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Esterline CMA-9000 Operator's Manual

Esterline CMA-9000 Operator's Manual

Flight management system

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Publication No. 9000-GEN-0150

Item No.: 930-600086-000

FLIGHT MANAGEMENT SYSTEM

Esterline CMC Electronics

600 Dr. Frederik Philips Boulevard

Ville Saint-Laurent, Quebec, Canada

H4M 2S9

This page is printed under user's responsibility

and must not be retained for reference

OPERATOR'S MANUAL

OPERATIONAL PROGRAM

S/W 169-614876-300

CMA-9000

November 19, 2009

Revision 2 March 01, 2010

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Page 1 OPERATOR'S MANUAL FLIGHT MANAGEMENT SYSTEM CMA-9000 OPERATIONAL PROGRAM S/W 169-614876-300 Esterline CMC Electronics 600 Dr. Frederik Philips Boulevard Ville Saint-Laurent, Quebec, Canada H4M 2S9 Publication No. 9000-GEN-0150 November 19, 2009 Item No.: 930-600086-000 Revision 2 March 01, 2010 This page is printed under user's responsibility...
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WE VALUE YOUR COMMENTS PLEASE EVALUATE OUR PUBLICATION AND LET US KNOW Although we constantly strive for accuracy and clarity, we may make errors on occasion. If we do, we would appreciate your comments to improve this manual. Please web-based Customer Support Request...
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Page 5: Operator's Manual
Section 8 Direct-To/Intercept Section 9 Holding Pattern Navigation Section 10 Tactical Functions Section 11 Navigation Sensors Section 12 CMA-9000 FMS Pages - Radio Tuning Section 13 Performance Functions Section 14 RNP Capability Section 15 MCDU Functions Section 16 Abnormal Procedures...
Page 6: Operator's Manual
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Page 7: Table Of Contents
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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............................
Page 8: November
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Page 9: System Overview
A world-wide subscription navigation database, stored in a non-volatile memory, provides the CMA-9000 FMS with information on waypoints, navaids and airports. In addition the database is capable of storing customer defined routes and waypoints. The CMA-9000 FMS is a Flight Management System (FMS) which also integrates the functionality of Radio Management System (RMS) and Control Display Unit (CDU) into a standalone, cockpit mounted enclosure.
Page 10: Component Description
The keyboard panel is integrally lit from a panel light dimming bus. The CMA-9000 FMS panel is illustrated in Section 2 along with an explanation of the keys and their function.
Page 11: Navigation Modes
In this case, when in the military navigation option, the CMA-9000 FMS will nevertheless compute a NP value using the available data. In this same case, when in the civil navigation option, the CMA-9000 FMS will make the NP value unavailable.
Page 12: Gps
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 CMA-9000 FMS will revert to the Dead Reckoning (DR) mode of navigation, the GPS integrity annunciator will illuminate, and the “GPS NAV LOST”...
Page 13: Kalman Filter
North-South velocity; • East-West velocity. The CMA-9000 FMS is using the raw INS position and velocities provided by the EGI or Inertial equipment. E. KALMAN FILTER The KALMAN sensor interface is used when stand-alone GPS navigation and radio navigation are not possible.
Page 14: Military Navigation Mode
The navigation modes selection logic is geared to accuracy performance and the CMA-9000 FMS will not necessarily force mode transitions based on the integrity. Some integrity monitoring is nevertheless performed to raise alarms. The pilot is expected to consider navigation mode alarms and force navigation sensor selections if necessary.
Page 15: Hybrid Gps/Inertial
A. Hybrid GPS/Inertial The hybrid GPS/INS mode is offered only when the CMA-9000 FMS is configured in military mode and an EGI is configured. The highest priority will be given to the hybrid GPS/INS sensor if it is configured and no invalid flag is associated to its combined GPS/INS solution.
Page 16: Dme/Dme
North-South velocity; • East-West velocity. The CMA-9000 FMS is using the raw INS position and velocities provided by the EGI or Inertial sensor. G. DVS The CMA-9000 FMS uses the Doppler Velocity Sensor position and velocities complemented with the pitch, roll and selected heading for navigation.
Page 17: Kalman Filter
Initiation of the KALMAN navigation mode is automatic upon loss of GPS and radio navigation. The CMA-9000 FMS will use the Attitude and Heading Reference System (AHRS), and the GPS, to provide a KALMAN filter navigation mode. In this mode, the primary navigation sensor will be a GPS receiver.
Page 18 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NORTH WIND DIRECTION (WD) BEARING TO WAYPOINT (BRG) WINDSPEED (WS) DESIRED TRACK DRIFT (DTK) ANGLE (DA) RIGHT TRACK ANGLE ERROR GROUND (TKE) LEFT TRACK ANGLE (TK) HEADING (HDG) CROSS-TRACK DISTANCE (XTK) LEFT 0012033 Figure 1-1 Navigation Relationships...
Page 19: Terminal Area Operations And Gps Instrument Approaches
(AP/FD) system. Angular inputs to the CMA-9000 FMS may be referenced to either magnetic or true north. The input mode is installation dependent as defined in the Airplane/Rotorcraft Flight Manual Supplement. The reference used for the CMA-9000 FMS angular displays and outputs to the flight instruments, can also be selected by the operator.
Page 20: Acronyms And Abbreviations
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACRONYMS AND ABBREVIATIONS Above (altitude) Air-To-Air AAIM Aircraft Autonomous Integrity Monitoring Aircraft ACCUR Accuracy ACID Aircraft Identifier Active ACMS Aircraft Conditioning Monitoring System Acquisition mode Air Data Computer Automatic Direction Finder Air Data Inertial Reference System...
Page 21 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Final Approach Course to fix Configuration Checker Clear Primary (CM1) or Secondary (CM2) COM radio Canadian Marconi (Avionics) Command Communications Management Unit Communication COMMS Communication Radios Connection CONC Concentrator COORD Coordinates Compass Computed Air Release Point...
Page 22 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Estimated External Sub-System Estimated Time of Arrival Estimated Time Enroute Electronic Warfare EXEC Execute Final Approach Fix Failure Detection and Exclusion Final Approach Fix Front panel Function Key Flight Level Flight Flight Management (FM1, FM2)
Page 23 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Initial Approach Fix Indicated Airspeed Intercom ICAO International Civil Aviation Organisation Identifier IDENT Identifier Identifier Intermediate Fix IFDS Integrated Flight Display System Instrument Flight Rules in Hg Inches of Mercury Instrument Landing System Innner Marker...
Page 24 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Minimum Descent Altitude MDA-DA Minimum Descent Altitude-Decision Altitude Mean Effective Wind MGRS Military Grid Reference System Mega Hertz Maritime Identification Digits Minute Microwave Landing System Middle Marker Modified Mark Message MSLA Mean Sea Level Altitude...
Page 25 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM A method of setting the altimeter to compensate for changes in barometric pressure and runway elevation. Pilot receives information from airfield and adjusts his altimeter accordingly and it will read zero altitude at touchdown on the runway.
Page 26 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Supplemental Type Certificate Status SURF Surface SYNC Synchronization Tactical Direct-To Angle referenced to True North TACAN Tactical Air Navigation TACT Tactical True Air Speed TACAN Touchdown Fix when not RW TransDowN Trailing Edge Telephone...
Page 27 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM West Wind Direction Waypoint Windspeed Weight World Geodetic System Weight Weather Radar XFILL Cross FMS Fill XPDR Transponder Transmit Extended Trailing Edge Point Cross Track Zulu (UTC) time This page is printed under user's responsibility...
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Page 29 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 2 - CMA-9000 FMS CONTROL AND DISPLAY CONTENTS Subject Page GENERAL ................................2-1 CMA-9000 FMS and MCDU DISPLAY PANEL ....................2-1 GENERAL RULES OF DISPLAY OPERATION ....................2-16 WAYPOINT NAMES AND OTHER CONVENTIONS ..................2-19...
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Page 31: General
CMA-9000 FMS and MCDU DISPLAY PANEL The front panel arrangement of the CMA-9000 FMS is illustrated in Figure 2-1. The data is presented on a 3 X 4 inch Active Matrix Liquid Crystal Display (AMLCD). The display format is partitioned into specifically defined areas.
Page 32 FAIL CMC ELECTRONICS INIT LEGS PROG EXEC RADIO TPDR MARK HOLD 0611006 Figure 2-1 CMA-9000 FMS Front Panel (Hardware variation 030/430) This page is printed under user's responsibility and must not be retained for reference Page 2-2 November 19, 2009...
Page 33 CMA-9000 FLIGHT MANAGEMENT SYSTEM FAIL CMC ELECTRONICS INIT LEGS PROG EXEC RADIO HOLD 0610006 Figure 2-2 CMA-9000 FMS Front Panel (Hardware variation 001/101/301/501) This page is printed under user's responsibility and must not be retained for reference Page 2-3 November 19, 2009...
Page 34 FAIL CMC ELECTRONICS INIT LEGS PROG EXEC RADIO FUEL MARK HOLD 0610007 Figure 2-3 CMA-9000 FMS Front Panel (Hardware variation 002/003/005/102/103/302/303/502/503) This page is printed under user's responsibility and must not be retained for reference Page 2-4 November 19, 2009...
Page 35 CMA-9000 FLIGHT MANAGEMENT SYSTEM FAIL CMC ELECTRONICS INIT LEGS PROG EXEC RADIO VNAV HOLD 0611003 Figure 2-4 CMA-9000 FMS Front Panel (Hardware variation 045/445) This page is printed under user's responsibility and must not be retained for reference Page 2-5 November 19, 2009...
Page 36 FAIL CMC ELECTRONICS INIT LEGS PROG EXEC RADIO TACT VNAV HOLD 0610005 Figure 2-5 CMA-9000 FMS Front Panel (Hardware variation 050) This page is printed under user's responsibility and must not be retained for reference Page 2-6 November 19, 2009...
Page 37 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 2-6 CMA-9000 FMS Front Panel (Hardware variation 106/506) This page is printed under user's responsibility and must not be retained for reference Page 2-7 November 19, 2009...
Page 38 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 2-7 CMA-9000 FMS Front Panel (Hardware variation 290) This page is printed under user's responsibility and must not be retained for reference Page 2-8 November 19, 2009...
Page 39 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 2-8 CMA-9000 FMS Front Panel (Hardware variation 060/460) This page is printed under user's responsibility and must not be retained for reference Page 2-9 November 19, 2009...
Page 40 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 2-9 CMA-9000 FMS Front Panel (Hardware variation 070/470) This page is printed under user's responsibility and must not be retained for reference Page 2-10 November 19, 2009...
Page 41 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The items mentioned in the first column are used for referencing to annunciators and keys of Figure 2-1. Display Screen: Provides 14 lines of 24 characters. The color and font size conventions used in the display are configurable. Each item can be displayed with a predefined color and a predefined font size.
Page 42 CMA-9000 FLIGHT MANAGEMENT SYSTEM ANNUNCIATORS: The following are the possible annunciators which are avaialble for the different CMA-9000 H/W panel variations. NOTE: That the physical location of these annunciators may vary depending on the specific panel (see front panel figures provided earlier in this section for specific panel variation annunciator locations).
Page 43 KEYS AND ANNUNCIATORS- Items 10-33: 10. Line Select Keys (LSK) - There are twelve LSKs on the CMA-9000 FMS panel, six on either side of the display. LSKs are identified by their location from top to bottom of the screen and as left or right, e.g. LSK 1L, LSK 6R.
Page 44 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 17. HOLD Key (all variations except 106/290/506) - if no holding pattern exists in the flight plan, 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 flight plan, accesses the HOLD page for the definition of holding pattern parameters at the designated waypoint or present position.
Page 45 33. SQK_IDT key (VAR 001/101/301/501) - Provides a quick access function to Squawk ident of the active ATC transponder. MARK Key (all variations except 290) - when pressed creates a Mark On Top waypoint with the CMA-9000 FMS present position. It provides access to the PREDEF WPT 2/2 page where this waypoint is stored (if CFG KEY 2 is configured to MARK).
Page 46: General Rules Of Display Operation
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GENERAL RULES OF DISPLAY OPERATION The operating procedures detailed in the following sections are governed by a general set of rules for CMA- 9000 FMS operation. Familiarity with these rules will greatly simplify the process of learning system operation.
Page 47 They must must be acknowledged by pressing the CLR key before data entry can take place. B. Maintenance Alert • Indicates a particular CMA-9000 FMS failure condition. • Displayed in amber on the MAINT MESSAGES page. •...
Page 48 MSG key or by pressing and holding the[ INIT REF] key for more than 1 second. When more than one new alert message occurs, the CMA-9000 FMS MSG annunciator will stay illuminated until all the messages have been viewed in turn by pressing the [CLR] key which deletes the current message and displays the next one.
Page 49: Waypoint Names And Other Conventions
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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...
Page 50 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Course Legends - courses may be displayed with the following legends depending on the leg type, as listed below: Indicates a course leg inbound to the next waypoint FR FIX Indicates a course outbound from the FIX...
Page 51 PREFLIGHT..............................3-2 START-UP AND INITIALIZATION........................3-2 ACTIVE DATABASE SELECTION........................3-5 CMA-9000 FMS DISPLAY SETUP ........................3-6 SYSTEM POSITION, DATE AND TIME UPDATE................... 3-7 ANGULAR REFERENCES FOR NAVIGATION AND DISPLAY ..............3-8 ACTIVE ROUTE SELECTION USING THE CUSTOM ROUTE NAME............3-10 ROUTE SELECTION FROM THE LIST OF CUSTOM ROUTES ..............
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Page 53: Condensed Preflight Process
CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 3 PREFLIGHT CONDENSED PREFLIGHT PROCESS This page sequence gives an overview of the Preflight operations of the CMA-9000 FMS. The intent of each step is summarized on the next page. If radios are used FMS1 IDENT...
Page 54: Preflight
1. Verify that all relevant circuit breakers are on. 2. The CMA-9000 FMS will show a white display while testing the FAIL, MSG, POS, OFST, NPA, TX1, TX2, HF, V/UHF, IND, RNP, GSM, SMS and EXEC annunciators. Refer to section 2 for applicable annunciator.
Page 55 <SETUP POS INIT> 3. Adjust the intensity of the CMA-9000 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.
Page 56 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 4. If RADIO page is displayed then press [INIT REF], <IDENT> (LSK 1L) to display the IDENT 1/2 page. FMS1 IDENT N A V D A T A B A S E A C T I V E...
Page 57: Active Database Selection
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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.
Page 58 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CMA-9000 FMS DISPLAY SETUP From the IDENT 1/2 page, go to DISPLAY 1/1 page, by pressing [INIT REF] and <DISPLAY> (LSK 4L). DISPLAY <PARALLAX D I S P L A Y >COLOR <INIT/REF 1. Press LSK 1L and adjust display PARALLAX for proper viewing angle.
Page 59: System Position, Date And Time Update
Initialization of position, date and time is not normally required. If GPS is available, the CMA-9000 FMS internal clock is updated to GPS-based UTC and date. Unless an INS 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.
Page 60: Angular References For Navigation And Display
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 4. Move the new date to the DATE field by pressing LSK 5R. To initialize the position use the POS INIT/REF 1/2 page: POS INIT/REF F M S P O S 26.28 W122 18.67...
Page 61 Swiss Grid position is defined as Northing and Easting coordinates up to 999 km, locating a position to within 10 meter square. The CMA-9000 FMS is able to display to full range of the Swiss Grid coordinate system. However, the CMA-9000 FMS will only accept manual entries within the following limits:...
Page 62: Active Route Selection Using The Custom Route Name
1/X page only if a DMAP (ELBIT, EURONAV, or EURONAV_A702 type only) is configured. NOTE: When loading a custom route in flight, the CMA-9000 FMS will append a "+" to the custom route identifier on the RTE page thus indicating that the custom route has been appended to the end of the current flight plan.
Page 63: Route Selection From The List Of Custom Routes
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ROUTE SELECTION FROM THE LIST OF CUSTOM ROUTES With the ACT or MOD RTE 1/X page displayed: Display the custom routes by pressing <CO ROUTES> (LSK 4R). SELECT CO ROUTE KSEAPANC KSEAPANC1 KSEAPANC2 L O A D >DIRECT...
Page 64: Active Route Selection Using The User Route Name
"MOD" status in the title line changes to "ACT". The selected route is now active. NOTE: When loading a user route in flight, the CMA-9000 FMS will append a "+" to the user route identifier on the ROUTE page thus indicating that the user route has been appended to the end of the current flight plan.
Page 65: Route Selection From The List Of User Routes
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ROUTE SELECTION FROM THE LIST OF USER ROUTES With the ACT or MOD RTE 1/X page displayed: Display the user routes by pressing <USER ROUTES> (LSK 5R). USER ROUTES 0 0 0 1 M 0 0 0 9 M...
Page 66: Building A Route Via Waypoint Insertion
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM BUILDING A ROUTE VIA WAYPOINT INSERTION When no custom 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.
Page 67: Building A Route Via Airway Insertion
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM BUILDING A ROUTE VIA AIRWAY INSERTION When no custom 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.
Page 68: Building A Departure Procedure
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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. NOTE: The route structure can be modified by defining the waypoint identifier at which the desired airway is terminated and repeating the procedure for entering the following airways.
Page 69: Verifying Active Route Legs By Course And Distance
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 CMA-9000 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.
Page 70: Accessing Init/Ref Index Pages
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACCESSING INIT/REF INDEX PAGES Display the INIT/REF INDEX 1/2 page by pressing [INIT REF]. FMS1 INIT/REF INDEX 1/2 <IDENT WPT DATA> <POS INIT WPT LISTS> <CTR LEGS NEAREST> <FIX INFO MARK ON TOP> <SETUP NAV STATUS>...
Page 71: Cruise Performance Parameters Initialization (If Configured)
Cruise Wind values. Upon a warm or cold start, the CMA-9000 FMS will keep the Cruise TAS value prior to the power down. Upon a change in configuration, the CMA-9000 FMS will set the Cruise TAS value in accordance with the aircraft type:...
Page 72: Fuel Performance Parameters Initialization (If Configured)
FUEL AND WEIGHT PERFORMANCE PARAMETERS INITIALIZATION (if configured) If the FUEL+WEIGHTS option is configured for the FUEL pages, the CMA-9000 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.
Page 73 • The quantities are displayed in white when there is no difference between the gross weight sent by the IFDS and the CMA-9000 FMS-computed gross weight. This page is printed under user's responsibility and must not be retained for reference...
Page 74: Efis Display (Efis-Equipped Aircraft Only And If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM EFIS DISPLAY (EFIS-EQUIPPED AIRCRAFT ONLY and if configured) Display the INIT/REF INDEX 2/2 page by pressing [INIT REF], [PREV] or [ NEXT]. FMS1 INIT/REF INDEX 2/2 SIMULATE> TIMER> <PLAN DATA EFIS> <FUEL DATA LOAD>...
Page 75: Gps Satellite Deselection (If Configured)
Otherwise ensure that no satellites are deselected. DUAL FMS OPERATIONS In dual CMA-9000 FMS installations, the operator can set the CMA-9000 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.
Page 76: Synchronized Operations
CMA-9000 FMSs overriding any existing flight plan. SYNCHRONIZED OPERATIONS NOTE: To operate correctly in the synchronized mode the CMA-9000 FMSs must contain the same databases. Furthermore the active database must be the same in all CMA-9000 FMSs.
Page 77 • Fuel data Only one CMA-9000 FMS can change an active flight plan at any time. If one CMA-9000 FMS is already in MOD status (route modifications in progress), any attempt to change the flight plan of another CMA-9000 FMS will bring in view the “...
Page 78: Independent Operation
INDEPENDENT OPERATION In the independent mode of operation, all entries made on either CMA-9000 FMS are not reflected on the other CMA-9000 FMS. However, the active or inactive flight plan can still be copied from one CMA-9000 FMS to the other via the RTE XFILL prompt (LSK 4L) on the RTE 1/1 page.
Page 79 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 4 - DEPARTURES CONTENTS Subject Page INTRODUCTION .............................. 4-1 SID SPECIFICATION IN FLIGHT ........................4-3 CONDENSED SID AND SID TRANSITION PROCESS .................. 4-3 STANDARD INSTRUMENT DEPARTURE (SID) SELECTION ..............4-4 ALTIMETER SETTING............................. 4-6...
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Page 81: Introduction
CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 4 DEPARTURES CAUTION: In case of disagreement between the published SID information and CMA-9000 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.
Page 82 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CHATY TWO DEPARTURE (CHARTY2.CHARTY) (PILOT NAV) Figure 4-1 Typical Standard Instrument Departure with Transition Procedure This page is printed under user's responsibility and must not be retained for reference Page 4-2 November 19, 2009...
Page 83: Sid Specification In Flight
Where required by the magnitude of the track angle change, the CMA-9000 FMS will 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.
Page 84: Standard Instrument Departure (Sid) Selection
• From DEPARTURES 1/1. NOTE: If the CMA-9000 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.
Page 85 Display the desired RUNWAY by pressing the PREV or NEXT key as required, and select the RUNWAY by pressing the appropriate right hand LSK. The message “SET QNH” will be displayed in the scratchpad if the CMA-9000 FMS is not receiving Baro corrected altitude. (See ALTIMETER SETTING procedure in this section). This message is installation dependent and will not be displayed if deconfigured.
Page 86: Altimeter Setting
8. Make the selected SID and SID transition active by pressing EXEC. The message “SET QNH” will be displayed in the scratchpad if the CMA-9000 FMS is not receiving Baro- corrected altitude. (See ALTIMETER SETTING procedure in this section). This message is installation dependent and will not be displayed if deconfigured.
Page 87 • EGI hybrid inertial altitude. *For installation including GPS and EGI, the CMA-9000 FMS will select the altitude from the GPS used for navigation (civil or military from EGI). For entries, units are automatically detected and decimal point entry is not required.
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Page 89 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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 PLACE/BEARING/DISTANCE WAYPOINTS .................... 5-4 PLACE/BEARING-PLACE/BEARING WAYPOINTS ................5-4 ALONG-TRACK WAYPOINTS........................
Page 90: Subject Page
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 5 - ENROUTE CONTENTS Subject Page ROUTE 2 OPTION ............................5-33 INACTIVE ROUTE MANIPULATIONS (SUMMARY)................5-34 INACTIVE ROUTE MANIPULATIONS (DETAILED STEPS) ..............5-34 NEAREST............................... 5-36 TIMER (If configured) ........................... 5-39 TIMER 1/1 page (If configured) ........................5-39...
Page 91: Condensed En-Route Process
SECTION 5 ENROUTE CONDENSED EN-ROUTE PROCESS This page sequence gives an overview of the CMA-9000 FMS pages used in the en-route phase of flight. The intent of each step is summarized on the next page. ACT RTE 1 LEGS 2 9 9 3 9 .
Page 92 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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 direct- to/intercept, fly-over or holding procedures performed on these pages.
Page 93: 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 CMA-9000 changes from terminal to en- route phase of flight, with the following indications: 1.
Page 94: Inserting Waypoints
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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.
Page 95: Along-Track Waypoints
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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.
Page 96: Latitude/Longitude Waypoints
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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.
Page 97: Inserting A Radial-To Segment
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INSERTING A RADIAL-TO SEGMENT A Radial-To segment is first defined in the RADIAL-TO page accessed in one of the following ways: • by pressing [INIT REF], <DES+SAR> or <TACTICAL> (LSK 6R), entering the waypoint ident in the REF ID field at LSK 1L and then pressing <RADIAL-TO>...
Page 98: Route Discontinuities
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Press the LSK (1L, 2L, 3L, 4L or 5L) where the segment is to be inserted. NOTES: a) If the reference point is not part of the selected route, then the segment is inserted between the waypoint corresponding to the LSK pressed and the following waypoint.
Page 99: Route Discontinuity Close-Up
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM A ROUTE DISCONTINUITY can be inserted into the flight plan by selecting RTE DISCON (LSK 1R) on the the DES+SAR or TACTICAL 1/2 or INACT DES+SAR or TACTICAL 2/2 page. The active or inactive RTE x LEGS page will be displayed with "...
Page 100: By Clear Key
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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.
Page 101: To Convert To Fly-By From Fly-Over
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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.
Page 102: Leg Sequencing
LEG SEQUENCING A. FLY-BY WAYPOINTS The CMA-9000 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.
Page 103 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM WPT04 (fly-over) Act wpt = WPT04 Act wpt = WPT03 WPT03 (fly-by) Sequence WPT02 at bisector (fly-by) Act wpt = WPT02 WPT01 LEGEND: Entered flight plan displayed on GAMA EFIS Flight path followed by Guidance...
Page 104: Eta And Efa
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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 <LEGS ETA> (LSK 6R).
Page 105: Waypoint Latitude/Longitude Display
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM WAYPOINT LATITUDE/LONGITUDE DISPLAY Display the coordinates for each waypoint by pressing [LEGS], <LEGS ETA> (LSK 6R), <LEGS POS> (LSK 6R). ACT RTE 1 LEGS POS 1/2 CAFTA. 1 8 T Y Q 3 6 4 3 8 7 3 2...
Page 106: Progress Along The Route (Distance-To-Go, Eta)
CMA-9000 FLIGHT MANAGEMENT SYSTEM PROGRESS ALONG THE ROUTE (DISTANCE-TO-GO, ETA) NOTE: Similar information is available on PROGRESS 1/3 and PROGRESS 2/3 page, when CMA-9000 FMS is configured for the three set PROGRESS pages. Display the PROGRESS 1/4 page by pressing [PROG].
Page 107: Required Time Of Arrival Computation
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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 FROM and TO waypoints become the same and the TO waypoint course is replaced by the title "HOLD AT".
Page 108: Wind Components, Navigation Angles And Air Data
QNH altimeter setting and QNH Altimeter Ref (if configured). NOTE: The QNH ALTIMETER REF is displayed at 6R and therefore computed by the CMA-9000 FMS only when the 4-page set PROGRESS is configured and when the pressure altitude (from ADC) and hybrid INS/GPS altitude (from the EGI/GPS) are available.
Page 109: Offset Track Initiation
Navigation and guidance will now be relative to the offset track. If the CMA-9000 FMS is autopilot-coupled, the CMA-9000 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.
Page 110: Offset Track Cancellation
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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 •...
Page 111: Position Fix Info Display
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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 INFO>. FIX INFO F I X C R S / D I S R E F TO<...
Page 112: Downtrack Fix Creation
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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], <FIX INFO>. 1. Move the waypoint identifier into the "fix" field by pressing LSK 1L.
