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Esterline CMA-9000 Operator'S Manual Download Page 756

 OPERATOR’S 

MANUAL 

 

CMA-9000 FLIGHT MANAGEMENT SYSTEM 

 
 

 

 

Page E-6 

 

November 19, 2009 

SYSTEM ALERT 
MESSAGE 

DESCRIPTION ACTION 

APPLICABLE 
CONFIGURA-TION 

DME/DME NAV 
LOST 

DME-DME navigation can no 
longer be used as a means of 
navigation. 
If FMS was in DME-DME 
navigation mode, it automatically 
reverts to the next available 
navigation mode. 

CAUTION: 

In aircraft installations consisting 
of dual FMS interfaced with dual 
DME transceivers, the alert 
message “DME/DME NAV 
LOST” could be erroneously 
triggered upon the loss of one of 
the two DME receivers.  The 
problem occurs when one FMS 
has lost its single DME input: the 
DME/DME navigation is still 
provided by the off-side FMS via 
FMS cross-talk.  The DME/DME 
NAV LOST message should be 
ignored in this case. 

Verify if identified DME 
transceiver operates 
normally. 
 
Use another navigation 
sensor as a means of primary 
navigation. 
 
Advise maintenance. 

DME interface 

DME CONTROL 
LOST 
DME1 CONTROL 
LOST 
DME2 CONTROL 
LOST 
 

The FMS cannot control the 
DME which is paired with the 
NAV radio. 
The FMS detects a failure with 
the DME channel used for 
manual tuning via the NAV radio. 

Control DME from another 
source.  
DME receiver is no longer 
operational, use other 
navigation aids. 
 
Advise maintenance. 

DME interface 

DVS NAV LOST 

The FMS detects a total loss of 
DVS input data on the onside 
and offside FMSs. 
DVS sensor can no longer be 
used for navigation. 

Ensure that DVS is powered.  
Verify if the DVS operates 
normally. 
Advise maintenance. 

Doppler interface 

EFIS INPUT LOST 

The FMS detects a total loss of 
EFIS input data on the onside 
and offside FMSs. 

Ensure that EFIS is powered.  
Verify if the EFIS(s) 
operate(s) normally. 
Advise maintenance. 

EFIS interface 

EGI POS DIFF 

The FMS detects a position 
difference between pure GPS 
solution and INS/GPS solution 
greater than maximum accuracy 
of the two sensors 
or  
The FMS detects a degraded 
operation mode of the EGI. 

Use another navigation 
sensor as a means of primary 
navigation. 
 
Advise maintenance. 

EGI Interface 
and 
Nav cross-check configured 

END OF ROUTE 

Passing the last waypoint in the 
route. FMS steering becomes 
invalid. 

Select RTE LEGS page to 
enter additional waypoints to 
resume FMS steering. 

All configurations 

ENTER 
POS/DATE/TIME 

FMS battery failure detected 
invalidating the RTC date/time 
and current position. 

Enter date, time and position. 
 
Advise maintenance. Master 
Caution is active. 

All configurations 

This page is printed under user's responsibility

 

and must not be retained for reference

Summary of Contents for CMA-9000

Page 1: ...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...

Page 2: ...This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 3: ...our web based Customer Support Request form at http www cmcelectronics ca customer support request form aspx to inform us of any correction or send us a marked up copy of this publication using the fo...

Page 4: ...This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 5: ...igation 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 Sect...

Page 6: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page TC 2 November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 7: ...VOR DME TACAN 1 5 D Inertial 1 5 E KALMAN FILTER 1 5 F DEAD RECKONING DR 1 5 MILITARY NAVIGATION MODE 1 6 A Hybrid GPS Inertial 1 7 B GPS or cGPS mGPS for dual GPS installations 1 7 C DME DME 1 8 D V...

Page 8: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 1 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 9: ...N Civil and Military installations External GPS Civil certified or Military not approved for civil certified installation External Embedded GPS INS EGI Military not approved for civil certified instal...

Page 10: ...nt panel sense any change in the cockpit ambient light level This results in an increase or decrease in display brightness relative to a manual brightness setting The second option consists in an exte...

Page 11: ...gation 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 W...

Page 12: ...nd 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 integrit...

Page 13: ...avigation mode In this mode the primary navigation sensor will be a GPS receiver The AHRS is used as a dead reckoning navigation system by emulating an Inertial Navigation System INS with a KALMAN fil...

Page 14: ...tion option integrity is only required and defined for navigation solutions with GPS input during the approach phase Not having integrity does not prevent a navigation mode solution from being used ho...

Page 15: ...S will remain selected for navigation but the GPS Integrity annunciator will illuminate and the GPS POS UNCERTAIN alert message will be displayed NOTE This message is enabled in either of the followin...

Page 16: ...ation solution from the DME DESELECT page D VOR DME TACAN VOR DME navigation is used in areas with sparse DME coverage where there are less than three DME stations available This mode combines co loca...

Page 17: ...d on the performance of the AHRS used typically 2 minutes I DEAD RECKONING DR When the external sensor data inputs become insufficient to maintain the normal navigation modes the CMA 9000 FMS reverts...

Page 18: ...K HEADING HDG BEARING TO WAYPOINT BRG WINDSPEED WS DESIRED COURSE LINE GREAT CIRCLE BETWEEN WAYPOINTS CROSS TRACK DISTANCE XTK LEFT TRACK ANGLE ERROR TKE LEFT 0012033 GROUND SPEED GS TRUE AIR SPEED TA...

Page 19: ...rrival Routes STAR STAR transitions GPS and GPS overlay instrument approaches and approach transitions can be selected from for the departure arrival airports These procedure may be modified on the LE...

Page 20: ...l AHCAS Advanced Helicopter Cockpit and Avionics System AHRS Attitude Heading Reference System ALT Altitude AMLCD Active Matrix Liquid Crystal Display AMU Audio Management Unit ANP Actual Navigation P...

Page 21: ...ation DF Direct To Fix DGNSS Differential Global Navigation Satellite System DIFF Differential DISCON Route Discontinuity DIS Distance DIST Distance DLU Data Loader Unit DMAP Digital Map DME Distance...

Page 22: ...sion GLNS GLONASS GLONASS Global Navigation Satellite System Russian GMT Greenwich Mean Time GNS Global Navigation System GNSSU Global Navigation System Sensor Unit GPIAL GPS Position Integrity Alert...

Page 23: ...nce System ITU Telecommunication Union JOY Joystick KG Kilogram KT Knot s L Left LAT Latitude or Lateral LB Pound LDA Landing distance available LDR Light Detector LIB Library LNAV Lateral Navigation...

Page 24: ...es To Airmen NP Navigation Performance NPA Non Precision Approach NVx Primary NV1 or secondary NV2 NAV radio NVM Non Volatile Memory VNAV Vertical Navigation NVIS Night Vision Imaging System O Overfly...

Page 25: ...emote Control Unit RCV Receive only REC Flight Recorder REF Reference REL Relative RES Reserve RESEL Reselect RF Radio Frequency RFMS Rotorcraft Flight Manual Supplement RIB Radio Interface Board RMS...

Page 26: ...ive TRANS Transition TRK Track TRG Transmit on Guard TSE Total System Error TSO Technical Standard Order TTFF Time To First Fix TTG Time To Go TTS Time To Station TX1 V UHF1 Transmitting TX2 V UHF2 Tr...

Page 27: ...tion WPT Waypoint WS Windspeed WT Weight WGS World Geodetic System WGT Weight WXR Weather Radar XFILL Cross FMS Fill XPDR Transponder XMT Transmit XTE Extended Trailing Edge Point XTK Cross Track Z Zu...

Page 28: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 1 20 November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 29: ...ION 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 This...

Page 30: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 2 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 31: ...acters The CMA 9000 FMS and the MCDU have a full alphanumeric keyboard with special function keys These special function keys are in fact Front Panel Function Keys FFKs e g INIT REF RTE DEP ARR etc Th...

Page 32: ...ROG EXEC A H O V D K R Y B I P W E L S Z C J Q X F M T G N U 1 2 3 4 5 6 7 8 9 0 0611006 CMC ELECTRONICS TX1 MARK 9 12 13 14 11 10 1 2 3 4 5 6 8 7 15 16 17 18 19 20 32 21 22 23 24 25 26 27 28 29 30 31...

Page 33: ...RTE RADIO ANS SP FIX CLR BRT LEGS HOLD PROG EXEC A H O V D K R Y B I P W E L S Z C J Q X F M T G N U 1 2 3 4 5 6 7 8 9 0 0610006 CMC ELECTRONICS GSM SQK IDT Figure 2 2 CMA 9000 FMS Front Panel Hardwar...

Page 34: ...FUEL SP FIX CLR BRT LEGS HOLD PROG EXEC A H O V D K R Y B I P W E L S Z C J Q X F M T G N U 1 2 3 4 5 6 7 8 9 0 0610007 CMC ELECTRONICS GSM MARK Figure 2 3 CMA 9000 FMS Front Panel Hardware variation...

Page 35: ...REF ARR RTE RADIO VNAV SP FIX CLR BRT LEGS HOLD PROG EXEC A H O V D K R Y B I P W E L S Z C J Q X F M T G N U 1 2 3 4 5 6 7 8 9 0 0611003 CMC ELECTRONICS FMC Figure 2 4 CMA 9000 FMS Front Panel Hardwa...

Page 36: ...REF ARR RTE RADIO TACT VNAV SP ATC CLR BRT LEGS HOLD PROG EXEC A H O V D K R Y B I P W E L S Z C J Q X F M T G N U 1 2 3 4 5 6 7 8 9 0 0610005 CMC ELECTRONICS Figure 2 5 CMA 9000 FMS Front Panel Hard...

Page 37: ...UAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 2 7 November 19 2009 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...

Page 38: ...ANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 2 8 November 19 2009 Figure 2 7 CMA 9000 FMS Front Panel Hardware variation 290 This page is printed under user s responsibility and must not be retained f...

Page 39: ...UAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 2 9 November 19 2009 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...

Page 40: ...AL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 2 10 November 19 2009 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...

Page 41: ...sequence hold exit initiation MAGENTA Depending on configuration used in normal video or reverse video to identify the active TO waypoint on ACT RTE LEGS 1 X and PROGRESS pages RED Reserved for maint...

Page 42: ...on causing it remains POS Annunciator illuminates when the CMA 9000 FMS is in dead reckoning navigation mode RNP Annunciator illuminates when the FMS ANP exceeds the RNP for the phase of flight OFST A...

Page 43: ...active the CMA 9000 FMS will continue to use the previous active data for navigation and guidance even though it is not displayed Any modification can be erased cancelled prior to EXECution by pressi...

Page 44: ...second time Priority is given to GSM FUEL Key VAR 002 003 005 102 103 106 302 303 502 503 506 Provides a quick access function to Fuel estimation and status pages TACT VAR 050 provides access to tact...

Page 45: ...n the MENU annunciator will also be turned on The FMS requests attention e g MENU light on when the MCDU is logged on a subsystem different from the FMS and the FMS generated a new alert or maintenanc...

Page 46: ...ge layouts page prompts and data entry rules Figure 2 10 Basic Display Format MOD RTE1 LEGS 1 2 299o 2 25 N M CAFTA A THEN ROUTE D ISCONTIN UI TY YZP01 299o 10 6N M YZP02 ERASE LEGS ETA PAGE NUMBER AN...

Page 47: ...e Recall list or placed only on the Message Recall list depending on the system configuration REFER TO APPENDIX E OF THIS MANUAL FOR THE LIST OF MESSAGES ALERT MESSAGES A Sytem Alert Require immediate...

Page 48: ...status will return to ACT status in normal video Slash Rule the slash key is used to separate two items of data entered in the same data field such as wind direction and speed If a single entry is ma...

Page 49: ...tude are created by adding a sequence number to the prefix WPT DME ARC Waypoints the waypoint name in the navigation database is created by adding the radial from the DME station in degrees followed b...

Page 50: ...FIX HDG Indicates a heading leg HOLD AT Replaces the TO WPT course on RTE LEGS 1 X and PROGRESS 1 4 pages when navigating a holding pattern P T Appended to the courses of the outbound legs of the pro...

Page 51: ...INSERTION 3 14 BUILDING A ROUTE VIA AIRWAY INSERTION 3 15 BUILDING A DEPARTURE PROCEDURE 3 16 VERIFYING ACTIVE ROUTE LEGS BY COURSE AND DISTANCE 3 17 INITIAL LEG 3 17 CANCELLING ANY PROCEDURE OR ROUT...

Page 52: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 3 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 53: ...UTES O FF SET N M ACT RTE 1 LEGS 1 2 264o 12 8 N M JOH H 262o 11 3N M D173J 280 1600A 263o RA RC ANC 10 6N M D233J 1600A 053o CR S 10 0N M ANC oFAF 053o CR S 5 0 9N M RW06R oFAF LEGS LEGS ETA FMS1 SET...

Page 54: ...RINC 743A GPS is configured check that GPS satellites are not deselected or deselected according to NOTAMs A detailed description of each display page is contained in Appendix A Radio display pages ar...

Page 55: ...this key will always increase brightness 1R 2R 3R 4R 5R 6R FMS1 IDENT 1 2 NAV DATA BA SE AC TI VE KLMWW069 7 OCT10 NOV06 09 S EC OND KLMWW069 7 NOV07 DE C0 4 09 OP PROG RA M C FG NO 614876 3 00 0 0777...

