ETA), next waypoint, wind, current track and ground speed (TK/GS), track angle error and cross track (TKE/XTK), Required and Actual Navigation Performance (RNP/ANP), navigation display cross-track deviation scaling, and Navigation Mode. If entered, the Flight Number is displayed on the page title. 5. PROGRESS 2/4 - displays identifier of the last (FROM) waypoint overflown, its crossing altitude (ALT) and actual time of arrival (ATA). Displays the distance to go (DTG), estimate time of arrival (ETA), for the ACTIVE, NEXT and DESTINATION waypoints of the route. This page also displays the tuned VOR identifier(s) and frequency(ies) (based on the selected configuration). If entered, the Flight Number is displayed on the page title. 6. RTA PROGRESS 3/4 - used to compute the TAS required to reach a waypoint at a required time of arrival (RTA). After entry of RTA waypoint, page allows a WIND entry used to refine recommended RTA TAS computations. 7. PROGRESS 4/4 - displays the wind components (HEADWIND or TAILWIND, CROSSWIND), Heading and Drift Angle (HDG/DA), True Air Speed (TAS), Magnetic Variation, System Altitude in feet (ALT), System Altitude in meters (when configured) and QNH Altimeter setting (QNH SET). If entered, the Flight Number is displayed on the page title. NOTE: Refer to Performance VNAV (Section 18) for Performance VNAV variations of PROGRESS pages. or: If the 3-page set of PROGRESS pages is configured then above steps 4, 5, 6, and 7 are replaced with: 4. PROGRESS 1/3 - displays identifier of the last (FROM) waypoint overflown, its crossing altitude (ALT) and actual time of arrival (ATA). Displays the distance to go (DTG), estimate time of arrival (ETA), for the ACTIVE, NEXT and DESTINATION waypoints of the route. Also displays Required and Actual Navigation Performance (RNP/ANP), navigation display cross-track deviation scaling, and Navigation Mode. If entered, the Flight Number is displayed on the page title. 5. PROGRESS 2/3 - used to compute the TAS required to reach a waypoint at a required time of arrival (RTA). After entry of RTA waypoint, page allows a WIND entry used to refine recommended RTA TAS computations.
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6. PROGRESS 3/3 - displays the wind components (HEADWIND or TAILWIND, CROSSWIND), True/ Magnetic Wind, True Air Speed (TAS), Heading and Drift Angle (HDG/DA), Track and Ground Speed (TK/GS), Magnetic Variation, Track Angle and Cross-track error (TKE/XTK), System Altitude in feet (ALT), System Altitude in meters (when configured) and QNH altimeter setting (QNH SET). If entered, the Flight Number is displayed on the page title. Detailed descriptions of each display page are contained in Appendix A. Sections 6 and 7 describe arrival and approach procedures. Direct-to and holding pattern procedures are contained in Sections 9 and 10 respectively.
LEAVING THE TERMINAL AREA On leaving the terminal area, when the radial distance from the departure airport becomes greater than 33 nm or the aircraft climbs above 16,000 feet above airport elevation, the FMS transitions from terminal to en-route phase of flight, with the following indications: 1. HSI lateral deviation sensitivity changes from 1 nm to 2 nm full scale over a ten (10) second period. NOTE: Enroute lateral deviation sensitivity may vary depending of the values supported by the HSI. Refer also to Section 15, RNP. 2. On the PROGRESS 1/3 or 1/4 page the RNP value changes from 1 nm to 2 nm.
DISPLAYING THE LEGS OF THE ROUTE Display the ACT RTE x LEGS 1/X page by pressing the [LEGS] functional key. The active leg and the next four legs are displayed. NOTE: Depending on the configuration, the active waypoint identifier is displayed in magenta or reverse video magenta or reverse video green. Display all the flight plan legs in sequence by pressing [NEXT] as often as required. NOTE: The maximum number of waypoints in a flight plan allowed by the system is 199 (e.g. maximum of 40 LEGS page can be used). The legs of the inactive route can also be viewed in the RTE x LEGS 1/X page by pressing the prompt (LSK 6L) on the ACT RTE x LEGS page. NOTE: The pages related to an inactive route are displayed in cyan.
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INSERTING WAYPOINTS A. PLACE/BEARING/DISTANCE WAYPOINTS With the desired reference waypoint identifier in the scratchpad by keyboard entry or LSK action: 1. Key the bearing and distance separated by a slash (/), into the scratchpad. e.g.: YZP320/45. 2. Display the desired insert location in the route by pressing [LEGS], and [NEXT] or [PREV] as required. Move the waypoint to the desired place in the route by pressing the appropriate LSK. The new waypoint is inserted ahead of the existing waypoint. The new waypoint identifier is created with a name based on the first three characters of the reference waypoint identifier followed by a sequence number, e.g.: YZP01. 3. Verify the waypoint entry by checking the course and distance of the previous and next legs.