Page 113 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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"...
Page 114 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ABEAM CROSSING ANN 216/60 REFERENCE MOCA1 RADIAL CROSSING ANN 175/80 DISTANCE CROSSING ANN 163/100 G704127.cdr Figure 5-2 Typical Downtrack Fix Creation This page is printed under user's responsibility and must not be retained for reference...
Page 115: Current Navigation Mode Status
< G P S NOTE: The current navigation mode (NAV MODE) of the CMA-9000 FMS is displayed at LSK 6L. The Required Navigation Performance (RNP) for the phase of flight and the current estimated navigation performance (ANP) are displayed in nautical miles. The Required Navigation Performance (RNP) may be manually entered by keying in RNP in nautical miles (e.g.
Page 116: Gps Sensor And Satellite Status
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GPS SENSOR AND SATELLITE STATUS Display the NAV STATUS INDEX 1/1 page by pressing [INIT REF], <NAV STATUS> (LSK 5R). NAV STATUS INDEX 1/1 <PREDICT RAIM GPS> <GLONASS DME> <DVS VOR/DME/TCN> <INS/GPS INS> <INS/DVS <INIT/REF...
Page 117: Predictive Raim Requests
CAUTION: It is not recommended to perform manual predictive RAIM requests when the aircraft is about to enter the approach phase of flight as the CMA-9000 FMS automatically sends predictive RAIM requests as well. No manual predictive RAIM request should be done when the aircraft is within DTG=6 nm to the FAF waypoint.
Page 118: Predictive Raim Satellite Deselection
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 2. Key the ETA for the new waypoint into the scratchpad and move it to the ETA field by pressing LSK 2L. The range of arrival times appears on the right side of the display and after a short delay the predicted HIL value for each arrival time is displayed.
Page 119: Glonass Status 1/2
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GLONASS STATUS 1/2 Display the GLONASS STATUS 1/2 page by pressing [INIT/REF], <NAV STATUS>, <GLONASS>. GLONASS STATUS 1/2 O P M O D E N A V S A T V I S S A T T R K...
Page 120: Waypoint Information From The Navigation Database
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM WAYPOINT INFORMATION FROM THE NAVIGATION DATABASE 1. Key in the desired identifier (waypoint, navaid, airport, temporary waypoint), or copy it into the scratchpad from any other page. 2. Display the WPT DATA 1/2 page by pressing [INIT REF], <WPT DATA> (LSK 1R).
Page 121 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The display reverts to the page where the duplicated identifier was entered, with the selected identifier in the data field. When the operator enters in the flight plan (active or inactive) a waypoint identifier which is not unique, then the "SELECT WPT"...
Page 122: Rnp Modification
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RNP MODIFICATION Refer to Section 15 RNP Capability for a detailed description of the CMA-9000 FMS RNP capability. Display the PROGRESS 1/3 or 1/4 page by pressing [PROG]. ACT PROGRESS 2 8 0 D T G E T A <...
Page 123: Route 2 Option
When configured with RTE 2 option, two independent routes (RTE 1 and RTE 2) may reside in the CMA-9000 FMS at the same time. The CMA-9000 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.
Page 124: Inactive Route Manipulations (Summary)
Next, press <CONFIRM>, (LSK 6R) to save the modifications or <CANCEL> (LSK 6L) to delete them. NOTE: In the case of a dual CMA-9000 FMS installation, the inactive route modification is cross-talked to the off- side FMS upon pressing the <CONFIRM> prompt.
Page 125 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 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. RTE2 LEGS 2 9 9 3 9 .
Page 126: Nearest
NEAREST The CMA-9000 FMS presents information about the current airspace by providing bearing and distance with respect to a center reference waypoint of the 50 closest waypoints within a distance of 640 nautical miles for either of the following categories of waypoints: •...
Page 127 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM A. Display NEAREST AIRPORT 1/X page: NEAREST AIRPORT 1/13 I D / B R G / D I S / N A M E C F Y F 1 2 5 / 0 . 4 N M...
Page 128 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. DISPLAY NEAREST VHF NAV: NEAREST VHF NAV I D / B R G / D I S I D / B R G / D I S M R S 0 3 6 / 0 .
Page 129: Timer (If Configured)
The CMA-9000 FMS provides a timer, which may be used as a count-up or countdown timer, and which will generate a TIMER ALARM alert message upon expiration. The CMA-9000 FMS allows the user to either enter in an alarm time or a count-down value (range from 0 to 23 hours, 59 minutes and 59 seconds).
Page 130 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Display after an alarm time is entered: TIMER A L A R M T I M E C O U N T D O W N 1234:12 ----:-- ADD 5 MIN> ADD 15 MIN>...
Page 131 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 6 - ARRIVALS CONTENTS Subject Page INTRODUCTION ..............................6-1 CONDENSED ARRIVAL PROCESS ......................... 6-2 STANDARD TERMINAL ARRIVAL ROUTE (STAR) SELECTION ..............6-2 This page is printed under user's responsibility and must not be retained for reference...
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Page 133 STAR and the first waypoint of the approach transition are identical. Arrival waypoints may include speed and altitude constraint advisories. If the aircraft installation provides only a pressure altitude input to the CMA-9000 FMS, manual entry of the altimeter correction is necessary to convert this input to baro-corrected altitude.
Page 134 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CONDENSED ARRIVAL PROCESS This page provides an overview of the process of selecting the arrival procedures. The intent of each step is summarized on the next page. 1. MOD, ACT ROUTE - select departure/arrival index page.
Page 135 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ANCHORAGE, ALASKA ANCHORAGE INTL 118.4 ANCHORAGE INTL ATIS AMOTT FIVE ARRIVAL (AMOTT.AMOTT5) ELMENDORF AFB ALASKA ANCHORAGE Intl Direct distance from Amott Int to: Anchorage Intl 43 NM ANCHORAGE ALASKA Direct distance from ANC VOR to:...
Page 136 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The ARRIVALS 1/X page for the selected airport is displayed, with the airport name included in the title line. Lists of STARs, approaches and runways for that airport are displayed. PANC ARRIVALS S T A R S...
Page 137 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: For certain types of STAR and STAR transition, the selection of the approach or approach transition may also be required before the STAR waypoints are loaded into the route from the navigation database. The message !SELECT TRANS/APPR/RWY is then displayed in the scratchpad.
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Page 139 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 7 - APPROACH CONTENTS Subject Page SECTION 7-1 LATERAL NAVIGATION......................7-1 GENERAL ................................ 7-1 CONDENSED APPROACH PROCESS ......................7-4 ENTERING THE TERMINAL AREA ........................ 7-8 ALTIMETER CORRECTION ..........................7-8 GPS INSTRUMENT APPROACH SELECTION .................... 7-10 VECTORING TO FINAL APPROACH FIX ....................
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Page 141: Section 7-1 Lateral Navigation
Baro-corrected altitude is required to enable automatic sequencing of procedure legs with altitude terminations. If the aircraft installation provides only a pressure altitude input to the CMA-9000 FMS, manual entry of the altimeter correction on the PROGRESS 1/X page is necessary to derive the baro-corrected altitude. Refer to the approved AFMS/RFMS for further details.
Page 142 CMA-9000 FLIGHT MANAGEMENT SYSTEM The CMA-9000 FMS provides navigation and guidance in the normal fashion for the two outbound legs of the procedure turn, followed by a turn to intercept the final approach course inbound to the final approach fix. When the maximum allowable procedure turn distance is less than 10 nm, the length of the first outbound leg may be reduced.
Page 143 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 7-1 Typical Arrival Procedure This page is printed under user's responsibility and must not be retained for reference Page 7-3 November 19, 2009...
Page 144: Condensed Approach Process
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CONDENSED APPROACH PROCESS The following describes the process of selecting the approach procedures. 1. MOD, ACT ROUTE - select departure/arrival index page. 2. DEP/ARR INDEX - select arrival at desired airport (origin or destination).
Page 145 <ERASE ROUTE> NOTE: For CMA-9000 FMS arrivals, the selection of the approach transition may not be necessary in order to avoid duplication of numerous legs. (The STAR procedure may lead up to the FAF already). 4. Display the first approach leg (normally the approach transition waypoint, if selected) by pressing [LEGS] and [PREV] or [NEXT] as required.
Page 146 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ANCHORAGE, ALASKA ANCHORAGE INTL 5400' VOR or GPS Rwy 6R 8000' 114.3 ANC 2100' 144' PANC Apt. Elev ANC VOR [D233J] D10.0 R-350 (IAF) Lake Hood (IAF) D5.1 Merrill Strip CAMPBELL LAKE [RWØ6R] ANCHORAGE 338 CMQ 114.3 ANC...
Page 147 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 5. Close-up the route discontinuity if present, as described in Section 5. RTE 1 LEGS 0 4 2 3 6 . 8 2 3 3 P - T 3 . 0 0 A N C...
Page 148: Entering The Terminal Area
CMA-9000 FMS using the manually-entered altimeter setting provides the automatic waypoint sequence function for altitude-terminated legs of the missed approach. An error in the CMA-9000 FMS altimeter setting may therefore cause the aircraft to exceed the protected airspace due to an early or late waypoint sequence.
Page 149 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT PROGRESS H E A D W I N D C R O S S W I N D 0 2 7 R 4 4 H D G / D A T A S...
Page 150: Gps Instrument Approach Selection
NOTE: Selection of a new destination airport will result in the deletion of all approach and missed approach waypoints from the flight plan. NOTE: If a holding pattern is defined at the FAF, the CMA-9000 FMS will stay in terminal phase of flight on entering the hold and execute the approach on exiting the hold.
Page 151 If the Predictive RAIM of the CMA-9000 FMS determines the approach integrity will not be available at the FAF and/or the MAP, the CMA-9000 FMS remains in the terminal phase of flight and the following occurs at 2 nm inbound to the FAF: •...
Page 152: Vectoring To Final Approach Fix
NOTE: In GPS overlay approaches, there may be a difference between the distance-to-go displayed by the CMA-9000 FMS and the DME distance from the facility shown on the approach chart. Operators need to take this into account when interpreting the CMA-9000 FMS distance information.
Page 153: Circling Approaches
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 3. Verify the course and distance of the leg to the TO WPT, and make the direct-to intercept active by pressing EXEC. Navigation and guidance to intercept the inbound course to the FAF on the current heading is provided.
Page 154: Vfr Approaches
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 4. Verify the course of the intercept leg and distance to the to waypoint. NOTE: Do not press [EXEC] until visibility conditions permit the circling maneuver to the landing runway. Navigation and guidance displays and autopilot/flight director operation will continue to be referenced to the current leg of the original instrument approach procedure until [EXEC] is pressed.
Page 155: Missed Approach Initiation
CAUTION: If direct-to navigation is executed at low altitude while in the approach phase of flight, an immediate normal direct-to maneuver is performed, and the CMA-9000 FMS reverts to terminal phase of flight. The crew remains responsible at all times for complying with all obstacle avoidance and altitude restrictions during the direct-to navigation.
Page 156 The CMA-9000 FMS reverts to the terminal phase of flight. 3. If the autopilot/flight director mode is changed from LNAV-engaged to any other mode, the CMA-9000 FMS steering signal output will no longer be used, however the CMA-9000 FMS remains in the approach phase of flight.
Page 157: New Approach After A Missed Approach
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM With ACT RTE LEGS 1/X displayed: ACT RTE 1 LEGS 0 5 3 C R S 3 . 0 9 RW06R /oMAP 0 5 3 C R S 0 . 7 4 (544) R 2 0 0 H D G 1 2 .
Page 158: Modifying Approach Procedures
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 1. Delete the "<ACT>" approach by pressing LSK 1R. All approaches and runways are displayed. 2. Select the desired approach (and transition) by pressing the appropriate right hand LSK(s). NOTE: If the same approach is to be flown a second time, delete and reselect the existing approach, or approach transition, by pressing LSK 1R or LSK 2R and then pressing the appropriate right hand LSK(s).
Page 159: Approach Mode Deselection
<RTE 2 LEGS LEGS ETA> The CMA-9000 FMS provides automatic, autopilot-coupled interception of a DME arc at the arc's starting point. Interception of the arc at an intermediate point on the arc must be accomplished manually, as follows: 1. Disengage LNAV.
Page 160 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 4. Re-engage LNAV. Autopilot-coupled interception of the arc at an intermediate point on the arc may be accomplished by moving the arc's starting point along the arc to the desired radial from the DME station as follows: With the arc's starting waypoint identifier in scratchpad: 1.
Page 161: Deletion Of Procedure Turns
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DELETION OF PROCEDURE TURNS If an approach transition including a procedure turn has been loaded into the route, it can be readily deleted and converted into a straight-in approach. With the ACT or MOD RTE x LEGS 1/X page displayed: 1.
Page 162: Section 7-2 Vertical Navigation
CAUTION: When the VNAV approach function is utilised during non-precision approaches, it is mandatory for the crew to have the VNAV approach page displayed on the CMA-9000 Display Panel. In all instances, the altimeter MUST remain the primary altitude source for the crew.
Page 163 CMA-9000 FLIGHT MANAGEMENT SYSTEM CAUTION: In warm temperature conditions, the temperature compensated altitudes presented on the VNAV Approach and LEGS CMA-9000 Display Panel pages will be lower than the charted procedure altitudes. Temperature compensation is applied to altitudes for all approach and approach transition waypoints.
Page 164 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM VDEV 50 FT MINIMUM ALTITUDE RESTRICTION TCH = 50 FT RUNWAY THRESHOLD ELEVATION 0101031 Figure 7-3 Profile View of Vertical Path for a VNAV Approach HSI SCALE TO CHANGE ADVISORY MESSAGE APPROACH CAP GLDEPATH...
Page 165: Procedure For Selecting Vertical Navigation
V P A - 3 . 0 0 2. If baro-corrected altitude is not available to the FMS then QNH entry from CMA-9000 Display Panel pages must be performed. In this case white boxes are displayed at LSK 6L Enter the QNH value (refer to NOTE [1]).
Page 166 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 5. When the glidepath is active, current aircraft altitude relative to the vertical path is indicated by the installation dependent vertical deviation/glideslope pointer. The computed vertical deviation and target vertical speed are displayed on the active VNAV Approach page [NOTE 5].
Page 167: Vnav Approach Termination
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTES: [1]: CMA-9000 Display Panel entry of QNH can be in inHg or mb. Decimal point need not be entered. Local altimeter setting within terminal area is a mandatory input to enable VNAV approach guidance.
Page 168: Section 7-3 Tactical Approach
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 7-3 TACTICAL APPROACH See Section 11 for specifics on the TACTICAL APPROACH function. This page is printed under user's responsibility and must not be retained for reference Page 7-28 November 19, 2009...
Page 169 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 8 - POST FLIGHT PROCEDURES CONTENTS Subject Page POSITION ACCURACY CHECK - FLIGHT TERMINATION .................. 8-1 TAKE-OFF AND LANDING TIMES (if configured)....................8-2 This page is printed under user's responsibility and must not be retained for reference...
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Page 171 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 8 POST-FLIGHT PROCEDURES POSITION ACCURACY CHECK - FLIGHT TERMINATION 1. With the INIT/REF INDEX 1/2 page displayed, press POS INIT (LSK 2L). POS INIT/REF F M S P O S 26.28 W122 18.67...
Page 172 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TAKE-OFF AND LANDING TIMES (if configured) FLIGHT LOG T A K E O F F L A N D I N G 1 2 3 5 . 4 1 3 3 5 . 4...
Page 173 CONTENTS Subject Page INTRODUCTION..............................9-1 NAVIGATION OF DIRECT-TO A WAYPOINT WHEN CMA-9000 FMS IS CONFIGURED FOR A "STANDARD" DIRECT-TO ........................... 9-1 DIRECT-TO A WAYPOINT PROCEDURE......................9-3 A. DIRECT-TO A WAYPOINT IN THE ACTIVE ROUTE ................9-3 B. DIRECT-TO AN OFF-ROUTE WAYPOINT ....................9-3 C.
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Page 175: Introduction
NAVIGATION OF DIRECT-TO A WAYPOINT WHEN CMA-9000 FMS IS CONFIGURED FOR A "STANDARD" DIRECT-TO When a Direct-to a waypoint procedure is executed the CMA-9000 FMS calculates an intercept course to the waypoint based on the aircraft velocity, present position, track, and wind velocity.
Page 176 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PPOS 0703001 Figure 9-1 "Standard" Direct-To a Waypoint Procedure This page is printed under user's responsibility and must not be retained for reference Page 9-2 November 19, 2009...
Page 177: Direct-To A Waypoint Procedure
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DIRECT-TO A WAYPOINT PROCEDURE A. DIRECT-TO A WAYPOINT IN THE ACTIVE ROUTE 1. Display ACT RTE x LEGS 1/X page by pressing [LEGS]. 2. Display the desired waypoint by pressing [NEXT] or [PREV] as required.
Page 178: Direct-To A Waypoint In The Inactive Route
When the CMA-9000 FMS is in Track/Heading Hold mode, continuous checks are performed by the CMA- 9000 FMS to determine if the intercept is achievable. These checks are performed when Track/Heading Hold is first activated and are repeated periodically until the leg is captured by the CMA-9000 FMS steering function.
Page 179 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 1. If the predicted intercept point is very close (e.g. less than 0.1 nm) to the leg's termination waypoint and the airplane is turned from a valid heading intercept, then a path is calculated direct-to the waypoint and a DIRECT TO FIX alert message is displayed.
Page 180 (value which was frozen at the moment the AFCS LNAV switch was pressed). B. When configured to remain wings level, the CMA-9000 FMS keeps the roll command to a zero value until initiating the turn to capture the intercept leg. If the intercept is not achievable the FMS will trigger the alert message “NOT ON INTERCEPT HDG”...
Page 181: Direct-To A Waypoint With An Intercept Procedure
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DIRECT-TO A WAYPOINT WITH AN INTERCEPT PROCEDURE A. ON THE DEFAULT INBOUND COURSE (LEG INTERCEPT) Enter the identifier of the desired direct-to waypoint in the scratchpad: 1. Display the first ACT LEGS page by pressing LEGS.
Page 182: On A Manually Entered Inbound Course (Course Intercept)
TO waypoint on the current track/heading. NOTE: If a new heading clearance is received to intercept the inbound course, steering aircraft to new heading and re-engaging LNAV will cause the CMA-9000 FMS to fly the new intercept heading. This page is printed under user's responsibility...
Page 183 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 10 - HOLDING PATTERN NAVIGATION CONTENTS Subject Page GENERAL ................................. 10-1 ENTRY PROCEDURES............................ 10-2 A. SECTOR 1 APPROACH - PARALLEL ENTRY ..................10-2 B. SECTOR 2 APPROACH - OFFSET ENTRY (also called TEARDROP) ..........10-4 C.
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Page 185: General
HOLDING PATTERN NAVIGATION GENERAL The CMA-9000 FMS can navigate a race-track holding pattern at a holding fix. The parameters of the desired holding pattern may either be entered before take-off or while flying enroute. The holding fix is entered as a waypoint.
Page 186: Entry Procedures
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ENTRY PROCEDURES The entry into the holding pattern will be according to the track angle in relationship to the three entry sectors shown below. 70º 40º 70º 0603001 A. SECTOR 1 APPROACH - PARALLEL ENTRY 1.
Page 187 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MUR/O SHU/H SHU/H SHU/H 0709252 Figure 10-1 Parallel Entry This page is printed under user's responsibility and must not be retained for reference Page 10-3 November 19, 2009...
Page 188: Sector 2 Approach - Offset Entry (Also Called Teardrop)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. SECTOR 2 APPROACH - OFFSET ENTRY (also called TEARDROP) 1. On reaching the holding fix, the aircraft will turn to the heading required to fly a 40° track relative to the reciprocal of the inbound track on the holding side; then: The following figures show the teardrop entry and expected aircraft guidance on a typical* GAMA EFIS display.
Page 189 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 10-2 Teardrop Entry This page is printed under user's responsibility and must not be retained for reference Page 10-5 November 19, 2009...
Page 190: Sector 3 Approach - Direct Entry
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 2. Fly outbound until the turn distance needed to acquire the inbound leg is reached; and then: 3. Turn right to intercept the inbound track of the holding pattern. 4. On the second arrival over the holding fix, the aircraft will turn right to follow the holding pattern.
Page 191 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MUR/O SHU/H MUR/O SHU/H 0709250 Figure 10-3 Direct Entry This page is printed under user's responsibility and must not be retained for reference Page 10-7 November 19, 2009...
Page 192: Holding Pattern Geometry
NOTE: When buffet protection is configured, the CMA-9000 FMS removes the buffet limit during a hold to ensure that the bank angle limit does not cause an increase in the holding pattern area.
Page 193 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Key in "/H". RTE 1 LEGS 2 9 9 3 9 . 6 CAFTA 2 9 8 1 5 4 3 0 7 8 6 . 7 MOCA1 3 0 6 1 6 5...
Page 194 A navigation database holding pattern used for a course reversal is identified as EXIT TYPE “ONCE”. The exit of this type of holding pattern is performed automatically by the CMA-9000 FMS upon completion of the entry procedure (e.g.: second crossing of the holding fix).
Page 195: Holding Pattern At An Off-Route Waypoint
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HOLDING PATTERN AT AN OFF-ROUTE WAYPOINT Key a valid off-route waypoint identifier followed by /H into the scratchpad (e.g.: KILLA/H). NOTE: If the waypoint is not in the navigation database, the temporary waypoint should be created and inserted in the desired location in the route (as described in Section 5) before defining the holding pattern.
Page 196: Holding Pattern At Present Position
The present position is defined at the moment the [EXEC] key is pressed. The "MOD" status in the title line changes to "ACT". The CMA-9000 FMS performs a standard entry to the hold. If the inbound course is not aligned with the current course, an appropriate standard hold entry procedure will be followed.
Page 197: Modifying An Existing Hold
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MODIFYING AN EXISTING HOLD A. PRIOR TO HOLD ENTRY 1. Display the HOLD 1/X page by pressing [HOLD]. 2. Modify the holding parameters. HOLD page title line will display MOD HOLD. 3. Verify the new pattern parameters, and accept them by pressing [EXEC].
Page 198: Exiting A Holding Pattern
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM EXITING A HOLDING PATTERN A. EXIT OVER FIX (HOLD AT) WAYPOINT 1. Display the ACT HOLD 1/X page by pressing [HOLD]. (Refer to HOLD 1/1 page in Appendix A for details.) ACT RTE 1 HOLD...
Page 199: Exit By Direct-To Navigation To The Holding Fix
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. EXIT BY DIRECT-TO NAVIGATION TO THE HOLDING FIX Perform a standard direct-to procedure to the holding fix. When the direct-to is executed, navigation and guidance is provided for an immediate turn towards the inbound holding course.
Page 200: Holding Pattern Deletion
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 3. Confirm the resume hold procedure by pressing <EXEC> (LSK 6R). The "RESUME HOLD" prompt is changed to EXIT HOLD, the status changes to IN PROGRESS, and the <NEW HOLD> promtps is displayed. "MOD" status in the title line changes to "ACT", and the EXEC annunciator extinguishes.
Page 201 CENTRAL CLEAR? (If configured)......................11-34 BACKTRACK ROUTE (If configured)......................11-35 RENDEZ-VOUS WITH A MOVING WAYPOINT (If configured) ..............11-37 NAVIGATION OF DIRECT-TO A WAYPOINT WHEN CMA-9000 FMS IS CONFIGURED FOR A "MOVING DTK" DIRECT-TO............................11-38 NAVIGATION OF TACTICAL DIRECT-TO A WAYPOINT ................. 11-39 TACTICAL DIRECT-TO A WAYPOINT PROCEDURE................
Page 202 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 11 - TACTICAL FUNCTIONS CONTENTS Subject Page CALCULATED AIR RELEASE POINT (CARP) AND HIGH ALTITUDE RELEASE POINT (HARP) (If configured) ............................... 11-59 INITIATION OF A CARP/HARP PROCEDURE................... 11-62 CARP PLAN 1/3 (If configured) ......................... 11-65 CARP PLAN 2/3 (If configured) .........................
Page 203: Search Pattern (If Configured)
The starting point of the search pattern is entered as a waypoint. This waypoint may be pre-selected, so that upon reaching it, the CMA-9000 FMS will provide guidance to enter and continue the defined pattern until such time as the pattern is terminated either automatically or by operator action.
Page 204 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 1) EXPANDING SQUARE START 2) CREEPING LADDER LENGTH 3) SECTOR SEARCH 0709268 Figure 11-1 Search Patterns The FMS treats SAR waypoints as fly-by waypoints (e.g. involving turn anticipation). Crews should be aware of this characteristic when defining the search on the SAR page. Refer to Figure 11-2 (a), which is an example of a ladder pattern for a search field of 5 nm in width that needs to be flown with a track spacing of 1 nm.
Page 205 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 11-2 Ladder Search Pattern Details The following table provide the value for twice the turn radius. It can be added to the search area when entering leg length for ladder pattern searches or diameter for the sector pattern searches.
Page 206 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM When entering the ladder search, the FMS treats the entry waypoint of the search pattern as a fly-over. Hence the crew should ensure that the pattern is entered without a significant course change at the pattern entry waypoint, to avoid a large overshoot.
Page 207: Search Pattern In The Active Route
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SEARCH PATTERN IN THE ACTIVE ROUTE Display the ACT RTE x LEGS 1/X page by pressing the [LEGS] functional key. Enter “/S” in the scratchpad. The RTE LEGS 1/X page is displayed with "/S" in the scratchpad.
Page 208 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 6. For LADDER search, key in the leg width (between 0.1 and 4.0 nautical miles) into the scratchpad and move it to the TRACK SPACING field by pressing LSK 2R. and/or: 7. For SECTOR search, key in the angle (between 5 and 90 degrees) into the scratchpad and move it to the ANGLE field by pressing LSK 2R.
Page 209 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE 1 SECTOR 1/1 D I A M E T E R ARRIE R E F I D A N G L E ----- S A R B R G M A X G S...
Page 210 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 3. Press [INIT REF], <DES+SAR> or <TACTICAL> (LSK 6R). The DES+SAR or TACTICAL 1/2 page is displayed with the respective waypoint displayed in the REF ID field (LSK 1L). DES+SAR R E F I D ARRIE RTE DISCON>...
Page 211 8. Press ACTIVATE (LSK 6R) and the EXEC functional key. The waypoint identifier followed by “/S” is inserted in the flight plan and the CMA-9000 FMS will provide guidance for the defined search pattern as soon as the search origin will be reached.
Page 212 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 2. Enter the waypoint identifier in the ID field. RTE 1 SQUARE 1/1 T R A C K S P A C I N G ARRIE R E F I D ----- S A R B R G...
Page 213 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 5. Press the [EXEC] functional key. The search pattern is added as the first waypoint in the legs page followed by a discontinuity and the original flight plan. ACT RTE 1 LEGS 2 5 4 5 5 .
Page 214: Search Pattern In The Inactive Route
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SEARCH PATTERN IN THE INACTIVE ROUTE The same steps can be applied for the insertion of the search pattern procedures in the inactive route. Press <DES+SAR> or <TACTICAL> [NEXT] to access the INACT DES+SAR or TACTICAL 2/2 page. These steps relate to the inactive route pages: RTE y 1/X and RTE y LEGS 1/X.