Page 56: ...correct maintenance action is required 6 Verify the date of the active database cycle If all identification data is correct system start up and initialization is complete 1R 2R 3R 4R 5R 6R FMS1 IDENT...

Page 57: ...nterchange of cycle dates The active database cycle is displayed in large font The active database can only be changed on the ground Display the IDENT 2 2 page by pressing INIT REF IDENT and NEXT This...

Page 58: ...LSK 1L and adjust display PARALLAX for proper viewing angle 2 Press DISPLAY LSK 3L and select color or monochrome for this test Re select color thereafter 3 Press INIT REF LSK 6L 4 Press IDENT LSK 1L...

Page 59: ...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 aft...

Page 60: ...position to the POSITION field by pressing LSK 1R ANGULAR REFERENCES FOR NAVIGATION AND DISPLAY Display the INIT REF INDEX 1 2 page by pressing INIT REF From the INIT REF INDEX 1 2 page display the S...

Page 61: ...essage prompts the crew to check the angular reference If the true mag cockpit switch is installed the FMS uses the switch to determine the angular display reference If the switch was set to Mag previ...

Page 62: ...EURONAV_A702 DMAP configured the CMA 9000 FMS will automatically display the RTE x LEGS 1 X page if valid DMAP waypoints are received and DMAP APPEND mode is ON If the DMAP APPEND mode is OFF and val...

Page 63: ...Display the desired route by pressing NEXT or PREV as often as required 2 Select route identifier by pressing the appropriate LSK 3 Select the direction in which the route is loaded by toggling DIREC...

Page 64: ...ORIGIN and DEST identifiers 4 Enter flight number into the scratchpad Move to the FLT NO field by pressing LSK 2R 5 Accept the new active route by pressing EXEC MOD status in the title line changes to...

Page 65: ...sing LSK 5L 4 The RTE 1 X page is re displayed Verify the ORIGIN and DEST identifiers 5 Accept the new active route by pressing EXEC When airborne selecting a user route will replace the destination w...

Page 66: ...he first waypoint into the scratchpad and move it to the TO WPT location by pressing LSK 1L The direct course and distance from present position to the TO WPT is computed and displayed and the INTC CR...

Page 67: ...E x 2 X page by pressing NEXT 4 Key the identifier of the first waypoint into the scratchpad and move it to the TO location by pressing LSK 1R DIRECT is displayed below VIA indicating that the first f...

Page 68: ...ady inserted waypoint The route structure can also be modified by adding and or erasing waypoints on the selected RTE x LEGS page 8 Display the first leg by pressing LEGS and PREV or NEXT as required...

Page 69: ...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: ...K 4R are installation dependent and thus may not appear as shown above LSK 5R appears only when the aircraft is on ground for maintenance database loading LSK 6R appears only when the aircraft is on g...

Page 71: ...modifiable Cruise TAS and Cruise Wind values Upon a warm or cold start the CMA 9000 FMS will keep the Cruise TAS value prior to the power down Upon a change in configuration the CMA 9000 FMS will set...

Page 72: ...y estimated by subtracting the fuel consumption based on the average fuel flow The display of the GWT units will match the display of the fuel flow units that is if the fuel flow is displayed in Kg Hr...

Page 73: ...into the RESERVE field by pressing LSK 2L 6 Key in the aircraft empty weight e g 5000 and move it into the EMPTY WT field by pressing LSK 1R 7 Key in the optional equipment weight e g 700 and move it...

Page 74: ...ts are configured at the time of installation 1 Add the desired element to the EFIS display by pressing the appropriate LSK until ON is displayed Transmission of selected data to the EFIS will be init...

Page 75: ...rtup in either synchronized or independent mode From the INIT REF INDEX 1 2 page display the SETUP 1 1 page by pressing SETUP LSK 5L 1 Select either INDEPENDENT or SYNCHRONIZED mode of operation NOTE...

Page 76: ...ized mode the CMA 9000 FMSs must contain the same databases Furthermore the active database must be the same in all CMA 9000 FMSs In the synchronized mode of operation the following items are automati...

Page 77: ...message in the scratchpad In synchronized mode both CMA 9000 FMS will use the best system sensor for navigation and guidance computations unless deselected on the DESELECT 1 1 page Therefore CMA 9000...

Page 78: ...ion and if the navigation mode is GPS the alert message GPS GPS POS DISAGREE is displayed in the scratchpad if the CMA 9000 FMS position is significantly different than that of the other CMA 9000 FMS...

Page 79: ...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 T...

Page 80: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 4 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 81: ...the correct order SID transitions are appended to the route after the SID and are usually separated from it by a route discontinuity unless the last waypoint of the SID and the first waypoint of the...

Page 82: ...URE CHATU2 CHATY RWYS 6L R AND 7L R DME REQUIRED TAKE OFF Runways 6L R Climb via a 040 heading for vector to V 23 Thence via transition or assigned route Runways 7L R Climb via a 070 heading for vecto...

Page 83: ...ID SPECIFICATION IN FLIGHT The CMA 9000 FMS allows the insertion of a SID procedure in flight providing the CMA 9000 FMS is configured as a ROTOR type aircraft The CMA 9000 FMS allows the activation i...

Page 84: ...d 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 a...

Page 85: ...opriate left hand LSK The SID list is replaced by the selected SID with the legend SEL beside the name Transitions available for the selected SID are listed below the SID under the heading TRANS If no...

Page 86: ...tive 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...

Page 87: ...ude from the GPS used for navigation civil or military from EGI For entries units are automatically detected and decimal point entry is not required NOTE This altimeter setting will be used until afte...

Page 88: ...OPERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 4 8 November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 89: ...ROM FLY BY 5 10 B TO CONVERT TO FLY BY FROM FLY OVER 5 11 LEG SEQUENCING 5 12 A FLY BY WAYPOINTS 5 12 B FLY OVER WAYPOINTS 5 12 ETA AND EFA 5 14 WAYPOINT LATITUDE LONGITUDE DISPLAY 5 15 PROGRESS ALONG...

Page 90: ...5 ii November 19 2009 ROUTE 2 OPTION 5 33 A INACTIVE ROUTE MANIPULATIONS SUMMARY 5 34 B INACTIVE ROUTE MANIPULATIONS DETAILED STEPS 5 34 NEAREST 5 36 TIMER If configured 5 39 TIMER 1 1 page If configu...

Page 91: ...YQ 364 3 8732 YZP 18 T YQ 224 0 6672 MOCA1 19 T YQ 222 2 8732 BKA 19 T YQ 364 3 8732 KILLA 19 T YQ 364 3 8732 LEGS ETA LEGS ACT PROGRESS 1 4 280T DTGN M ET A CAFTA 35 2 1817 9 Z 280T TOU 8 8 3N M 1830...

Page 92: ...and Drift Angle HDG DA True Air Speed TAS Magnetic Variation System Altitude in feet ALT System Altitude in meters when configured QNH Altimeter setting QNH SET and QNH Altimeter Reference QNH REF or...

Page 93: ...ves a QNH input that indicates a non standard altimeter setting Refer to SET QNH message logic in Section E for more details DISPLAYING THE LEGS OF THE ROUTE Display the ACT RTE x LEGS 1 X page by pre...

Page 94: ...ystem allows for a maximum of 99 temporary waypoints in a flight plan B PLACE BEARING PLACE BEARING WAYPOINTS With the first reference waypoint identifier in the scratchpad 1 Key into the scratchpad t...

Page 95: ...point key in distance e g KILLA 20 or 3 To move an initial DME ARC fix along the arc key in desired radial from the DME station e g D173J 203 then 4 Display the reference waypoint location in the rout...

Page 96: ...nce number e g WPT01 Alternatively the waypoint name can be automatically named using the latitude and longitude degree components e g N60W120 This option is selectable through configuration pages NOT...

Page 97: ...EXT for the INACT DES SAR or TACTICAL 2 2 entering the waypoint ident in the REF ID field at LSK 1L and RADIAL TO LSK 4R 1 Enter the parameters defining a Radial To procedure waypoint identifier inbou...

Page 98: ...e reference waypoint This is an abnormal situation where the Radial To flight path is flown back and forth at the reference waypoint A discontinuity is created at the next waypoint 5 The insertion way...

Page 99: ...field by pressing PREV as often as required 4 Move the waypoint to the THEN field by pressing the appropriate LSK 5 Verify the entry by checking course and distance of the previous and next legs 6 Mak...

Page 100: ...n anticipation as coded in the navigation database By default all waypoints including manually entered temporary waypoints are initially defined as fly by unless specifically coded as fly over Any way...

Page 101: ...by particularly the final approach fix and missed approach holding fix The crew will remain responsible at all times for remaining within protected airspace and for compliance with all altitude const...

Page 102: ...the active waypoint is displayed in white reverse video on the LEGS and PROGRESS pages Also during that period the waypoint alert information sent to the EFIS will remain on to indicate the transition...

Page 103: ...T03 fly by Act wpt WPT04 WPT04 fly over LEGEND Entered flight plan displayed on GAMA EFIS Flight path followed by Guidance Bisector Wayline TAD Turn Anticipation Distance Waypoint symbol WPTXX Waypoin...

Page 104: ...nstead of ETAs and they are based on the CRZ TAS as entered in the PLAN DATA page EFAs are based either on the current fuel flow and ground speed if a fuel computer is configured or on the fuel flow e...

Page 105: ...nt modifications are not permitted on the RTE x LEGS POS Y X page 2 The position displayed on the ACT RTE x LEGS POS or RTE x LEGS POS page depends on the selection for the coordinate system made on t...

Page 106: ...e desired RNP value and then press LSK 5L Manually entered RNP value will be displayed in large font size NOTE If the entered RNP exceeds the default RNP for the phase of flight an alert message VERIF...

Page 107: ...ent TAS REQUIRED TIME OF ARRIVAL COMPUTATION With the desired waypoint identifier in the scratchpad Display the RTA PROGRESS 3 4 or 2 3 page by pressing PROG PREV PREV or PROG NEXT respectively 1 Move...

Page 108: ...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 The HEADWIND TAILWIND field disp...

Page 109: ...000 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...

Page 110: ...Display the ACT RTE x 1 X page by pressing RTE 1 Set the offset value to zero by entering 0 zero into the scratchpad and moving it into the OFFSET field by pressing LSK 6R or 2 Delete the offset value...

Page 111: ...FIX to the aircraft are displayed The displayed reference of the bearing radial e g true or magnetic North is consistent with the other navigation angles as described in the SETUP page in Section 3 2...

Page 112: ...y in the radial e g 175 and press LSK 3L or LSK 4L or 3 To create a downtrack fix along the flight plan where the distance from the entered fix intersects key in distance e g 80 and press LSK 3L or LS...

Page 113: ...hen the FIX is a 7 character waypoint identifier the intersection is displayed as a waypoint coordinate 6 Display the desired location in the route by pressing LEGS and NEXT or PREV as required 7 Move...

Page 114: ...A 100NM ANN REFERENCE FIX MOCA1 60NM R 216 ANN 216 60 ABEAM CROSSING R 1 7 5 RADIAL CROSSING ANN 175 80 DISTANCE CROSSING ANN 163 100 YZP 4 G704127 cdr Figure 5 2 Typical Downtrack Fix Creation This p...

Page 115: ...miles e g 1 0 and moving it to the RNP field by pressing LSK 5L If the entered RNP exceeds the RNP for the phase of flight then the VERIFY RNP VALUE alert message is raised Refer to Section 15 RNP Ca...

Page 116: ...S DVS prompts are displayed only if their interfaces are configured For dual GPS installations with a civll GPS and a Litton LN 100GT EGI configured selection of LSK 1R will display the following page...

Page 117: ...deo and at intervals of 5 minutes before and after the ETA up to a maximum of 15 minutes After a short delay the results of the predictive RAIM computation are displayed for each arrival time The poss...

Page 118: ...fferent speed or making a flight plan change conduct the approach with other approved equipment or discontinue IFR operations PREDICTIVE RAIM SATELLITE DESELECTION Display the GPS SAT DESELECT page by...

Page 119: ...2 page is only used to display the GLONASS transmitted parameters The field descriptions are identical to the GPS STATUS 2 2 page The GLONASS page is displayed in cyan color to emphasize the fact tha...

Page 120: ...ccurrences of the entered identifier are found in the navigation database The duplicated identifier is incorporated into the page title line Duplicated identifiers are listed on as many pages as neces...

Page 121: ...copied using the FMS line select key on the RTE x LEGS page or the PROGRESS page or the RTE x page in the flight plan active or inactive a close up to that particular waypoint will be done if the wayp...

Page 122: ...NP value exceeds the default RNP for the phase of flight then the alert message VERIFY RNP VALUE will be displayed in the scratchpad 2 To revert to the default RNP for the phase of flight press CLR th...

Page 123: ...those of the active route When configuring the NO xFMS option the prompt ERASE RTEx appears at LSK 4L when RTE x is defined It allows to erase the RTE x 1 Display the ACT RTE x 1 X page by pressing RT...

Page 124: ...e inactive route press LSK 6R on the inactive RTE page followed by pressing the EXEC key NOTE The following RTE COPY procedures highlight the basic steps required to select then activate a second rout...

Page 125: ...s ACTIVATE LSK 6R to the inactive route 7 The RTE 2 LEGS page is displayed Press the EXEC key to confirm activation of RTE 2 1R 2R 3R 4R 5R 6R RTE2 LEGS 1 5 299o 39 6 N M CAFTA 298o 15 4 N M YZP 307o...