MOD 1L 2L 3L
RTE 1 LEGS
2/4
299o
39.6N M
298o
154N M
CAFTA YZP01
2R
THEN -- ROUTE DISCONTINUITY -
4L
MOCA1
5L
BKA
6L
306o
1R
165N M
3R 4R 5R
LEGS ETA>
6R
4. Make the modified route active by pressing [EXEC]. NOTE: The system allows for a maximum of 99 temporary waypoints in a flight plan. B. PLACE/BEARING-PLACE/BEARING WAYPOINTS With the first reference waypoint identifier in the scratchpad: 1. Key into the scratchpad the bearing of the waypoint from the first reference waypoint followed by a slash (/) and the second reference waypoint and bearing e.g. CAFTA268/YZP148. 2. Display the desired insert location in the route by pressing [LEGS] and [NEXT] or [PREV] as required. 3. Move the waypoint to the desired place in the route by pressing the appropriate LSK. The new waypoint is inserted ahead of the existing waypoint. The new waypoint identifier is created based on the identifier of the first reference waypoint as described in the previous procedure, e.g. CAF01. 4. Verify the waypoint entry by checking the course and distance of the previous and next legs.
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5. Make the modified route active by pressing [EXEC]. Waypoints entered by means of place/bearing-place/bearing will be displayed as place/bearing/distance waypoints, based on the first reference waypoint. NOTE: The system allows for a maximum of 99 temporary waypoints in a flight plan. C. ALONG-TRACK WAYPOINTS An along-track waypoint lies on the inbound (outbound) course to (from) the reference waypoint at the selected distance. No course change occurs at the along-track waypoint. With the reference waypoint identifier in the scratchpad: 1. To enter a new waypoint AFTER the reference waypoint, key in /, and distance, e.g. KILLA/20. or: 2. To enter a new waypoint BEFORE the reference waypoint, key in /, [+/-], distance, e.g. KILLA/-20. or: 3. To move an initial DME ARC fix along the arc, key in /, desired radial from the DME station, e.g. D173J/203. then: 4. Display the reference waypoint location in the route by pressing [LEGS] and [NEXT] or [PREV] as required. 5. Move the waypoint to the reference waypoint in the route by pressing the appropriate LSK. NOTE: All along-track waypoints must be inserted at the reference waypoint location, independently of their actual relative position relative to that waypoint. 6. Verify the waypoint entry by checking the course and distance of the previous and next legs. 7. Make the modified route active by pressing [EXEC]. NOTE: If the leg created by the along-track waypoint overlaps an adjacent waypoint, such that a course reversal is created, the along-track waypoint is not accepted and the data entry error message "!OUT OF RANGE" is displayed. D. LATITUDE/LONGITUDE WAYPOINTS 1. Key the coordinates into the scratchpad (LATITUDE, LONGITUDE) e.g. N60W146. NOTE: Coordinates must be entered with whole degrees and optionally whole minutes with a resolution of up to 0.01 minutes. 2. Display the desired insert location in the route by pressing [LEGS] and [NEXT] or [PREV] as required. 3. Move the waypoint to the desired place in route by pressing the appropriate LSK. 4. Verify the waypoint entry by checking course and distance of the previous and next legs.
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5. Make the modified route active by pressing [EXEC]. The waypoint name is automatically named "WPT" followed by a sequence number (e.g. WPT01). Alternatively, the waypoint name can be automatically named using the latitude and longitude degree components (e.g. N60W120). This option is selectable through configuration pages. NOTE: The system allows maximum 99 temporary waypoints in a flight plan. E. NAVIGATION DATABASE WAYPOINTS 1. Key the new waypoint identifier into the scratchpad. 2. Display the desired insert location in the route by pressing [LEGS] and [NEXT] or [PREV] as required. 3. Move the waypoint to the desired place in the route by pressing the appropriate LSK. If the identifier is not found in the navigation database, the message "!NOT IN DATABASE" will be displayed in the scratchpad. 4. Verify the waypoint entry by checking course and distance of the previous and next legs. 5. Make the modified route active by pressing [EXEC].
ROUTE DISCONTINUITIES Under normal conditions, the active route will form a continuous path of linked waypoints (legs). However, a ROUTE DISCONTINUITY will be inserted into the flight plan at the end of a procedure/airway if it cannot be linked with the next procedure/airway, when the entered waypoint is not part of the existing active flight plan or following a manually-sequenced leg (ex: radar vector). Under these conditions, “THEN” followed by a boxed data field and ROUTE DISCONTINUITY lines are inserted immediately after the new waypoint. Along-track waypoints do not create a ROUTE DISCONTINUITY.