Page 215: Search Pattern Using The Search And Rescue Menu
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SEARCH PATTERN USING THE SEARCH AND RESCUE MENU 1. Display the SQUARE/SECTOR/LADDER 1/1 page by pressing [INIT REF], <DES+SAR> or <TACTICAL>, and choose one of the three search patterns. 2. Define a search pattern origin by either entering a previously defined ID (Nav, Custom, User database or Temporary waypoint), or by defining a position relative to a REF ID (Nav, Custom, User database or Temporary waypoint).
Page 216 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE 1 SQUARE 1/1 T R A C K S P A C I N G PPOS R E F I D ----- S A R B R G M A X G S...
Page 217: Modifying An Existing Search Pattern
Direct-To course. B. AUTOMATIC EXIT After 80 search waypoints, the CMA-9000 FMS will automatically sequence to the next flight plan waypoint. The advisory message "END OF SEARCH" will then appear in the scratchpad. DISPLAYING THE SEARCH PATTERN PARAMETERS AFTER SEARCH DEFINITION Display the SQUARE/SECTOR/LADDER 1/1 page by pressing [INIT REF], <DES+SAR>...
Page 218: Search Pattern Deletion
MARK ON TOP (If configured) The CMA-9000 FMS can store the current system position in the predefined store point label "ONTOP". This position is displayed on the PREDEF WPT 2/2 page and can be used also for creating a new user waypoint.
Page 219 <NEW USER WPT DES+SAR> Pressing <MARK>, (LSK 5R) stores the current CMA-9000 FMS system position in the predefined store point label “MARK ON TOP”. B. {If CFG KEY 2 is configured to MARK}. The [MARK] functional key becomes active and the softkey <MARK ON TOP>...
Page 220: Hover Procedure (Transdown To Hover) (If Configured)
• In the first phase the CMA-9000 FMS computes a trajectory in order to put the aircraft in the correct wind direction. The helicopter is brought to a point TDN facing the wind. The TDN point located at the same altitude as the beginning of the maneuver is obtained by calculating a guided automatic transition distance (DTRA) to the MRK point.
Page 221 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM • One input allows the CMA-9000 FMS to receive a position for the MRK point from an external device such as a Weather Radar or DMAP. • The other input (installation-dependent) allows the CMA-9000 FMS to receive a position for the MRK point, to activate and execute the hover procedure by pressing an external push-button.
Page 222 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MARK WIND 0109018 Figure 11-4 WIND MARK 0109017 Figure 11-5 This page is printed under user's responsibility and must not be retained for reference Page 11-20 Revision 1 December 08, 2009...
Page 223 MRK point if needed. Otherwise press [EXEC] to insert the TDN and MRK waypoints in the flight plan and initiate the guidance. NOTE: The Hover height is entered on the AFCS and displayed on the CMA-9000 FMS HOVER page. One of the following actions can be used to exit the hover procedure: •...
Page 224 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM After the <ACTIVATE> key (LSK 6R) has been pressed, the HOVER 1/1 page is displayed: HOVER WPT01 M A R K O N T O P P O S N 4 0 0 9 . 6 1 W 0 8 9 2 0 .
Page 225: User Database
- - R O U T E D I S C O N T I N U I T Y - KLAX LEGS ETA> TRANSITION DOWN USER DATABASE The CMA-9000 FMS contains a User database which is used to store user waypoints and user routes. User waypoints can be: • entered from the scratchpad or •...
Page 226: Manual Entry Of A Fixed User Waypoint In The Database
3. Enter the position at LSK 1R or enter the Bearing/Distance at position LSK 2L. By entering a Bearing/Distance, the CMA-9000 FMS computes a position using as reference the present position and displays the coordinates of the user waypoint to be displayed on LSK 1R. The number of available waypoints are displayed in the “FREE=“field (a maximum of 460 user waypoints can be defined).
Page 227: Manual Entry Of A Moving User Waypoint In The Database
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 4. When the mandatory fields are filled (e.g. name and position of the new user waypoint), a CANCEL/CONFIRM prompt is displayed. Press <CONFIRM> to accept (LSK 6R) or <CANCEL> (LSK 6L). B. MANUAL ENTRY OF A MOVING USER WAYPOINT IN THE DATABASE Access the USER WPT 1/2 page by pressing [INIT REF], <WPT DATA>...
Page 228 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 6. After confirming, the moving waypoint is saved in the user database and can be viewed in the user waypoint list (user waypoints are displayed in alphabetical order on the USER WPT LIST 1/1 page).
Page 229: Manual Entry Of An Airport Type User Waypoint In The Database
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. MANUAL ENTRY OF AN AIRPORT TYPE USER WAYPOINT IN THE DATABASE Access the USER WPT 1/2 page by pressing [INIT REF], <WPT DATA> (LSK 1R), and <NEW USER WPT> (LSK 6L). 1. Enter the waypoint identifier in the ID field at LSK 1L.
Page 230 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM USER WPT ADFF I D / P O S F R E E = 4 5 9 12.23 043 32.12 B R G / D I S /115 T Y P E >FIXED R E F W P T I D...
Page 231: Delete All The User Waypoints From The User Database
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. DELETE ALL THE USER WAYPOINTS FROM THE USER DATABASE All the user waypoints can be deleted from the user database using a single prompt DELETE ALL on the USER WPT 2/2 page. The same prompt is also available from the USER WPT LIST X/Y page.
Page 232: View All The User Waypoints In The Database
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM F. VIEW ALL THE USER WAYPOINTS IN THE DATABASE The complete list of the user waypoints can be viewed by pressing [INIT REF], <WPT LISTS>, <USER WPT>. Up to 10 user waypoints are displayed on a single page and a maximum of 460 waypoints can be defined.
Page 233: Creating A User Waypoint From A Mark On Top Or A Joystick Position
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM USER WPT I D / P O S F R E E = 4 5 8 12.23 043 32.12 B R G / D I S /115 T Y P E >FIXED R E F W P T I D...
Page 234: Creating A User Waypoint From A Flir Position
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 1. By pressing the <NEW USER WPT> prompt (LSK 6L) the USER WPT 1/2 page is displayed and the most recent acquired position (between the MARK ON TOP and the LAST JOYSTICK) is transferred to the REF WPT ID and POS field.
Page 235: Saving The Database For Use By Another Aircraft
I D L E 0 0 0 0 LOAD> <INIT/REF SAVE> 2. Press SAVE (LSK 6R) to start data download from the CMA-9000 FMS to the Data Loader Unit (only when aircraft on ground). DATA LOAD T Y P E >USER_DATA...
Page 236: Central Clear? (If Configured)
CMA-9000 FLIGHT MANAGEMENT SYSTEM CENTRAL CLEAR? (If configured) When configured, the CMA-9000 FMS accepts a Central Clear command via an external input or via an FMS command from a line select key. When the external option is selected, the aircraft installation provides the means to action this input.
Page 237: Backtrack Route (If Configured)
NOTE: The origin of a SAR or HOLDING procedure is included in the inverse route. When a manual Direct-To or a Direct-To with Intercept is performed in the active route, the CMA-9000 FMS adds a temporary waypoint to the inverse route to mark the present position except when on ground or during the special procedures mentioned above.
Page 238 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM When the Inactive route is engaged, the CMA-9000 FMS keeps the existent waypoints in the backtrack route and continues adding waypoints to the same backtrack route list as the new route is flown. The backtrack route records the waypoint attribute (flyby or flyover).
Page 239: Rendez-Vous With A Moving Waypoint (If Configured)
The rendez-vous position is recomputed as long as the Time To Go (TTG) is over one minute. In the case of an achievable rendez-vous, the CMA-9000 FMS uses the rendez-vous position in the flight plan and provides guidance data relative to the direct course computed inbound to this rendez-vous position.
Page 240: Navigation Of Direct-To A Waypoint When Cma-9000 Fms Is Configured For A "Moving Dtk" Direct-To
FD/AP based on the aircraft present position and track. Initially the CMA-9000 FMS uses the bearing from the aircraft position to the Direct-To waypoint as the intercept course, because the aircraft position is changing the intercept course changes. The aircraft remains on the variable intercept course and consequently the lateral deviation is kept centered until the track angle error becomes smaller than +/-2 degrees.
Page 241: Navigation Of Tactical Direct-To A Waypoint
CMA-9000 FLIGHT MANAGEMENT SYSTEM NAVIGATION OF TACTICAL DIRECT-TO A WAYPOINT When a Tactical Direct-To a waypoint procedure is executed, the CMA-9000 FMS provides Roll steering, track angle error and lateral deviation guidance to the FD/AP based on the aircraft present position and track.
Page 242: Tactical Direct-To A Waypoint In The Inactive Route
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 6. Move the waypoint identifier to the TO WPT field by pressing LSK 1L. "ACT" status on the title line is replaced by "MOD". The direct course and distance from aircraft present position to the TO waypoint is displayed.
Page 243: Bulls Eye (If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM BULLS EYE (If configured) Display BULLS EYE 1/3 page by pressing [INIT REF], <BULLS EYE> {if no CFG KEY is configured to BULL} or [BULL] {if any CFG KEY is configured to BULL}. Press [NEXT] or [PREV] to scroll to page 2/3 or 3/3.
Page 244 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. After modifying the Bulls Eye waypoint and entering all mandatory fields. BULLS EYE BULL B U L L I D / P O S 26.20 E004 52.32 B R G / D I S...
Page 245 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 3. Then the Bulls Eye target point can be created (use BULLS EYE 2/3 page). Definition of Bulls Eye Target can be achieved by typing a waypoint ident (from any FMS databases) on LSK 1L. This will take the waypoint coordinates and the ident and assigned them to the Bulls Eye Target point.
Page 246 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Initial entry page for moving Bulls Eye target. BULLS EYE BETGT T G T I D / P O S B R G / D I S T K / G S /---...
Page 247 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. After entering DELETE on the Bulls Eye Target waypoint. BULLS EYE BETGT T G T I D / P O S 26.20 E004 52.32 B R G / D I S T K / G S...
Page 248 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM When a rendezvous point is achievable, the rendezvous bearing and distance relative to the aircraft present position and to the Bulls Eye reference point are displayed. Also, the Bulls Eye target estimate time of arrival (ETA) or estimated time en-route (ETE) and delta altitude are displayed on LSK 5L and LSK 5R respectively.
Page 249: Tactical Approach (If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TACTICAL APPROACH (if configured) NOTE: The TACTICAL APPROACH function has been designed to make as much use of the FMS’s already existing VNAV approach mode function. Consequently, much of the logic which tactical approaches uses is exactly the same as that which applies to the VNAV approach function.
Page 250 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 11-7 Tactical Approach Lateral Profile Geometry TIAF VDEV is relative to this segment (FMS TFAF calculated) Altitude constraint @ TIAF (user definable or (user definable or FMS calculated) FMS calculated) Altitude constraint @ TFAF...
Page 251 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM When mandatory entries are entered the FMS will compute the coordinates and altitude constraints of the TIAF, TFAF, MAP, TMAP1, TMAP2 waypoints using the default tactical approach parameters. TACTICAL APPR 1/3 R E F W P T I D...
Page 252 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Modified Tactical Approach Parameters Will be recomputed Path Affected Distance NOTE: Altitude constraints of tactical approach waypoints remain constant when the following parameters are changed. • TIAF coordinates, Vertical & TIAF-to-TFAF distance (LSK 2L) •...
Page 253 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The second Tactical Approach page presents the information related to the Tactical Missed Approach segment. The FMS automatically generates a Tactical Missed Approach procedure based on default parameters. Refer to Figure 11-9 and 11-10 for lateral and vertical Tactical Missed Approach Profiles.
Page 254 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TMAP2 TMAP1 Final Approach Course (user definable) (user definable) MAP-TO-TMAP1 (user definable) Figure 11-9 Tactical Missed Approach Lateral Profile Geometry TMAP2 CLIMB GRADIENT 2 (FMS calculated) TMAP1 CLIMB GRADIENT 1 (FMS calculated) Altitude constraint...
Page 255 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Modified Tactical Missed Approach Parameters Will be recomputed Path Affected Distance NOTE: Altitude constraints of tactical approach waypoints remain constant when the following parameters are changed. • TMAP1 coordinates Vertical & • TMAP2 coordinates...
Page 256 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Parameters Unit Minimum Default Maximum TIAF-to-TFAF distance 2.00 3.00 20.00 TFAF-to-MAP distance 4.00 5.00 20.00 MAP-to-TMAP1 distance 1.00 2.00 10.00 TMAP1-to-TMAP2 distance 1.00 4.00 20.00 Initial Approach Angle (IAA) -10.0 -3.0 Vertical Path Angle (VPA) -10.0...
Page 257 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Figure 11-11 Tactical Approach VDEV indication CAUTION: The VDEV provided by the FMS is always to the Final Approach segment as depicted on Figure 11-11. See additional details on the TACTICAL APPR page in Appendix A.
Page 258: Entering A Tactical Approach
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ENTERING A TACTICAL APPROACH A flight plan can only contain a single approach and/or arrival procedure at any given time. Should an approach already exist in a flight plan, this would need to be removed from the flight plan before the tactical approach can be inserted.
Page 259: Tactical Approach Selection From Database (Optional)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TACTICAL APPROACH SELECTION FROM DATABASE (Optional) When a Tactical Approach database is loaded in the FMS the crew can select a tactical approach from the ARRIVALS page. PANC ARRIVALS S T A R S...
Page 260: Modification Of A Tactical Approach In Flight Plan
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MODIFICATION OF A TACTICAL APPROACH IN FLIGHT PLAN 1. This is achieved by going to the TACTICAL APPR page via any means (e.g. entering /A on top of the tactical approach MAP on the LEGS page or via the DES+SAR or TACTICAL page 2/4) and changing the desired tactical approach parameter(s) only when the "TO"...
Page 261: Calculated Air Release Point (Carp) And High Altitude Release Point (Harp) (If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CALCULATED AIR RELEASE POINT (CARP) AND HIGH ALTITUDE RELEASE POINT (HARP) (If configured) NOTE: Hereafter, unless specifically mentioned references to ‘Calculated Air Release Point’ or ‘CARP’ also includes and pertains to the following procedures: Custom HARP, Custom HAHO, Free Fall.
Page 262 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E S C A P E P O IN T W P T 1 0 ( E S C ) T R A IL IN G E D G E (T E ) E X T E N D E D T R A IL IN G E D G E...
Page 263 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM WPT10 WIND DIRECTION ESCAPE POINT PARACHUTIST MAX DRIVE DISTANCE RED LIGHT GREEN LIGHT SLOWDOWN POINT POINT IMPACT(PI) WPT09 IDENTIFICATION TURNING POINT POINT Figure 11-13 Typical HAHO Profile This page is printed under user's responsibility...
Page 264: Initiation Of A Carp/Harp Procedure
EFIS, “CARP Active” and “At CARP” remote annunciators, CARP PROGRESS page displays and CMA-9000 Display Panel scratchpad advisories. Two CARP procedures may be simultaneously defined, one on the active route and another on the inactive route.
Page 265 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Execute the following steps: 1. Manually type CRP01/C in the scratchpad. 2. Selected the flight plan location on the LEGS page. This automatically inserts the CARP procedure in the selected flight plan location and brings up the CARP PLAN 1/3 page in MOD state.
Page 266 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 4. The CUST CARP selected CARP PLAN 1/3 page is displayed. RTE1 CARP PLAN 1/3 T Y P E >CUST CARP ----- IDENT POINT (IP) - - - o - - . - - - - - - o - - . - -...
Page 267: Carp Plan 1/3 (If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. The FREE FALL selected CARP PLAN 1/3 page is displayed. RTE1 CARP PLAN 1/3 T Y P E >FREE FALL ----- IDENT POINT (IP) - - - o - - . - - - - - - o - - . - -...
Page 268 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Active status and sample inputs - Custom HARP. ACT RTE1 CARP PLAN 1/3 T Y P E >CUST HARP CDFB I D E N T P O I N T ( I P ) N 4 5 0 0 .
Page 269 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT/MOD/" " RTE x (title): ACT indicates that the EXECuted CARP procedure is active (CARP Active discrete is on). MOD indicates the CARP procedure modifications have not been EXECuted yet. A blank field indicates the CARP procedure: •...
Page 270: Carp Plan 2/3 (If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ERASE [6L]: Cancel any active route modifications and/or any CARP parameter changes. Only displayed when the page is displaying the MOD status. If by pressing ERASE the CARP procedure is removed from the flight plan, then the LEGS page is automatically displayed.
Page 271 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Custom HARP view: RTE1 CARP PLAN 2/3 P I E L E V S D D I S T 5000 3 . 1 I A S / H A T - D R O P -...
Page 272 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT/MOD/" " RTE x (title): ACT indicates that the EXECuted CARP procedure is active (CARP Active discrete is on). MOD indicates the CARP procedure modifications have not been EXECuted yet. A blank field indicates the CARP procedure: •...
Page 273 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HI MEAN WIND [4L]: Displayed for CUST HARP only. Mean Effective Wind (MEW) direction and speed (()/(kt) or (T)/(kt) from the drop altitude to the actuation altitude to be used in the FMS CARP calculations. Unit used depends on current display setup (true or mag).The default display is computed by the FMS based on current...
Page 274: Carp Plan 3/3 (If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP PLAN 3/3 (If configured) Display CARP PLAN 3/3 page by pressing [INIT REF], <DES+SAR> or <TACTICAL>, [NEXT], <CARP>, [PREV] when a CARP procedure is in the displayed flight plan or [TACT], [PREV] when TACT key is configured and a CARP procedure is in the displayed flight plan.
Page 275 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Custom HAHO view: RTE1 CARP PLAN 3/3 F T T 5 3 . 4 S E C E X I T T I M E 45.0 S E C D E C E L Q U O...
Page 276 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HORIZONTAL DISTANCE [1L]: Displayed for Free Fall only. Horizontal distance of fall, in meters, traveled by the load. Extracted from the free fall ballistic data tables. Default display is boxes. Range [0..999]. VERT DIST [1R]: Displayed for CUST CARP and CUST HARP only. Vertical distance (ft) traveled by the load until stabilization.
Page 277: Carp Progress X/X (When X/X = 4/4 If 3 Page Set And Carp Is Configured Or X/X = 5/5 If 4 Page Set And Carp Is Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ERASE [6L]: Cancel any active route modifications and/or any CARP parameter changes. Only displayed when the page is displaying the MOD status. If by pressing ERASE the CARP procedure is removed from the flight plan, then the LEGS page is automatically displayed.
Page 278 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Display with CARP procedure in the flight plan. ACT CARP PROGRESS 5/5 C A R P P O S N E A R C A R P N 4 5 0 0 . 0 0 W 0 7 2 0 0 .
Page 279 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP ETE (3L): Estimated Time (sec) EnRoute (ETE) to CRP (green light) waypoint or XTE (red light) once CRP has been sequenced or ESC once XTE is sequenced. The “CARP” indication changes to “XTE” upon sequencing the CRP waypoint.
Page 280: Carp Sequence Of Events
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP SEQUENCE OF EVENTS The following table presents normal events and actions related to CARP procedures. The ordering is typical, but may vary based on the entered geometry, mission, and ballistic parameters. Event FMS Action Operator Action •...
Page 281 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Event FMS Action Operator Action • “SLOWDOWN” advisory message displayed on the • Begins slowdown Slowdown waypoint (SD) is reached scratchpad and altitude change • Current and Target TAS and Altitude displayed on to mission values.
Page 282: Carp Alert Messages
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP ALERT MESSAGES The FMS monitors the altitude, speed, and cross-track error during a CARP procedure. The altitude and speed errors are obtained using the entered mission Indicated Air Speed (IAS) and Height Above Terrain (HAT) values on the CARP PLAN pages.
Page 283: Exit From Carp
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. At one minute from the CRP waypoint, the alert messages “CARP ALT NOT MET” or “CARP TAS NOT MET”, and “NO CARP SOLUTION” are raised. If the situation is corrected prior to 10 seconds to CRP, then the situation reverts to A or B;...
Page 284: Carp Wind Entry
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP WIND ENTRY The FMS allows for entry of forecast winds at 4 different flight levels in order to compute a more accurate CARP lateral profile. If a CARP flight plan already exists, then entering CARP winds is applied to the modified flight plan.
Page 285: Position Updates For Carp - General
A "temporary" update used to implement a coordinate frame shift of CARP flight plan waypoint positions from a local coordinate system to the coordinate system used by the CMA-9000. This is useful when the aircraft is flying in a region where the local terrain map/database being used is very precise relative to some local Identification Point (IP) landmark (e.g.
Page 286: Carp Mark Temporary Position Update
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP MARK TEMPORARY POSITION UPDATE When the CARP status is ACTIVE and there is at least a period of 10 seconds before reaching the CRP (green light) waypoint and a CARP solution exists (e.g. the NO CARP SOLUTION scratchpad message is not being annunciated), then the CARP MARK prompt appears on both the TMP UPDATE POS page and CARP PROGRESS page.
Page 287: Ending A Temporary Carp Position Update
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 3. At LSK 1R, enter the desired relative bearing/distance or crosstrack offset at to the known position, as applicable. 4. Press the EXEC key. ENDING A TEMPORARY CARP POSITION UPDATE A CARP temporary position update will end automatically when either: 1.
Page 288: Cospas/Sarsat Distress Beacon Handling (If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COSPAS/SARSAT DISTRESS BEACON HANDLING (If configured) NOTE: The FMS allows communication with DF equipment (DF-935-12, DF-430-102, or DF-430-112) which provides information related to COSPAS/SARSAT distress beacons. Distress beacon information can be used by the FMS for navigation purposes.
Page 289 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM In order to uncluttered the EFIS & DMAP displays, the operator can define which beacon received are to be displayed on EFIS & DMAP; this is done by: 1. Defining if the received beacon needs to be displayed or not (setting is done from the detail beacon page named SARSAT DATA page).
Page 290: Target Position Reception (From Atos And/Or Radar, If Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TARGET POSITION RECEPTION (from ATOS and/or RADAR, if configured) If configured, the Galileo Avionic ATOS LW equipment (Airborne Tactical Observation and Surveillance System – Light Weight) and/or FIAR 1500B RADAR equipment can transfer to the FMS a target position upon operator selection.
Page 291: Atos Flight Plan Transfer To Fms (If Atos Is Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DES+SAR [6R] or TACTICAL [6R]: When TACT key is configured, the DES+SAR prompt is replaced by TACTICAL. In this case, the prompt gives access to the TACTICAL page instead of the DES+SAR page. When there is no data in the scratchpad, selection of this key will create a temporary waypoint with the Radar Target or the ATOS Target position (the most recent one received is selected) and the temporary waypoint ID is entered in the REF ID field of the DES+SAR 1/Y (or TACTICAL 1/Y) page.
Page 292 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. MISSION page is displayed when a flight plan transfer request is received from the ATOS equipment. Furthermore, reception by the FMS of a request from the ATOS to transfer its mission flight plan waypoints is also communicated to the flight crew by displaying the ATOS TRANSFER REQUESTED status advisory scratchpad message.
Page 293 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM This page is displayed when the flight plan transfer from the ATOS failed. MISSION R A D A R T A R G E T 1 3 1 5 : 1 0 N 4 5 ° 3 4 . 2 5 W 1 2 2 ° 4 5 . 1 2...
Page 294: Fms Waypoint Transmission To Radar (If Fiar 1500B Radar Is Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS WAYPOINT TRANSMISSION TO RADAR (if FIAR 1500B RADAR is configured) When the FIAR 1500B RADAR is configured, the FMS continuously transmits (up to) the first 10 active flight plan waypoints* to the FIAR 1500B RADAR equipment.
Page 295 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 12 - NAVIGATION SENSORS CONTENTS Subject Page GENERAL ................................12-1 GPS NAVIGATION (CIVIL) ..........................12-1 GLOBAL POSITIONING SYSTEM PAGES (ARINC 743A/ARINC 743/TRIMBLE TA-12 format)....12-2 MILITARY GPS NAVIGATION.........................12-4 EGI NAVIGATION ............................12-4 INS/GPS SYSTEM PAGES (EGI format)......................12-5 INS/DVS NAVIGATION MODE (SAGEM EGI configuration only) .............12-10...
Page 296 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM This Page Intentionally Left Blank This page is printed under user's responsibility and must not be retained for reference Page 12-ii November 19, 2009...
Page 297: General
99.99999% of the time without a satellite failure, and 99.9% of the time in the presence of a satellite failure. The HIL is compared in the CMA-9000 FMS to the value required for the phase of flight (alert limit), and an alert is generated when the integrity value exceeds the alert limit.
Page 298: Global Positioning System Pages (Arinc 743A/Arinc 743/Trimble Ta-12 Format)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The combination of a GPS INT annunciator as well as an alert message GPS NAV LOST provides an indication between the loss of FDE (Failure Detection and Exclusion) availability and the loss of navigation.
Page 299 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 2. Display the GPS STATUS 2/2 page by pressing [INIT REF], <NAV STATUS> (LSK 5R), <GPS> (LSK 1R), [NEXT]. For dual GPS installations (civil & Litton LN-100GT EGI), display the cGPS STATUS 2/2 page by pressing [PREV] or [NEXT].
Page 300: Military Gps Navigation
In addition to the hybrid INS/GPS the EGI also provides a pure GPS and a pure INS position solutions. The CMA-9000 FMS reverts to the pure GPS position or to another sensor when the quality factor or integrity of the INS/GPS has degraded below what is required for the phase of flight. In this case the CMA-9000 FMS may select the pure GPS or pure INS position (available with the Litton LN-100 GT EGI) if the remaining sensors are not fit for navigation.
Page 301: Ins/Gps System Pages (Egi Format)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INS/GPS SYSTEM PAGES (EGI format) There are no data entries on these pages except for the INS STATUS page when in ALIGN mode. For additional information refer to Appendix A. 1. Display the GPS STATUS 1/2 page by pressing [INIT REF], <NAV STATUS> (LSK 5R), <GPS> (LSK 1R).
Page 302 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. LITTON LN_100GT EGI with dual GPS configured: GPS STATUS P O S I T I O N N 4 5 3 4 . 2 5 W 0 7 3 3 8 . 0...
Page 303 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. LITTON LN_100GT EGI installation: GPS STATUS K E Y S T A T U S F A I L C O D E K E Y V E R 0 0 0 0...
Page 304 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 4. Display the INS/GPS STATUS 2/2 page by pressing [INIT REF], <NAV STATUS> (LSK 5R), <INS/GPS> (LSK 5R) and [NEXT]. A. SAGEM SIGMA50H EGI installation: INS/GPS STATUS 2/2 H D G / D A 0 6 0 .
Page 305 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 5. Display the INS STATUS 1/1 page by pressing [INIT REF], <NAV STATUS> (LSK 5R) and <INS> (LSK 5R). NOTE: The INS STATUS 1/1 page is available only when the LITTON LN_100GT EGI is configured.
Page 306: Ins/Dvs Navigation Mode (Sagem Egi Configuration Only)
INS/DVS NAVIGATION MODE (SAGEM EGI configuration only) A stand-alone inertial/DVS navigation mode is selected for use by the CMA-9000 FMS when higher priority navigation modes are unavailable or not adequate for the phase of flight. For additional information refer to Section 1.
Page 307 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM EGI status, position, accuracy, TK and GS are displayed. INS/DVS STATUS 1/2 P O S I T I O N N 4 5 3 4 . 2 5 W 1 2 2 4 5 . 1 2...