Page 126: ...rom the closest to the farthest By default the reference point is selected to be the current position of the aircraft The first time the NEAREST page is accessed after a cold start the center referenc...

Page 127: ...SK of the desired destination and then pressing DES SAR or TACTICAL LSK 6R The DES SAR or TACTICAL 1 2 page is displayed and the selected waypoint identifier is inserted in the REF ID filed LSK 1L The...

Page 128: ...s set to the present position PPOS when the page is accessed after a cold start The center reference waypoint can be selected from any of the following databases Navigation Database Custom Database Us...

Page 129: ...larm time was set then the time remaining is displayed in the countdown field Similarly if a countdown time was set the corresponding alarm time is displayed Once activated the CMA 9000 FMS enables th...

Page 130: ...1 1 ALARM T IM E COUN TD OWN 1234 12z ADD 5 MIN ADD 15 MIN ADD 30 MIN START CLEAR 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R TIMER 1 1 ALARM T IM E COUN TD OWN z 2354 56 ADD 5 MIN START CLEAR 1L 2L 3L 4L 5L...

Page 131: ...Page 6 i November 19 2009 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 r...

Page 132: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 6 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 133: ...ute discontinuity For certain types of STAR and transition the waypoints may not be loaded into the route until the approach is selected Approach transitions are appended to the route after the STAR a...

Page 134: ...ke the modified route active A detailed description of each page appears in Appendix A STANDARD TERMINAL ARRIVAL ROUTE STAR SELECTION This procedure is based on the STAR and STAR transition depicted i...

Page 135: ...MENDORF AFB ALASKA 213 ANCHORAGE ALASKA Merrill 213 ANCHORAGE Intl 144 Direct distance from Amott Int to Anchorage Intl 43 NM Direct distance from ANC VOR to Anchorage Intl 6 NM N NOT TO SCALE AMOTT F...

Page 136: ...h has already been selected then only those STARs applicable to that approach will be displayed 3 Display the desired STAR transition by pressing the PREV or NEXT key as required and select the transi...

Page 137: ...e speed advisory and procedural leg type information of each STAR leg in turn pressing NEXT as required to display all legs 7 Make the selected STAR and STAR transition active by pressing EXEC On re d...

Page 138: ...OPERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 6 6 November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 139: ...12 CIRCLING APPROACHES 7 13 VFR APPROACHES 7 14 MISSED APPROACH INITIATION 7 15 NEW APPROACH AFTER A MISSED APPROACH 7 17 MODIFYING APPROACH PROCEDURES 7 18 APPROACH MODE DESELECTION 7 19 DME ARC INT...

Page 140: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 7 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 141: ...itude constraint advisories Figure 7 1 shows a typical approach involving a full procedure turn and missed approach If a runway is selected rather than an approach only the runway threshold waypoint i...

Page 142: ...rpose except when the FAF is the TO WPT The distance from the procedure turn reference fix can be monitored using the FIX page as described in Section 5 Deletion of the procedure turn reference fix or...

Page 143: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 7 3 November 19 2009 Figure 7 1 Typical Arrival Procedure This page is printed under user s responsibility and must not be retained for referenc...

Page 144: ...es are listed on the right hand side of the page followed by the runways The selected STAR and STAR transition are displayed on the left hand side of the page with the legend ACT beside the name If a...

Page 145: ...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 app...

Page 146: ...3 2 0 0 h d g 053 356 IAF D173J 1 0 D M E A r c 10 DM E Arc 1 6 0 0 N o P T 1600 NoPT MISSED APCH FIX 2 0 0 h d g D 2 1 8 3 5 3 A N C 1 1 4 3 1 7 3 ENA 037 117 6 NAPTO 5 0 1 in 5NM 5 10 15 61 10 61 00...

Page 147: ...roach transition active by pressing EXEC On re display of the ARRIVALS page the active approach and approach transition are shown with the ACT legend beside the name 1R 2R 3R 4R 5R 6R MOD RTE 1 LEGS 2...

Page 148: ...TION The CMA 9000 FMS altimeter setting entry should be verified using standard crew cross check procedures because of the potential impact on missed approach navigation and guidance The baro correcte...

Page 149: ...cimal point entry is not required NOTE This altimeter setting will be used until after landing or until leaving the terminal area The altimeter setting is cancelled and the field displays dashes on le...

Page 150: ...arming of the approach mode the ARM APPROACH advisory message is repeated if the approach mode has not yet been armed At 2 nm inbound to the FAF With GPS approach integrity predicted to exist at the F...

Page 151: ...or military navigation configurations without a Predictive RAIM function available the current GPS Group NP Navigation Performance value is used in place of Predictive RAIM HIL and assumed to be the s...

Page 152: ...at when flying a GPS overlay approach a charted track defined by a VOR radial may differ slightly from the CMA 9000 FMS displayed course due to differences in the magnetic variation value used to defi...

Page 153: ...GPS or GPS overlay instrument approach procedure loaded into the route and made active 1 At a convenient time prepare for the circling maneuver by entering the landing runway number in the scratchpad...

Page 154: ...vigation with or without an intercept to the missed approach holding fix or to an intermediate missed approach waypoint will initiate the required navigation and guidance VFR APPROACHES Display the AR...

Page 155: ...erminated leg earlier than would normally be the case and in some cases will result in an immediate turn upon crossing the Missed Approach Point in the direction of the leg following the altitude term...

Page 156: ...tiated by pressing the TOGA switch the LNAV autopilot flight director mode automatically remains valid The CMA 9000 FMS reverts to the terminal phase of flight 3 If the autopilot flight director mode...

Page 157: ...the missed approach manouver is to press the TOGA switch NEW APPROACH AFTER A MISSED APPROACH With the desired ARRIVALS 1 1 page displayed 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 1 053o CR S 3 0 9N M RW06R...

Page 158: ...re is desired simply close up the route discontinuity by copying the first waypoint of the new approach procedure to the scratchpad and pressing LSK 2L Make the new route active by pressing EXEC MODIF...

Page 159: ...avigation to any waypoint as described in Section 9 or 3 if not yet at the FAF by defining a holding pattern at the FAF as described in Section 10 DME ARC INTERCEPTION The CMA 9000 FMS provides automa...

Page 160: ...ered radial e g D220J 4 Make the modified route active by pressing EXEC Once established on the arc the HSI course pointer displays the tangential course along the arc path Lateral deviation is measur...

Page 161: ...MOD route and the FAF waypoint becomes the TO WPT with the correct inbound course to the FAF displayed as the default intercept course NOTE The procedure turn also can be deleted by deleting the refer...

Page 162: ...to FAF and limited to 0 6 nm from FAF up to the runway threshold If the aircraft position is outside this zone defining the glidepath width or if the aircraft is not inbound to the landing runway ver...

Page 163: ...nd the FAF charted altitude The indicated altitude will be 50 ft or more above the FAF charted altitude The reason for this difference is because the FMS computes the target vertical profile using the...

Page 164: ...Profile View of Vertical Path for a VNAV Approach FAF MAP HSI SCALE TO CHANGE ADVISORY MESSAGE 3NM 3NM 2NM 2NM 0403010 GPS APPROACH CAP ANNUNCIATOR INBOUND COURSE 6NM 6NM GLDEPATH WIDTH VDEV FS 500FT...

Page 165: ...rature of 25 C is reported at the destination airport enter 25 in the scratchpad Press LSK 5L and then press the EXEC key All altitudes including the MDA DA for approach and approach transition waypoi...

Page 166: ...tes when crossing the runway threshold If sequencing the missed approach point and the same approach is re selected the entered MDA DA value is retained Similarly the QNH and Airport Temp entries are...

Page 167: ...rcraft is outside of the zone defined by the glidepath width as specified above or if the aircraft is not inbound to the landing runway Target vertical speed and vertical deviation is not displayed on...

Page 168: ...GHT MANAGEMENT SYSTEM Page 7 28 November 19 2009 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...

Page 169: ...8 i November 19 2009 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...

Page 170: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 8 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 171: ...point in flight by copying the present position into the scratchpad by pressing LSK 1R This frozen present position can be stored for later analysis as a temporary waypoint at the end of the active ro...

Page 172: ...LSK 6L NOTE The initial takeoff time should only be reset following a ground to air transition for FIXED wing aircraft and the first ground to air transition following a cold start on the ground for R...

Page 173: ...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 DIRECT TO A WAYPOINT IN THE INACTIVE ROUTE 9 4 NAVIGATION OF DIRECT TO WITH INTERCEPT 9...

Page 174: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 9 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 175: ...ding and the Direct To a waypoint procedures NOTE The direct to function can be defined as standard or moving_dtk via a configurable option In addition to this selection a tactical direct to function...

Page 176: ...MENT SYSTEM Page 9 2 November 19 2009 00 33 3 0 27 2 4 2 1 18 1 5 1 2 09 0 6 03 WP2 WP1 PPOS 0703001 Figure 9 1 Standard Direct To a Waypoint Procedure This page is printed under user s responsibility...

Page 177: ...status in the title line is replaced by ACT Navigation and guidance change to the new leg from present position to the TO waypoint If autopilot coupled the aircraft will immediately start to turn towa...

Page 178: ...rse inbound to the waypoint The mode used is dependent on the aircraft installation The CMA 9000 FMS initially enters a Track Hold mode TRK configuration or a Heading Hold HDG configuration mode or ke...

Page 179: ...TO FIX alert message is displayed The display of guidance data remains relative to the intercept course 0703003 INTERCEPT FIX NEXT WAYPOINT SET UP DIRECT TO INTERCEPT LEG ON MCDU AND EXECUTE PROCEDUR...

Page 180: ...n to Track Heading Hold mode using the new aircraft track heading If the CMA 9000 FMS LNAV discrete is not configured the information regarding the AFCS Auto Flight Control System LNAV status is sent...

Page 181: ...rse by pressing INTC CRS LSK 6R The default inbound course changes to LARGE font and is copied to the TO WPT course The current track heading will not intercept the inbound course prior to reaching th...

Page 182: ...cept the inbound course prior to reaching the TO WPT a NOT ON INTERCEPT TRK or NOT ON INTERCEPT HDG advisory message will be displayed 5 Verify the course and distance of the leg to the TO WPT NOTE If...

Page 183: ...G PATTERN AT AN OFF ROUTE WAYPOINT 10 11 HOLDING PATTERN AT PRESENT POSITION 10 12 SECOND HOLDING PATTERN 10 12 MODIFYING AN EXISTING HOLD 10 13 A PRIOR TO HOLD ENTRY 10 13 B AFTER HOLD ENTRY INITIATE...

Page 184: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 10 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for referenc...

Page 185: ...ction The shape and terminology of the figure below depicts a right turn holding pattern For left turn holding patterns the corresponding entry and holding procedures are symmetrical with respect to t...

Page 186: ...el entry and expected aircraft guidance on a typical GAMA EFIS display For COLLINS EFIS 84 display system no holding pattern is displayed rather the crew is provided with an HL or HR appended to the h...

Page 187: ...FLIGHT MANAGEMENT SYSTEM Page 10 3 November 19 2009 SHU H 0709252 02 03 01 SHU H MUR O 02 03 01 SHU H 02 03 01 Figure 10 1 Parallel Entry This page is printed under user s responsibility and must not...

Page 188: ...ed with an HL or HR appended to the holding fix s waypoint name to indicate a left or right hand rotation hold pattern respectively NOTE The advisory message TEARDROP HOLD ENTRY is displayed as soon a...

Page 189: ...OPERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 10 5 November 19 2009 Figure 10 2 Teardrop Entry This page is printed under user s responsibility and must not be retained for reference...

Page 190: ...COLLINS EFIS 84 display system no holding pattern is displayed rather the crew is provided with an HL or HR appended to the holding fix s waypoint name to indicate a left or right hand rotation hold p...

Page 191: ...9000 FLIGHT MANAGEMENT SYSTEM Page 10 7 November 19 2009 0709250 SHU H 02 03 01 MUR O SHU H 02 03 01 MUR O Figure 10 3 Direct Entry This page is printed under user s responsibility and must not be re...

Page 192: ...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 Aircraft Type Altitud...

Page 193: ...he navigation database speed and altitude restrictions are also displayed When the aircraft crosses 14000 ft the HOLD leg time does not change automatically 3 Change the turn direction by pressing LSK...

Page 194: ...ypoint the course to the TO WPT displayed on the RTE x LEGS 1 X and PROGRESS 1 3 or 1 4 pages is replaced by the legend HOLD AT and a HOLD prompt is displayed at LSK 6R A navigation database holding p...

Page 195: ...he MOD HOLD page is displayed Modify the holding pattern parameters as required following the manual entry procedure described previously 3 Verify the holding pattern parameters and arm the hold by pr...

Page 196: ...entry to the hold If the inbound course is not aligned with the current course an appropriate standard hold entry procedure will be followed NOTE A holding pattern at present position can only be ini...

Page 197: ...g HOLD When the aircraft is in the holding pattern the ACT HOLD page is displayed 2 Modify the holding parameters The HOLD page title line will change from ACT HOLD to MOD HOLD 3 Verify the new patter...

Page 198: ...applicable to the first outbound turn towards the holding fix to exit the holding pattern over the fix followed by continuation of the active route The immediate turn is not applicable for the very fi...

Page 199: ...n Appendix A for details 2 Resume the exit hold procedure by pressing ONCE LSK 5L The RESUME HOLD prompt disappear the status changes to RESUMING HOLD the exit type changes to MANUAL and the ERASE pro...