MOD
RTE 1 LEGS
2/4
299o
39.6N M
298o
154N M
320o
45.0N M
1L
CAFTA
2L
YZP
3L
YZP01
4L
5L
KILLA
6L
300-320 FL350B
1R 2R 3R
THEN -- ROUTE DISCONTINUITY -
4R 5R
LEGS ETA>
6R
A ROUTE DISCONTINUITY can be inserted into the flight plan by selecting RTE DISCON on the INIT/REF 2/2 " in the scratchpad. Insert the page. The active or inactive RTE x LEGS page will be displayed with " " into the flight plan by pressing the appropriate left LSK. The ROUTE DISCONTINUITY will be inserted " before the selected waypoint.
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ROUTE DISCONTINUITY CLOSE-UP CAUTION: Close-ups can occur only upwards, e.g. moving a downtrack waypoint to an earlier location. Moving a waypoint downwards (e.g. to a later location) causes the waypoint to be DUPLICATED into the new location. A discontinuity that follows a manually-sequenced leg (e.g. radar vector) cannot be removed unless the associated leg is also removed With ACT (or MOD) LEGS page displayed showing "THEN" and "ROUTE DISCONTINUITY" lines: 1. Display the next desired waypoint in the route by pressing [NEXT] as required. 2
Key in, or copy the waypoint identifier into the scratchpad by pressing the appropriate LSK.
3. Display the page with the THEN box data field by pressing [PREV] as often as required. 4. Move the waypoint to the THEN field by pressing the appropriate LSK except for discontinuity following a manual leg (e.g. radar vector). In the latter case, the discontinuity needs to be removed using a close-up on the manual vector itself. 5. Verify the entry by checking course and distance of the previous and next legs. 6. Make the modified route active by pressing [EXEC]. NOTE: To minimize keystrokes, the close-up of a route discontinuity should be performed before EXECuting the route modification which causes it.
WAYPOINT DELETION A. BY CLOSE-UP METHOD 1. Display the waypoint to be deleted by pressing [LEGS] and [NEXT] or [PREV] as required. 2. Copy the waypoint identifier following the one to be deleted into the scratchpad by pressing appropriate LSK.
the
3. Move the waypoint to the location of the waypoint to be deleted by pressing the appropriate LSK. The selected waypoint is deleted from the route. 4. Verify the entry by checking the course and distance of the previous and next legs. 5. Make the modified route active by pressing [EXEC]. NOTE: In this case, a ROUTE DISCONTINUITY is not created. "Close up" is the simplest method to delete a number of consecutive waypoints, but this can also be performed by a series of [CLR] key operations.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
B. BY CLEAR KEY 1. Start the deletion by pressing [CLR]. "DELETE" message is displayed in the scratchpad. NOTE: "DELETE" is displayed only when the scratchpad is empty. 2. Display the desired waypoint by pressing [LEGS], and [NEXT] or [PREV] as required. 3. Delete the selected waypoint by pressing the appropriate LSK. A "ROUTE DISCONTINUITY" is inserted in place of the deleted waypoint. Any holding pattern associated with the deleted waypoint will also be deleted. 4. Verify the entry by checking course and distance of the previous and next legs. 5. Make the modified route active by pressing [EXEC].
FLY-OVER AND FLY-BY WAYPOINTS Waypoints are loaded into the route as fly-by (with turn anticipation) or fly-over (no turn anticipation) as coded in the navigation database. By default, all waypoints, including manually-entered temporary waypoints, are initially defined as fly-by unless specifically coded as fly-over. Any waypoint can be converted from one type to the other, with the exception that the missed approach waypoint is always defined as a fly-over waypoint and cannot be modified. With any ACT or MOD RTE x LEGS page displayed: A. TO CONVERT TO FLY-OVER FROM FLY-BY 1. Display the INIT/REF 2/2 page, and select "FLY-OVER" by pressing [INIT REF], [NEXT]. The ACT RTE x LEGS 1/X page is displayed with "/O" in the scratchpad. or: Key in "/O". 2. Display the desired waypoint by pressing [LEGS], and [PREV] or [NEXT] as required (on the active or inactive route). 3. Move the "/O" to the waypoint location by pressing the appropriate left hand LSK. The legend "/O" is displayed to the right of the waypoint name. 4. Make this route modification active by pressing [EXEC]. The waypoint is now defined as a fly-over waypoint and turn anticipation is inhibited for that waypoint only. The switch to the next leg will occur automatically on crossing over or abeam the waypoint.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
B. TO CONVERT TO FLY-BY FROM FLY-OVER CAUTION: Special care should be taken if any fly-over waypoint extracted from the navigation database is converted to fly-by (particularly the final approach fix and missed approach holding fix). The crew will remain responsible at all times for remaining within protected airspace, and for compliance with all altitude constraints. 1. Display the desired waypoint by pressing [LEGS] and [PREV] or [NEXT] as required. 2. Key in “/”, and move the “/" to the waypoint location by pressing the appropriate left hand LSK. The legend "/O" is removed from the waypoint name. 3. Make this route modification active by pressing [EXEC]. The waypoint is now defined as a fly-by waypoint and turn anticipation will occur at the appropriate distance prior to reaching that waypoint. NOTE: An inactive route waypoint can also be converted to "FLY-OVER". NOTE: The missed approach waypoint is always defined as a fly-over waypoint, and cannot be converted to fly-by. Any holding pattern defined at a waypoint is cancelled if that waypoint is converted to a fly-over waypoint.