Page 308: Position Update
CMA-9000 FLIGHT MANAGEMENT SYSTEM POSITION UPDATE This section describes the procedure to update the INS or the DVS position with the CMA-9000 FMS-computed or other known positions. It is applicable for the INS/GPS, INS/DVS, and pure inertial or DVS modes.
Page 309 • indirectly with a waypoint ID at (LSK 1L), if desired add a distance/bearing offset at (LSK 1R). • or by toggling (LSK 1L) to the CMA-9000 FMS or the joystick selection and selecting the corresponding position. • Press the MARK key.
Page 310 / 2 . 0 0 <CANCEL CONFIRM> MARK function key not configured, changing the reference with the CMA-9000 FMS position: A. UPDATE POS 1/1 default state; the CMA-9000 FMS position is used by default. UPDATE POS R E F >...
Page 311 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. UPDATE POS 1/1 sensors selected, MARK key pressed, position update ready to be confirmed and sensors to be updated (INS/DVS and INS/GPS) selected. UPDATE POS R E F B R G / D I S T >...
Page 312: Dme Navigation
CHECK QF DME NAVIGATION The DME/DME navigation mode is selected for use by the CMA-9000 FMS when higher priority navigation modes are unavailable or not adequate for the phase of flight. For additional information refer to Section 1. DME/DME is used in areas with sufficient DME coverage and for which the appropriate navigation database is installed.
Page 313: Dme Station Monitor
DME STATION MONITOR The DME page displays those stations used by the CMA-9000 FMS in DME navigation. A total of six DME stations may be used to determine the aircraft's position. At least three stations are required to navigate in DME/DME mode.
Page 314: Dme Station Deselection
In some situations, the operator may choose to deselect a DME station due to known problems with the station so as to prevent the CMA-9000 FMS from using this station in its DME station selection process for DME navigation. To deselect a DME station, proceed as follows: 1.
Page 315: Vor/Dme Or Vor/Dme/Tacan Navigation Mode
For additional information refer to Section 1. The CMA-9000 FMS uses the VOR or TACAN radial bearing in conjunction with a DME or TACAN slant range from a manually tuned VOR/DME and/or TACAN stations to compute a VOR/DME/TACAN-based position.
Page 316 Depending on the DVS installed in the aircraft, the CMA-9000 FMS will receive and process x and y velocity data which, when combined with heading and attitude allows the CMA-9000 FMS to compute the aircraft position, ground speed, altitude, status and maintenance data.
Page 317 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM A. RDN-85 DVS installation. 1. Display the DVS STATUS 1/2 page via the NAV STATUS INDEX 1/1 page. 2. The velocity in each of the three axes and the DVS functional mode are displayed.
Page 318 The system wind being displayed here is the same as may be observed on the PROGRESS 1/4 page. For the DVS, the wind value is used by the CMA-9000 FMS in the estimation of surface water current. This page is printed under user's responsibility...
Page 319: Inertial Navigation Via Kalman Filter
Navigation mode automatically reverts to inertial upon loss of GPS and radio navigation. The CMA-9000 FMS is using the Attitude and Heading Reference System (AHRS), and the GPS to provide a KALMAN Filter navigation mode. In this mode, the primary navigation sensor is the GPS receiver. The AHRS is used as a dead-reckoning navigation system by emulating an Inertial Navigation System (INS) with a KALMAN Filter performing closed-loop GPS based correction and alignment of the INS position.
Page 320: Kalman Status 1/1 Page
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CMA-9000 AHRS Data Kalman Correction Figure 12-1 KALMAN Filter Block Diagram The KALMAN Filter models the evolution of the AHRS errors according to the AHRS model. As long as GPS can provide measurement data with integrity, the AHRS errors can be continuously estimated and corrected in the emulated INS navigator.
Page 321: Inertial Navigation Mode
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INERTIAL NAVIGATION MODE The purpose of the FMS/inertial sensors interface is to provide a stand-alone inertial navigation mode for use when stand-alone GPS navigation and radio navigation are not possible. Reversion to the inertial navigation mode is automatic upon loss of GPS and radio navigation.
Page 322 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. LTN_101, LASEREF_V and ADIRU installation: IRS1 STATUS P O S I T I O N N 4 5 3 4 . 2 5 W 1 2 2 4 5 . 1 2 M O D E...
Page 323: Inertial - Position Initialization Process
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The crew can monitor the number of inertial sensors are used for navigation in the POS INIT 2/3 page by pressing [INIT REF], <POS INIT> (LSK 2R), [NEXT]. The number of inertial used for navigation is displayed next to the IRS mode.
Page 324: Irs System Pages
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM IRS SYSTEM PAGES There are no data entries on these pages except for the INS STATUS page when in ALIGN mode. For additional information refer to Appendix A. 1. Display the IRS STATUS 1/1 page by pressing [INIT REF], <NAV STATUS> and <IRS>.
Page 325: Inertial Navigation On High Latitude
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INERTIAL NAVIGATION ON HIGH LATITUDE When the system mixed inertial latitude exceeds 85 degrees N or S, the FMS will cease to compute a mixed inertial position. The system inertial position will slowly transition to coincide with the position of the inertial sensor closest to the mixed inertial position computed before the FMS present position latitude exceeded N-S 85 degrees.
Page 326 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM This Page Intentionally Left Blank This page is printed under user's responsibility and must not be retained for reference Page 12-30 November 19, 2009...
Page 327 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 13 - CMA-9000 FMS PAGES - RADIO TUNING CONTENTS Subject Page GENERAL ...............................13-1 RADIO TUNING LIBRARY ..........................13-2 RADIO 1/X or 2/X (Horizontal display format) .....................13-2 RADIO 2/X PAGE (Horizontal display format).....................13-9 RADIO 1/X or 2/X (Vertical display format)....................13-12 RADIO 2/X PAGE (Vertical display format) ....................13-16...
Page 328 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 13 - CMA-9000 FMS PAGES - RADIO TUNING CONTENTS Subject Page PHONE SEND SMS 3/3 ..........................13-67 PHONE PRECANNED SMS 1/1 ........................13-68 PHONE SMS MESSAGE 1/1 ........................13-70 PHONE STORED SMS 1/1 ...........................13-71 PHONE STORED SMS 1/N...........................13-72 PHONE DIALED TOP 1/N..........................13-73...
Page 329: General
(as confirmed by the INDEPENDENT OP alert message). The CMA-9000 FMS provides control and display of the active/standby frequencies and settings of all the radios interfaced on the RADIO Page. This page provides tuning entries and access to more detailed radio control pages, where self-test and radio modes can be selected.
Page 330: Radio Tuning Library
COM (VHF), NAV, ADF, VUHF, ATC, DF and Volume Control are supported. The RADIO 1/X page can be configured as the default cold start power up page of the CMA-9000 FMS. The RADIO 1/X page is displayed by pressing [RADIO].
Page 331 If the tuning operation is not successful they are displayed in small amber font as a warning to the pilot. The CMA-9000 FMS can be configured to allow burst tuning; either by CMA-9000 Display Panel entry or by a dedicated radio control head.
Page 332 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Operating Frequencies and Ranges: The operating frequencies for the Navigation and Communication radios are shown in the table below. An error message will appear in the scratchpad if invalid entries are made. RADIO LOWER LIMIT...
Page 333 CMA-9000 FLIGHT MANAGEMENT SYSTEM The CMA-9000 FMS also provides with the capability to tune V/UHF radios. For a frequency in the VHF band, the CMA-9000 FMS sets the modulation mode depending on the frequency band. For frequency in the UHF band, the modulation mode is selectable by the user.
Page 334 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIO <VHF1 1 1 8 . 4 0 0 ↔ 1 2 5 . 1 5 0 <VHF2 ↔ 1 2 4 . 6 5 0 151.000 Y J N - - - - <NAV1...
Page 335 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: It is also possible; for certain HF and V/UHF radios, to configure an external discrete which would inhibit access to the dedicated radio’s FMS control pages. In such cases, FMS NOT IN CTRL will be displayed in the field where the radio’s tuning information is normally displayed on this RADIO page.
Page 336 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ATCx [5R]: Used to display and modify the ATC active and standby codes from the current active transponder or from the last active transponder when toggled back to standby mode. Default value will be the primary transponder at power-up (cold start) when both transponders are in standby mode.
Page 337 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIO 2/X PAGE (Horizontal display format) Press [RADIO] [NEXT] to display RADIO 2/X page. The RADIO 2/4 page is only available when configured. RADIO <VUF1 ↔ 1 2 1 . 5 0 0 243.000 <VUF2...
Page 338 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Single SRT-651/N-F V/UHF radio configured in Maritime SHIP and DF modes active. Also, HF radio being control by alternate cockpit control panel: RADIO C 0 1 M - S H I P D F C 0 5 <VUHF...
Page 339 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Single SRT-651/N-F V/UHF radio configured - V/UHF not being controlled by FMS: RADIO VUHF F M S N O T I N C T R L O F F <DF SCAN 1 4 5 . 8 7 5 <ADF1...
Page 340: Radio 1/X Or 2/X (Vertical Display Format)
(e.g. 01//122.5). In this case the frequency entered will be that of the corresponding preset or ident from the library. The CMA-9000 FMS allows the user to select the previous/next preset from the library by entering '+' or '-' in the scratchpad and pressing the associated softkey.
Page 341 If the tuning operation is not successful they are displayed in small amber font as a warning to the pilot. The CMA-9000 FMS can be configured to allow burst tuning; either by CMA-9000 Display Panel entry or by a dedicated radio control head.
Page 342 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Radio Models Frequency / Channel Range Channel Spacing Band / Modulation (MHz) (KHz) SRT-651/N-A 30.000 - 87.975 108.000 - VHF/FM 117.975 VHF/AM SRT-651/N-F 118.000 - 155.975 VHF/AM 156.000 - 173.975 25 or 25/8.33* VHF/FM 225.000 - 399.975...
Page 343 Squawk (18 seconds). During the duration of the squawk, the CMA-9000 FMS is inhibit the toggle operation. If the transponder is in standby, an inverse video 'SBY' is displayed below the fixed caption ATC field.
Page 344: Radio 2/X Page (Vertical Display Format)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIO 2/X PAGE (Vertical display format) Press [RADIO] [NEXT] to display RADIO 2/X page. NOTE: This page is only available in the vertical configuration of radio top page. RADIO <COM1 COM2> <NAV1 NAV2> <ATC1 ADF1>...
Page 345 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIO TEST X/Y (2/Y or 3/Y or …) PAGE The RADIO top pages and RADIO TEST pages are configurable. However, the radio names (same acronyms as on the RADIO top pages) that appear are the ones whose self-test capability have been configured.
Page 346: Radio Test X/Y (2/Y Or 3/Y Or
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DME1 TEST [xL] and DME2 TEST [xR]: Displays DME test status & results. Where x = 1, 2, 3, 4, or 5. Other radios not shown in the figure that can be configured are: DF, COM, ADF, VUHF.
Page 347: Radio Pwr X/Y (2/Y Or 3/Y
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DF [1R]: Access to the DF LIBRARY 1/N page. FM1 [2R]: Access to the FM1 LIBRARY 1/N page. FM2 [3R]: Access to the FM2 LIBRARY 1/N page. UHF [4R]: Access to the UHF LIBRARY 1/N page.
Page 348: Navigation Radios (Nav Dme Radio)
50 KHz NOTE: The CMA-9000 FMS does not accept out of range values. An error message will appear in the scratchpad if invalid entries are made by the user. If the FMS has been disable for radio tuning via a discrete input, entries made to these radios will generate an error message "RADIO TUNING...
Page 349: Navigation Radios (Nav
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAVIGATION RADIOS (NAV Page 1/2) This page allows the pilot to control the operation of the NAV and DME radios by transmitting and receiving digital labels capable of controlling up to 2 NAV and 2 DME radios.
Page 350 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DME HOLD [4L], [4R]: Toggles DME hold status for the DME radio (not applicable for the VIR-31). The possible values are OFF and ON. For the VIR-32/DME-42 radio installation, this field is used as a status field only which means it cannot be toggled.
Page 351: Navigation Radios (Adf Radio)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAV1 MODE [1L]: Toggles NAV1 mode status for the NAV radio. The possible values are AUTOMATIC or MANUAL. NAV2 MODE [1R]: Same as above, but referencing NAV2 instead of NAV1. NAV1 TEST [3L]: Toggles NAV1 test status & results. Toggle options for test status are READY, CONFIRM?, STARTED.
Page 352: Navigation Radios (Adf
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAVIGATION RADIOS (ADF Page 1/2) This page allows the pilot to control the operation of up to 2 ADF units. Display the first ADF RADIO page from the horizontal configuration by pressing [RADIO], <ADF#> or [RADIO], [NEXT], <ADF#>...
Page 353 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAVIGATION RADIOS (ADF Page 2/2) This page allows the pilot to control the operation of up to 2 ADF units. NOTE: This page is only displayed if radio test is configured. Display the second ADF RADIO page from the horizontal configuration by pressing [RADIO], <ADF#>, [NEXT] or [RADIO], [NEXT], <ADF#>, [NEXT] or [RADIO], [RADIO], <ADF#>, [NEXT].
Page 354: Navigation Radios (Df Page 1/1 Or 1/2)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAVIGATION RADIOS (DF Page 1/1 or 1/2) The FMS will support the following Rockwell-Collins radios: • DF-430-102 • DF-935-12 In the frequency range and channel spacing specified below, in addition to ARGOS (401.650MHz) and...
Page 355 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. DF is in DF mode and FREQ sub-mode. Tactical frequency is not detected and the data is not available. B E A C O N S 130.000 1 4 9 . 8 7 5...
Page 356 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: When the SAR mode is active, the letter “S” will be seen in small green font on the RADIO X/Y page as shown just below. When the SCAN sub-mode is active, the word “SCAN” is also seen on RADIO X/Y page shown just below.
Page 357 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM F. DF is in SAR mode and 243 sub-mode. 243MHz beacon detected and data is displayed. B E A C O N S 243.000 2 4 3 1 3 0 . 0 0 0...
Page 358 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAVIGATION RADIOS (DF Page 2/2) This page is only available when "DF TEST" is configured. Display the first DF RADIO page from the horizontal configuration by pressing [RADIO], <DF>, [NEXT] or [RADIO], [NEXT], <DF>, [NEXT] or [RADIO], [RADIO], <DF>, [NEXT].
Page 359: Communication Radios (Vhf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: The FMS does not accept out of range values. An error message will appear in the scratchpad if invalid entries are made by the user. If the COM Frequency Source Selection discrete is set then entries made will generate an error message “RADIO TUNING DISABLED”...
Page 360 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SQUELCH [3R]: Same as above, but referencing COM2 instead of COM1. VOICE/DATA [5R]: When voice/data control is configured and for the VHF-422 and VHF-4000 VHF radios only, allows the crew to place the VHF radio in either the VOICE or DATA mode.
Page 361: Communication Radios (Rs-422 Fm1 Radio)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COMMUNICATION RADIOS (RS-422 FM1 RADIO) This page allows the pilot to control the operation of the FUG8 radio. The channel number is modified via scratchpad entry and then pressing [1L]. A channel entry can also be made via the FM1 library page.
Page 362: Communication Radios (Rs-422 Fm2 Radio)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM LIBRARY [6R]: Access to FM1 LIBRARY page (last page viewed). COMMUNICATION RADIOS (RS-422 FM2 RADIO) This page allows the pilot to control the operation of the FUG9 radio. The channel number is modified via scratchpad entry and then pressing [1L].
Page 363: Communication Radios (Rs-422 Uhf Radio)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PWR (5R): Indicates the power status (indicator only). Possible values are ON and blank. LIBRARY [6R]: Access to FM2 LIBRARY page (last page viewed). COMMUNICATION RADIOS (RS-422 UHF RADIO) This page allows the pilot to control the operation of the UHF radio. The frequency is modified via scratchpad entry and then pressing [1L].
Page 364 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COMMUNICATION RADIOS (VUHF RADIO) The VUHF radio equipment name is COM, however it can also be configured as COM1/COM2 or COM3/COM4 or VUF/VUHF or VUF1/VUF2. NOTE: The case displayed in this section is the “VUF” configuration.
Page 365 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Channel Designator Transmitting Frequencies (MHz) Ship Stations Coast Stations 156.025 160.625 156.050 160.650 156.075 160.675 156.100 160.700 156.125 160.725 156.150 160.750 156.175 160.775 156.200 160.800 156.225 160.825 156.250 160.850 156.275 160.875 156.300 156.300 156.325 160.925...
Page 366: Communication Radios (Vuf Radio Page 1/3) - For Srt-651/N-A V/Uhf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Channel Designator Transmitting Frequencies (MHz) Ship Stations Coast Stations 157.250 161.850 157.275 161.875 157.300 161.900 157.325 161.925 157.350 161.950 157.375 161.975 157.400 162.000 157.425 162.025 Figure 13-5: Maritime Channel-Frequency Pairing COMMUNICATION RADIOS (VUF RADIO Page 1/3) – for SRT-651/N-A V/UHF radio This page allows the pilot to control the operation of the VUHF radios by transmitting and receiving digital labels capable of controlling up to two SRT-651/N-A V/UHF radios.
Page 367 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM VUF1 [1L]: Display and modify the active/standby preset number and frequency/channel of the VUF1 radio. Entry from the keyboard is validated and then the frequency and preset/channel, if available, are placed in the standby field below the active field, otherwise an error message is displayed in the scratchpad. If the scratchpad is empty it toggles between active/standby identifiers.
Page 368: Communication Radios (Vuf Radio Page 2/3) - For Srt-651/N-A V/Uhf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COMMUNICATION RADIOS (VUF RADIO Page 2/3) – for SRT-651/N-A V/UHF radio This page allows the pilot to control the operation of the VUHF radios by transmitting and receiving digital labels capable of controlling up to two SRT-651/N-A V/UHF radios.
Page 369: Communication Radios (Vuf Radio Page 3/3) - For Srt-651/N-A V/Uhf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COMMUNICATION RADIOS (VUF RADIO Page 3/3) – for SRT-651/N-A V/UHF radio This page allows the pilot to control the operation of the VUHF radios by transmitting and receiving digital labels capable of controlling up to two SRT-651/N-A V/UHF radios.
Page 370: Communication Radios (Vuf Radio Page 1/3) - For Srt-651/N-F V/Uhf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DESENS (3L)/(3R): Display/control current desensitization mode state ON or OFF. When the VUHF STAT CTRL is configured to ENABLE, the GUARD ANT function option is displayed in large font white color with a caret in large font green color pointing inward; otherwise it is displayed in small font white color for the left and right side respectively.
Page 371 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The next several pages will show various examples the VUHF page layout following activation/selection of several V/UHF functions. Selection of TUNE 243 activates the 243 Emergency Guard Precedence: VUHF V U H F E M E R 243.000...
Page 372 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM VUHF [1L]: Display and modify the active/standby preset number and frequency/channel of the VUHF radio. Entry from the keyboard is validated and then the frequency and preset/channel, if available, are placed in the standby field below the active field, otherwise an error message is displayed in the scratchpad. Preset and channel are displayed in small font green color.
Page 373: Communication Radios (Vuhf Radio Page 2/3) - For Srt-651/N-F V/Uhf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TUNE 243 [5L]: Selection activates the emergency 243 guard precedence mode within the V/UHF radio. The FMS will then set the V/UHF control parameters as follows: • active frequency will be set to 243.000 •...
Page 374: Communication Radios (Vuhf Radio Page 3/3) - For Srt-651/N-F V/Uhf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Any of the following conditions will cause the DF mode to automatically be set to OFF: • activation of the TUNE GUARD function • the DF mode is already ON and RX MODE is changed from TR_G to TR •...
Page 375: Communication Radios (Hf Radio)
RADIO [6L]: Access to the RADIO top level page where the VUHF radio is located. COMMUNICATION RADIOS (HF RADIO) The CMA-9000 FMS also provides with the capability to tune HF radios. FREQ BAND LOWER LIMIT UPPER LIMIT 2000.0 KHz...
Page 376: Communication Radios (Hf Radio
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HF [1L]/[1R]: Display and modify the active/standby preset number and frequency/channel of the HF radio. Entry from the keyboard is validated and then the frequency and preset/channel, if available, are placed in the standby field below the active field, otherwise an error message is displayed in the scratchpad. If the scratchpad is empty it toggles between active/standby identifiers.
Page 377: Transponders (Atc
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TRANSPONDERS (ATC RADIO) The FMS supports the following ATC Radios in the code range and channel spacing specified below: NOTE: ATC Radio equipment name can be configured as “ATC”, “XPDR” or “TPDR”. ATCRBS MODE A...
Page 378 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ATC1 [1L]: Displays and allows modification of the active and standby identity code for the ATC1 transponder. Enter identifier in scratchpad and press LSK 1L. Entry may be made to the standby position only when a new value is in the scratchpad.
Page 379 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TRANSPONDERS (ATC Page 2/2) This page allows the pilot to control the operation of the ATC radios by transmitting and receiving digital labels capable of controlling up to 2 ATC units. NOTE: This page is only displayed if radio test is configured.
Page 380 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIO [6L]: Access to the RADIO top level page where the ATC transponder is located. CTL [6R]: Available only when the transponder is configured to be controlled by either the FMS or an external Mission Computer, otherwise this field is blank.
Page 381 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM IDENT [5L]: Allows the crew to add the Special Position Identification "IDENT" pulse to the IFF Mode 3/A reply. It is possible to re-initiate the "IDENT" period at any time, including those times during which it is already being transmitted.
Page 382 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MD 1 CODE [1L]: Used to display and set the two or four digit IFF Mode 1 code. The FMS displays a tuned active code in large font white color. During the tuning process, the active code is displayed in large font inverse white color.
Page 383 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIOS VOLUME 1/1 PAGE The page is only available when the MC has failed and the FMS has taken the control of the volume levels. Access to the RADIO VOLUME page is only available when the FMS has the control of the AMU.
Page 384 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE TOP 1/1 This page allows the pilot to access phone sub pages. This is the top level entry page for the phone system (either HCS or Iridium). Display PHONE TOP 1/1 page by pressing [RADIO], <PHONE>.
Page 385 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE VOICE CALL 1/2 This page allows the pilot to transmit/receive Phone Voice Calls. Display PHONE VOICE CALL 1/2 page by pressing [RADIO], <PHONE>, <VOICE CALL> (When the PHONE or HCS is configured) NOTE: The PHONE can only be configured in the "vertical" configuration option of the RADIO top page.
Page 386 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SELECT NAME OR PHONE# [1R]: If the phone number or the name/phone number exceeds 24 characters, then it will be possible to see the extra characters by pressing this soft key. The display will scroll to show the extra characters.
Page 387 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE VOICE CALL 2/2 This page allows the pilot to transmit/receive Phone Voice Calls. Display PHONE VOICE CALL 2/2 page by pressing [RADIO], <PHONE>, <VOICE CALL> [NEXT] (When the PHONE or HCS is configured) NOTE: The PHONE can only be configured in the "vertical"...
Page 388 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE STATUS (3L): Displays the phone status. For the GSM phone, the possible values are: CONNECTION ACTIVE, CONNECTION NOT ACTIVE, INCOMING CALL and GSM FAULT. For the iridium phone, the possible values are: -----------, READY, UNAVAILABLE, UNKNOWN, RINGING, IN PROGRESS.
Page 389 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE READ SMS 1/N This page provides the pilot with access to incoming SMS text messages received from the Phone. The incoming messages are listed in order of age (most recent message on top). The messages are assigned a name which includes its time of reception of the format selected on the CONFIG->DISPLAY->DATE selection.
Page 390: Phone Send Sms 3/3
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE SEND SMS 1/3 This page allows the pilot to select the person to whom the SMS is for. Display PHONE SEND SMS 1/3 page by pressing [RADIO], <PHONE>, <SEND SMS>. (When the PHONE or HCS is configured) NOTE: The PHONE can only be configured in the "vertical"...
Page 391 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM POWER [4R]: (not shown on figure) Turns the phone ON or OFF. Only applicable to GSM phone. Not applicable to Iridium configuration. NOTE: Will display dashes when communication is totally lost. WRITE TXT [5R]: Goes into text editing mode. When WRITE TXT is selected, the page 2/3 is automatically displayed.
Page 392 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM This page is displayed as follows once the SMS text message has been edited and is ready to be transmitted (READY TO TRANSMIT mode): NOTE: The message to be transmitted can only contain a maximum of 160 alphanumeric characters.
Page 393 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SAVE SMS [4R]: This prompt is only available in READY TO TX mode. The default value is READY. When pressed, the text is saved in the first available slot. Each subsequent press will "push" the older message saved to the slot n+1 (queue principle).
Page 394 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM POS REPORT [6L]: When operating in EDIT mode, pressing this key enters the current date & time, the flight identifier (as entered on the RTE page) and the current aircraft position (in whatever format selected on the SETUP page).
Page 395 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE SEND SMS 3/3 This page allows the pilot to enables the pilot to monitor SMS call status & to hang-up during an SMS transmission. Access to the PHONE: SEND SMS 3/3 page, from the vertical configuration, is as follows: [RADIO], <PHONE>, <SEND SMS>...
Page 396: Phone Precanned Sms 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE PRECANNED SMS 1/1 Display PHONE PRECANNED SMS 1/1 page by pressing [RADIO], <PHONE>, <PRE-CANNED SMS> (When the PHONE or HCS is configured), or  [ANS] (When the HCS (GSM phone) and ANS key are configured and no new unread message nor new received call) NOTE: The PHONE can only be configured in the "vertical"...
Page 397 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MISSION1 [1L]: Pressing this key can lead to two different results: 1. If the "MISSION 1" pre-canned SMS text message contains additional text, then the displayed page will automatically change to the SEND SMS page and the “MISSION 1” template SMS text message will be automatically loaded into this page.
Page 398: Phone Sms Message 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PHONE SMS MESSAGE 1/1 This page provides the operator with a display of the incoming SMS text messages. There is a maximum of 160 characters (or 6 lines maximum) that are available for the incoming SMS text message. An auto wrap feature will break lines between words for readability.
Page 399: Phone Stored Sms 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM READ NEW [6R]: This prompt will only be displayed when a new SMS text message is received (as indicated by the <SMS> annunciator becoming lit) while this page is already displaying a previously received SMS text message.