Page 200: ...and the EXEC annunciator extinguishes HOLDING PATTERN DELETION A PRIOR TO ENTRY 1 Display the desired holding waypoint by pressing LEGS NEXT or PREV as required 2 Key in 3 Cancel the hold by pressing...

Page 201: ...TE A USER WAYPOINT FROM THE USER DATABASE 11 27 E DELETE ALL THE USER WAYPOINTS FROM THE USER DATABASE 11 29 F VIEW ALL THE USER WAYPOINTS IN THE DATABASE 11 30 G CREATING A USER WAYPOINT FROM A DMAP...

Page 202: ...11 75 CARP SEQUENCE OF EVENTS 11 78 CARP ALERT MESSAGES 11 80 EXIT FROM CARP 11 81 CARP RE ENTRY 11 81 CARP WIND ENTRY 11 82 CARP SPEED TARGET ON DISPLAY SYSTEM 11 82 POSITION UPDATES FOR CARP GENERAL...

Page 203: ...rs of the desired search pattern may either be entered before take off or while en route to the search area Based on parameters entered the FMS computes the maximum ground speed at which the search sh...

Page 204: ...mple 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 When defining the dimensions of the search area it is recommended to increase the leg l...

Page 205: ...Angle degrees 15 20 25 30 50 0 3 0 2 0 2 0 1 60 0 4 0 3 0 2 0 2 70 0 5 0 4 0 3 0 2 80 0 7 0 5 0 4 0 3 90 0 9 0 6 0 5 0 4 100 1 1 0 8 0 6 0 5 110 1 3 1 0 0 8 0 6 120 1 6 1 2 0 9 0 7 130 1 8 1 4 1 1 0 9...

Page 206: ...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 over...

Page 207: ...any search parameters 3 Change the pattern type by pressing PREV or NEXT By pressing once the NEXT functional key the MOD RTE x LADDER 1 1 page is displayed Another press of the NEXT functional key wi...

Page 208: ...needed key in the new search bearing into the scratchpad and move it to the SAR BRG field by pressing LSK 3R then 9 Verify the NEW search pattern parameters 1R 2R 3R 4R 5R 6R MOD RTE 1 SQUARE 1 1 ID...

Page 209: ...nly one search pattern may be defined in the route at a given time A second possibility for defining a search pattern at a route waypoint is the following 1 Display the ACT RTE x LEGS 1 X page by pres...

Page 210: ...e ACT RTE x LEGS 1 X page is displayed with the respective waypoint followed by S displayed in the scratchpad 1R 2R 3R 4R 5R 6R DES SAR 1 2 REF ID ARRIE RTE DISCON RAD DIS T NM HOVER SQUARE HOLD LADDE...

Page 211: ...ess 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 a...

Page 212: ...ing LSK 6R The MOD RTE x SQUARE 1 1 page is displayed 1R 2R 3R 4R 5R 6R RTE 1 SQUARE 1 1 ID TRACK SP AC ING ARRIE 1 0N M REF ID SA R BRG 000T MAX GS ACTIV E SAR 72 KT SQ UARE CANCEL ACTIVATE 1L 2L 3L...

Page 213: ...h the status ACT reverse video white appended to the prompt if an activated square search pattern is in the flight plan 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 3 254o 55 6N M ARRIE S THEN ROUTE D ISCONTIN...

Page 214: ...the search pattern 1 Display the RTE x LEGS page so that the search pattern can be inserted at the desired location in the route by pressing LEGS and NEXT as required 2 Move the waypoint entry to the...

Page 215: ...rect To navigation to the search pattern origin SEARCH PATTERN AT PRESENT POSITION IN FLIGHT ONLY 1 Display the default values of the search parameters SQUARE LADDER SECTOR 1 X page by pressing INIT R...

Page 216: ...Cuting a search at the present position PPOS S is shown in the first position of the ACT RTE x LEGS 1 X page If subsequently a Direct To a waypoint not existent in the current route is performed then...

Page 217: ...and accept them by pressing the ACTIVATE and EXEC keys EXITING A SEARCH PATTERN A EXIT BY DIRECT TO NAVIGATION TO ANY WAYPOINT Perform a standard Direct To procedure to any waypoint When the Direct T...

Page 218: ...This position is displayed on the PREDEF WPT 2 2 page and can be used also for creating a new user waypoint This function allows the operator to create a waypoint instantly when flying over a landmar...

Page 219: ...t configured 1R 2R 3R 4R 5R 6R PREDEF WPT 2 2 MARK ON T OP 13 15 10z N45o 34 25 W122 o 4 5 12 LAST JO YS TICK 11 48 57z N44o 12 34 W100 o 0 1 02 LAST PL S 12 34 12z N43o 56 78 W095 o 1 7 66 PLS DAT A...

Page 220: ...d DVS DVS configuration only Refer to the UPDATE POS in section 12 HOVER PROCEDURE TRANSDOWN TO HOVER If configured The CMA 9000 FMS can also manage a transdown profile to hover based on the definitio...

Page 221: ...ption of the procedure request wind direction frozen at procedure execution time wind module frozen when overflying the TDN waypoint CAUTION The transdown to hover procedure will be executed over flat...

Page 222: ...000 FLIGHT MANAGEMENT SYSTEM Page 11 20 Revision 1 December 08 2009 TDN MARK WIND 0109018 Figure 11 4 TDN MARK WIND 0109017 Figure 11 5 This page is printed under user s responsibility and must not be...

Page 223: ...of a waypoint can be changed as long as there is no hover procedure defined in the active route If the system wind is not available the wind parameters can be entered manually on the PROGRESS 1 4 pag...

Page 224: ...ALT HOVER H EI GHT 2560 F T 8 0 F T TRUE WI ND VELOC IT IES 020T 45K T VX 25 5 K T VY 25 5 K T ERASE 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R MOD RTE 1 LEGS 1 2 286o 2 8 N M WPT02 OTDN 2 5 5 o 0 1N M WPT01...

Page 225: ...database The aircraft installation provides the means to action this input User waypoints can be defined as different types Waypoint fixed or moving Airport VHF NAV TACAN only A new user waypoint can...

Page 226: ...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 1R 2R 3R 4R 5R 6R USER WPT 1 2 ID POS F...

Page 227: ...osition at LSK 1R or the Bearing Distance at position LSK 2L 4 Enter the Track and Ground Speed of the moving waypoint at LSK 2R 5 When the mandatory fields are filled a CANCEL CONFIRM prompt is displ...

Page 228: ...visualized and modified by pressing the corresponding LSK on the USER WPT LIST 1 X page The WPT DATA 1 1 page will be displayed and changes can be performed on the parameters If a moving waypoint whi...

Page 229: ...nter the airport ELEVATION at LSK 5R mandatory field When the mandatory fields are completed e g name and position of the new user waypoint a CANCEL CONFIRM prompt is displayed Press CONFIRM LSK 6R to...

Page 230: ...LSK 6L 1R 2R 3R 4R 5R 6R USER WPT 1 2 ADFF ID P OS FRE E 459 N45o 12 23 043o 32 12 BRG DIS 223T 115N M TYPE FIXED REF WPT I D RA D DIS 000o 0 00N M REF WPT P OS o o CANCEL DELETE CONFIRM 1L 2L 3L 4L 5...

Page 231: ...page press the DELETE ALL prompt LSK 6R and a CANCEL CONFIRM prompt is displayed Press CONFIRM LSK 6R to accept or CANCEL LSK 6L NOTE If a moving waypoint is present in the active or modified route pr...

Page 232: ...ess the DMAP WPT X Y page press INIT REF WPT LISTS LSK 2R and DMAP WPT LSK 2L 1 Press the key corresponding to the reference identifier of the waypoint to store in the user database at LSK 1L 2L 3L or...

Page 233: ...ition appears on the PREDEF WPT 2 2 page at LSK 1R Mark On Top and LSK 2R Last Joystick 1R 2R 3R 4R 5R 6R PREDEF WPT 2 2 MARK ON T OP 12 34 12z N45 34 25 W122 4 5 12 LAST JO YS TICK 11 48 57z N44 12 3...

Page 234: ...LSK 1R FLIR POS 1 By pressing the NEW USER WPT prompt LSK 6L the USER WPT 1 2 page is displayed and enters the last updated position of the FLIR into POS field at LSK 1L The identifier FLIR is display...

Page 235: ...DATA LOAD the DATA LOAD 1 1 page is displayed Toggle the TYPE prompt LSK 1L till it indicates USER_DATA 2 Press SAVE LSK 6R to start data download from the CMA 9000 FMS to the Data Loader Unit only wh...

Page 236: ...MA 9000 FMS will purge its internal memory of all User route s User waypoint s Temporary waypoint s DMAP waypoint s Predefined waypoint s Active route Inverse route Inactive route Sarsat waypoint s Bu...

Page 237: ...s flown as a Direct To Fix ARINC 424 DF leg type Activation of the backtrack route while in flight is configurable with two following options The resulting modified route consists of A Configuration O...

Page 238: ...ing the BACKTRACK prompt LSK 5L When the backtrack route is selected the CMA 9000 FMS creates a temporary waypoint to mark the present position This temporary waypoint is inserted in the modified rout...

Page 239: ...ers a rendez vous unachievable in any of the following conditions 1 The moving waypoint is the active waypoint and interception of the moving waypoint is not possible within a traveling distance of 50...

Page 240: ...he roll steering the lateral deviation does not yet convey useful information When the track angle error becomes smaller than 2 degrees the intercept course becomes fixed in space The lateral deviatio...

Page 241: ...entifier in the REF ID field 3 Press TACT DTO LSK 5R 4 The waypoint identifier followed by the T qualifier is displayed in the scratchpad and the ACT RTE x LEGS 1 X page is displayed 5 Move the waypoi...

Page 242: ...TO A WAYPOINT IN THE INACTIVE ROUTE 1 Display the INACT DES SAR OR TACTICAL 2 2 page by pressing INIT REF DES SAR or TACTICAL NEXT 2 Enter the waypoint identifier in the REF ID field 3 Press TACT DTO...

Page 243: ...Eye reference point Bulls Eye can also be defined by entering directly coordinates on LSK 1R In this case the ident will always be BULL 2 An alternative way can also be made using a reference waypoin...

Page 244: ...EYE 3 3 BULL BULL ID POS N43o 26 20 E004o 52 32 BRG DIS 015 T 270N M REF WPT I D RA D DIS ABCDE 000o 0 0N M REF WPT P OS N43o 26 20 E004o 52 32 CANCEL SAVE CONFIRM 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R...

Page 245: ...ined as either a fixed waypoint or a moving waypoint This selection is made via the LSK 3L When the Bulls Eye target is a moving waypoint a track and ground speed is required to be entered This entry...

Page 246: ...WPT I D RA D DIS o N M REF WPT P OS o o SARSAT WPT DES SAR 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R BULLS EYE 2 3 BETGT TGT ID POSAC T RTE N43o 26 20 E004o 52 32 BRG DIS TK GS 015 T 270N M 111 T 222K T TY...

Page 247: ...t of the active route 1R 2R 3R 4R 5R 6R BULLS EYE 2 3 BETGT TGT ID POS N43o 26 20 E004o 52 32 BRG DIS TK GS 015 T 270N M 111 T 222K T TYPE MS L ALT MOVING F T REF WPT I D RA D DIS BULL 000o 0 0N M REF...

Page 248: ...LSK 5L and LSK 5R respectively C When the Bulls Eye Target rendezvous is unachievable D When the Bulls Eye Target is fixed 1R 2R 3R 4R 5R 6R BULLS EYE 1 3 PPOS REF BULL 01 0 o 33 0N M FR TGT POS BE TG...

Page 249: ...ory vertical guidance e g Vertical Track Deviation while conducting a tactical approach The FMS also provides lateral guidance to conduct the approach and the missed approach segment of the tactical a...

Page 250: ...tion user definable 50 feet MSL VPA user definable or FMS calculated Altitude constraint MAP MAP TFAF to MAP user definable TIAF to TFAF user definable TFAF TIAF Altitude constraint TFAF user definabl...

Page 251: ...TION It is the crew s responsibility to ensure that the appropriate transition level for the tactical approach destination was correctly entered The crew can manually overwrite the length default valu...

Page 252: ...to TFAF altitude if computed TFAF is higher than TIAF Vertical Course NOTE Altitude constraints VPA IAA and climb gradients remain the same when the following parameters are changed Initial Approach...

Page 253: ...annot be modified by the crew NOTE Runway Elevation is displayed for information only and cannot be modified by the crew on this page The crew can manually overwrite the default length values of the 2...

Page 254: ...l Profile Geometry Runway elevation user definable 50 feet MSL Altitude constraint MAP MAP Altitude constraint TMAP1 user definable or FMS computed value TMAP1 Altitude constraint TMAP2 user definable...

Page 255: ...oordinates Lateral Altitude NOTE The TIAF TFAF MAP TMAP1 and TMAP2 coordinates remain the same when the following parameters are changed TMAP1 altitude constraint LSK 2R CLBGRD1 CLBGRD2 TMAP2 altitude...

Page 256: ...ch Course 30o Table 11 4 Tactical Approach default minimum and maximum values As a result of the aforementioned manual entries the FMS presents to the crew on the RTE X LEGS page the tactical approach...

Page 257: ...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 Ap...

Page 258: ...tical approach 3 Via the TACT APPR prompt located on DES SAR or TACTICAL 2 4 or DES SAR or TACTICAL 4 4 for the inactive route As is the case for other waypoints entered via the DES SAR or TACTICAL pa...