LEG SEQUENCING A. FLY-BY WAYPOINTS The FMS sequences fly-by waypoints when crossing the bisector of the active leg and next leg, or when passing the wayline of the active leg, whichever occurs first. In certain exceptional cases where the next leg is short, sequencing may occur based on crossing the wayline of the next leg, if that is the first situation to occur. If the aircraft is performing a downwind approach to a runway, sequencing of the FAF will only be possible after the aircraft has turned towards the runway. During the first half of the fly-by leg transition, between the initial turn point and the leg switching point (bisector), the active waypoint is displayed in white reverse video on the LEGS and PROGRESS pages. CAUTION: If the active flight path presents unreasonable geometry (combination of ground speed, track changes and closely located waypoints that prevent the definition of a flyable path) the crew should be ready to disengage the LNAV. B. LARGE COURSE CHANGES Regardless of the phase of flight, a fly-by leg transition involving a course change greater than 125 degrees that is not part of a published procedure, will trigger the COURSE CHANGE>125 AHEAD status advisory scratchpad message (via FMS configuration, this message can alternatively be configured as a system alert message).
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
C. FLY-OVER WAYPOINTS The FMS sequences fly-over waypoints when passing the wayline of the active leg. Refer to Figure 5-1 for an example.
ACT
RTE 1 LEGS
2/4
299o
39.6N M
298o
154N M
1L
CAFTA
2L
YZP
3L
MOCA1
4L
BKA
5L
KILLA
6L
/o
307o
86.7N M
306o
165N M
282o
197N M
1R 2R 3R 4R 5R
LEGS ETA>
6R
NOTE: For both fly-by and fly-over waypoints, when the installed display system supports a turn direction symbol, the FMS will display the turn point and direction for the active leg (and down- path transitions in some configurations), when the latter is not represented by a circular path and has a significant course change. Depending on the installed EFIS model, the turn information may also be displayed for down-path forced direction turns involving course change exceeding 170 degrees. The turn information is also displayed for procedural waypoints.
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
Figure 5-1 Bi-Sector and Circular Transition
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OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
ETA AND EFA Display the desired waypoint in the route by pressing [LEGS], [PREV] or [NEXT] as required. 1. Display the ACT RTE x LEGS ETA 1/X or RTE x LEGS ETA 1/X page by pressing (LSK 6R).
ACT RTE 1 LEGS ETA 1/4 1L
CAFTA
ETA 1916
EFA(K G ) 1328
2L
YZP
1950
1185
3L
MOCA1
2000
1179
4L
BKA
2044
950
4R
5L
KILLA
2127
792
5R
6L
LEGS WIND>
1R 2R 3R
6R
ETAs are based on measured wind and forecast waypoint winds (performance data is also used if it is available). While on ground, ETEs are displayed instead of ETAs and they are based on the CRZ TAS as entered in the PLAN DATA page. EFAs are based either on the current fuel flow and ground speed if a fuel computer is configured or on the fuel flow entered by the pilot on the FUEL 1/2 page. NOTE: Refer to Performance VNAV (Section 18) for details on the basis of the ETE/ETA/EFA calculations when Performance VNAV is enabled. 2. Return to the previously displayed RTE x LEGS page by pressing [LEGS] or the prompt at LSK 6L. NOTE: Lateral flight plan modifications are not permitted on the RTE X LEGS ETA page.