Page 400: Phone Stored Sms 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SMS1 to SMS10 [1L to 5R]: Access to STORED SMS page x/10 to display the stored SMS text messages. PHONE TOP [6L]: Access to PHONE top page. CANCEL [6L]: Cancels the deletion of a saved SMS.
Page 401 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM [1R] [5R]: When the message text contains more than 10 lines up and down cursors appear at position 1R and 5R to allow scrolling window movement. The 1R prompt will move the window one line up and the 5R prompt will move the window one line down.
Page 402: Com Library 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM [1L]: Display of called name (if available) and called number. [1R]: Display of date & time the call was made & call type. The call type option is either CALL: or SMS:. [2L..5L] & [2R.5R]: Display of n+1, n+2,n+3, n+4, n+5 calls made (next in history). Where n is based on the page number.
Page 403 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM • Ex: To change 04/ABC /111.050 to 04/ABC /112.075 at LSK 2L press the following keys: a) “//112.075” and LSK 2L or b) LSK 2L to transfer the current library record into the scratchpad, press the [CLR] key 5 times to erase the 5 last characters of the frequency, then enter the new frequency by pressing [2],[.],[0],[7],[5] and...
Page 404: Nav Library 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAV LIBRARY 1/N This page allows the pilot to view and modify the preset numbers, identifiers and frequencies that are stored in the NAV radio library. Display NAV LIBRARY 1/N page from the horizontal configuration by pressing [RADIO], [NEXT], <NAV> or [RADIO], <NAVx>, <LIBRARY>.
Page 405: Adf Library 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADF LIBRARY 1/N This page allows the pilot to view and modify the preset numbers, idents and frequencies that are stored in the ADF radio library. The functionality of the page is the same as the COM or NAV LIBRARY page.
Page 406: Fm1/Fm2 Library 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RS-422 FM1/FM2 LIBRARY 1/N This page allows the pilot to view and modify the preset numbers, identifiers and channels that are stored in the FM1/FM2 radio library. The functionality of the page is the same as the COM or NAV LIBRARY page.
Page 407: Uhf Library 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RS-422 UHF LIBRARY 1/N This page allows the pilot to view and modify the preset numbers, identifiers and frequencies that are stored in the UHF radio library. The functionality of the page is the same as the FM1 LIBRARY page.
Page 408 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM VUHF LIBRARY 1/N (SRT-651 V/UHF RADIOS) This page allows the pilot to view and modify the preset frequencies in the VUHF library. It also allows user to select an entry and set the preset frequency in the active or standby field.
Page 409 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM [1L],[2L],[3L],[4L],[5L]: Display and modify VUHF library entries. Same comments as for the COM library entry apply here except that the modulation must be added with a slash as the last entry. Refer to COM LIBRARY page fields [1L], [2L],[3L],[4L], [5L] for data entry rules.
Page 410: Phone Library 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM To add a new record into the Phone Library, key into the scratchpad the name and the phone number separated by a slash symbol (“/”) and press the line select key associated with the last library record (displayed with dashes).
Page 411: Df Library 1/N
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAME & PHONE # [1L] - [5L]: Name & phone number. Two mode of operation: entry or selection. In entry mode, pressing the softkey will transfer the content of the scratchpad to this field. The name will appear on top of the associated phone number.
Page 412: Hf Library 1/N (Srt-170/M2)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The maximum number of DF LIBRARY entries is 99. The maximum number of DF LIBRARY pages is 20. The [NEXT] and [PREV] keys are used to scroll forward or backward in the preset numbers.
Page 413 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HF LIBRARY P R / I D E N T / F R E Q ( K H Z ) 01/HF01 /2000.0 A C T 05/HF02 /12345.6 S B Y 08/HF03 /10750.0 46/HF04 /29999.9 56/HF05 /18112.2...
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Page 415 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 14 - PERFORMANCE FUNCTIONS CONTENTS Subject Page FUEL PERFORMANCE CALCULATION ......................14-1 FUEL REMAINING AT ANY WAYPOINT......................14-5 SIMULATION FUNCTIONS ..........................14-5 A. SIMUL FLY AWAY FUNCTION ........................14-6 B. SIMUL OEI CRUISE FUNCTION ........................14-6 C.
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Page 417 The CMA-9000 FMS will accept total remaining quantity of fuel and fuel flow information from the fuel computer system. If a fuel computer system is not configured or has failed, the CMA-9000 FMS allows the operator to manually enter on the RTE x FUEL page the total fuel quantity and the fuel flow.
Page 418 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Display the INIT/REF INDEX 2/2 page by pressing [INIT REF], [PREV] or [NEXT]. Display the RTE x FUEL 1/2 page by pressing FUEL (LSK 5L) on the INIT/REF INDEX 2/2 page or the [FUEL] functional key (if configured).
Page 419 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Display the RTE x FUEL 2/2 page by pressing [NEXT] or [PREV]. FUEL option configured: ACT RTE 1 FUEL F U E L + R E S 1700 R E S E R V E U N I T <...
Page 420 IFDS and the CMA-9000 FMS-computed gross weight. NOTE: “EST” is displayed after “FUEL” on each of the title page (see below) when specific conditions are met (refer to the NOTE related to the FUEL 1/2 page description herein).
Page 421: Fuel Remaining At Any Waypoint
The CMA-9000 FMS provides Fly Away and OEI Cruise simulation functions, which allow the pilot to determine in advance the consequences of the loss of an engine in hover or cruise operation. The CMA-9000 FMS also provides a RTE x LEGS page simulation that allows the pilot to perform simulated ETA/EFA computations on the inactive route.
Page 422: Simul Fly Away Function
Upon opening the SIMUL FLY AWAY 1/3 page or selecting the "RESTORE DEFAULTS" prompt on the same page, the CMA-9000 FMS initializes to the default value (values received from other aircraft sub- systems) the current gross weight, current baro-corrected altitude, current outside air temperature and current wind.
Page 423: Simul Fly Away 1/3 (If Simul Pg Option Configured)
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SIMUL FLY AWAY 1/3 (If SIMUL PG option Configured) Display SIMUL FLY AWAY 1/3 page by pressing [INIT REF], [NEXT] and < SIMULATE> (LSK 2R). SIMUL FLY AWAY G R O S S W T...
Page 424: Simul Rtex 3/3 Or 1/1 (If Simul Pg And Rte2 Options Is Configured)
ETA/EFA computed for the waypoints of the inactive route. NOTE: If the inactive route does not exist, the CMA-9000 FMS copies the active route into the inactive route when the inactive route LEGS ETA/EFA page is accessed in order to perform simulated ETA/EFA computations.
Page 425 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 15 RNP CAPABILITY CONTENTS Subject Page OVERVIEW ............................... 15-1 FLIGHT TECHNICAL ERROR.......................... 15-1 PERFORMANCE, MONITORING AND ALERTING ..................15-2 GPS NAVIGATION MODE ..........................15-2 A. ACCURACY .............................. 15-2 B. INTEGRITY ............................... 15-2 C. CONTINUITY............................. 15-2 DME/DME NAVIGATION MODE........................
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Page 427 RNP CAPABILITY OVERVIEW When installed in accordance with AC 20-130A or equivalent, the CMA-9000 FMS is eligible for TGL-10 P- RNAV and AC 90-100 approvals. The information to support RNP approvals is contained in this section . This section describes RNP capabilities for the CMA-9000 Flight Management System (FMS) when the civil navigation configuration is set.
Page 428 NOTE: That the condition has to be present for 30 seconds before the message is displayed in en-route and terminal phase of flight and for 10 seconds when in approach phase of flight. In GPS mode, the CMA-9000 FMS activates the INT (integrity) lamp when the HIL exceeds the current RNP. GPS NAVIGATION MODE A.
Page 429 B. INTEGRITY Based on typical MTBF values of the VOR ground facilities and of the VOR receivers, the CMA-9000 FMS has a probability of misdetection by hardware of a failure condition that would cause the VOR-DME per flight hour.
Page 430 The inertial navigation mode in RNP airspace is time limited based on the current RNP. In Terminal phase of flight the inertial navigation mode must not be used more than 30 minutes after the CMA-9000 is placed in the inertial navigation mode. In Enroute phase of flight, its usage can be extended to 60 minutes. The Inertial navigation mode is not available for the approach mode.
Page 431 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 16 - MCDU FUNCTIONS CONTENTS Subject Page MCDU SUBSYSTEM CONTROL (if configured) ..................16-1 TANDEM MODE (if TANDEM is configured)....................16-2 This page is printed under user's responsibility and must not be retained for reference...
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Page 433 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 16 MCDU FUNCTIONS MCDU SUBSYSTEM CONTROL (if configured) The FMS has the built in capability to interface with External Sub-Systems (ESS) through ARINC 739 protocol and act as a MCDU for these external sub-systems. After a FMS cold start, automatic logon into an ESS is possible if there is at least one ESS configured in the auto logon priority list.
Page 434 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TANDEM MODE (if TANDEM is configured) The Tandem Mode consists of 2 FMSs namely the 'Trainer' and 'Student' FMS. The tandem mode implies that the Trainer’s FMS will act as a MCDU and will be connected through the A739 protocol to one external subsystem which is the Student FMS.
Page 435 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTION 17 - ABNORMAL PROCEDURES CONTENTS Subject Page POWER INTERRUPTIONS ..........................17-1 HIGH TEMPERATURE OPERATIONS ......................17-1 EQUIPMENT DESELECTION .......................... 17-2 TAS INPUT DESELECTION (OPTIONAL)....................... 17-3 OPERATION WITH FAILED TAS INPUT......................17-3 OPERATION WITH A FAILED ALTITUDE INPUT ..................17-4 HEADING INPUT DESELECTION (OPTIONAL) .....................
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Page 437: Power Interruptions
POWER INTERRUPTIONS A short CMA-9000 FMS power interruption, lasting less than 7 seconds in the air or less than 90 seconds on the ground (depending on the configuration), will have no impact on the active flight plan of the CMA-9000 FMS.
Page 438: Equipment Deselection
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM EQUIPMENT DESELECTION CAUTION: For installations in which GPS is the only navigation sensor, deselection of the GPS input will cause reversion to dead reckoning mode. See below and refer to the AFMS/RFMS for details.
Page 439: Tas Input Deselection (Optional)
NOTE: VOR, DME, DVS, INS, INS/GPS, INS/DVS, KALMAN and XFMS prompts are only displayed if such equipments are interfaced with the CMA-9000 FMS. Refer to the AFMS for details. If an equipment is suspected of being intermittent or unreliable, it should be manually deselected to prevent the possibility of navigation error.
Page 440: Operation With A Failed Altitude Input
GPS instrument approach. With a good satellite constellation, no altitude aiding may, in fact, be necessary. Therefore the loss of the altitude input to the CMA-9000 FMS may have no impact on the operation of the flight, with the exception that manual waypoint sequencing will be required for altitude-terminated legs.
Page 441: Navigation In Dead Reckoning (Dr) Mode
DR operation. The rate at which accuracy degrades depends on the quality of the source of the heading and speed inputs. The CMA-9000 FMS may therefore only maintain its normal accuracy if DR operation does not exceed three to five minutes duration (at typical speeds;...
Page 442: Operation With Failed Heading Input
2. Display the POS INIT/REF 1/2 page by pressing [INIT REF], <POS INIT> (LSK 2L). 3. When directly overhead the known reference position, enter the scratchpad coordinates into the CMA-9000 FMS POS field by pressing LSK 1R. The CMA-9000 FMS position is immediately updated to the new coordinates.
Page 443 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX A - CMA-9000 FMS DISPLAY PAGES - DETAILED DESCRIPTIONS CONTENTS Subject Page ARRIVALS 1/X..............................A-1 BULLS EYE 1/3 (if Tactical Config BULLS EYE is configured)..............A-4 BULLS EYE 2/3 (if Tactical Config BULLS EYE is configured)..............A-6 BULLS EYE 3/3 (if Tactical Config BULLS EYE is configured)..............A-10...
Page 444 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX A - CMA-9000 FMS DISPLAY PAGES - DETAILED DESCRIPTIONS Subject Page IDENT 2/2................................A-77 INACT DES+SAR 2/2 (if CARP and TACTICAL APPR are not configured) ..........A-78 INACT DES+SAR 2/4 (if CARP or TACTICAL APPR is configured)............A-78 INACT DES+SAR 4/4 (if CARP or TACTICAL APPR is configured)............A-81...
Page 445 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX A - CMA-9000 FMS DISPLAY PAGES - DETAILED DESCRIPTIONS Subject Page SARSAT WPT 1/2............................A-183 SARSAT WPT 2/2............................A-185 SELECT CO ROUTE 1/X..........................A-186 SELECT NAVAID {name } 1/X........................A-187 SELECT WPT {name} 1/X..........................A-187 SETUP 1/1...............................A-188 SIMUL FLY AWAY 1/3 page (If SIMUL configured and RTE2 configured)..........A-190 SIMUL FLY AWAY 1/2 page (if SIMUL configured only) ................A-190...
Page 446 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM This Page Intentionally Left Blank This page is printed under user's responsibility and must not be retained for reference Page A-iv November 19, 2009...
Page 447: Arrivals 1/X
CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX A CMA-9000 FMS DISPLAY PAGES - DETAILED DESCRIPTIONS NOTE: In the key sequences shown to display the pages; square brackets “[ ]” indicate a function key, angle brackets “< >” indicate a line select key (left and right softkeys).
Page 448 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display after all selections executed: PANC ARRIVALS S T A R S R T E 1 A P P R O A C H E S AMOTT5<ACT> <ACT>VORD06R T R A N S T R A N S <ACT>...
Page 449 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STARS [1L,2L,3L,4L,5L]: Alphabetical listing of all STARS applicable to the airport. Line selection of the desired STAR removes all other STARS and non-applicable approaches/runways and displays a listing of applicable arrival transitions. Deletion of the Selected/Active STAR cancels any STAR, STAR transition selections (line selection toggles the STAR, STAR transition status between selected and not selected).
Page 450: Bulls Eye 1/3 (If Tactical Config Bulls Eye Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM BULLS EYE 1/3 (if Tactical Config BULLS EYE is configured) Display BULLS EYE 1/3 page by pressing [INIT REF], <BULLS EYE> {if no CFG KEY is configured to BULL} or [BULL] {if any CFG KEY is configured to BULL} or [TACT],<BULL TOP> {if TACT key configured, and BULLS TOP configured on TACTICAL page.}.
Page 451 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM When the Bulls EyeTarget is fixed. BULLS EYE P P O S R E F < B U L L 0 1 0 / 3 3 . 0 T G T P O S...
Page 452: Bulls Eye 2/3 (If Tactical Config Bulls Eye Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM EFIS [6L]: Access to the EFIS 1/1 page. This field is only displayed when one of the following EFIS is configured: SPERRY, SPERRY2, GAMA, SEXTANT, ROCKWELL, ROCKWELL2, ROCKWELL3, BARCO, AHCAS2, MEGGIT, or Primus Epic, otherwise, this field is blank.
Page 453 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. When no Bulls Eye Target waypoint has been entered but the type is set to MOVING. BULLS EYE BETGT T G T I D / P O S B R G / D I S...
Page 454 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. After entering DELETE on the Bulls Eye Target waypoint: BULLS EYE TGT01 T G T I D / P O S N43°26.20 E004°52.32 B R G / D I S T K / G S...
Page 455 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TK/GS [2R]: Track angle and ground speed of a moving Bulls Eye Target waypoint. This field is only displayed if the selected Bulls Eye Target is a moving waypoint. Entry is allowed on this field only when the Bulls Eye Target is manually defined.
Page 456: Bulls Eye 3/3 (If Tactical Config Bulls Eye Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM BULLS EYE 3/3 (if Tactical Config BULLS EYE is configured) Display BULLS EYE 3/3 page by pressing [INIT REF], <BULLS EYE>, [PREV] {if not configured on one of the INIT/REF pages} or [TACT],<BULL WPT> {if TACT key configured, and BULLS WPT configured on TACTICAL page.} or [BULL], [PREV] {if CFG KEY 5 is configured to BULL} The BULLS EYE 3/3 pages allow creation or selection of the Bulls Eye waypoint.
Page 457 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. After selection of the Bulls Eye waypoint: BULLS EYE BUL01 B U L L I D / P O S N43°26.20 E004°52.32 B R G / D I S /270 R E F W P T I D...
Page 458 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM BULL ID [1L]: Bulls Eye waypoint identifier (5 characters max.). Entry of an ID triggers a search in all the FMS databases for the requested waypoint. Once the selected waypoint is determined, the ID/POS, BRG/DIS and TYPE fields are updated with the waypoint data.
Page 459: Carp Plan 1/3 (If Carp Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP PLAN 1/3 (If CARP configured) Display CARP PLAN 1/3 page by pressing [INIT REF], <DES+SAR> or <TACTICAL>, [NEXT], <CARP> {when a CARP procedure is in the displayed flight plan} or [TACT], <CARP> {when TACT key is configured and a CARP procedure is in the displayed flight plan} Automatically accessed whenever /C is entered over a CARP procedure on the LEGS page.
Page 460 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. ACTive status and sample inputs - Custom HAHO. ACT RTE1 CARP PLAN 1/3 T Y P E >CUST HAHO CDFB I D E N T P O I N T ( I P ) N 4 5 0 0 .
Page 461 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PI [3L]: Waypoint Identifier of the Point of Impact (PI). The entry may be in the form of a place-bearing-distance (wptidBRG/DIS, e.g. WPT07012/112). If an PI position is entered in LSK [3R], then a temporary waypoint is automatically created and the identifier (WPTXX) is displayed in [3L].
Page 462: Carp Plan 2/3 (If Carp Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP PLAN 2/3 (If CARP configured) Display CARP PLAN 2/3 page by pressing [INIT REF], <DES+SAR> or <TACTICAL>, [NEXT], <CARP>, [NEXT] {when a CARP procedure is in the displayed flight plan} or [TACT], <CARP>,[NEXT] {when TACT key is configured and a CARP procedure is in the displayed flight plan} Automatically accessed whenever /C is entered over a CARP procedure on the LEGS page, [NEXT].
Page 463 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Custom HAHO view: RTE1 CARP PLAN 2/3 P I E L E V S D D I S T 5000 3 . 1 I A S / H A T - D R O P -...
Page 464 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DROP IAS/HAT [2L]: Mission Indicated Air Speed (knts) and Height Above Terrain (HAT) (ft) planned for the drop. The default is boxes. A manual entry is required. When the entered HAT is less than the entered VERT DIST value, an invalid data entry message is displayed.
Page 465: Carp Plan 3/3 (If Carp Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP PROGRESS [6L]: Access to CARP PROGRESS page. ERASE [6L]: Cancel any active route modifications and/or any CARP parameter changes. Only displayed when the page is displaying the MOD status. If by pressing ERASE the CARP procedure is removed from the flight plan, then the LEGS page is automatically displayed.
Page 466 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Custom HARP view: RTE1 CARP PLAN 3/3 F T T V E R T D I S T 1560 5 3 . 4 S E C E X I T T I M E F A L L C O N S T 45.0...
Page 467 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT/MOD/" " RTEx (title): ACT indicates that the EXECuted CARP procedure is active (CARP Active discrete is on). MOD indicates the CARP procedure modifications have not been EXECuted yet. A blank field indicates the CARP procedure: •...
Page 468: Carp Progress X/X (When X/X = 4/4 If 3 Page Set And Carp Is Configured Or X/X = 5/5 If 4 Page Set And Carp Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DRIVE FACTOR [4R]: Displayed for CUST HAHO only. Drive safety factor (%). Percentage of the total computed drive distance to be used for safety reasons. Default value is 80%. Range [0..100]. DECEL DIST [5L]: Displayed for CUST HARP only. Deceleration Distance (ft). The distance the load descends from actuation to full deployment of the parachute.
Page 469 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Display with CARP procedure in the flight plan. ACT CARP PROGRESS 5/5 C A R P P O S N E A R C A R P N 4 5 0 0 . 0 0 W 0 7 2 0 0 .
Page 470 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM XTK DISTANCE (2R): Cross Track Offset (feet) from the desired path line defined by the CRP (Green Light) point and the XTE(Red Light) point as computed by the FMS. Field not displayed when CARP procedure not yet in flight plan.
Page 471: Central Clear ? (If Tactical Config Central Clear Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CENTRAL CLEAR ? (if Tactical Config CENTRAL CLEAR is configured) Display CENTRAL CLEAR ? page by pressing [INIT/REF], [NEXT], <CENTRAL CLEAR> { if not configured on TACTICAL page} Or [TACT], <CENTRAL CLEAR> {if TACT key is configured and CENTRAL CLEAR configured on TACTICAL...
Page 472: Data Load 1/1 (If Aircraft Is On Ground
ESS (2L to 5L), (1R to 3R): Displays the installed sub-systems. Prompt leads to the ESS FAILURE page. When the external sub-system name is unknown (Menu Text Exchange failed), the CMA-9000 FMS displays 4 dashes (----) besides the prompt. The installed sub-systems have a dedicated key. For example, ESS1 is displayed at LSK 1L, ESS2 is displayed at LSK 2L and so on.
Page 473 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. With ARINC 615 DLU, during load: DATA LOAD T Y P E >RADIO DATA S T A T U S L O A D I N G F I L E 0 0 1 4 <ABORT...
Page 474 OEI model data tables. TACT_APPR Tactical approaches database In order to load files from the Targa DLU (e.g. PDP/3-DOS DLU) to the CMA-9000 FMS, the following file extension convention is used (otherwise, file transfer is not performed): DATA TYPE FILE EXTENSION USER_DATA *.UDB...
Page 475 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DEP/ARR INDEX 1/1 This page provides access to arrival and departure for origin and destination airport. Display the DEP/ARR INDEX 1/1 page by pressing: [DEP/ARR] (if on ground). or [DEP/ARR] (if airborne and midway point of active route not reached yet). or From ARRIVALS 1/1 page.
Page 476 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. DEP/ARR Index during an edit of INACTIVE route: DEP/ARR INDEX 1/1 A C T R T E 1 KSEA PANC ARR> R T E 2 <DEP KSEA ARR> PANC ARR> <CANCEL SAVE? CONFIRM>...
Page 477: Departures 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DEPARTURES 1/X This page provides a listing of all-departing procedures and runways for the selected airport. The selected or activated SIDS, SIDS transition, and runways are displayed. Display the DEPARTURES 1/X page by pressing the corresponding <DEP> prompt on the DEP/ARR INDEX 1/1 page, or [DEP/ARR] (if on ground and route active).
Page 478 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display after all selections are executed: KBFI DEPARTURES 1/1 S I D S R T E 1 R U N W A Y S LACRES<ACT> <ACT> T R A N S VAMPS <ACT>...
Page 479 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM KBFI (title): Airport identifier (all page data applies only to the identified airport). RTE(#): Display related route number. SIDS [1L,2L,3L,4L,5L]: Alphabetical listing of all SIDS applicable to the airport. Line selection of the desired SID removes all other SIDS and non-applicable runways and displays a listing of applicable departure transitions.
Page 480: Des+Sar 1/2 (If Carp And Tactical Appr Are Not Configured
REF ID [1L]: Storage of the reference identifier. If there is a valid position in the scratchpad when the page is opened, then the CMA-9000 FMS creates a temporary waypoint at that position and places the identifier in this field. If the reference identifier is a moving waypoint, the following prompts are blanked and disabled on this page: <SQUARE, <LADDER, <SECTOR, <FLY OVER, HOVER>, HOLD>, RADIAL-TO>...
Page 481 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HOVER [2R]: Appears when configured. • HOVER waypoint not entered in the field REF ID of the DES+SAR page: Display the Hover page. If a HOVER pattern is already in the selected route, the active data is displayed.
Page 482: Des+Sar 2/4 (If Carp Or Tactical Appr Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TACT DTO [5R]: Appears when the MILITARY NAVIGATION option is configured: • Tactical Direct-to waypoint not entered in the field REF ID of the DES+SAR page: Display the RTE x LEGS 1/X page with only /T in the scratchpad.
Page 483: Deselect 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CARP [3R]: Displayed when CARP is configured. Pressing the line select key: • If SAR waypoint is not entered in field REF ID of the DES+SAR page and no CARP procedure exists in the flight plan then display the LEGS page with CRP01/C in the scratchpad.
Page 484 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Display with GPS (ARINC 743A format) and APIRS interfaces configured: DESELECT T A S G P S >FAIL VALID< H D G D M E >VALID DESEL< D V S V O R / D M E / T C N >ACQ...
Page 485 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TAS [1L]: Displays the TAS status (VALID or FAIL), when pressed toggles between VALID/DESEL or ACQ/DESEL options to control usage of true airspeed in the navigation solution. HDG [2L]: Displays the HDG status (VALID or FAIL), when pressed toggles between VALID/DESEL or ACQ/DESEL options to control usage of HDG in the navigation solution.
Page 486: Display 1/1
Display DMAP WPT 1/X page by pressing [INIT REF], <WPT LISTS> and <DMAP WPT>. The DMAP WPT page displays the list of waypoints received from the DMAP. Upon entry (manual or automatic), the CMA-9000 FMS automatically displays the DMAP WPT X/X page containing the last received waypoint.
Page 487 (1L-4L): Displays the coordinate position stored in the defined digital map waypoint ‘nnnM’, where nnn is a CMA-9000 FMS sequence number from 001 to 999 assigned when a new waypoint is received from the digital map. The only allowed scratchpad entry in those fields is the [CLR] key entry which will delete the selected DMAP waypoint.
Page 488: Vhf Nav Deselect 1/X (If Dme Interface Is Configured
This page enables the user to deselect VHF navaids (up to 25 stations can be added to the deselection list) and prevent the CMA-9000 FMS from using it for DME-DME navigation and VOR auto-tuning logic. It also allows a deselected station to be reselected by deleting it from the deselection list. The list is not retained on power up.
Page 489 DME STATUS 1/1 (if DME/DME interface is configured) The DME STATUS 1/1 page displays the DME stations selected by the CMA-9000 FMS for DME-DME navigation. Up to six stations are displayed. For each station the identifier (ID), status (STAT), frequency (FREQ) and distance (DIS) are given.
Page 490: Dvs Status 1/2 (Only If Doppler Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM POSITION (5R): Display DME derived position. Display depends on the selected coordinates system and datum. NAV STATUS [6L]: Returns to NAV STATUS INDEX 1/1 page. DME DESEL [6R]: Access to VHF NAV DESELECT 1/X page.
Page 491 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ANV353 DVS DVS STATUS V E L O C I T I E S + 2 5 . 5 K T S + 5 . 5 6 K T S + 2 5 0 0...
Page 492: Dvs Status 2/2 (Only If Doppler Is Configured
TEST, SILENCE, LAND, CALM SEA, SEA, MEMORY, SPEED NOT COMPUTED or PREPOSITIONING INS. For ANV353: INIT,OPER,MAINT,FAIL,********,blank ******** is displayed if “no activity” from the STATUS word. Blank is displayed when the CMA-9000 FMS requests: • a boresight change. • or a BIT command.
Page 493: Efis 1/X (If Efis Interface Is Configured
TRUE/MAG WIND [1L]: Display of the current wind direction and speed (in knots). If the wind cannot be computed by the CMA-9000 FMS, a large font is used and manual entry of a wind value is allowed; otherwise, manual entries are not permitted and the value is displayed in small font. The direction is in degrees TRUE or MAG, defaulted to the WIND REF configuration option, and has a 0 to 359 degrees range.
Page 494: Ess Failure 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM BULLS EYE [3R]: Enables or disables the output of Bulls Eye waypoints to EFIS. Toggle options: ON/OFF. Displayed only if BULLS EYE is configured. INIT/REF [6L]: Returns to the INIT/REF INDEX 2/2 page. ESS FAILURE 1/1 The ESS FAILURE 1/1 page displays the error messages when the communication with the selected external sub-system is failed.