Page 259: ...nsuring the following 1 For the active flight plan none of the 3 tactical approach created waypoints e g TA01 TA02 or RWY THR WPT are the TO waypoint and then entering a in the scratchpad and line sel...

Page 260: ...efore the tactical approach procedure in the flight plan After this the operator can access the tactical approach procedure via DES SAR or TACTICAL page 2 4 to make any necessary changes DELETING A TA...

Page 261: ...the same direction as the landing zone and the wings are level upon reaching the slow down point 3 Slowdown Point SD FMS computed waypoint used to signal to the pilot that the altitude and speed must...

Page 262: ...IN T S D T U R N IN G P O IN T T P ID E N T IF IC A T IO N P O IN T IP W IN D D IR E C T IO N E S C A P E P O IN T E S C W P T 1 0 W P T 0 9 D R O P Z O N E F T D T R A IL IN G E D G E T E E X T E N...

Page 263: ...S E W PARACHUTIST MAX DRIVE DISTANCE CRP GREEN LIGHT POINT IMPACT PI SLOWDOWN POINT IDENTIFICATION POINT WIND DIRECTION RED LIGHT ESCAPE POINT WPT10 WPT09 80 TURNING POINT Figure 11 13 Typical HAHO P...

Page 264: ...ther on the inactive route INITIATION OF A CARP HARP PROCEDURE A CARP procedure can be initiated via the following methods A Assuming no CARP procedure is already included in the flight plan 1 Press I...

Page 265: ...y mission parameters ballistic data local pressure and wind data as defined in the CARP PLAN pages in Appendix A 5 Press EXEC If insufficient parameters are entered then pressing the EXEC key will dis...

Page 266: ...1 3 TYPE CUST CARP IDENT POINT IP o o POINT IMPACT PI o o TRAILING EDGE TE o o ZONE WI DT H ESC T IME 0 30N M 3 0S E C ERASE 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R MOD RTE1 CARP PLAN 1 3 TYPE CUST HARP I...

Page 267: ...e The CARP PLAN pages are used to define the parameters for a CARP procedure The CARP procedure may be defined in either the active or inactive route A Active status and sample inputs Custom CARP 1R 2...

Page 268: ...T IME 0 30N M 3 0S E C CARP PROGRESS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R ACT RTE1 CARP PLAN 1 3 TYPE CUST HAHO CDFB IDE NT POINT IP N45o 00 00 W072 o 0 0 00 WPT07 PO IN T IMPACT PI N45o 00 02 W072o 00...

Page 269: ...n a temporary waypoint is automatically created and the identifier WPTXX is displayed in 3L Otherwise a database waypoint identifier may be entered in this field PI 3R Latitude and Longitude coordinat...

Page 270: ...int using relative bearing and distance as offsets e g WPT12123 60 defines a position with a bearing of 123 degrees and distance of 60 nm relative to WPT12 Invalid entries in terms of format or range...

Page 271: ...N H G CARP PROGRESS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R RTE1 CARP PLAN 2 3 PI ELEV SD D IST 5000F T 3 1N M IAS HAT DROP T EMP 156K T 1560F T 20 0o C SAFETY FA CTOR 1560F T WIND MEAN WIND G RO UND 020...

Page 272: ...be greater than the entered safety factor for CUST HAHO DROP TEMP 2R Static air temperature C at the drop altitude The default is the FMS value taken from the ADC at the current altitude corrected fo...

Page 273: ...nto account both the FMS predicted value at the actuation altitude and the entered ground wind If the actuation HAT has not yet been entered dashes are displayed Range 0 360 0 99 PI QNH 5R Altimeter s...

Page 274: ...on the LEGS page PREV A Custom CARP view B Custom HARP view 1R 2R 3R 4R 5R 6R RTE1 CARP PLAN 3 3 FTT VERT D IST 53 4S E C 1560F T EXIT TI ME FALL CO NST 45 0S E C 72 0S E C DECEL Q UO DEPL R ATE 8 4S...

Page 275: ...he sum of Exit time and Deceleration Quotient time When FTT is directly obtainable from ballistic table then a manual entry may be performed The value then appears in large font while fields DECEL QUO...

Page 276: ...s manually entered then dashes are displayed Range 0 99 9 Not displayed for Free Fall DEPL RATE 3R Displayed for CUST CARP and CUST HARP only Deployed rate of fall in feet second Sea level standard da...

Page 277: ...ayed The user may then correct the parameters press CANCEL or remove the procedure from the flight plan 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...

Page 278: ...the A C is beyond the CARP drop zone and prior to the Escape ESC waypoint ATK DISTANCE 2L Along Track Distance nm to the CRP green light or XTE or ESC waypoint along the path defined by the flight pl...

Page 279: ...point at which point the altitude derived from the Mission HAT is displayed Once the altitude used for the CRP waypoint calculations is frozen this frozen altitude value is then displayed until the CA...

Page 280: ...equired time of arrival PROGRESS RTA page may be used as an aid Less than 20 minutes to CRP or active waypoint is a CARP procedure waypoint CARP ACTIVE remote annunciator illuminates ACTIVE state disp...

Page 281: ...E and ESC waypoint positions are frozen Less than 5 seconds to CRP 5 SEC TO CARP advisory message displayed on the scratchpad AT CARP remote annunciator extinguishes AT CARP state displayed on the CAR...

Page 282: ...ssage CARP ALT NOT MET or CARP TAS NOT MET is raised The message is displayed until the error is removed NOTE At 10 seconds prior to reaching the CRP waypoint the TARGET TAS and ALTITUDE seen on the C...

Page 283: ...en the CRP Green Light and XTE Red Light waypoints and the cross track error is larger than half the drop zone width as was defined in the CARP PLAN 1 3 page CARP advisory messages and remote annuncia...

Page 284: ...2 Flight level entries shown numerical decreasing order on positions LSK 1L to 4L 3 Once confirmed a specific wind level entry can be deleted using the CLR key and then line selecting to the desired f...

Page 285: ...e 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 fly...

Page 286: ...appropriate REF ID field Typically the REF ID is the IP Identification Point waypoint when this optional waypoint has been defined as part of the CARP procedure 2 As the aircraft flies over or abeam...

Page 287: ...ay only be performed while the CARP waypoint positions are not frozen e g before 10 seconds to CRP To perform a manual CANCEL UPDATE the following steps must be taken 1 Press CANCEL UPDATE on the TMP...

Page 288: ...REF ID default is present position of aircraft The reference identifier REF ID can be set to any reference waypoint of the FMS Access to details on a specific beacon is achieve by pressing the associ...

Page 289: ...CS Last reception time or age of beacon signal the time age can be swapped by toggling LSK 2R Beacon s registration country Beacon s auxiliary radio location device Beacon s 15 hexadecimal identifier...

Page 290: ...GET POSITION status advisory scratchpad message The operator can then access the newly received position by going to the MISSION page When the ATOS and or RADAR is configured this page can viewed by s...

Page 291: ...is the crew s responsibility to ensure that the appropriate Target Position Radar or ATOS is selected time in inverse video white before creating a new user waypoint or accessing the DES SAR page Thus...

Page 292: ...cated at LSK 3R D This page is displayed when the flight plan transfer from the ATOS has been received successfully 1R 2R 3R 4R 5R 6R MISSION 1 1 RADAR T AR GET z ATOS TA RG ET z ATOS T RA NSFER ST AT...

Page 293: ...ination airports currently in the active route if any are defined or the FMS will create an origin airport named ORIG with the coordinates of the first mission data waypoint received from the ATOS and...

Page 294: ...the corresponding waypoint number used on the RADAR display For waypoints without identifier created by the FMS parenthesis e g are displayed to indicate that no identifier is defined For example when...

Page 295: ...tion only 12 10 POSITION UPDATE 12 12 DME NAVIGATION 12 16 DME STATION MONITOR 12 17 DME STATION DESELECTION 12 18 DME STATION RESELECTION 12 18 VOR DME OR VOR DME TACAN NAVIGATION MODE 12 19 VOR DME...

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Page 297: ...he position solution are checked for failure by a Receiver Autonomous Integrity Monitor RAIM It is understood that satellite failures are unannounced and can occur at any instant The RAIM continuously...

Page 298: ...acquired it will be tracked to an elevation angle of 0 above the horizon Typical time to first fix TTFF values are 55 seconds initialized and 120 seconds un initialized e g search the sky mode Satell...

Page 299: ...civil Litton LN 100GT EGI 1R 2R 3R 4R 5R 6R GPS STATUS 2 2 POS IT ION N45o 30 91 W073 o 3 8 02 TK GS VE R SPD 072 o 600K T 220F T M I N MS L ALT 120 00F T GPS H EI GHT 119 51F T UTC D ATE 1506 24Z JU...

Page 300: ...y degrades the EGI outputs in a progressive manner with more of the INS contribution in the solution In general the contribution of the INS drift when the geometry is not optimal it remains small and...

Page 301: ...S LSK 5R GPS LSK 1R mGPS LSK 2R A SAGEM SIGMA50H EGI installation B LITTON LN_100GT EGI installation 1R 2R 3R 4R 5R 6R GPS STATUS 1 2 POS IT ION N45o 34 25 W073 o 3 8 0 MODE HOR A CCURACY INIT 0 45N M...

Page 302: ...I installation 1R 2R 3R 4R 5R 6R GPS STATUS 2 2 KEY STA TU S FAIL C ODE KEY VER 0000 SA T TRK 5 GDOP P DOP 11 0 40 3 HOR DOP VE R DOP 2 1 1 0 RAIM HI L W IND 0 34N M 120T 15K T NAV STATUS 1L 2L 3L 4L...

Page 303: ...iled and blanks when data is not available 1R 2R 3R 4R 5R 6R GPS STATUS 2 2 KEY STA TU S FAIL C ODE KEY VER 0000 SAT VIS SA T TRK 8 5 GDOP P DOP 11 0 40 3 HOR DOP VE R DOP 2 1 1 0 EHE 20 M NAV STATUS...

Page 304: ...stallation B LITTON LN_100GT EGI installation 1R 2R 3R 4R 5R 6R INS GPS STATUS 2 2 HDG DA 060 0o L 01 5o PITCH R OL L D015 0o R1 0 5o AAIM HI L W IND 0 34N M 120T 15K T NAV STATUS 1L 2L 3L 4L 5L 6L 1R...

Page 305: ...0 to 50 1R 2R 3R 4R 5R 6R INS STATUS 1 1 POS IT ION N45o 34 25 W122 o 4 5 12 MODE ACC UR ACY NAVIGATI ON 2 50N M HDG DA TK GS 060 o L015 o 045 o 1 40K T PITCH R OL L ALT D015 0o R1 0 0o 50 00F T VERT...

Page 306: ...modes are unavailable or not adequate for the phase of flight For additional information refer to Section 1 The EGI INS DVS navigation mode is based on a hybrid solution based on INS position and DVS...

Page 307: ...h and Roll are displayed on page 2 2 1R 2R 3R 4R 5R 6R INS DVS STATUS 1 2 POS IT ION N45o 34 25 W122 o 4 5 12 MODE HOR ACC UR ACY HYB DVS SE L 0 50N M TK GS 045 o 228K T HYBRIDI ZA TION ON NAV STATUS...

Page 308: ...is accessed by pressing the MARK function key the MARK softkey from the PREDEF WPT and the UPDATE POS pages If configured or from the weather radar or AHCAS EFIS Joystick For additional information re...

Page 309: ...ds to the time when the joystick position was received The desired joystick position can be replaced by another known position by entering the position in the UPDATE POS field at LSK 2R directly from...

Page 310: ...ATE POS 1 1 REF FMS INS GPS ACCUR 0 0 7N M N45o 28 08 W073 o 4 4 48 A CCUR POS D IFF INS DVS 0 07 000 o 0 00 INS GPS 1 10 090 o 1 00 DVS 2 01 180 o 2 00 PREDEF WPT MARK 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5...

Page 311: ...lected 1R 2R 3R 4R 5R 6R UPDATE POS 1 1 REF BRG DI ST FMS INS DVS ACCUR 0 0 7N M N45o 28 08 W073o 44 48 A CCUR POS D IFF INS DVS 0 07 000 o 0 00 INS GPS 1 10 045 o 1 00 DVS 2 01 180 o 2 00 CANCEL CONF...

Page 312: ...r a DME station is lost or acquired the FMS system may sense a position change This situation is similar to when the FMS switches between navigation modes GPS DME DME VOR DME inertial DR etc when the...

Page 313: ...for DME navigation the frequencies tuned and the slant range distances Associated with each station is a status that indicates the following REJ station not used in determining a position fix rejecte...

Page 314: ...to view all DME stations deselected Insertion of more than 5 stations is achieved by moving a station entered in the scratchpad to any of the line select key locations 1 through 5 2 Key the DME stati...

Page 315: ...ed to the autopilot this newly sensed cross track error causes lateral steering command and an aircraft heading change as the FMS autopilot attempts to intercept and capture the recalculated desired t...

Page 316: ...corresponding navigation mode will be given the lowest priority 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...

Page 317: ...Display the DVS STATUS 1 2 page via the NAV STATUS INDEX 1 2 page 2 The velocity in each of the three axes the DVS operational mode the beam and surface status are displayed 3 The RF mode in effect i...

Page 318: ...medium font and manual entries are not permitted When the scratchpad is empty and A C is outside the polar region latitude between N73 and S60 pressing LSK 1L will toggle between the True and Magneti...