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Page 5-12 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
WAYPOINT WIND ENTRY AND ETA Display the desired waypoint in the route by pressing LEGS, PREV or NEXT as required. NOTES: • The figure below reflects the single wind entry per waypoint configuration. If the FMS is configured for the 4Level Wind Option, refer to next sub-section. • When Performance VNAV is configured, by default 4-Level Wind is enabled. Refer to Performance VNAV (Section 18) for further details. 1. Display ACT RTE LEGS WND 1/X page by pressing [LEGS], and .
ACT RTE 1 LEGS WND 2/4 ETA 1916
WIND 000T/ 0
1L
CAFTA
2L
YZP
1950
000 /
0
3L
MOCA1
2000
000T/
0
4L
BKA
2044
000T/
0
4R
5L
KILLA
2127
000T/
0
5R
6L
T
LEGS POS>
1R 2R 3R
6R
ETAs are based on measured wind and forecast waypoint winds (performance data is also used if available). While on ground, ETEs are displayed instead of ETAs and they are based on the CRZ TAS as entered in the PLAN DATA page. NOTE: Wind entries are shown in large fonts while propagated winds are shown in normal font size. The measured wind information is blended with these forecast winds for computation of downtrack ETAs. The FMS linearly blends the current wind ahead of the aircraft for 250nm. Beyond that distance, the FMS does not use the measured wind and uses only forecast winds.
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Page 5-13 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
2. Enter the forecasted true wind, e.g. 80/50, at a waypoint, e.g. MOCA1 (LSK 3R). propagated forward until the next waypoint with a wind entry or until the end of route.
This wind will be
NOTE: Forecast winds are linearly interpolated between waypoints.
MOD RTE 1 LEGS WND 2/4 1L
CAFTA
ETA 1916
WIND 000T/ 0
2L
YZP
1950
000T/
3L
MOCA1
2000
080T/ 50
4L
BKA
2044
080T/ 50
4R
5L
KILLA
2127
080T/ 50
5R
6L
LEGS POS>
6R
0
1R 2R 3R
3. Confirm wind entry by pressing the EXEC key. 4. Return to the previously displayed LEGS page by pressing LEGS or the LEGS prompt at LSK 6L. NOTE: Lateral flight plan modifications are not permitted on the LEGS ETA/WND page. In addition to predicted winds, the FMS uses predicted TAS to compute ETA and ETE at each waypoint. The predicted TAS is computed by linear blending of measured TAS at aircraft position and cruise TAS entry.
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Page 5-14 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
4-LEVEL WIND OPTION The FMS provides a configurable option allowing entering forecast winds at four different flight levels. The same four levels are used for all waypoints. However, each waypoint can have its specific wind entries. 1. Display ACT RTE LEGS WND 1/X page by pressing [LEGS], and .
ACT RTE 1 LEGS WND 1/4 ETE 00+49
WIND 000T/ 0>
1R
1L
CAFTA
2L
YZP
01+05
300 / 90►
2R
3L
MOCA1
01+15
300T/ 85>
3R
4L
BKA
01+22
290 / 20>
4R
5L
KILLA
01+42
280T/ 15>
5R
6L
LEGS POS>
6R
T
T
2. Press the right hand side LSK corresponding to the waypoint where the wind entry is required, e.g. CAFTA.
ACT CAFTA 1L
ALT F L ---
WIND
2/17
DIR/SPD 1R
2L
2R
3L
3R
4L
4R
5L
5R
6L
LEGS WIND>
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6R
Page 5-15 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
3. Enter the flight level in the scratchpad, e.g. 100, and then press LSK 1L.
MOD CAFTA 1L
ALT FL---
WIND
2/17
DIR/SPD 1R
2L
2R
3L 4L
3R F L 100
T
000 /
0
5L 6L
4R 5R
LEGS WIND>
6R
4. Enter the wind direction and speed at LSK 4R, e.g. 090/70. 5. Repeat the procedure for up to 4 winds. Press the EXEC key to complete the wind entry. NOTE
The first wind entry is displayed on line 4. Upon entry of subsequent flight level, the entries get re-ordered by decreasing flight level from line 1 to line 4.
ACT CAFTA 1L 2L 3L 4L
ALT F L 200 F L 150 F L 125 F L 100
WIND
2/17
DIR/SPD
140T / 3 0 T
135 / 40 T
100 / 50 T
090 / 70
5L 6L
1R 2R 3R 4R 5R
LEGS WIND>
6R
NOTE: A wind entry at a given flight level is propagated forward at the same flight level to the end of the route, or until the occurrence of the next forecast wind at the same flight level. 6. Use the NEXT key to advance to the next waypoint, e.g. page 2/5 YZP. procedure if a change of wind is predicted at the specified flight level.