Page 495: Fix Info 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FIX INFO 1/1 The FIX page provides bearing or course and distance information relative to an entered FIX. Distance To Go (DTG) and ETA are displayed for radial, distance and abeam intersections. The FIX entry must be a valid waypoint or navaid.
Page 496: Flight Log 1/1 (If Flight Log Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CRS/DIS(1L): Distance when REF is TO. Course/Distance to FIX from present position. NOTE: Downtrack fixes are not possible with seven-character waypoints. FLIGHT LOG 1/1 (if Flight Log is configured) Display FLIGHT LOG 1/1 page by pressing [INIT REF], [NEXT] and <FLIGHT LOG>.
Page 497: Fuel 1/2 Page (If Fuel Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FUEL 1/2 page (if FUEL is configured) Display FUEL 1/2 page by pressing [INIT REF], [NEXT] and <FUEL> or [FUEL] (if the FUEL hard-key is configured). A. Display of fuel route page when route is activated and executed:...
Page 498 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display of fuel route page when the active RTE is being modified: RTE 1 FUEL M A X R A N G E G R O S S W T 7 6 0...
Page 499 If the CMA-9000 FMS is cold started, the aircraft on ground and the fuel flow is not available from fuel sensor "-----" is displayed.
Page 500 9000 FMS receives fuel weight or fuel flow from the fuel computer. If the gross weight is not received from an external source and the CMA-9000 FMS FUEL_PG option is not configured with detailed weights, to FUEL+WEIGHTS, then an internally computed value is displayed (in normal white font): Gross weight is then calculated from the previous gross weight minus the change in fuel weight.
Page 501: Fuel 2/2 Page (If Fuel Or Fuel+Weights Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FUEL 2/2 page (if FUEL or FUEL+WEIGHTS is configured) Display FUEL 2/2 page by pressing [INIT REF], [NEXT], <FUEL> and [NEXT] or [FUEL] (if the FUEL hard-key is configured), and [NEXT]. A. Display of fuel route page, when route is activated and executed:...
Page 502 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display of fuel route page when the active RTE being modified: RTE 1 FUEL F U E L + R E S E M P T Y W T 1700 5000 R E S E R V E...
Page 503 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT FUEL(title): When the fuel sensor is used for calculating the active flight plan. ACT FUEL EST(title): For display conditions, refer to corresponding field of FUEL 1/2 page description herein. MOD FUEL(title): When the fuel sensor is used for calculating the modified flight plan.
Page 504 UNIT [5R]: Displays/selects current units for weight display (e.g. kilograms (kg) or pounds (lb)). NOTE: For a Sextant IFDS EFIS installation, when there is a discrepancy between the gross weight calculated by the CMA-9000 FMS and the one received from the IFDS, all the data fields are displayed in amber. CONFIRM [6R]: {If ERASE MODS is configured as CONFIRM} Confirm the changes made to the inactive route.
Page 505: Glonass Status 2/2 (If Glonass Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SAT TRK (2R): Number of satellites tracked. HOR FOM (3L): Horizontal Figure Of Merit (meters). VER FOM (3R): Vertical Figure Of Merit (meters). HOR DOP (4L): Horizontal Dilution Of Precision (no units). This is a measurement of overall positional and temporal accuracy in the horizontal plane.
Page 506: Gps Deselect 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GPS DESELECT 1/1 Display the GPS DESELECT 1/1 page by pressing [INIT/ REF], <NAV STATUS>, <DESELECT>, <GPS> GPS DESELECT c G P S VALID< m G P S VALID< <DESELECT cGPS [1R]: When selected, it toggles between VALID/DESEL or ACQ/DESEL options to control usage of the civil GPS in the navigation solution.
Page 507 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM IDENT [1L]: Any valid waypoint identifier where GPS integrity predictions are required. NOTE: Defaults to destination airport on initial display of the page. ETA [2L]: Estimated time of arrival when GPS integrity predictions are required.
Page 508 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DESEL [1L]: Deselect satellite Pseudo Range Number (PRN). The number is 2 digits from 01 to 32. RESEL [2L]: Reselect satellite Pseudo Range Number (PRN). The number is 2 digits from 01 to 32.
Page 509: Gps Status 1/2 Or Cgps Status 1/2 (If Arinc 743/743A Gps Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GPS STATUS 1/2 or cGPS STATUS 1/2 (if ARINC 743/743A GPS is configured) Display the GPS STATUS 1/2 page by pressing [INIT REF], <NAV STATUS> and <GPS> Display the cGPS STATUS 1/2 page by pressing [INIT/REF], <NAV STATUS>, <GPS>,<cGPS> {if dual GPS (civil &...
Page 510: Gps Status 2/2 Or Cgps Status 2/2 (If Arinc 743/743A Gps Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GPS STATUS 2/2 or cGPS STATUS 2/2 (if ARINC 743/743A GPS is configured) Display GPS STATUS 2/2 page by pressing [INIT REF], <NAV STATUS>, <GPS> and [NEXT] Display cGPS STATUS 2/2 page by pressing [INIT/REF], <NAV STATUS>, <cGPS>, [NEXT] {if dual GPS (civil &...
Page 511: Gps Status 1/2 (Egi Is Configured) Or
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GPS STATUS 1/2 (EGI is configured) or mGPS STATUS 1/2 (dual GPS: LN-100GT w/ civil GPS) Display GPS STATUS 1/2 page by pressing [INIT REF], <NAV STATUS> and <GPS>. Display mGPS STATUS 1/2 page by pressing [INIT/REF], <NAV STATUS>, <GPS>, <mGPS>, (if dual GPS (civil &...
Page 512 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MODE (2L): Displays the GPS operational status. The possible indications depend on the EGI configuration as indicated in the following table: LN_100GT SIGMA50H Mode (EGI) (EGI) FAIL Fault mode 3D position calculation mode 2D position calculation mode...
Page 513: Gps Status 2/2 (Egi Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM GPS STATUS 2/2 (EGI is configured) Display GPS STATUS 2/2 page by pressing [INIT REF], <NAV STATUS>, <GPS> and [NEXT]. A. SIGMA50H: GPS STATUS K E Y S T A T U S F A I L C O D E...
Page 514 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM KEY STATUS (1L): Displays GPS key status (highest to lowest display priority): Key Status LN_100GT SIGMA50H (EGI) (EGI) PPS-SM FAIL Circuit failure. ZEROIZE ERR Erase failure. KEY LOAD ERR Key loading error (parity error,…) NO KEY Key is missing.
Page 515: Hold 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HOLD 1/X • [HOLD] If a holding FIX already exists in the route. • Automatically accessed whenever a proposed holding fix was entered on the RTE LEGS page (e.g. appending ‘/H’ to an existing waypoint).
Page 516 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. After hold entry initiated: ACT RTE 1 HOLD F I X S P D / T G T A L T KILLA 220/ 5000A T U R N D I R F I X E T A >RIGHT...
Page 517 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM F. When the exit was armed and the RESUME HOLD prompt was pressed: RTE 1 HOLD F I X S P D / T G T A L T KILLA 220/ 5000A T U R N D I R F I X E T A >RIGHT...
Page 518 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM After EXECution, but prior to hold entry (exit type AT TGT ALT displayed): RTE 1 HOLD F I X S P D / T G T A L T FA23 210/ 5000A T U R N D I R F I X E T A >LEFT...
Page 519 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ERASE [6L]: Used to erase all route modifications in progress including HOLD definition. The prompt is not available for inactive route modifications. If confirm erase route modifications is configured, then upon pressing ERASE a confirmation is requested by displaying CANCEL and CONFIRM prompts on line select keys 6L and 6R respectively.
Page 520: Hover 1/1 (If Hover Configured, A/C Configured As Rotor, Ralt Equipment Configured And Active Route Displayed
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HOVER 1/1 (if HOVER configured, A/C configured as ROTOR, RALT equipment configured and Active route displayed) This page is used to enter the hover point, verify the parameters for the Transdown to hover procedure and activate the procedure.
Page 521 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Displayed when the Hover procedure has been executed ([EXEC] key): HOVER WPT01 M A R K O N T O P P O S N 4 0 0 9 . 6 1 W 0 8 9 2 0 .
Page 522: Ident 1/2
This page displays the effective expiry dates for the current and next cycle databases and enables the pilot to manually select the active navigation database. The loaded custom and user databases are also identified. The page allows the identification of the configured software in the CMA-9000 FMS and provide validity check for the configuration.
Page 523 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM USER DATABASE (5L): Displays the user database Identifier. Up to 9 characters may be shown. Stars “********” are shown when no user database is loaded. Blanks are shown when the database identifier is not valid or the loaded database modified.
Page 524: Inact Des+Sar 2/2 (If Carp And Tactical Appr Are Not Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TACTICAL DATABASE (5L): Displays the tactical approach database name. The name may contain up to 14 characters. “**************” is shown when no database is loaded. If Tactical APPR is not configured, this field is blank.
Page 525 REF ID [1L]: Storage of the reference identifier. If there is a valid position in the scratchpad when the page is opened, then the CMA-9000 FMS creates a temporary waypoint at that position and places the identifier in this field.
Page 526 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SECTOR [5L]: Appears when configured. The status “ACT” (reverse video cyan) is appended to the prompt if an activated sector search pattern is in the inactive flight plan. Pressing the line select key: • If SAR waypoint is not defined or is part of the Route, display the SECTOR page.
Page 527: Inact Des+Sar 4/4 (If Carp Or Tactical Appr Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INACT DES+SAR 4/4 (if CARP or TACTICAL APPR is configured) The page title is INACT TACTICAL if the TACT key is configured. Display DES+SAR 4/4 page by pressing: [INIT REF],<NEAREST>,<AIRPORT>,<DES+SAR> and [PREV] or [INIT REF],<NEAREST>,<VHF NAV>,<DES+SAR> and [PREV] or [INIT REF],<NEAREST>,<NDB>,<DES+SAR>...
Page 528 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DES+SAR R E F I D WPT03 R A D / D I S - - - / - - - - CARP> TACT APPR> REF ID [1L]: Storage of the reference identifier. If there is a valid position in the scratchpad when the page is opened, then the FMS will create a temporary waypoint at that position and places the identifier in this field.
Page 529 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INIT/REF INDEX 1/2 Display the INIT/REF INDEX 1/2 page by pressing [INIT REF]. NOTE: FMS ID “FMSx” will not be shown when cross-FMS is not configured. Displays {If PREDEF is configured and MARK key is not configured, display {If configured for SEARCH} and if EFIS Step mode is configured}.
Page 530 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display MARK key configured and {If PREDEF configured}. FMS1 INIT/REF INDEX 1/2 <IDENT WPT DATA> <POS INIT WPT LISTS> NEAREST> <FIX INFO <SETUP NAV STATUS> <MSG RECALL DES+SAR> AIR DATA LOST D. Display {If PREDEF configured, MARK key configured and, ATOS or/and FIAR 1500B RADAR configured}.
Page 531 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MARK ON TOP [4R]: Store the current CMA-9000 FMS system position in the predefined store point label ‘ONTOP’, and jump to the PREDEF WPT 2/2 page {if PREDEF WPT configured and MARK key is not configured}.
Page 532 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FLIGHT LOG [6L]: Access to FLIGHT LOG 1/1 page (If FLIGHT LOG is configured). DISPLAY [1R]: Access to DISPLAY 1/1 page, which contains parallax adjustment and display selection. SIMULATE [2R]: Access to the SIMUL FLY AWAY 1/3 page {if SIMUL is configured and RTE2 is configured} or access to the SIMUL FLY AWAY 1/2 page {if SIMUL is configured only}.
Page 533 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Page displayed when INS is in GROUND ALIGN mode 100 to 50: INS STATUS 1/1 P O S I T I O N M O D E A C C U R A C Y...
Page 534 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Page displayed for ADIRU, LTN_101 and LASEREF_V: IRS1 STATUS 1/1 P O S I T I O N N 4 5 3 4 . 2 5 W 1 2 2 4 5 . 1 2...
Page 535 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM POSITION (1R): • For EGI: Displays inertial position. • For LTN92: Displays pure inertial position. • For LTN_101, ADIRU or LASEREF_V: Displays pure inertial position. ACCURACY (2R): For EGI: Displays INS quality factor (in nm).
Page 536: Ins/Dvs Status 1/2 (Sagem Egi Configuration Only
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INS/DVS STATUS 1/2 (SAGEM EGI configuration only) Display the INS/DVS STATUS 1/2 page by pressing [INIT REF], <NAV STATUS> and <INS/DVS>. This page displays the outputs of the INS/DVS navigator as well as some INS/DVS inputs from the EGI. Control over the hybridization mode is also provided.
Page 537: Ins/Dvs Status 2/2 (Sagem Egi Configuration Only
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INS/DVS STATUS 2/2 (SAGEM EGI configuration only) Display the INS/DVS STATUS 2/2 page by pressing [INIT REF], <NAV STATUS> and <INS/DVS> and [NEXT]. INS/DVS STATUS 2/2 H D G / D A 0 6 0 . 0...
Page 538: Ins/Gps Status 2/2 (If Egi Interface Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INIT: EGI not in Navigation mode, Hybrid solution is not available. FAIL: EGI failure of GPS, INS or device, Hybrid solution is not available. HYB GPS SEL: Hybrid solution is available but no GPS updates being incorporated in the INS-GPS Kalman filter because GPS unavailable for the last 8 seconds.
Page 539: Irsx Accuracy X/X (X: 1, 2 Or 3; If Irsx Is In Nav Mode
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM IRSx ACCURACY X/X (X: 1, 2 or 3; if IRSx is in NAV mode) For LTN-92, LTN_101, ADIRU and LASEREF_V Display IRSx ACCURACY X/X page by pressing [INIT REF], <NAV STATUS> and <IRS>, <ACCURACY>.
Page 540 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM IRSx MALF MESSAGE X/X (X: 1, 2 or 3; If an IRS fault is present) For LTN-92. Display IRSx MALF MESSAGE X/X page by pressing [INIT REF], <NAV STATUS> and <IRS>, <MALFUNCT>. From IRSx STATUS X/X page, <MALFUNCT>...
Page 541: Kalman Status 1/1 (If Apirs Interface Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM KALMAN STATUS 1/1 (if APIRS interface is configured) Display KALMAN STATUS 1/1 page by pressing [INIT REF], <NAV STATUS> and <KALMAN>. A. When LAT/LONG is selected: KALMAN STATUS O P M O D E...
Page 542: Maint Messages 1/X
CMA-9000 FLIGHT MANAGEMENT SYSTEM MAINT MESSAGES 1/X This page displays all CMA-9000 FMS hardware related messages and all maintenance advisory messages which require maintenance action. It is displayed only if any message related to internal failure are detected, otherwise MAINT MSG prompt will not be displayed on the MESSAGE RECALL page and this page will not be available.
Page 543: Mcdu Menu X/X {If There Is At Least One External Sub-System Configured
FMUs are reporting the same message or that the FMS is operating in independent mode. System alert messages will cause both the CMA-9000 FMS MSG annunciator and the remote CMA-9000 FMS MSG annunciator to illuminate until all new alert messages have been cleared/acknowledged by the pilot. Once all alert messages have been viewed either via the scratchpad or by going to the MESSAGE RECALL page, the CMA-9000 FMS MSG annunciator and the remote CMA-9000 FMS MSG annunciator will turn off.
Page 544: Mission 1/1 (If Atos Or/And Radar Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Display MESSAGE RECALL 1/1 page by pressing [INIT REF], and <MSG RECALL>. Or [INIT REF] key is held down for more than 1 second. MESSAGE RECALL 1/1 F M S *VUHF1 CONTROL LOST *TACAN NAV LOST...
Page 545 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ATOS TARGET [2L,2R]: Displays ATOS Target position. Selection of 2L or 2R line key will place the ATOS Target position in the scratchpad. A time stamp is displayed above this line, showing the last time an ATOS Target position has been received.
Page 546 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAV STATUS INDEX 1/1 Display the NAV STATUS INDEX 1/1 page by pressing [INIT REF] and <NAV STATUS>. This page provides an access to the various Navigation Status pages. Only pages for which the equipment is configured are displayed.
Page 547 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PREDICT RAIM [1L]: Not shown. Access to GPS PREDICT RAIM 1/1 page. GPS [1R]: Access to GPS STATUS 1/2 page or the GPS NAV STATUS INDEX 1/1 page when dual GPS(Civil/Military) configured. GLONASS [2L]: Access to GLONASS STATUS 1/2 page.
Page 548 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NEAREST 1/1 Display a selectable, categorized list of navigation types to which the function NEAREST is to be applied by pressing [INIT REF], <NEAREST> or [INIT/ REF], <BULLS EYE>, [PREV], <NEAREST> {if Tactical Config BULLS EYE is configured}.
Page 549: Nearest Airport 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NEAREST AIRPORT 1/X Display the NEAREST AIRPORT 1/X page by pressing [INIT REF], <NEAREST> and <AIRPORT>. This page displays an ordered list by distance of the closest 50 airports that are within a radius of 640 nm with respect to the center reference identifier.
Page 550: Nearest Vhf Nav 1/X (Also Applicable For Nearest Ndb, Custom Wpt, And User Wpt
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NEAREST VHF NAV 1/X (also applicable for NEAREST NDB, CUSTOM WPT, and USER WPT) Display the NEAREST VHF 1/X page by pressing [INIT REF], <NEAREST> and <VHF NAV>. {also applicable for NEAREST NDB, CUSTOM WPT AND USER WPT}.
Page 551: Parallax Adjust 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PARALLAX ADJUST 1/1 This page provides vertical and horizontal display adjustment. The operator can move up, down, left and/or right of the display to adjust for parallax errors. PARALLAX ADJUST 1/1 page is accessed by pressing [INIT REF], [NEXT], <DISPLAY> and <PARALLAX>.
Page 552 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TRANS ALT [1L]: When a modification is made to the origin airport or associated departure procedure, this field will be updated to show the navigation database extracted value, if one exists, otherwise the FMS default value will be displayed.
Page 553: Pos Init/Ref 1/2 (If Egi Is Configured) Or Pos Init/Ref 1/3 (If Irs Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CRZ WIND [1R]: Enter the wind at cruise altitude (direction-true/speed-knots). Used for flight planning. NOTE: This is not the system computed wind (0° to 360°/0 Knots to 200 Knots). CRZ TAS [2R]: TAS (knots) at cruise altitude. Used for flight planning. This is not the system TAS (0 to 999 Knots).
Page 554 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. POS INIT/REF 1/2 page after START ALIGN selection: POS INIT/REF F M S P O S 26.28 W122 18.67 R E F W A Y P O I N T KBFI N 4 7 3 1 .
Page 555 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM F. POS INIT/REF 1/2 page in NAV mode: POS INIT/REF F M S P O S G P S 26.28 W122 18.67 I N S M O D E N A V T I M E N A V I G A T I O N 0 0 H 3 4 .
Page 556 FMS POS [1L or 1R]: FMS position on power up, this corresponds to the last computed position stored in the CMA-9000 FMS. Manual entry is allowed (in DR modes only). The navigation mode is also displayed. REF WAYPOINT [2L]: If ROTOR is configured. Reference waypoint; any waypoint accepted . Blank on liftoff.
Page 557 INS is in STANDBY mode. Manual entry can be via keyboard or line selecting CMA-9000 FMS POS or REF WAYPOINT coordinates (N/S 00° to 90°, E/W 000° to 180°). A DELETE from the scratchpad clears the field if no alignment was performed.
Page 558 <POS INIT> and [NEXT]. The CMA-9000 FMS continuously monitors and displays the CMA-9000 FMS position, bearing and range of each navigation mode position with respect to the CMA-9000 FMS position, and the accuracy of the navigation sensor positions. The accuracy shown is the sensor accuracy except for the INS (valid for an inertial sensor but not for the inertial frame of an EGI).
Page 559 0 . 8 4 <SETUP ROUTE> FMS POS [1L]: Displays current CMA-9000 FMS system position and the navigation mode. MODE [2L]: Displays the names for each of the navigation modes that are configured. The active navigation mode will be highlighted.
Page 560 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM INS/GPS GPS (cGPS/mGPS) (see note 2) INS (not shown - same line as INS/DVS) H ON Hybrid ON FAIL Fault mode A### Alignment mode HSEL Hybrid 3D navigation mode T### Test mode Mode selected...
Page 561 (95%) of each navigation mode. BRG (2R): Displayed only if the LSK is toggled to display BRG. Bearing from the CMA-9000 FMS position to each navigation mode position is displayed relative to True (superscript T indicates true North) or Magnetic North (based on the setting on the SETUP page).
Page 562 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM POS INIT/REF 3/3 (if LTN-92, LTN101, ADIRU or LASEREF_V interface is configured) Display the POS INIT/REF 3/3 page by pressing [INIT REF], <POS INIT>, [NEXT] and [NEXT] or [INIT REF], <IDENT>, <POS IINIT>, [NEXT] and [NEXT].
Page 563: Predef Wpt 1/X (If Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM IRSx (3L, 4L, 5L): If LTN-92 is configured. Displays IRSx updated inertial position. Data line displays: • When position valid: position data; • When position invalid: blanks; • When position failed or not received: asterisks.
Page 564 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS POS [1L,1R]: Displays the CMA-9000 FMS system current position solution and its source. Selection of 1L or 1R line key will place the present position in the scratchpad. TO WAYPOINT [2L]: Displays the identifier of the current TO waypoint. Selection of 2L line key will place the identifier of the TO Waypoint in the scratchpad (provided the waypoint is not a conditional waypoint).
Page 565: Predef Wpt 2/X (If Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PREDEF WPT 2/X (If configured) Display the PREDEF WPT 2/X page by pressing [INIT REF], <WPT LISTS>, <PREDEF WPT> and [NEXT] or [MARK] {if CFG KEY 2 configured to MARK and UPDATE POS page not being displayed} or {if Joystick position fix received {WXR or AHCAS EFIS is configured}.
Page 566 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM LAST PLS [3L,3R]: • PLS AN/ARS6 configured: Displays the last Personnel Locator System position received. Selection of 3L or 3R line select key will place the PLS position in the scratchpad. A time stamp is displayed above this line, showing the last time a PLS position has been received.
Page 567 PLS waypoint position regardless of this prompt value). MARK [4R]: Not Shown. {Displayed if MARK hard key not configured}. Store the current CMA-9000 FMS On Top position and display in the MARK ON TOP field (1R). The positions on the UPDATE POS page are also frozen.
Page 568: Predef Wpt 3/3 (If Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PREDEF WPT 3/3 (If configured) Display the PREDEF WPT 3/3 page by pressing [INIT/REF], <WPT LISTS>, <PREDEF WPT>, [NEXT], [NEXT] [MARK], [NEXT] {if CFG KEY configured to MARK and UPDATE POS page not being displayed} [TACT], <FLIR>...
Page 569: Progress 1/3 (When 3-Page Set Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PROGRESS 1/3 (when 3-page set is configured) This page provides the progress of various parameters to the user. Access PROGRESS 1/3 page by pressing [PROG]. This page becomes PROGRESS 1/4 when CARP is configured.
Page 570 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. When SAR part of the active route: PROGRESS 1/3 F R O M A L T A T A DIRECT F L 0 0 5 2 0 4 8 . 5 D T G E T A <...
Page 571 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ETA (2R): Display Estimated Time of Arrival (ETA) at waypoint. NOTE: When the aircraft is on ground, the ETE (estimated time en route) to the waypoint is displayed instead of the ETA if the PLAN DATA page is configured. If they are not configured, the field is blank.
Page 572: Progress 3/3 (When 3-Page Set Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NEXT WPT [6R]: Not Shown. Prompt is displayed when automatic waypoint sequencing is not possible. Examples include when the active leg is vector, or an altitude-terminated leg without a Baro-corrected altitude input. Pressing NEXT WPT results in an immediate transition of navigation and guidance to the next waypoint in the flight plan.
Page 573 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TRUE/MAG WIND [2L]: Current true wind direction and speed (in knots). Displayed in small font when the wind value is computed by the FMS, in large font when the value is frozen. When the scratchpad is empty, and A/C is outside the polar region (latitude between N73 and S60), pressing LSK 2L will toggle between the True and Magnetic display options.
Page 574: Progress 1/4 (When 4-Page Set Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM QNH SET [6L]: Displayed when no baro-corrected altitude is received from the ADC and either a pressure or an IRS baro-inertial altitude is available. Displayed, in small font, when a baro-correction (QNH) is received from an external source.
Page 575 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. When ETE is selected: ACT PROGRESS 2 8 0 D T G E T E < ARRIE 3 5 . 2 0 0 + 2 0 . 2 2 8 0 8 8 . 3 0 0 + 3 2 . 2...
Page 576 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DESIRED TRACK (DSTK) (1L): True (superscript T)/Magnetic ( ) Desired track to the active waypoint changed to "HOLD AT" during holding pattern, or “EXIT HOLD” when holding pattern exit is armed. NOTE: Prefix: turn direction (Left, either, Right)Suffix: Angle type (crs-course, hdg-heading) ACTIVE WAYPOINT (1L): Active waypoint identifier in reverse video.
Page 577 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TRUE/MAG WIND [3L]: Current true wind direction and speed (in knots). Displayed in small font when the wind value is computed by the FMS, in large font when the value is frozen (see definition below). When the scratchpad is empty and A/C is outside the polar region (latitude between N73 and S60), pressing LSK 3L will toggle between the True and Magnetic display options.
Page 578 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HSI SCALE (5R): Entry and display of HSI full scale deviation (in nautical miles). Entry is only allowed during the en-route phase of flight. Either 1 nm or 5 nm can be entered as the HSI scale. {Displayed only if EFIS is configured and not configured for en-route navigation}.
Page 579 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PROGRESS 2/4 (when 4-page set is configured) Display ACT PROGRESS 2/4 page by pressing [PROG] and then [NEXT]. This page becomes ACT PROGRESS 2/5 when CARP is configured. A. When ETE selected: ACT PROGRESS...
Page 580 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. When SAR part of the active route: ACT PROGRESS F R O M A L T A T A DIRECT 5 0 0 1 8 0 3 . 1 D T G E T E <...
Page 581: Progress 4/4 (When 4-Page Set Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DTG (2L): Cumulative distance-to-go from present position to waypoint along the flight plan route. ETA (2R): Estimated time of arrival at waypoint. On selection will change to ETE (also effects a change on PROGRESS 1/4).
Page 582 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM If QNH is available (via proper configuration). ACT PROGRESS H E A D W I N D C R O S S W I N D H D G / D A T A S...
Page 583 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM METRIC ALT [5R]: CMA-9000 FMS system altitude, displayed in meters. Displayed only if selected in the display configuration. QNH SET [6L]: Displayed when no baro-corrected altitude is received from the ADC and either a pressure or an IRS baro-inertial altitude is available.
Page 584 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADAR ID X-REF 1/1 (if FIAR 1500B RADAR is configured) Display the RADAR ID X-REF 1/1 page by pressing [INIT REF], <MISSION>, <RADAR ID X-REF {if the PREDEF PG is not configured or configured with the MARK key also configured} and {the FIAR 1500B RADAR is configured}.
Page 585: Radial
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIAL-TO 1/1 Display RADIAL-TO 1/1 page by pressing [INIT REF], <DES+SAR> or <TACTICAL>, enter identifier in the REF ID field, and <RADIAL-TO> or [INIT REF], <DES+SAR> or <TACTICAL>, <RADIAL-TO> or appending ‘/R’ to an existing waypoint on the RTE LEGS page.
Page 586: Rta Progress 2/3 (When 3-Page Set Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTA PROGRESS 2/3 (when 3-page set is configured) This page is used to evaluate the required True airspeed (TAS) to reach a waypoint at the required time of arrival (RTA), or to evaluate the estimated time of arrival at the RTA waypoint under different TAS and wind conditions.
Page 587: Rta Progress 3/4 (When 4-Page Set Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTA WIND [3L]: Displayed only after entry of the RTA waypoint. Wind used for RTA or recommended RTA TAS computation. In flight, default value is system wind; on ground, default value is cruise wind from the PLAN DATA 1/1 page (if configured);...
Page 588 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. PROGRESS Index during a MOD: RTA PROGRESS 3/4 R T A W P T R T A CAFTA 1 9 3 8 . 0 R T A T A S D I S...
Page 589: Rte X 1/X
<ERASE R0.0 The following page is displayed when a user route or custom route is activated in DIRECT mode and executed, and aircraft is airborne (single CMA-9000 FMS installation): ACT RTE 1 O R I G I N D E S T...
Page 590 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Page display when route activated and executed, and aircraft airborne (dual/triple CMA-9000 FMS installation): ACT RTE 1 O R I G I N D E S T KSEA PANC R U N W A Y...