Page 319: ...ontinuous navigation whenever the GPS is not available The GPS receiver has bounded but noisy positioning and velocity errors and the GPS navigation solution is subject to the availability of the GPS...

Page 320: ...the AHRS quality worse the AHRS quality the quicker the INS navigator will diverge from the true GPS position Also the GPS receiver will calibrate the INS emulator to the GPS accuracy The KALMAN Filte...

Page 321: ...ation mode and the ANP is within the phase of flight limit each FMS calculates a bias vector between its system position and the mixed inertial position When the inertial navigation mode becomes activ...

Page 322: ...34 25 W122 o 4 5 12 MODE NAV HDG DA TK GS 060 o R99 o 045 o 1 40K T PITCH R OL L ALT D15o R 10 o 5000FT VERT SP D 175 FT MIN START TEST NAV STATUS ACCURACY 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R POS INI...

Page 323: ...IRS POSITION field of the POS INIT page Upon pilot entry of latitude and longitude the FMS initializes its onside IRS and cross talks the initialization data to the other FMS s On receipt of the init...

Page 324: ...nd LASEREF_V 1R 2R 3R 4R 5R 6R IRS1 STATUS 1 1 POS IT ION N45o 34 25 W122 o 4 5 12 MODE PGM N UM BER NAV 92 0 4 13 HDG DA TK GS 060 o L15 o 045 o 1 40K T PITCH R OL L ALT D15o R 10 o 5000F T VERT SP D...

Page 325: ...speed information used by the FMS will be taken from the nearest IRS The other inertial sensor s will be automatically rejected If the selected nearest inertial sensor fails the system will select the...

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Page 327: ...IOS RS 422 FM1 RADIO 13 33 COMMUNICATION RADIOS RS 422 FM2 RADIO 13 34 COMMUNICATION RADIOS RS 422 UHF RADIO 13 35 COMMUNICATION RADIOS VUHF RADIO 13 36 COMMUNICATION RADIOS VUF RADIO Page 1 3 for SRT...

Page 328: ...1 13 70 PHONE STORED SMS 1 1 13 71 PHONE STORED SMS 1 N 13 72 PHONE DIALED TOP 1 N 13 73 COM LIBRARY 1 N 13 74 NAV LIBRARY 1 N 13 76 ADF LIBRARY 1 N 13 77 RS 422 FM1 FM2 LIBRARY 1 N 13 78 RS 422 UHF...

Page 329: ...active and standby frequency entry control of all radio modes including self test and a pilot entered library In certain installation architectures supporting multiple FMSs the crew should attempt to...

Page 330: ...ault cold start power up page of the CMA 9000 FMS The RADIO 1 X page is displayed by pressing RADIO The CMA 9000 FMS provides alert mechanisms to inform the pilot of radio failures Alerts messages are...

Page 331: ...scratchpad if invalid entries are made by the user In some installations the tuning can be achieved either from the FMS or from a backup controller If the radio tuning is disabled from the FMS entrie...

Page 332: ...LOWER LIMIT UPPER LIMIT INCREMENT TRANSPONDER 0 octal 7777 octal 1 COM 118 000 MHz 135 975 MHz 136 975 MHz 151 975 MHz see Note 1 25 kHz see Note 3 COM 118 000 MHz 136 975 MHz 151 990 MHz see Note 1...

Page 333: ...3 The COM radio frequencies with increments of 25 kHz 4 The upper limit of the COM radio frequencies with increments of 8 33 kHz 5 Certain frequencies in the maritime band 156 000 173 975 can also be...

Page 334: ...R RADIO 1 4 0 4 05 VHF1 118 400 125 150 VHF2 151 000 124 650 Y JN A NAV1 115 80 116 70 Y UL YQB NAV2 116 30 112 80 SBY ATC1 2200 1500 CTL C1 C2 IC N 1 N2 VOL FMS 7 6 4 3 3 1L 2L 3L 4L 5L 6L 1R 2R 3R 4...

Page 335: ...s in the scratchpad If the scratchpad is empty it toggles active standby frequencies VHF2 2R Display and modify the VHF active and standby frequencies presets Entry may be made to the standby position...

Page 336: ...s to the Volume Control page when the FMS has control of the AMU VOL 6R Provides information as to which equipment FMS MC has control over the AMU and displays the specific radio volume level NOTE The...

Page 337: ...1L 2L 3L 4L 5L 6L RADIO 2 4 04 05 VUF1 243 000 121 500 16 06 VUF2 156 800 156 300 01 ADF1 407 0 343 5 07 08 ADF2 333 0 222 5 HF 12000 0 6844 5 SDETECT ED DF SCAN 145 875 1R 2R 3R 4R 5R 6R 1L 2L 3L 4L...

Page 338: ...n 1R 2R 3R 4R 5R 6R 1L 2L 3L 4L 5L 6L RADIO 2 4 C01 M SHIP DF C05 VUHF 156 050 156 250 OFF DF SCAN 145 875 01 ADF1 407 0 343 5 07 08 ADF2 333 0 222 5 HF FMS NOT IN CT RL 1R 2R 3R 4R 5R 6R 1L 2L 3L 4L...

Page 339: ...verse white video indicates guard frequency is being tuned M CST normal white video indicates maritime coast is active M SHIP normal white video indicates maritime ship is active DF normal white video...

Page 340: ...e stand by active frequency channel and vice versa when the scratchpad is empty The CMA 9000 FMS allows the user to select a frequency by entering one of the following elements in the scratchpad and p...

Page 341: ...mmunication radios the following applies A frequency or channel can be selected by entering the desired value in the scratchpad and pressing the associated line select key These radios do not provide...

Page 342: ...PAGE Type COM NAV ATC ADF VUHF Only SRT 651 N A V UHF radio variant can be configured in vertical radio page layout NOTE XX below is based on the configured position of each radio It can be anything b...

Page 343: ...ad is empty it toggles between active standby idents Also displays the Transponder mode C Altitude mode on blank Altitude mode off below the fixed caption ATC field When the SQK IDT key is pressed the...

Page 344: ...he FM1 page if configured PHONE TOP 6L Access to the PHONE TOP 1 1 page if PHONE or HCS is configured COM2 XX Access to the COM page if configured NAV2 XX Access to the NAV page if configured ADF1 XX...

Page 345: ...red to Yes in the Display Config maintenance page NOTE The page number is based on the number of RADIO top page s Unless accessed for the first time the page may display the results of radio test prev...

Page 346: ...dingly Individual radio library and self test functions are then accessible from the specific radio equipment Hence the RADIO page s numbering X Y will vary depending on the number of radios installed...

Page 347: ...Y The RADIO PWR page provides the capability of controlling specific radio power state or all radio power states at once Display and access to the RADIO PWR page will only be available when at least o...

Page 348: ...NAVIGATION RADIOS NAV DME RADIO NOTE NAV Radio equipment name can be configured as NAV VOR or VIR The FMS will support the following NAV and DME Radios in the frequency range and channel spacing spec...

Page 349: ...is prompt the text AUTO or MAN as a function of what has been configured to highlight whether or not the VOR auto tuning mode is activated or not Toggling between auto tuning and manual tuning can be...

Page 350: ...s is as described for RADIO 1 N page The standby frequencies are entered as stated for the RADIO 1 N page However the display is always large white font since there is no tuning done on the standby fr...

Page 351: ...page where the NAV radio is located NAVIGATION RADIOS ADF RADIO The FMS will support the following ADF Radios in the frequency range and channel spacing specified below RADIO MODEL FREQUENCY RANGE CHA...

Page 352: ...mber and frequency of the ADF2 radio Selecting LSK_1R when the scratchpad is empty will toggle the standby and the active preset frequency MODE 3L 3R Displays mode status for the ADF radio Pressing th...

Page 353: ...XT or RADIO RADIO ADF NEXT NOTE The ADF ident suffix x e g ADF ADF1 and the side left or right where the ADF units appear are depending on the installation configuration ADF1 TEST 5L Toggles ADF1 test...

Page 354: ...SARSAT N A Figure 13 2 DF 1 DF Frequency Range and Channel Spacing NOTE The FMS generates a warning message in the scratchpad whenever the user enters out of range values or invalid data NOTE For COS...

Page 355: ...tected C S data is available and displayed LOCK C S prompt is displayed since multiple beacons are detected SCAN is displayed in the active frequency field Frequency toggle prompt is not displayed in...

Page 356: ...and 243MHz beacons detected C S data is available and displayed UNLOCK C S prompt is displayed since the DF is currently synchronized with one of the C S beacons SCAN is displayed in the active frequ...

Page 357: ...e and sub mode the following is displayed In any DF sub mode the modulation and AGC Automatic Gain Control values of the beacon defined by the user s tactical frequency if available or In SAR SCAN mod...

Page 358: ...ow RADIO MODELS CHANNEL RANGE CHANNEL SPACING NOTE VC 401B VC 401C VHF 422 VHF 4000 118 000 to 135 975 118 000 to 136 975 118 000 to 151 975 118 000 to 136 990 118 000 to 151 990 25 MHz 25 MHz 25 MHz...

Page 359: ...XT VHF or RADIO RADIO DETAILS VHF or RADIO RADIO VHF NOTE The COM VHF radio equipment name can also be configured as COM or VHF The VHF ident suffix x e g VHF VHF1 and the side left or right where the...

Page 360: ...NEXT or RADIO NEXT VHF NEXT or RADIO RADIO VHF NEXT Display the second VHF 2 2 page from the vertical configuration by pressing RADIO NEXT VHF NEXT or RADIO RADIO DETAILS VHF NEXT or RADIO RADIO VHF N...

Page 361: ...softkey selects the next option The possible values are ON and OFF MODE STATUS 5L Displays FUG8 mode status The possible values are OK PARAM ERROR H W ERROR PWR OFF and CH UNSLECTBL RADIO 6L Access t...

Page 362: ...Y SQUELCH 4L Displays squelch status for the FUG9 radio Pressing this softkey selects the next option The possible values are ON and OFF MODE STATUS 5L Displays FUG9 mode status The possible values ar...

Page 363: ...gle the standby and active frequencies GUARD 3L Displays guard receiver status for the UHF radio Pressing this softkey selects the next option The possible values are ON and OFF SQUELCH 4L Displays sq...

Page 364: ...5 UHF FM 243 000 4 Figure 13 4 VUHF Radio Model Frequency Channel Range Channel Spacing Band Modulation and Emergency Guard Band Frequency NOTE 1 The Channel Range and spacing are configurable items I...

Page 365: ...50 156 450 69 156 475 156 475 10 156 500 156 500 70 156 525 156 525 11 156 550 156 550 71 156 575 156 575 12 156 600 156 600 72 156 625 156 625 13 156 650 156 650 73 156 675 156 675 14 156 700 156 700...

Page 366: ...ge from the horizontal configuration by pressing RADIO VUF or RADIO NEXT VUF or RADIO RADIO VUF Display the first VUF 1 3 page from the vertical configuration by pressing RADIO NEXT VUF or RADIO RADIO...

Page 367: ...re present in the standby field At that time a frequency channel needs to be entered in the standby field first before the active standby field toggling is allowed otherwise a warning message will be...

Page 368: ...default VUF power level is displayed in small font white color SQUELCH 2L 2R Display squelch status for the VUHF radio The possible values are OFF and ON PTT 3L 3R Enable the PTT switch The status fie...

Page 369: ...ntrol current guard antenna selection status 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 g...

Page 370: ...ported by the radio otherwise the field is blanked CBIT is displayed in small font green color and CBIT error codes is displayed in small font white color for the left and right side respectively The...

Page 371: ...TYPE is set to SHIP on VUHF page 2 3 NOTE for the maritime mode MAR TYPE on VUHF 2 3 and consequently on VUHF 1 3 will automatically be set as function of the entered maritime band frequency 1R 2R 3R...

Page 372: ...xt to the text at LSK 1L 1R as well on the corresponding V UHF radio s line on the top RADIO page e g RADIO 1 X or 2 X Also once this prompt is activated the prompt itself is removed from view until t...

Page 373: ...m the horizontal configuration by pressing RADIO VUHF NEXT when the VUHF radio is installed on the first RADIO top page or RADIO NEXT VUHF NEXT when the VUHF radio is installed on the second RADIO top...

Page 374: ...rol the operation of the SRT 651 N F VUHF radio Display the first VUHF 3 3 page from the horizontal configuration by pressing RADIO VUHF NEXT NEXT when the VUHF radio is installed on the first RADIO t...

Page 375: ...d if failures occur and are reported by the radio otherwise the field is blanked M CODE is displayed in small font green color and M CODE error codes is displayed in small font white color for the lef...

Page 376: ...6L Access to the RADIO top level page where the HF radio is located LIBRARY 6R Access the HF LIBRARY 1 N page COMMUNICATION RADIOS HF RADIO Page 2 2 This page allows the pilot to control the operation...

Page 377: ...RADIO 1 2 page from the horizontal configuration by pressing RADIO ATC or RADIO NEXT ATC or RADIO RADIO ATC or ATC TPDR or XPDR Display the first ATC RADIO 1 2 page from the vertical configuration by...

Page 378: ...yed in the scratchpad MODE C 3L Toggles ATC1 SSR Mode C functions for the ATC radio The possible values are ON and OFF MODE C 3R Same as above but referencing ATC2 instead of ATC1 NOTE New code and se...

Page 379: ...C equipment name can also be configured as TPDR or XPDR The ATC ident suffix x e g ATC ATC1 and the side left or right where the ATC units appear is depending on the installation configuration ATC1 TE...