Repeat the DIR/SPD entry
NOTE: The wind entry is shown in a large font size at the page where first entered. The propagated winds on other pages are shown in normal font size.
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Page 5-16 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
7. The flight level can be changed at any waypoint. scratchpad.
Press the CLR key.
DELETE is displayed in the
Delete the flight level by pressing either LSK 1L, 2L, 3L, or 4L. Next, re-enter a new flight level and wind as described above. NOTE: The new flight level and wind is propagated throughout the flight plan. The same four flight levels are used throughout the flight plan, but each waypoint can have its specific wind entries. 8. Return to the LEGS WIND page by pressing LSK 6R. Waypoints where a wind entry was made have a filled-in prompt, whereas where no entry was made, the prompt is a “greater than” symbol. 9. On the LEGS WND page, the displayed wind data is the result of the blending of measured wind at aircraft position with waypoint wind. This blended wind is used for the calculation of ETAs.
ACT RTE 1 LEGS WND 2/4 ETA 1916
WIND 140T/ 30>
1R
1L
CAFTA
2L
YZP
1950
140 / 30>
2R
3L
MOCA1
2000
140T/ 30>
3R
4L
BKA
2044
140 / 30>
4R
5L
KILLA
2127
140T/ 30>
5R
6L
LEGS POS>
6R
T
T
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Page 5-17 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
WAYPOINT LATITUDE/LONGITUDE DISPLAY Display the coordinates for each waypoint by pressing [LEGS], (LSK 6R), (LSK 6R).
ACT RTE 1 LEGS POS 1/2 1L
CAFTA
2L
YZP
3L
MOCA1
4L
BKA
5L
KILLA
RNP 1.00N M . N51o17.72 W129o05.32 RNP 1.00N M N53o15.13 W131o48.42 N54o30.18 W133o01.90 N56o51.57 W135o33.08
1R 2R 3R 4R 5R
N58o44.98 W140o35.10
6L
LEGS>
6R
Return to the LEGS page by pressing [LEGS] or the prompt (LSK 6R). NOTES: 1. Flight plan waypoint modifications are not permitted on the RTE x LEGS POS Y/X page. 2. The position displayed on the ACT RTE x LEGS POS or RTE x LEGS POS page depends on the selection for the coordinate system made on the SETUP 1/1 page. 3. RNP value for the leg is also displayed if a value is defined in the Navigational Database.
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Page 5-18 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
PROGRESS ALONG THE ROUTE (DISTANCE-TO-GO, ETA) NOTE: Similar information is available on PROGRESS 1/3 and PROGRESS 2/3 page, when the FMS is configured for the 3-page set of PROGRESS pages. NOTE: Layout of PROGRESS pages is substantially different when Airbus A300/A310 Performance VNAV function is enabled. Refer to section 18A accordingly. Display the PROGRESS 1/4 page by pressing [PROG].
PROGRESS 280T
1L 2L 3L 4L 5L 6L
DTGN M 35.2
ARRIE 280T
TOU /o TRUE W I N D >020T/ 45K T RNP/ANP 1.00/0.05N M NAV MODE
1/4 ETA 1817<
88.3
1830 TK/GS 281T/228K T XTK L0.00N M DEV SCALE 1.0N M
1R 2R 3R 4R 5R 6R
1. When operating outside the polar area, the crew can toggle the display reference of the wind direction to either TRUE or MAGNETIC by pressing LSK 3L. Upon entry in the polar area, the wind direction reference is forced to TRUE and the toggling is inhibited. 2. Display PROGRESS 2/4 page by pressing [NEXT].
PROGRESS FROM
1L
SEA
2L
ARRIE
3L
TOU
4L
PANC
TO
2/4
ALTF T 1300 DTGN M 17.2
ATA 1803 ETE 00+17<
1R
68.7
00+30
3R
1279
05+47
4R
NEXT DEST
2R
5L
5R
6L
6R
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Page 5-19 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
PROGRESS 1/4 and 2/4 pages always show the information for the currently active route. Route modifications which have not yet been EXECuted are ignored. NOTE: When established in a hold, the active waypoint course is replaced by the title "HOLD AT". The ATA is the time of entry of the hold, on the first crossing of the holding waypoint. The distance-to-go to the active waypoint is from present position direct to the holding waypoint. The ETA to the active waypoint is for the next crossing of the holding waypoint. The ETAs and distances to go for the next and destination waypoints are based on the holding waypoint location and current TAS.
REQUIRED TIME OF ARRIVAL COMPUTATION
With the desired waypoint identifier in the scratchpad: Display the RTA PROGRESS 3/4 or 2/3 page by pressing [PROG], [PREV], [PREV] or [PROG], [NEXT] respectively. 1. Move the waypoint identifier into the RTA WPT field by pressing LSK 1L.