Page 591 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM F. Page display after a DELETE of the ORIGIN or ERASE RTE1 key is pressed (for ROTOR aircraft type configuration): RTE 1 O R I G I N D E S T ----- -----...
Page 592 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Page display after selecting CONFIRM (in a single CMA-9000 FMS configuration): RTE 2 O R I G I N D E S T KSEA PANC R U N W A Y F L T N O...
Page 593 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM The following page is displayed when a user route or custom route is appended to an active route in INVERSE mode and executed: ACT RTE 1 O R I G I N D E S T...
Page 594 LEGS page). This option is only displayed when the displayed route is not empty and when the CMA-9000 FMS is configured for single mode of operation. NOTE: RTEx corresponds to RTE1 or RTE2 depending on which route is being displayed.
Page 595 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE 1 [6L]: Access to RTE 1 1/X page RTE 2 [6L]: Access to RTE 2 1/X page ERASE [6L]: Displayed only when a route modification is in progress. Pressing this key will undo all changes to the route and return to the ACT Route status.
Page 596: Rte X 2/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE x 2/X Access RTE x 2/X page by either pressing [RTE], [NEXT]; or from POS INIT/REF 2/X page, <ROUTE>, [NEXT]; or from ARRIVALS 1/X page, <ROUTE>, [NEXT], or from DEPARTURES 1/X page, <ROUTE>, [NEXT], or from USER ROUTES 1/X page, <ROUTE>, [NEXT], or...
Page 597 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Inactive route page before editing: RTE 2 V I A LACRE3 HUMPP DIRECT RADDT J154 RAMMS DIRECT GWENS <RTE 1 ACTIV TE> D. Inactive route during modification: RTE 2 V I A LACRE3...
Page 598 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TO [1R to 5R]: To waypoints: • Valid entries are published waypoints, VHF navaids, runways, and ICAO airport identifiers. • Valid created waypoint types are: Place-Bearing-Distance (PBD), Lat/Long and Place-Bearing-Place-Bearing (PB-PB). • Waypoint on airway.
Page 599: Rte X Ladder 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE x LADDER 1/1 Display RTE x LADDER 1/1 page by pressing [INIT REF], <DES+SAR> or <TACTICAL>, and <LADDER> (active route) or [INIT REF], <DES+SAR> or <TACTICAL>, [NEXT], <LADDER> (inactive route) or [LEGS], “/S”...
Page 600 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM D. Search Pattern at a Route Waypoint – Inactive Route & modified Inactive Route only: 1. Enter “/S” or a valid waypoint identifier followed by “/S” in the scratchpad. 2. Display the desired waypoint location in the route by pressing [LEGS] (and [NEXT] as desired) and press the appropriate LSK to append the “/S”...
Page 601 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM G. LADDER SAR from the Active route LADDER 1/1 page (after pressing <ACTIVATE> (LSK 6R), before pressing [EXEC]): RTE 1 LADDER 1/1 L E G L E N G T H YUL02 R E F I D...
Page 602 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM J. Resuming a LADDER SAR from the Active route RTE x LADDER 1/1 page (before pressing [EXEC]): RTE 1 LADDER 1/1 L E G L E N G T H YUL02 R E F I D...
Page 603 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT/MOD/blank(STATUS): MOD indicates the search is not being executed. ACT indicates that the search pattern is being executed. "blank" indicates an executed search fix has not been reached or the search pattern for the inactive route is being displayed.
Page 604 EXEC lamp illuminates. The current waypoint field freezes to the number of the last TO search waypoint and the CMA-9000 FMS disables the steering command (upon EXEC key press). •...
Page 605: Rte X Legs 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM • For modified active route: CONFIRM is displayed if ERASE MODS is configured as CONFIRM. For modified inactive route: CONFIRM is used to confirm the changes made to the inactive route. However, when it is...
Page 606 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Active route with Route Discontinuity: ACT RTE 1 LEGS 2 9 9 3 9 . 6 N51W125 300-320 2 9 8 1 5 4 FL350B 3 2 0 4 5 . 0 YZP01...
Page 607 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. Inactive route modification in progress: RTE 2 LEGS 1 8 8 P - T 2 . 2 5 ANCPTR 1600A R 0 5 3 C R S 4 . 8 6 0 5 3 C R S 5 .
Page 608 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM H. Normal Active page with Temperature compensated altitudes: ACT RTE 1 LEGS 3 1 2 1 3 . 1 AGBEK 2 7 8 5 3 1 4 1 3 . 6 2348 3 1 4 3 .
Page 609 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM WAYPOINT IDENTIFIER [1L, 2L, 3L, 4L, 5L]: Up to 7 characters (5 characters if Tactical Approach is configured). Used for entry and/or display of any valid waypoint identifier. Valid entries are: Identifier, Latitude Longitude, Place/Bearing/Distance, Place/Bearing-Place/ Bearing and Along Track Distance.
Page 610 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ALTITUDE CONSTRAINTS (or RESTRICTIONS) [1R, 2R, 3R, 4R, 5R]: Display of mandatory altitude - constraints (coming from the Navigation Database or pilot-entered) in one of the following ways: • The suffix A identifies a crossing restriction at or above the displayed value (example display A: 1600A means cross D173J at or above 1600 feet).
Page 611 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CANCEL [6L]: {If ERASE MODS is configured as CONFIRM} Cancel the changes made to the inactive route. LEGS ETA [6R]: Access to the corresponding RTE LEGS ETA Y/X page. MAP CTR STEP [6R]: Prompt appears when EFIS CP is in PLAN mode. Used to move the center of the EFIS MAP display to the next waypoint in the flight plan.
Page 612: Rte X Legs Eta 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE x LEGS ETA 1/X Provides the ETA and EFA for each waypoint on the corresponding RTE LEGS Y/X page. Display ACT RTE LEGS ETA Y/X page by pressing [LEGS] and <LEGS ETA>. A. Normal ACTIVE format:...
Page 613 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM D. Active route erased: RTE 1 LEGS ETA 1/1 E T A E F A - E N D O F R O U T E - <RESTORE LEGS POS> E. Active route restored:...
Page 614 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Units configured to lbs using 5R prompt on FUEL page: ACT RTE 1 LEGS ETA 1/4 E T A E F A CAFTA 1 9 1 6 . 4 2 9 2 7 1 9 5 0 . 2 z...
Page 615 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE x LEGS POS 1/X Provides the position in latitude and longitude, using the WGS 84 Earth model, for each waypoint on the corresponding RTE LEGS Y/X page. Display ACT RTE LEGS POS 1/X page by pressing [LEGS], <LEGS ETA> and <LEGS POS > (active route) or [LEGS], <LEGS ETA>, <SIMUL RTEx >, <LEGS POS>...
Page 616 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. LEGS POS of INACTIVE route (when SIMUL page is configured: RTE 2 LEGS POS 1/2 CAFTA N 5 1 1 7 . 7 2 W 1 2 9 0 5 . 3 2 N 5 3 1 5 .
Page 617: Rte X Sector 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM LAT-LONG (1R, 2R, 3R, 4R, 5R): Display position of the waypoint identified on the previous line. LEGS [6R]: Returns to the corresponding RTE LEGS Y/X page. CONFIRM [6R]: Confirm the changes made to the inactive route.
Page 618 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. When inserting of modifying a SECTOR SAR from the Inactive route SECTOR 1/1 page: RTE 2 SECTOR 1/1 D I A M E T E R 10.0 R E F I D A N G L E...
Page 619 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM REF ID [2L]: Name of waypoint considered being a reference for the relative bearing/distance elements entered in the fields 3L and 4L. If a Search pattern waypoint is defined in route, the field is filled with 5 dashes “- ----“...
Page 620 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CANCEL [6L]: {If ERASE MODS is configured as CONFIRM} Erase all the fields and set the Search parameters back to their default values. For the inactive route only, it also cancel the modifications made to the inactive route and command display of the LEGS page, if the cancellation follow modifications to the inactive route.
Page 621: Rte X Square 1/1
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RTE x SQUARE 1/1 To access SQUARE 1/1page, press [INIT REF], <DES+SAR> or <TACTICAL> and <SQUARE> (active route) or [INIT REF], <DES+SAR> or <TACTICAL>, [NEXT], and <SQUARE> (inactive route) or [TACT], <SQUARE> {if TACT key configured and SQUARE configured on the TACTICAL page} or LEGS], “/S”...
Page 622 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. When inserting or modifying a SQUARE SAR from the Inactive route SQUARE 1/1 page: RTE 2 SQUARE 1/1 T R A C K S P A C I N G R E F I D...
Page 623 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RELATIVE BRG [3L]: The relative bearing of the search pattern entry waypoint compared to the reference REF. This field is displayed as long as REF ID contains an entry and the displayed default value is 000 000°.
Page 624 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CANCEL [6L]: {If ERASE MODS is configured as CONFIRM} Erase all the fields and set the search parameters back to their default values. For the inactive route only, it also cancel the modifications made to the inactive route and command display of the LEGS page, if the cancellation follow modifications to the inactive route.
Page 625: Sarsat Data 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SARSAT DATA 1/X The SARSAT DATA X/X page displays the COSPAS/SARSAT specific data regarding a SARSAT waypoint received from the DF equipment. Where the page number (X) varies from 1 to 8. Display SARSAT DATA 1/1 page: (if a DF is configured) press [INIT/REF], <WPT LISTS>, <SARSAT WPT>...
Page 626 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Same as previous display (PLB02) except that last SARSAT waypoint update had an invalid position. SARSAT DATA P L B 0 2 I D / P O S P 1 5 T E S T...
Page 627 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MESSAGE TYPE (1R): Displays “TEST” in reverse video white when the beacon is in Test mode. Otherwise the field is blank when the beacon is in normal operating mode (Distress). BEACON ID (2L): Display the vehicle identification. The identification can be one of these following possibilities for an aircraft (ELT beacon type): •...
Page 628 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM AUX LOC DEV (3R): Display the auxiliary radio-location device available on board of the distress aircraft or ship. The possible display are: • "NONE": No auxiliary radio-locating device • "121.5 MHz": 121.5MHz locator beacon •...
Page 629 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SARSAT WPT 1/2 The SARSAT WPT page displays the COSPAS/SARSAT waypoint(s) received from the Direction Finder (DF) equipment. Display SARSAT WPT 1/2 page: (if a DF is configured) press [INIT/REF], <WPT LISTS> and <SARSAT WPT>.
Page 630 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. When deletion of waypoint PLB02 has been confirmed. SARSAT WPT I D / A G E / B R G / D I S < > E L T 0 1 ( * * )
Page 631 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SARSAT WPT 2/2 This page enables the pilot to select the FMS update mode and the type of messages decoded from the DF. Display SARSAT WPT 2/2 page: (if a DF is configured) press [INIT/REF], <WPT LISTS> <SARSAT WPT> and [NEXT].
Page 632: Select Co Route 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SELECT CO ROUTE 1/X Display SELECT CO ROUTE 1/1 page by pressing [RTE] and <CO ROUTES>. SELECT CO ROUTE 1 2 0 1 1 4 0 1 1 2 0 2 L O A D >DIRECT...
Page 633 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SELECT NAVAID {name } 1/X Automatically displayed on entry of a navaid identifier that has duplicates in the navigation database. It is displayed only if the entry was made from the NAV radio page.
Page 634: Setup 1/1
NOTE: This toggle option is not available if the BARCO EFIS is configured and label 171 is properly received from the CMA-9000 FMS. The current status is displayed in small font (the prompt ">" is not displayed). This page is printed under user's responsibility...
Page 635 CANCEL [6L]: Used to cancel request to change CMA-9000 FMS cross-talk mode of operation. POS INIT [6L]: Accesses the POS INIT/REF 1/X page. CONFIRM [6R]: Used to confirm request to change CMA-9000 FMS cross-talk mode of operation (independent or synchronized).
Page 636: Simul Fly Away 1/3 Page (If Simul Configured And Rte2 Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SIMUL FLY AWAY 1/3 page (If SIMUL configured and RTE2 configured) SIMUL FLY AWAY 1/2 page (if SIMUL configured only) Display SIMUL FLY AWAY 1/3 or 1/2 page by pressing [INIT REF], [NEXT] and < SIMULATE>.
Page 637 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display after manual entry of Pressure-Altitude: SIMUL FLY AWAY G R O S S W T F L Y A W A Y H T 9 8 0 0 P R E S S A L T...
Page 638 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FLY AWAY HT [1R]: Fly away height. Minimum height to maintain in hover. This corresponds to the maximum drop in height upon loss of an engine during Hover. Calculated and displayed in normal video initially and upon entry of gross weight.
Page 639: Simul Oei Cruise 2/3 Page (If Simul Configured And Rte2 Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SIMUL OEI CRUISE 2/3 page (if SIMUL configured and RTE2 configured) SIMUL OEI CRUISE 2/2 page (if SIMUL configured only) Display SIMUL OEI CRUISE 2/3 or 2/2 page by pressing [INIT REF], [NEXT] and <SIMULATE> and [NEXT].
Page 640 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display after manual entry of Outside Air Temperature: SIMUL OEI CRUISE 2/3 G R O S S W T J E T T I S O N W T 1 0 6 0 0...
Page 641: Simul Rtex 3/3 Page Or 1/1 (If Simul Pg And Rte2 Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM OAT [4L]: Outside Air Temperature. Valid range -40°C to +50°C. Defaults to the current temperature in small font. Manual entry is displayed in large font and causes a recalculation of gross weight or fly away height depending on which data was being simulated as well as a recalculation of one engine inoperative out of ground effect weight.
Page 642 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. RTE COPY was selected: SIMUL RTE2 C R Z T A S C R Z W I N D 1 3 0 1 3 4 / 1 0 0 F U E L F L O W...
Page 643: Tactical X/Y Page (If Configured
Access to RTE x LEGS ETA 1/X page. NOTE: If the inactive route does not exist, the CMA-9000 FMS copies the active route into the inactive route when the inactive route LEGS ETA/EFA page is accessed in order to perform simulated ETA/EFA computations.
Page 644 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Page display example when 2 pages (one for the active and one for the inactive route) are used. In this example, SQUARE, LADDER, SECTOR, HOVER, BULLS EYE and TACT APPR are configured. TACTICAL R E F I D WPT03 BULL TOP>...
Page 645 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TACTICAL R E F I D WPT03 R A D / D I S - - - T / - - - - N M <TACT DTO <CARP Display of the inactive tactical page when 4 pages set is used.
Page 646 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM [3L] to [6L] and [1R] to [6R]: These keys permit to access one of the following pages according to the TACTICAL PG CONFIG option configuration: BULL TOP: Access the BULLS EYE 1/3 page. This prompt is not displayed for the inactive (INACT) TACTICAL page(s).
Page 647: Tactical Appr 1/3 Page (If Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SARSAT: Access the SARSAT WPT page. This prompt is not displayed for the inactive (INACT) TACTICAL page(s). SECTOR: The status “ACT” (reverse video white) is appended to the prompt if an activated sector search pattern is in the flight plan.
Page 648 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM 2. Automatically accessed whenever a proposed tactical approach has been entered on the LEGS page. This is done by inserting a waypoint,, say ABCDE, as the tactical approach runway threshold waypoint by typing ABCDE/A and inserting this into the LEGS page flight plan at the desired location 3.
Page 649 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. If “ERASE MODS” option is set to "CONFIRM" TACTICAL APPR 1/3 R E F W P T I D R A D / D I S - - - - - T I A F ( - 3 .
Page 650 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM F. nactive tactical approach page prior to confirmation: TACTICAL APPR 1/3 R E F W P T I D R A D / D I S - - - - - T I A F ( - 3 .
Page 651 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ii) TIAF-to-TFAF distance: The distance is left justified and displayed with 4 characters. A slash "/" must be typed before this value in the scratch pad followed by the desired distance. Refer to SWOP40603 for the minimum, maximum and default value of of TIAF-toTFAF distance.
Page 652: Tactical Appr 2/3 Page (If Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RWY ELEV [4R]: This field is a mandatory crew entry of the runway threshold elevation for the tactical approach. This field is used in defining the tactical approach geometry. The valid range for this field is -1000 to 25000.
Page 653 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. After modification of the TMAP1 to TMAP2 distance, but prior to execution: TACTICAL APPR 2/3 P A R K K M A P R W Y E L E V 0 9 0 / 2 .
Page 654 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. When VNAV tactical approach is active: ACT TACTICAL APPR 2/3 P A R K K M A P R W Y E L E V 0 9 0 / 5 . 0 0 N M...
Page 655 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT/MOD/" " (title): ACT will appear when the active waypoint is part of the tactical approach procedure. MOD will appear when the crew is in the process of modifying the flight plan. A blank field will indicate the tactical approach has been defined but is not yet active.
Page 656: Tactical Appr 3/3 Page (If Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RAD/DIS [5R]: Radial/distance from the reference position to the desired TMAP2 waypoint position. The values are blanked, when no REF WPT ID is defined, otherwise zeros are displayed as the default values. No entries are allowed, when the fields are blanked.
Page 657 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Display prior to EXECution: TACTICAL APPR 3/3 T A C T A P P R : T I A F 2 7 1 1 F T 3.00NM/-3.0 T F A F F A F 1 7 5 7 F T 5.00NM/-3.0...
Page 658 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. Display when VNAV tactical approach is active: ACT TACTICAL APPR 3/3 T A C T A P P R : T I A F 2 7 1 1 F T 3.00NM/-3.0 T F A F...
Page 659 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ACT/MOD/" " (title): ACT will appear when the active waypoint is part of the tactical approach procedure. MOD will appear when the crew is in the process of modifying the flight plan. A blank field will indicate the tactical approach has been defined but is not yet active.
Page 660: Timer 1/1 Page (If Timer Pg Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TIMER 1/1 page (if TIMER PG is configured) Display TIMER 1/1 page by pressing [INIT REF], [NEXT] and <TIMER>. The TIMER page is used to generate a “TIMER ALARM” alert message after a user specified alarm time was reached (count-up timer) or a certain time duration has elapsed (countdown timer).
Page 661 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Display after a countdown time is entered: TIMER A L A R M T I M E C O U N T D O W N ----:-- 2354:56 ADD 5 MIN> <START CLEAR>...
Page 662 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TITLE: TIMER ALARM TIME [1L]: Display and entry of a count-up alarm event time (UTC or local time based on SETUP page selection). If a countdown time was entered and activated (with START LSK 5L), the time at which the countdown timer will expire is displayed.
Page 663: Tmp Update Pos 2/2 (If Carp, Predef Pg And Either Egi Or Irs Are Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TMP UPDATE POS 2/2 (If CARP, PREDEF PG and either EGI or IRS are configured) Display TMP UPDATE POS 2/2 page by pressing: [INIT/REF], <POS INIT>, <UPDATE POS> and [NEXT] or [INIT/REF], <WPT LISTS>, <PREDEF WPT> and [NEXT], <UPDATE POS> and [NEXT] or [INIT/REF], <NAV STATUS>, <INS>, <UPDATE POS>...
Page 664 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. Display after toggle of [1L] on default display: TMP UPDATE POS 2/2 R E F B R G / D I S T >FMS /0.00 U P D A T E P O S I T I O N 28.08 W073...
Page 665 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM H. Display after pressing CANCEL UPDATE LSK: TMP UPDATE POS 2/2 R E F B R G / D I S T >CYUL < /2.10 U P D A T E P O S I T I O N 30.15 W073...
Page 666: Update Pos 1/1 (If Predef Page And Irs, Egi Or Dvs Interface Is Configured) Or Update Pos 1/2 (If Carp Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM POS DIFF (4R): This field displays the bearing and distance from the FMS position to the UPDATE POSITION. Prior to pressing the MARK key, the current FMS position is used, and after pressing the MARK key, the marked FMS position is used.
Page 667 2. If the MARK hard key was pressed, the PREDEF WPT page automatically appears with the MARK ON TOP field containing the CMA-9000 FMS position at the time the MARK key was pressed. If the MARK softkey was pressed, the UPDATE POS page is already being displayed.
Page 668 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Update POS 1/1 page by pressing the MARK key, all positions are frozen and sensors are selectable: UPDATE POS R E F > F M S ( I N S / D V S ) A C C U R 0 .
Page 669 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. Update POS 1/1 page pressing LSK 1L, the identifier entry prompt appears: UPDATE POS R E F >----- A C C U R A C C U R P O S D I F F I N S / D V S 0 .
Page 670 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM UPDATE POS 1/1 entering the true joystick position computes the update position. UPDATE POS R E F >JOYSTICK A C C U R 0 . 2 7 N 4 5 2 8 . 0 8 W 0 7 3 4 4 .
Page 671 When the CMA-9000 FMS - INS/GPS navigation is used as the reference, INS/GPS is displayed in parenthesis next to it. • When the CMA-9000 FMS - GPS navigation is used as the reference, GPS is displayed in parenthesis next to it. •...
Page 672 Displayed only when at least one sensor is selected for update. Selecting this softkey will cause the CMA-9000 FMS to update the selected sensors’ position to the update position and then unselect all sensors. The "!OUT OF RANGE" advisory message appears if the INS/GPS position difference with the reference position is greater than 15 nautical miles.
Page 673 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. When route is deleted: USER ROUTES 0 0 0 1 M 0 0 0 9 M W P T 0 1 W P T 0 9 W P T 0 1 W P T 1 0...
Page 674 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM USER WPT 1/2 Display the USER WPT 1/2 page, press [INIT REF], <WPT DATA>,<NEW USER WPT>. The USER WPT pages allow for the creation or modification of user waypoints. Moving waypoints can be created or modified if Moving waypoint is configured.
Page 675 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. After modifying data for an existing moving waypoint identifier in the active route: USER WPT ADFF I D / P O S A C T R T E 12.23 W043 32.12 B R G / D I S...
Page 676 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM D. After entering DELETE on an existing user waypoint identifier: USER WPT ADFF I D / P O S F R E E = 4 5 9 12.23 W043 32.12 B R G / D I S...
Page 677 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM TK/GS [2R]: Track angle and ground speed of moving waypoint. TK and GS values may be entered individually or simultaneously; a ‘/’ symbol appended to a value in the scratchpad indicates only the TK value must be updated.
Page 678 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM USER WPT 2/2 Display USER WPT 2/2 page to modify parameters of an existing waypoints by pressing [INIT_REF], <WPT DATA>, <NEW USER WPT> and [NEXT]. The USER WPT pages allows for the creation of new user waypoints of different class and types or the modification of existing user waypoints.
Page 679 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ID [1L]: User waypoint identifier with boxes as default value. Identical to USER WPT 1/1 page. FREE: Number of user waypoint free slots in user database (460 user waypoints max.) The number displayed is always the difference between 460 and number of fixed and moving waypoints (460 - no of fixed waypoints - no of moving waypoint).
Page 680: User Wpt List 1/X
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ELEVATION [5R]: Enter the elevation in feet (Airport and VHF NAV only). The default value is boxes, and the minimum/maximum values are –9999/+9999 ft. WPT DATA [6L]: Access to the WPT DATA 1/1 page.
Page 681 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM USER WPT LIST D I S N M D I S N M <BASET > GABRE 2 0 . 1 0 . 7 9 <BINDY > 2 8 . 9 8 2 . 7 <CIVET...
Page 682: Vnav Appr 1/1 Page (If Vnav Interfaces Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DEL ALL [6R]: Request to delete all user waypoints and triggers the CANCEL/CONFIRM prompts. If a moving waypoint is present in the active or modified route, then the error message “!MOV WPT IN ROUTE” will be displayed instead of the CANCEL/CONFIRM prompts.
Page 683 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM C. Destination Airport temperature is entered: ACT VNAV NDB24L M D A - D A 9 9 9 2 3 9 3 0 8 - 3 . 0 0 2 7 8 5 A G B E K...
Page 684 (including unit system toggling) are copied between VNAV and PROGRESS pages, and cross-talked between FMS. Upon leaving the terminal area, an altimeter setting entered from the CMA-9000 Display Panel is cancelled and the field displays boxes ("...
Page 685 NEXT WPT results in an immediate transition of navigation and guidance to the next waypoint in. VOR/DME/TCN STATUS 1/1 Page (if VOR, DME or TACAN interfaces are configured) The VOR/DME/TCN page displays the VOR, DME, and TACAN sensor inputs used in CMA-9000 FMS radial/distance radio navigator and the resulting position fix.
Page 686 VORx ID/FREQ/RAD (1L-Line 3, 2L-Line 5): Displays VOR station identifier and tuning frequency (MHz) from the interface (1 and 2 indicate the source of the VOR information). This field is blanked when the CMA-9000 FMS is unable to find the requested station (either due to invalid bearing, distance or values outside of thresholds) or when the value of the frequency is changed and is searching for the new station identifier.
Page 687: Wind 1/1 (If Carp Is Configured
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM WIND 1/1 (If CARP is configured) Allows entry and display of wind speed and direction for the selected waypoints at up to four different levels. Display WIND 1/1 page by pressing [INIT REF], and <DES+SAR> or <TACTICAL>, [NEXT], <CARP>, [NEXT] and <WIND>...
Page 688 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM CANCEL [6L]: Cancel the changes made to the inactive route. DIR/SPD [1R, 2R, 3R, 4R]: Allows entry of wind direction and speed for the given waypoint at the corresponding flight level. Entry is only allowed once a flight level has been entered.
Page 689 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM B. Display upon entry of an existing identifier in the fixed user waypoint database. The displayed page differs depending if displaying a moving or fixed waypoint and depending on the type and class. Large font used for...
Page 690 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM E. Display after deleting the user fixed waypoint, or moving waypoint. Deletion of a moving waypoint that is present in the active route or the modified route is rejected: WPT DATA FVRD W P T P O S N 0 3 2 1 .
Page 691 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Sample ICAO country codes (2 characters): EH= Europe, Netherlands EG= Europe, UK TYPE/CLASS (4L), (4R) upper line: Display of identifier type or VHF NAVAID class. Possible values are: AIRPORT: Airports NDB: Non-Directional Beacon waypoint...
Page 692 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM (DELETE?): Displayed between the CANCEL/CONFIRM prompts when the inactive route is in modification. CANCEL [6L]: Cancels the modifications performed to a user waypoint. CONFIRM [6R]: Confirms the modifications performed to a user waypoint. DES+SAR [6R] or TACTICAL [6R]: When TACT key is configured, the DES+SAR prompt is replaced by TACTICAL.
Page 693 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX B - NAVIGATION LEG TYPE DEFINITIONS CONTENTS Subject Page INTRODUCTION..............................B-1 DIRECT TO A FIX (WAYPOINT – DF LEG).......................B-1 TRACK BETWEEN FIXES (TF LEG) .........................B-1 COURSE TO A FIX (CF LEG) ..........................B-2 DME ARC TO A FIX OR CONSTANT RADIUS TO A FIX (AF AND RF LEGS)..........B-3 PROCEDURE TURN (PI LEG) ...........................B-4...
Page 694 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM This Page Intentionally Left Blank This page is printed under user's responsibility and must not be retained for reference Page B-ii November 19, 2009...
Page 695: Introduction
APPENDIX B NAVIGATION LEG TYPE DEFINITIONS INTRODUCTION For lateral guidance, the desired lateral route is entered into the CMA-9000 FMS through keyboard entries such as custom route, origin, destination, SID, waypoints, STAR and/or approach. Entries and selections of published procedures are translated using 20 different types of navigation legs to define the lateral path. Each of these types of legs is graphically illustrated with accompanying display in the following paragraphs.
Page 696: Course To A Fix (Cf Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE TO A FIX (CF LEG) This navigation leg is defined by an ending waypoint and a course into the waypoint. ACT RTE 1 LEGS 0 5 3 C R S 4 . 8 6...