Page 380: ...is not successful the code is displayed in small font amber color as a warning to the pilot If the transponder IDENT mode is active the code is displayed in large font inverse green color New code and...

Page 381: ...s EMERGENCY 5R Used to set or unset the EMERGENCY transmission the possible values are ON and OFF Setting this field to ON allows the crew to set the IFF master mode to ACTIVE Only for CIVIL emergency...

Page 382: ...tuning operation is not successful the code is displayed in small font amber color to indicate a tuning failure Any 8 digit octal mode S address can be entered Valid range for 8 digit code 00000000 7...

Page 383: ...essful the volume level is displayed in small font amber color as a warning to the pilot Furthermore the FMS will provide warnings if the AMU or radios fail or are not responding to the tuning request...

Page 384: ...VOICE CALL 1L Access to PHONE VOICE CALL page READ SMS 1R Access to PHONE READ SMS page DIALED 2L Access to PHONE DIALED TOP page SEND SMS 2R Access to PHONE SEND SMS page PRE CANNED SMS 3R Access to...

Page 385: ...ered the priority is given to the name e g only the name is considered and number is ignored NOTE When a phone number or name phone number exceed 24 characters this LSK is also used to return to the d...

Page 386: ...ill transmit a DIAL command to the phone transceiver using the displayed phone number When CALL is selected the page PHONE VOICE CALL 2 2 is automatically displayed For the Iridium phone This prompt i...

Page 387: ...NNECTION ERROR and GSM FAULT Display is blank if no voice call command has been initiated in the last 10 seconds For the Iridium phone the possible values are when communication is totally lost with t...

Page 388: ...green large font for 2 seconds For the Iridium phone This prompt is displayed only when there is a received call otherwise it is blank For the GSM phone in S W 300 This prompt is displayed only when...

Page 389: ...older ones read and unread are automatically deleted New messages appear in white large font until they are read Messages that have already been opened are displayed in small blue font Display PHONE...

Page 390: ...one in S W 300 Pressing this softkey will transfer the content of the scratchpad to this field If the scratchpad contains a phone number then only the phone number will appear If the scratchpad contai...

Page 391: ...e copy a text line 6 lines of text are displayed at a time The pilot can use NEXT and PREV to move the cursor up and down to scroll through the entire text message An auto wrap feature will break line...

Page 392: ...ode the scratchpad text is inserted on this line and the text below this line is pushed down one line 1R 3R When operating in EDIT mode and when the message text contains more than 6 lines up and down...

Page 393: ...sor is at the end of a line or the LEFT key 5L when the cursor is at the beginning of a line will cause the cursor to automatically wrap around to the next or previous line This entire field disappear...

Page 394: ...to PHONE top page This prompt is only available in READY TO TX mode CLEAR TXT 6R When operating in EDIT mode pressing this key clears the entire text message This prompt is only available when the me...

Page 395: ...transmission starts and remains blank if SMS transmitted properly The code is a 3 digit value received from the Iridium phone PHONE STATUS 3L Displays the phone status For the GSM phone the possible...

Page 396: ...tem the template location 1L 6R and an expanded text message template When the pre canned message contains additional template text the menu selection is shown with a large white font rather than a sm...

Page 397: ...y sent e g MISSION 1 is sent as the SMS text message This implies that the pre canned SMS text message is not loaded to the SEND SMS page under these circumstances When a pre canned message containing...

Page 398: ...ng a voice call message has higher priority or Pressing the ANSWER discrete input if discrete input configured NOTE The PHONE can only be configured in the vertical configuration option of the RADIO t...

Page 399: ...tored SMS text messages The maximum number of stored SMS text message is 10 Display PHONE STORED SMS 1 1 page by pressing RADIO PHONE STORED SMS When the PHONE or HCS is configured NOTE The PHONE can...

Page 400: ...s configured SMSx NOTE The PHONE can only be configured in the vertical configuration option of the RADIO top page This page is displayed as follows once the SMS text message has been selected This pa...

Page 401: ...if available phone number of called person type of transmission CALL or SMS date time The time of transmission is of the format selected on the CONFIG DISPLAY DATE selection For example ddmmmyy hhmm s...

Page 402: ...he slash symbol and press any of the line select keys that are associated with a library record LSK 1L LSK 2L LSK 3L LSK 4L or LSK 5L The new record will be added to the library The library will also...

Page 403: ...ot be displayed on the radio page field even though it was displayed in the scratchpad If COM1 is configured ACT1 2R Display active preset number modify active preset number and frequency of the COM1...

Page 404: ...er modify active preset number of the NAV1 radio SBY1 3R Display standby preset number modify standby preset number and frequency of the NAV1 radio If NAV2 is configured ACT2 4R Display active preset...

Page 405: ...number modify active preset number and frequency of the ADF1 radio SBY1 3R Display standby preset number modify standby preset number and frequency of the ADF1 radio If ADF2 is configured ACT2 4R Dis...

Page 406: ...t numbers 1L 2L 3L 4L 5L Preset identifier and frequency entries in the library Refer to text at the start of this section ACT 2R Display active preset number modify active preset number and Channel o...

Page 407: ...the start of this section ACT 2R Display active preset number modify active preset number and frequency of the UHF radio and access UHF RADIO page SBY 3R Display standby preset number modify standby...

Page 408: ...es is 99 The maximum number of VUHF LIBRARY pages is 20 The NEXT and PREV keys are used to scroll forward or backward in the preset numbers For the SRT 651 N F radio while in MAR SHIP or MAR COAST mod...

Page 409: ...he SRT 651 N A radio the maritime channel number is displayed in the form MXX where XX the maritime channel number when entering a valid library preset number the entry will be interpreted as a mariti...

Page 410: ...me should then be pressed to store the phone number If the phone number is longer than 24 characters then extra digits can be added using the characters Any digit after the characters will be appended...

Page 411: ...s replaced with the symbol The phone number is a maximum of 30 characters VOICE CALL 6L Access to the PHONE VOICE CALL 1 2 page The selected name number will be inserted on the VOICE CALL 1 2 page SEN...

Page 412: ...ill display the LIBRARY prompt only while the aircraft is on the ground e g field is blank while the aircraft is airborne When the prompt is present pressing the line select key will provide access to...

Page 413: ...while the aircraft is on the ground e g field is blank while the aircraft is airborne When the prompt is present pressing the line select key will provide access to the RADIO LIBRARY top level page NO...

Page 414: ...TOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 13 86 Revision 2 March 01 2010 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for refe...

Page 415: ...OINT 14 5 SIMULATION FUNCTIONS 14 5 A SIMUL FLY AWAY FUNCTION 14 6 B SIMUL OEI CRUISE FUNCTION 14 6 C SIMUL RTEx FUNCTION 14 6 SIMUL FLY AWAY 1 3 If SIMUL PG option Configured 14 7 SIMUL OEI CRUISE 2...

Page 416: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 14 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for referenc...

Page 417: ...of the Fuel page 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...

Page 418: ...t or estimated fuel weight excluding the reserve and fuel flow CAUTION On power interruptions the fuel units will revert to the configured units from maintenance page Verify units when reading or ente...

Page 419: ...aircraft empty weight e g 5000 and move it into the EMPTY WT field by pressing LSK 1R 7 Key in the optional equipment weight e g 700 and move it into the EQUIP WT field by pressing LSK 2R 8 Key in th...

Page 420: ...UEL 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 The inactive fuel route page is displayed in monochrome cyan...

Page 421: ...n to the destination airport coordinates excluding the missed approach procedure is not sufficient SIMULATION FUNCTIONS The CMA 9000 FMS provides Fly Away and OEI Cruise simulation functions which all...

Page 422: ...values received from other aircraft sub systems the current gross weight present baro corrected altitude and present outside air temperature Then it computes the jettison weight weight to lose in ord...

Page 423: ...e e g 25 and move it to the OAT field by pressing LSK 4L 5 Key in the wind speed e g 45 and move it to the WIND field by pressing LSK 5L SIMUL OEI CRUISE 2 3 If SIMUL PG option Configured Display SIMU...

Page 424: ...to perform simulated ETA EFA computations If an inactive route already exists the CMA 9000 FMS allows the pilot to copy the active route into the inactive route in order to perform simulated ETA EFA c...

Page 425: ...ION MODE 15 2 A ACCURACY 15 2 B INTEGRITY 15 2 C CONTINUITY 15 2 DME DME NAVIGATION MODE 15 3 A ACCURACY 15 3 B INTEGRITY 15 3 C CONTINUITY 15 3 VOR DME NAVIGATION MODE 15 3 A ACCURACY 15 3 B INTEGRIT...

Page 426: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 15 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for referenc...

Page 427: ...radial error of the estimated aircraft position The CMA 9000 FMS monitors the position estimation error and generates an alert when the ANP exceeds the current RNP In GPS navigation mode the FMS monit...

Page 428: ...requirements of AC20 130A A typical 95 probable position estimation radial error is 0 04 nm B INTEGRITY GPS based position integrity is the GPS HIL computed by the Receiver Autonomous Integrity Monito...

Page 429: ...ansceiver the CMA 9000 FMS meets the 10 4 per flight hour continuity requirement VOR DME NAVIGATION MODE The assumptions used to support the accuracy requirements are A minimum of one VOR and one DME...

Page 430: ...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 naviga...

Page 431: ...EM Page 16 i November 19 2009 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 respo...

Page 432: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 16 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for referenc...

Page 433: ...assigned ESS The MCDU MENU page displays all configured external sub systems and the internal FMS Display MCDU MENU X X page by pressing MENU The sub systems displayed have a dedicated key The interna...

Page 434: ...on the student FMS The trainer s FMS internal system is not affected by the entry An alpha numerical value entered in the scratchpad on any FMS is appended to the scratchpad data that is already being...

Page 435: ...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 17 4 NAVIGATION IN...

Page 436: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page 17 ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for referenc...

Page 437: ...craft is airborne will require pilot action to re select the active CMA 9000 FMS page and 1 Enter a valid TO waypoint on the RTE x LEGS 1 X page 2 Verify position and flight plan update if necessary 3...

Page 438: ...ay the DESELECT page by pressing INIT REF NAV STATUS LSK 5R and DESELECT LSK 6R Single GPS installed Dual GPS installed 1R 2R 3R 4R 5R 6R DESELECT 1 1 TAS GPS VALID VALID HDG DME VALID VALID DVS VOR D...

Page 439: ...LID or ACQ appears in the equipment s field TAS INPUT DESELECTION OPTIONAL If the TAS input is observed to be intermittent or unreliable this input should be manually deselected to prevent the possibi...

Page 440: ...tude aiding is required to achieve the level of integrity to conduct a GPS instrument approach With a good satellite constellation no altitude aiding may in fact be necessary Therefore the loss of the...

Page 441: ...is particularly necessary during periods of changing winds since the CMA 9000 FMS providing navigation data assumes constant wind during DR operation In an installation where digital True Airspeed TA...

Page 442: ...red 1 Prior to reaching a known reference position get this known reference position coordinates to the scratchpad by following one of these three methods If the known point is a flight plan waypoint...

Page 443: ...ONAV_A702 DMAP is configured A 40 VHF NAV DESELECT 1 X if DME interface is configured A 42 DME STATUS 1 1 if DME DME interface is configured A 43 DVS STATUS 1 2 Only if DOPPLER is configured A 44 DVS...

Page 444: ...is configured A 98 NAV STATUS INDEX 1 1 A 100 NEAREST 1 1 A 102 NEAREST AIRPORT 1 X A 103 NEAREST VHF NAV 1 X also applicable for NEAREST NDB CUSTOM WPT and USER WPT A 104 PARALLAX ADJUST 1 1 A 105 PL...

Page 445: ...d A 195 TACTICAL X Y page if configured A 197 TACTICAL APPR 1 3 page if configured A 201 TACTICAL APPR 2 3 page if configured A 206 TACTICAL APPR 3 3 page if configured A 210 TIMER 1 1 page if TIMER P...

Page 446: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page A iv November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 447: ...tactical approach approach transition or runway are displayed Access the ARRIVALS page either from DEP ARR INDEX 1 1 page press ARR or press DEP ARR if airborne and past midway point of active route A...

Page 448: ...er 1R 2R 3R 4R 5R 6R PANC ARRIVALS 1 1 STARS R TE 1 APPRO AC HES AMOTT5 ACT ACT VORD06R TRANS TR ANS ODK ACT ACT ANC DEP ARR ROUTE 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R PANC ARRIVALS 1 1 STARS R TE 2 AP...

Page 449: ...desired approach removes all other approaches runways and non applicable STARS and displays a listing of applicable approach transitions Deletion of the selected active approach cancels any approach...

Page 450: ...and part of the active route C When the Bulls Eye Target rendezvous is unachievable 1R 2R 3R 4R 5R 6R BULLS EYE 1 3 PPOS REF FR TGT POS ETA DELT A ALT F T EFIS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R BUL...

Page 451: ...he ident BERDV is displayed otherwise UNACHIEVABLE is displayed in inverse video white When the Bulls Eye Target is not defined or is a fixed waypoint the field is blank RDV POS BRG DIS 4L 4R Displays...

Page 452: ...The BULLS EYE 2 3 page allows selection or creation of the Bulls Eye Target waypoint It may be created as a moving waypoint when the configuration option is selected When the Bulls Eye Target waypoin...