ACT
RTA PROGRESS
RTA WPT
1L 2L 3L
CAFTA
RTA TAS 248K T RTA WIND 020T / 45K T
3/4
RTA 1938:10 DIS 288N M
1R 2R 3R
4L
4R
5L
5R
6L
6R
2. Key in the required time of arrival (e.g.: 1938) and move the entry into the RTA field by pressing RTA (LSK 1R). The computed ETA is replaced by the manual entry of RTA, displayed in LARGE font. The required TAS to reach the RTA waypoint at the required time is computed. RTA WIND is current wind or CRZ WIND if on the ground. Manual entry of the RTA TAS will result in a new ETA. Manual entry of RTA WIND alters the evaluation of the ETA for the given waypoint.
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Page 5-20 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
WIND COMPONENTS, NAVIGATION ANGLES AND AIR DATA Display the PROGRESS 3/3 or 4/4 page by pressing [PROG] and [PREV]. PROGRESS 3/3 or 4/4 page includes the display of wind, aircraft heading, drift angle, true air speed, magnetic variation, altitude, QNH altimeter setting and QNH Altimeter Ref (if configured). NOTE: Information related to QNH altimeter settings is located in Section 17. The HEADWIND (TAILWIND) field displays the present headwind or tailwind components in knots. The sense of the CROSSWIND component is the side FROM which the wind is blowing.
PROGRESS 1L 2L 3L 4L 5L 6L
HEADWIND 027K T HDG/DA 290o/ L11o MAGVAR E019.9o
4/4
CROSSWIND R44K T TAS 240K T
1R 2R 3R 4R
ALT(CORR) 34245F T QNH SET
5R
>2 9 . 9 2 I N H G
6R
OFFSET TRACK INITIATION Display the ACT RTE x 1/X page by pressing [RTE].
ACT
RTE 1
1/3
ORIGIN
DEST
RUNWAY
FLT NO
1L
KSEA
2L
-----
PANC
KL007
ROUTE
1R 2R
3L
KSEAPANC1
3R
4L
CO RTES>
4R
5L 6L
5R
OFFSET
R0.0N M
6R
1. Enter the desired track offset in nautical miles (e.g.: L10.0) and move the entry into the OFFSET field by pressing LSK 6R.
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Page 5-21 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
2. Initiate the capture of the offset track by pressing [EXEC]. Navigation and guidance will now be relative to the offset track. If the FMS is autopilot-coupled, the FMS will capture the offset track at a 45 degree angle if the offset value is greater than the normal cross-track limit. Offset route waypoints are located on the bisector of the angle between the original route legs. The OFST annunciator of the FMS illuminates.
OFFSET TRACK CANCELLATION Automatic Cancellation: An active offset path is automatically cancelled upon any of the following conditions: •
Active leg is not a TF (track to fix) or DF (direct to fix) leg; or
•
A direct-to/intercept is executed; or
•
Active leg is part of an approach; or
•
Holding Pattern defined on the active waypoint; or
•
Next leg is a DME arc
•
Active waypoint is designated as fly-over
Manual Cancellation: Display the ACT RTE x 1/X page by pressing [RTE]. 1. Set the offset value to zero by entering 0 (zero) into the scratchpad and moving it into the OFFSET field by pressing LSK 6R. or: 2. Delete the offset value by pressing [CLR] and then LSK 6R. 3. Initiate return to the original track by pressing [EXEC]. The advisory message "END OF OFFSET" is displayed in the scratchpad. The FMS OFST annunciator is turned off. Navigation and guidance will now be relative to the original track. If autopilot-coupled, the FMS will capture the original track at a 45 degree angle if the offset value was greater than the normal cross-track limit.
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Page 5-22 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
AIRWAY INTERCEPT Refer to section 9 (Direct-To with Intercept Course function).
POSITION FIX INFO DISPLAY With the desired waypoint identifier in the scratchpad: Display the FIX INFO 1/1 page by pressing [FIX] or [INIT REF], .
FIX
1L
ANN
FIX INFO
1/1
CRS/DIS o 310 / 456N M
REF
TO<
1R
3L
-- DOWNTRACK FIXES -RAD/DIS DTG ETA ---o/ - - - N M
4L
--- / - - - N M
4R
5L
5R
2L
o
6L
2R 3R
6R
1. Enter the waypoint identifier in the scratchpad and move it into the FIX field by pressing LSK 1L. The bearing (radial) and distance FROM the FIX to the aircraft are displayed. The displayed reference of the bearing (radial) (e.g. true or magnetic North) is consistent with the other navigation angles as described in the SETUP page in Section 3. 2. Display the reciprocal by pressing REF (LSK 1R).