Page 697: Dme Arc To A Fix Or Constant Radius To A Fix (Af And Rf Legs
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DME ARC TO A FIX OR CONSTANT RADIUS TO A FIX (AF AND RF LEGS) This navigation leg is an arc about a center fix. The leg goes clockwise (right arc), or counterclockwise (left arc) starting at a waypoint, or an intercept point on the radius, and terminates at a waypoint with a terminating tangential course.
Page 698: Procedure Turn (Pi Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PROCEDURE TURN (PI LEG) Refer to Section 7 for detailed information. This navigation leg is defined by a starting waypoint, an initial direction, a turn direction and a course to intercept on the following course to fix navigation leg.
Page 699: Holding Pattern (Hm, Hf, Ha Legs
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HOLDING PATTERN (HM, HF, HA LEGS) Refer to Section 10 for detailed information. This navigation leg is defined by a waypoint, a turn direction, an inbound course and a time or distance length. The leg terminates when: •...
Page 700: Course To An Altitude (Ca Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE TO AN ALTITUDE (CA LEG) This navigation leg is defined by a course from previous leg termination position and a target altitude. ACT RTE 1 LEGS 0 5 3 C R S 3 . 0 9...
Page 701: Course To A Dme Distance (Cd Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE TO A DME DISTANCE (CD LEG) This navigation leg is defined by a course from current aircraft position and terminates when reaching a distance from a DME Navaid. ACT RTE 1 LEGS 0 7 1 C R S 1 .
Page 702: Course To A Course Intercept (Ci Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE TO A COURSE INTERCEPT (CI LEG) This navigation leg is defined by a course from current aircraft position and terminates when a desired course which is referenced to a waypoint is intercepted and captured.
Page 703: Course To A Radial (Cr Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE TO A RADIAL (CR LEG) This navigation leg is defined by a course from current aircraft position and terminates when crossing a radial from a referenced waypoint. ACT RTE 1 LEGS 0 8 0 C R S 8 .
Page 704: Course From A Fix To An Altitude (Fa Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE FROM A FIX TO AN ALTITUDE (FA LEG) This navigation leg is defined by a waypoint, a course and an altitude termination. ACT RTE 1 LEGS 1 4 2 F R R W 1 4 5 .
Page 705: Course From A Fix To A Distance
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE FROM A FIX TO A DISTANCE This navigation leg is defined by a waypoint, a course and a distance to travel from the waypoint. ACT RTE 1 LEGS 2 3 3 F R C M C M 3 3 .
Page 706: Course From A Fix To A Dme Distance (Fd Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE FROM A FIX TO A DME DISTANCE (FD LEG) This navigation leg is defined by a waypoint and a course and terminates when reaching a distance from a DME Navaid. ACT RTE 1 LEGS...
Page 707: Course From A Fix To A Manual Termination (Fm Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM COURSE FROM A FIX TO A MANUAL TERMINATION (FM LEG) This navigation leg is defined by a waypoint and a course and terminates on pilot request. ACT RTE 1 LEGS 2 5 1 F R A G L I N...
Page 708: Heading To An Altitude (Va Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HEADING TO AN ALTITUDE (VA LEG) This navigation leg is defined by a heading from current aircraft position and terminates when reaching a target altitude. ACT RTE 1 LEGS 0 5 8 C R S 3 .
Page 709: Heading To A Dme Distance (Vd Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HEADING TO A DME DISTANCE (VD LEG) This navigation leg is defined by a heading from current aircraft position and terminates when reaching a distance from a DME Navaid. ACT RTE 1 LEGS 0 7 1 H D G 2 .
Page 710: Heading To A Course Intercept (Vi Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HEADING TO A COURSE INTERCEPT (VI LEG) This navigation leg is defined by a heading from current aircraft position and terminates when a desired course which is referenced to a waypoint is intercepted and captured.
Page 711: Heading To A Manual Termination (Vm Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HEADING TO A MANUAL TERMINATION (VM LEG) This navigation leg is defined by a heading from current aircraft position and terminates on pilot request. ACT RTE 1 LEGS 3 2 0 H D G...
Page 712: Heading To A Radial (Vr Leg
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM HEADING TO A RADIAL (VR LEG) This navigation leg is defined by a heading from current aircraft position and terminates when crossing a radial from a referenced waypoint. ACT RTE 1 LEGS 2 8 0 C R S 3 .
Page 713: Radial-To
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM RADIAL-TO This navigation leg is defined by an entry waypoint and a reference waypoint. The entry waypoint is created by the reverse to a radial and a distance to the reference waypoint. The reference waypoint can be a waypoint in the route or another waypoint.
Page 714: Search Pattern
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SEARCH PATTERN Refer to Section 11 for detailed information. This page is printed under user's responsibility and must not be retained for reference Page B-20 November 19, 2009...
Page 715 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX C - NAVIGATION DISPLAYS CONTENTS Subject Page APPENDIX C-1 NAVIGATION DISPLAYS – EHSI/EFIS..................C-1 INTRODUCTION..............................C-1 MAP MODE.................................C-2 PLAN MODE...............................C-3 EHSI DISPLAYS -- SYMBOLOGY AND COLORS....................C-4 NAVIGATION MODE AND ADVISORY MESSAGES..................C-5 EHSI/EFIS DISPLAYS -- NAVIGATION MODE AND ADVISORY MESSAGES..........C-9 APPENDIX C-2 NAVIGATION DISPLAYS - EFIS (GAMA STANDARDS)............C-10...
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Page 717: Introduction
NAVIGATION DISPLAYS – EHSI/EFIS INTRODUCTION The information displayed by the CMA-9000 FMS on the EHSI/EFIS flight instrument panel can be viewed in one of two modes: MAP or PLAN. The MAP mode can be configured to show a CENTER display. The two EHSI/EFIS modes and the CENTER mode are selected via the mode switch on the control panel.
Page 718: Map Mode
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MAP MODE In MAP mode, the EHSI/EFIS displays active and/or modified routes and background data relative to the aircraft position and the current heading. The background data, route data, navigation aids and airports, may be selectively removed using the NAVAID, ARPT and RTE DATA push buttons usually found on a typical EHSI/EFIS control panel (as shown above).
Page 719: Plan Mode
In PLAN mode the EHSI/EFIS displays the active and/or modified routes relative to true north and the center waypoint displayed on the CMA-9000 FMS RTE LEGS page. The center waypoint can be stepped through each waypoint in the route by pressing the MAP CTR STEP prompt on the RTE LEGS page.
Page 720: Ehsi Displays -- Symbology And Colors
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM LEKKO 1420.0z 179° /29 18.1 EHBK INKET LEKKO EHAM KLM00052 Typical CTR Mode In both MAP and PLAN modes the EHSI displays dynamic data and position pointers. The range of the MAP and PLAN display modes can be set to 5 , 10, 20, 40, 80, 160, 320 or 640 nautical miles via the range switch on the EHSI control panel.
Page 721: Navigation Mode And Advisory Messages
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAVIGATION MODE AND ADVISORY MESSAGES The EHSI/EFIS uses CMA-9000 FMS data to generate symbology and information described below. Presentation may vary from one EHSI/EFIS type to another. NAME SYMBOL APPLICABLE REMARKS MODE(S) Indicates ground track...
Page 722 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAME SYMBOL APPLICABLE REMARKS MODE(S) ACTIVE ROUTE (M) The active route is displayed with a continuous AMBOY ACTIVE ROUTE MAP CTR lines (M) between KILMR MODIFICATIONS PLAN waypoints. Active route modifications are displayed with short dashes (W)
Page 723 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAME SYMBOL APPLICABLE REMARKS MODE(S) HOLDING PATTERN A fixed size holding pattern ACTIVE (M) is displayed when selected MAP CTR MODIFICATION (W) or an instrument procedure PLAN with a holding pattern is INACTIVE (C )) selected into the route.
Page 724 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NAME SYMBOL APPLICABLE REMARKS MODE(S) ROUTE DATA When the RTE DATA P/B is ON, altitude and ETA for (M, W MAP CTR KILMR route waypoints can be 12000 PLAN displayed. 0835Z IRS POSITION * (W) When POS P/B is ON indicates IRS position.
Page 725: Ehsi/Efis Displays -- Navigation Mode And Advisory Messages
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM EHSI/EFIS DISPLAYS -- NAVIGATION MODE AND ADVISORY MESSAGES The EHSI/EFIS displays messages related to procedures, nav modes and nav alerts, as well as FMS alerts. The following are various type of messages that can be displayed: •...
Page 726: Introduction
MAP, ARC, or ROSE, selectable via the EFIS Mode Select Panel. In MAP mode, the CMA-9000 FMS is the primary source of data for the EFIS display. In this mode, the EFIS display shows the aircraft position relative to the route and other earth-referenced data, including VHF navaids, NDBs and airports.
Page 727 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM Navigation Display MAP Mode Navigation Display Arc Mode Navigation Display Rose Mode This page is printed under user's responsibility and must not be retained for reference Page C-11 November 19, 2009...
Page 728: Efis Displays
NOTE: For the IFDS type EFIS the distance indicated may be erroneous if the the actual DTW is greater than 655.35 nm. 2. Desired Course - the CMA-9000 FMS desired course when the source of course/track data is NAV. 3. Drift Angle - the drift angle is the difference between the computed track angle and the actual aircraft heading.
Page 729: Direct-To/Intercept Navigation
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DIRECT-TO/INTERCEPT NAVIGATION This example illustrates what would appear on the EFIS display after a Direct-To waypoint has been manually entered and executed via the FMS. A Direct-To waypoint with an Intercept is displayed in a similar manner. For more information on Direct-To/Intercept navigation, refer to Section 9.
Page 730: Standard Hold/Direct Entry
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STANDARD HOLD/DIRECT ENTRY Standard holding patterns and direct hold entries are both displayed in an identical manner on the EFIS. The display consists of four waypoints positioned in a rectangular pattern. The holding fix is labelled with the waypoint identifier, while the remaining waypoints are numbered from 01 to 03, in an order indicative of the holding pattern orientation and turn direction.
Page 731: Offset Entry
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM OFFSET ENTRY An offset entry is displayed as a triangular pattern in which the holding fix is labelled with the waypoint identifier. The remaining waypoints are numbered 01 and 02, in an order indicative of the holding pattern orientation and turn direction.
Page 732: Procedure Turn
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM PROCEDURE TURN Procedure turns are typically represented by three waypoints arranged in a V-shaped pattern. The naming convention for these waypoints indicates the turn direction at the end of each leg. Thus, in this example, a left turn is performed at ANCPTL and a right turn at ANCPTR.
Page 733: Route Discontinuity
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ROUTE DISCONTINUITY When the active route contains a discontinuity, all route waypoints within the current EFIS map scale are shown on the EFIS display. Waypoints following the discontinuity are left unconnected*. This example represents an active route with a discontinuity between waypoints YZT and PRYCE.
Page 734 The waypoint with the <CTR> cursor now appears at the bottom of the EFIS map display. 3. To return to an aircraft-centered display, go to any CMA-9000 FMS page other than the RTE x LEGS 1/X page, or press [LEGS].
Page 735 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX D - CMA-9000 FMS DISPLAY PAGES FLOW DIAGRAMS CONTENTS Subject Page FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 1 of 12) ................D-1 FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 2 of 12) ................D-3 FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 3 of 12) ................
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Page 737 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: This is a top down flow diagram. Dash lines represent configured items. FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 1 of 12) This page is printed under user's responsibility and must not be retained for reference...
Page 738 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: Dash lines represent configured items. FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 2 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-3/(D-4 blank) November 19, 2009...
Page 739 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 3 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-5/(D-6 blank) November 19, 2009...
Page 740 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 4 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-7/(D-8 blank) November 19, 2009...
Page 741 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: Dash lines represent configured items. FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 5 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-9/(D-10 blank) November 19, 2009...
Page 742 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: Dash lines represent configured items. FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 6 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-11/(D-12 blank) November 19, 2009...
Page 743 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM NOTE: Dash lines represent configured items. FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 7 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-13/(D-14 blank) November 19, 2009...
Page 744 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 8 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-15/(D-16 blank) November 19, 2009...
Page 745 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 9 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-17/(D-18 blank) November 19, 2009...
Page 746 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 10 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-19/(D-20 blank) November 19, 2009...
Page 747 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 11 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-21/(D-22 blank) November 19, 2009...
Page 748 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS (Sheet 12 of 12) This page is printed under user's responsibility and must not be retained for reference Page D-23/(D-24 blank) November 19, 2009...
Page 749 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM APPENDIX E - SYSTEM MESSAGES AND REMOTE ANNUNCIATORS CONTENTS Subject Page SYSTEM ALERT MESSAGES ........................... E-1 MAINTENANCE ALERT MESSAGES ......................E-19 MAINTENANCE ADVISORY MESSAGES ...................... E-21 STATUS ADVISORY MESSAGES........................E-29 DATA ENTRY ADVISORY MESSAGES......................E-38 REMOTE ANNUNCIATORS..........................
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Page 751 CMA-9000 FMS and configured through the CMA-9000 FMS maintenance pages (see Installation Manual). Alert messages are prioritized internally by the CMA-9000 FMS, with the highest displayed at the top and the lowest at the bottom of the MESSAGE RECALL page.
Page 752 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION 2 HOURS GPS The SA/AS GPS key will expire Enter the new key to avoid EGI interface KEY ALERT in two hours. the loss of the GPS navigation.
Page 753 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION CARP TAS NOT This message is enabled when Correct speed to achieve the Configurations supporting the TAS is not within 20 knots of mission TAS. CARP/HARP the TAS derived from the...
Page 754 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION CHECK TRUE/MAG Phase of flight is Approach or If required, change Angle All configurations Terminal and the angle reference to MAG via FMS reference is TRUE. SETUP page (or alternatively via external switch).
Page 755 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION DF CONTROL The FMS has detected one of Control DF DF-430-102 or LOST the following conditions: radio from DF-935 interface if a DF-430-102 is configured: another source •...
Page 756 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION DME/DME NAV DME-DME navigation can no Verify if identified DME DME interface LOST longer be used as a means of transceiver operates navigation. normally. If FMS was in DME-DME...
Page 757 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION FLIR INPUT LOST The FMS detects a total loss of Ensure that FLIR is powered. FLIR interface Forward Looking Infrared Radar input data. Verify if the FLIR operates normally.
Page 758 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION GPS-GPS POS The position difference between If during approach, perform Single civil GPS interface DISAGREE the two/three GPS exceeds the missed approach. per FMS position check limit defined in...
Page 759 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION HEADING INPUT Total loss of heading input. Refer to Operator’s Manual AHRS interface LOST When not in GPS navigation, the Section 16 for operation with FMS builds up an error during a failed heading input.
Page 760 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION INDEPENDENT OP In a dual/triple-FMS installation, Any automatically Multi-FMS installations the identified FMS is now synchronized item listed in operating independently of the Section 3-5 of the Operator’s...
Page 761 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION INS/GPS POS The FMS is using embedded Verify INS/GPS position and EGI interface UNCERTAIN INS/GPS (EGI) sensor position monitor HIL (Horizontal and no civil GPS interface data for which the sensor Integrity Limit).
Page 762 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION IRSx ON BAT Verify IRS AC power. IRS interface configured INS/IRS reports that AC power is too low and is operating on DC backup power. If the backup...
Page 763 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION MANUAL WPT Sequencing to the next waypoint Press NEXT WPT prompt All configurations SEQUENCE needs to be manually initiated by (LSK 6R) when required on the pilot.
Page 764 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION NOT ENOUGH Not enough fuel to get to Re- route to a closer Fuel computer interface FUEL destination. (Endurance Reserve destination. not included) is below Time To Go (TTG).
Page 765 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION SET AIRPORT Outside Air Temperature at the Enter temperature. VNAV TEMP destination airport is required. SET INS POS Manual alignment of the INS Perform alignment. EGI interface (EGI) is required.
Page 766: System Alert Messages
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION SET QNH (cont’d) If the IS&S EFIS is installed: If the message is If this message has been configured, and the FMS is triggered as a result of being...
Page 767 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION • Hover function TDN NOT During a hover maneuver, when The roll steering command is • Radar Altimeter interface POSSIBLE over-flying the TDN waypoint automatically disabled and...
Page 768 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM SYSTEM ALERT DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION • NAV interface VOR/DME/TCN TACAN failure has been Control the VOR or DME • DME interface NAV LOST detected in addition to a VOR receivers from another •...
Page 769: Maintenance Alert Messages
• Always associated with a specific system alert message. • Unless otherwise noted, the CMA-9000 Master Caution is active (e.g. FMS is not functional) for all the Maintenance Alert messages. • The associated message alert FMS DEGRADED suggests that the cause of the problem may be determined and that the FMS may be used in a degraded navigation mode.
Page 770 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM MAINTENANCE DESCRIPTION ACTION ASSOCIATED SYSTEM ALERT MESSAGE ALERT MESSAGE H/W PIT FAILED Programmable Interval Timer Do not use the FMS for FMS FAILED failure detected. SYSTEM navigation. FAILED displayed on MESSAGE RECALL page. Advise maintenance.
Page 771 • Lowest priority scratchpad messages (can be typed over and overwritten by any other message type). • Unless otherwise noted, the CMA-9000 Master Caution is inactive (e.g. FMS is still functional) for all the Maintenance Advisory messages. • Collector messages are messages that combine several fault conditions into a single alert message. (e.g.
Page 772 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADVISORY DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION AMU FAILED The FMS has detected a failure Control the AMU from another AMU interface of the AMU or a failure of the source. AMU communication bus. Advise maintenance.
Page 773 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADVISORY DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION • COM radio interface COM1 FAILED The FMS has detected a failure Control the COM/VUHF radio • VUHF radio interface COM2 FAILED of the COM radio or its from another source.
Page 774 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADVISORY DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION DVS CTRL FAILED Missing control data from the Degraded mode of operation Doppler interface Doppler velocity sensor. may still be available. Advise maintenance. EFIS1 FAILED EFIS failure or EFIS Ensure that EFIS is powered.
Page 775 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADVISORY DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION F/O EHSI FAILED The FMS has detected a F/O Ensure that F/O EHSI is EHSI interface EHSI input failure or a F/O EHSI powered. Verify F/O EHSI communication bus failure.
Page 776 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADVISORY DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION IRSx CHECK ADC LTN-92 INS or ADIRS reports LTN-92: Take note of INS IRS interface configured invalid ADC inputs. No usage of maintenance word contents on some or all ADC info.
Page 777 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADVISORY DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION • NAV radio interface NAV1 FAILED The FMS detects a failure with Try to control the NAV radio • NAV radio name is NAV2 FAILED the NAV (VOR/ILS) radio or the from another source.
Page 778 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM ADVISORY DESCRIPTION ACTION APPLICABLE MESSAGE CONFIGURA-TION UNABLE FMS-FMS In a dual-FMS installation, Any automatically Multi-FMS installations SYNC operator’s or automatic attempt synchronized item listed in to synchronize FMSs failed Section 3 of the Operator’s...
Page 779 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS ADVISORY MESSAGES • Status Advisory messages are messages which do not require immediate pilot action but require pilot awareness: Displayed in white on the scratchpad (until acknowledged). • Never displayed on the MESSAGE RECALL or MAINT MESSAGES page.
Page 780 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE BERDV The FMS detects that Check if the entered BULLS if Tactical Config BULLS UNACHIEVABLE interception of the moving Bulls EYE TARGET parameters EYE is Eye Target is not possible.
Page 781 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE CHECK TRANS i) the TRANS ALT field (for the ALT/LVL (cont’d) case that a new ORIGin or departure procedure(s) was added to the active flight plan); ii) the TRANS LVL field (for the...
Page 782 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE DIRECT TO FIX The FMS detects Upon flying a Review the intercept course All configurations Direct-To with intercept course entered. that the predicted intercept point is so close to the leg's...
Page 783 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE FMS NAV IN DR The FMS is receiving insufficient Take appropriate measure to All configurations navigation information from fly in manual mode. Verify other sensors. sensors power status and NOTE: The FMS is in dead self-test status.
Page 784 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE INS DRIFT FMS detects a position Advisory Civil GPS and EXCEEDS 2NM difference between the FMS EGI interface installed at current position and the INS the same time.
Page 785 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE PASSWORD The library password has been One of following radio is CHANGED successfully changed. configured COM VUHF VOR/ILS RED LIGHT The FMS detects the XTE (Red Stop CARP drop.
Page 786 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE TRANS ALT/LVL The FMS detects that all the Ensure that the correct If the message is MISMATCH following have occurred: TRANS ALT and TRANS LVL configured. a) the operator presses the are selected.
Page 787 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM STATUS DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE USING TRUE REF The FMS automatically reverts None. All configuration to True north angular reference upon entry in the polar region The flight crew acknowledges and the angular reference used...
Page 788 DATA ENTRY ADVISORY MESSAGES Data Entry Advisory messages are messages that are only displayed on the scratchpad. They indicate that the CMA-9000 FMS has determined that the user-entered data is incorrect. • Displayed in white on the scratchpad (until acknowledged) •...
Page 789 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE !BULLS EYE NOT if Tactical Config BULLS Operator is attempting to enter a Enter the Bulls Eye ALLOWED EYE is Bulls Eye or Bulls Eye Target...
Page 790 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE !CONFIRM Complete inactive route VNAV configured and Operator is trying to enter INACTIVE ROUTE modification or cancel it. second route configured temperature at destination airport while the inactive route is being modified.
Page 791 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE All configurations except for !ENTER Operator is attempting to execute Enter the DESTINATION ROTOR DESTINATION a flight plan without a destination airport. airport. Iridium phone interface...
Page 792 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE • One of the following radio !FUNCTION NOT Function invoked by the FMS None. is configured: AVAILABLE function key just pressed is not yet implemented in the FMS...
Page 793 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE • One of the following !IDENT NOT Entered radio station ident was Check identifier or re-enter a element is configured: FOUND not found in the navigation valid identifier.
Page 794 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE !INVALID APPR The selected approach transition If possible, select an alternate All configurations TRANS is invalid or corrupted. approach or approach transition. !INVALID An invalid channel was entered in Enter a valid channel.
Page 795 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE !INVALID SID Operator selected an invalid SID If possible, select alternate SID All configurations TRANS TRANS (error in database). or SID transition. !INVALID STAR Operator selected an invalid...
Page 796 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE !MOD IN The message is generated due to PROGRESS one of the following 2 conditions: 1) Cannot access the CTR RTE LEGS pages to preview the flight...
Page 797 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE All configurations !NO ENTRY Operator is attempting to enter Select correct data field for ALLOWED data into a non-entry data field. entry. For example, in a SID/STAR...
Page 798 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE !PHONE BOOK The FMS detects that the Cancel entry or remove HCS interface. ALREADY FULL operator tried to add a new unnecessary data to allow new phone identifier and number entry.
Page 799 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE All configurations !SELECT Selection of the STAR transition Select STAR transition, TRANS/APPR/RWY or approach or runway is required approach, or runway as before the STAR waypoints can appropriate.
Page 800 OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM DATA ENTRY DESCRIPTION ACTION APPLICABLE ADVISORY CONFIGURA-TION MESSAGE HCS interface !TOO MANY The operator has entered more Check the number and make DIGITS than 30 digits for the phone sure that the number of digits number.
Page 801: Remote Annunciators
OPERATOR’S MANUAL CMA-9000 FLIGHT MANAGEMENT SYSTEM REMOTE ANNUNCIATORS A. ANNUNCIATORS Outputs are provided to drive external annunciators to alert the pilot of system status or flight plan sequencing. NOTE: The actual legends and colors of the remote annunciators may vary depending on the installation.
Page 802: Navigation Flag
The EFIS annunciator, will be displayed under the operational or system hardware conditions listed below. At the same time, the validity of the CMA-9000 roll steering output signal will be set to INVALID, resulting in the disengagement of the autopilot/flight director LNAV mode.

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