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Page 5-23 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
DOWNTRACK FIX CREATION With the desired reference waypoint identifier in the scratchpad: Display the FIX INFO 1/1 page by pressing [FIX] or [INIT REF], . 1. Move the waypoint identifier into the "fix" field by pressing LSK 1L.
FIX
1L
ANN
FIX INFO
1/1
CRS/DIS o 310 / 466N M
REF
TO<
1R
3L
-- DOWNTRACK FIXES -RAD/DIS DTG ETA 175o/ 80 N M 4 2 0 N M 2033
4L
---o/ - - - N M
4R
5L
5R
6L
6R
2L
2R 3R
2. To create a downtrack fix along the flight plan where the radial from the entered "fix" intersects, key in the radial (e.g. 175) and press LSK 3L or LSK 4L. or: 3. To create a downtrack fix along the flight plan where the distance from the entered "fix" intersects, key in /, distance (e.g. /80) and press LSK 3L or LSK 4L. or: 4. To create a downtrack fix along the flight plan where the aircraft will be directly abeam the entered "fix", press (LSK 5L). The distance to go (DTG) and ETA to the intersection point are displayed. If the radial, distance or abeam fix does not intercept the route ahead of the aircraft, or the intersection point does not lie within 500 nm of the reference fix, then the advisory message "!INVALID INTERSECTION" is displayed. Figure 5-2 shows a typical downtrack fix creation involving the radial, distance or abeam fix intercepting the route ahead of the aircraft. The displayed reference of the bearing (radial) (e.g. true or magnetic North) is consistent with the other navigation angles as described in the SETUP page in Section 3.
FIX
1L 2L 3L 4L 5L 6L
ANN
FIX INFO
1/1
CRS/DIS o 310 / 456N M
REF
TO<
-- DOWNTRACK FIXES -RAD/DIS DTG ETA 175o/ 80 N M 5 4 7 N M 0307 o
1R 2R 3R
163 / 100N M
520N M
0239
ABEAM 216o/ 6 0 N M
4R
599N M
0400
5R
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6R
Page 5-24 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056) 5. Line select the intersection to the scratchpad by pressing LSK 3L, LSK 4L, or LSK 5L. The intersection is displayed as a Place Bearing/Distance in the scratchpad e.g. ANN216.3/60.2. NOTE: When the FIX is a 7-character waypoint identifier, the intersection is displayed as a waypoint coordinate. 6. Display the desired location in the route by pressing [LEGS] and [NEXT] or [PREV] as required. 7. Move the waypoint to the desired place in the route by pressing the appropriate LSK. 8. Verify the waypoint entry and make the modified route active by pressing [EXEC]. NOTE: When no intersection is found with the active Flight Plan, the FIX INFO page will retain the radial or distance entry. The EFIS will display a green circle around the FIX waypoint (if symbology is supported by the installed EFIS). It will also display the radial as a line extending from the FIX. The distance is displayed as a circle with its radius equal to the distance value entered. 10 0N
M
BKA
ABEAM CROSSING ANN 216/60
ANN
M 60N ° 6 1 R-2 R-1 75°
MOCA1
REFERENCE FIX RADIAL CROSSING ANN 175/80 DISTANCE CROSSING ANN 163/100
4
YZP
G704127.cdr
Figure 5-2 Typical Downtrack Fix Creation
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Page 5-25 July 17, 2013
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (930-600166-000 SW056)
CURRENT NAVIGATION MODE STATUS Display the PROGRESS 1/3 or 1/4 page by pressing [PROG].
PROGRESS 280T
1L 2L 3L 4L 5L 6L
ARRIE
1/4
DTGN M 35.2
ETA 1817<
280T
TOU 88.3 1830 TRUE W I N D TK/GS >020T / 45K T 281T/228K T RNP/ANP 1.00/0.05N M NAV MODE
XTK L0.00N M DEV SCALE 1.0N M
1R 2R 3R 4R 5R 6R
NOTE: The current navigation mode (NAV MODE) is displayed at LSK 6L. The Required Navigation Performance (RNP) and the current estimated navigation performance (ANP) are expressed in nautical miles. The Required Navigation Performance (RNP) can be manually overwritten by entering the desired value in LSK 5L. If the manually entered RNP exceeds the default RNP then the "VERIFY RNP VALUE" alert message is raised. Refer to Section 15 RNP Capability for additional information. More information on the navigation mode can be found on the POS INIT/REF 2/3. To access the POS INIT/REF 2/3 page press the