Page 453: ...M REF WPT P OS o o CANCEL SAVE CONFIRM 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R BULLS EYE 2 3 BETGT TGT ID POS N43 26 20 E004 52 32 BRG DIS 015T 270N M TYPE MS L ALT FIXED F T REF WPT I D RA D DIS BULL 00...

Page 454: ...in reverse white video when the Bulls Eye Target waypoint is present in the active route Only modification to a manually defined Bulls Eye Target is allowed in this state BRG DIS 2L Bearing and dista...

Page 455: ...ously a symbol preceding a value in the scratchpad indicates only the DIS value must be updated The minimum maximum values for the radial are 0 360 degrees and 0 999 NM for the distance REF WPT POS 5L...

Page 456: ...ng created or modified and all mandatory fields are entered CANCEL CONFIRM prompts will appear Leaving the BULLS EYE 3 3 page without confirmation will automatically perform a CANCEL A The page displa...

Page 457: ...F WPT I D RA D DIS o N M REF WPT P OS o o CANCEL SAVE CONFIRM 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R BULLS EYE 3 3 BUL01 BUL L ID POS N43 26 20 E004 52 32 BRG DIS 015T 270N M REF WPT I D RA D DIS o N M R...

Page 458: ...POS field the RAD DIS and the BULL ID will be reset to their default values and the POS and BRG DIS fields will be automatically updated Entering a moving waypoint as a reference will use the moving...

Page 459: ...e active or inactive route A ACTive status and sample inputs Custom CARP B ACTive status and sample inputs Custom HARP 1R 2R 3R 4R 5R 6R ACT RTE1 CARP PLAN 1 3 TYPE CUST CARP CDFB IDE NT POINT IP N45o...

Page 460: ...stance wptidBRG DIS e g WPT07012 112 If an IP position is entered in LSK 2R then a temporary waypoint is automatically created and the identifier WPTXX is displayed in 2L Otherwise a database waypoint...

Page 461: ...O DROP TIME 5L In case of Custom HAHO Time in seconds needed to perform all the intended drops Used to compute the best solution Default is dashes range 1 999 ESC TIME 5R Desired elapsed time s after...

Page 462: ...LEGS page NEXT A Custom CARP view B Custom HARP view 1R 2R 3R 4R 5R 6R RTE1 CARP PLAN 2 3 PI ELEV SD D IST 5000F T 3 1N M IAS HAT DROP T EMP 156K T 1560F T 20 0o C WIND MEAN WIND G RO UND 020T 45K T 0...

Page 463: ...play and entry of Slowdown Distance nm defined as the distance from the Slowdown point SD to the CARP green light waypoint CRP The default is the FMS computed value If insufficient CARP parameters are...

Page 464: ...ind is entered GROUND WND then the displayed value is modified to take into account both the FMS predicted value at the drop altitude and the entered ground wind Range 0 360 0 99 Not displayed for CUS...

Page 465: ...meters press CANCEL or remove the procedure from the flight plan NOTES Entering DELETE on any field causes it to resume its default value Pressing the RESET key on the CARP PLAN 3 3 page resets all pa...

Page 466: ...E C DECEL T IM E HV R ATE 3 4S E C 156 6F T S E C DECEL D IS T 380F T RESET CARP PROGRESS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R RTE1 CARP PLAN 3 3 FTT 53 4S E C EXIT TI ME 45 0S E C DECEL Q UO 8 4S E C...

Page 467: ...he exit of the first element from the airplane Value may be extracted from parachute ballistic data tables The default value is dashes If a value is entered for DECEL QUO then the default display is b...

Page 468: ...aying the MOD status If by pressing ERASE the CARP procedure is removed from the flight plan then the LEGS page is automatically displayed CANCEL 6L Cancel the changes made to the inactive route CONFI...

Page 469: ...The CARP mode is active and the A C is within the CARP drop zone This state begins 0 5 seconds before arriving at the CRP waypoint green light ESCAPE The CARP mode is active and the A C is beyond the...

Page 470: ...RGET ALT 4R Target altitude feet Only displayed after crossing the Slow Down SD waypoint or less than 60 seconds remain to the CRP waypoint at which point the altitude derived from the Mission HAT is...

Page 471: ...s the central clear when requested on the INIT REF 2 2 page Pressing this prompt also returns to the INIT REF 2 2 page COMM STATUS 1 1 Display COMM STATUS 1 1 page by pressing MENU COMM one MCDU page...

Page 472: ...stems MCDU MENU 6L Returns to MCDU MENU X X page DATA LOAD 1 1 if aircraft is on ground Display DATA LOAD 1 1 page by pressing INIT REF NEXT DATA LOAD A With ARINC 615 DLU initial display NOTE If the...

Page 473: ...3R 4R 5R 6R DATA LOAD 1 1 TYPE RADIO DATA STATUS LOADING FI LE 001 4K B ABORT 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R DATA LOAD 1 1 TYPE CONFIG 0 STATUS IDLE 000 0K B LOAD SAVE 1L 2L 3L 4L 5L 6L 1R 2R 3R...

Page 474: ...ctical 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...

Page 475: ...ay point of active route not reached yet or From ARRIVALS 1 1 page or From DEPARTURES 1 1 A Active DEP ARR Index B DEP ARR Index during a MOD in active RTE2 1R 2R 3R 4R 5R 6R DEP ARR INDEX 1 1 AC T RT...

Page 476: ...TORE 6L Displayed only if the RTE was erased on the RTE 1 X page Used to restore the active route CANCEL 6L If ERASE MODS is configured as CONFIRM Cancel the changes made to the inactive route ARR 1R...

Page 477: ...the corresponding DEP prompt on the DEP ARR INDEX 1 1 page or DEP ARR if on ground and route active A Initial Display B Display after SIDS selected and runway selected 1R 2R 3R 4R 5R 6R KBFI DEPARTUR...

Page 478: ...5R 6R KBFI DEPARTURES 1 1 SIDS R TE 1 RU NW AYS LACRES ACT ACT 13R TRANS VAMPS ACT DEP ARR ROUTE 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R KBFI DEPARTURES 1 1 SIDS R TE 2 RU NW AYS LACRES SEL SEL 13R TRANS...

Page 479: ...RR 6L Returns to the DEP ARR INDEX 1 1 page unless a route modification is in progress ERASE 6L Cancel any route modifications and or any departure selections If confirm and erase route modifications...

Page 480: ...ctive route is not being modified 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 waypoin...

Page 481: ...try anywhere in the flight plan SECTOR 5L Appears when configured The status ACT reverse video white is appended to the prompt if an activated sector search pattern is in the flight plan SAR waypoint...

Page 482: ...B DES SAR and NEXT or INIT REF NEAREST USER WPTS DES SAR and NEXT or INIT REF NEAREST CUSTOM WPTS DES SAR and NEXT or INIT REF DES SAR and NEXT or INIT REF WPT LISTS DMAP WPT DES SAR and NEXT or INIT...

Page 483: ...ion on the CONFIG page is configured If no SAR waypoint is entered in the field REF ID of the DES SAR page and no previously defined tactical approach Runway Threshold Waypoint then display default LE...

Page 484: ...AS GPS FAIL VALID HDG DME VALID DESEL DVS VOR DM E TCN ACQ ACQ K AL MAN ACQ NAV STATUS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R DESELECT 1 1 TAS GPS FAIL VALID HDG DME VALID DESEL DVS VOR D ME TCN ACQ ACQ...

Page 485: ...f single GPS is configured then when selected it toggles between VALID DESEL or ACQ DESEL options to control usage of the GPS in the navigation solution If dual GPS is configured it acts as a prompt w...

Page 486: ...text in green INIT REF 6L Returns to INIT REF 1 2 page DMAP WPT 1 X if ELBIT EURONAV or EURONAV_A702 DMAP is configured Display DMAP WPT 1 X page by pressing INIT REF WPT LISTS and DMAP WPT The DMAP...

Page 487: ...chpad selection of this line key will open the USER WPT 1 2 page with the coordinates and the DMAP waypoint identifier entered for the definition of a new user waypoint The operator has to simply ente...

Page 488: ...he corresponding softkey Up to 25 stations can be added to the deselection list A new page is automatically added when it is needed TYPE 1L 2L 3L 4L 5L Displays VHF navaid type in the third column The...

Page 489: ...er DME IDENTIFIER in the first column STAT 1L 2L 3L Tuning STATUS in the second column REJ DME station is not used in determining position due to bad geometry N A Station not responding to tuning FREQ...

Page 490: ...NIT REF NAV STATUS and DVS The DVS STATUS 1 1 page displays velocity measurements and the status of the Doppler Velocity Sensor A RDN 85 DVS displayed in Normal Video B RDN 85 DVS displayed in Reverse...

Page 491: ...MEMORY mode For all other modes the display is in normal video NOTE When the DVS status is FAILED or the DVS mode is PREPOSITIONING INS or SPEED NOT COMPUTED for the RDN 85 DVS the velocities will be...

Page 492: ...ceived from the DVS the status is displayed in medium font STATUS 5L Displays the Surface status sent by the ANV 353 DVS Possible values for this field are SEA LAND This field is displayed only when a...

Page 493: ...or MAG following the TRUE MAG discrete with a range of 0 to 359 degrees Default value on cold start is 0 degree and 0 knot NAV STATUS 6L Access to NAV STATUS INDEX 1 1 page EFIS 1 X if EFIS interface...

Page 494: ...the communication with the selected external sub system is failed Display ESS FAILURE 1 1 page by pressing MENU COMM and ESSx TITLE The title shows the external sub system selected from the COMM page...

Page 495: ...al line Distances are displayed on EHSI as a circle around the fix ABEAM 5L Initially the ABEAM prompt is displayed Line selecting ABEAM displays radial distance distance to go and ETA at the abeam in...

Page 496: ...owing take off INIT REF 6L Returns to INIT REF INDEX 2 2 page LANDING 1R Display the last landing zulu time hours and minutes when the aircraft is on the ground When the aircraft is airborne blanks ar...

Page 497: ...ground or 3 manually entered values for FUEL FLOW LSK 3L or FUEL WEIGHT LSK 2R B The inactive fuel route page RTE 1 or RTE 2 is displayed in monochrome cyan to distinguish it from the active route 1R...

Page 498: ...e is displayed and either fuel flow or fuel quantity are configured but are not received from sensors for calculations for the active flight plan or aircraft on ground or manually entered values for F...

Page 499: ...only if the SIMUL_PG option is not configured and will be displayed in large font When the fuel flow from the fuel sensor is no longer received the last valid fuel flow value received is stored as a m...

Page 500: ...entry and may be manually updated by the user in large white font FUEL WT 2R Displays the fuel weight excluding reserve For the active route fuel page the current calculated fuel weight from the fuel...

Page 501: ...displayed after FUEL in reverse video on each of the title page see above when the Active route is displayed and specific conditions are met refer to the NOTE in the FUEL 1 2 page description herein...

Page 502: ...en route activated and executed 1R 2R 3R 4R 5R 6R MOD RTE 1 FUEL 2 2 FUEL RE S EMP TY WT 1700K G 5000K G RESERVE EQU IP WT 300K G 700K G CR EW WT 300K G CAR GO WT 2000K G U NIT K G ERASE 1L 2L 3L 4L 5...

Page 503: ...s unavailable from the sensor and if the SIMUL_PG option is not configured The value is displayed in large font with a value in between 0 to 655360 kg or lb In this case the entry of a parameter also...

Page 504: ...he changes made to the inactive route GLONASS STATUS 1 2 if GLONASS is configured Display the GLONASS STATUS 1 2 page by pressing INIT REF NAV STATUS and GLONASS OP MODE 1L GLONASS receiver operationa...

Page 505: ...STATUS 6L Returns to NAV STATUS INDEX 1 1 page GLONASS STATUS 2 2 if GLONASS is configured Display the GLONASS STATUS 1 2 page by pressing INIT REF NAV STATUS GLONASS and NEXT POSITION 1L 1R GLONASS p...

Page 506: ...in the navigation solution DESELECT 6L Access DESELECT 1 1 page GPS PREDICT RAIM 1 1 if ARINC 743A is configured Used to predict future GPS integrity at any required space time point Display the GPS...

Page 507: ...of flight that should be navigable with GPS at the entered position identifier and time ETA 15 minutes by intervals of 5 minutes Possible GPS integrity status NONE GPS would not meet en route navigati...

Page 508: ...ellites are indicated in WHITE reverse video color PREDICT RAIM 6L Returns to the GPS PREDICT RAIM 1 1 page GPS NAV STATUS INDEX 1 1 Display the GPS NAV STATUS INDEX 1 1 page by pressing INIT REF NAV...

Page 509: ...cted SAT VIS 2L Number of healthy satellites visible 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 Horizont...

Page 510: ...l Coordinated Time UTC NAV STATUS 6L Access to NAV STATUS INDEX 1 1 page POSITION 1R GPS position LATITUDE and LONGITUDE VER SPD 2R GPS Vertical Velocity feet per minute MSL ALT 3R GPS Mean Sea Level...

Page 511: ...T 0 45N M TK GS MS L ALT 072o 150 K T 50 00F T VERT SP D VER ACC UR ACY 220 F T M I N 36F T UTC D ATE 1506 24Z JUL1 1 04 NAV STATUS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R GPS STATUS 1 2 POS IT ION N45 o...

Page 512: ...D T 2D position and time calculation mode X DSEL Deselected X X TK GS 3L Ground track angle degrees and Ground Speed knots VERT SPD 4L Displays GPS vertical velocity in Ft min UTC 5L Displays GPS Univ...

Page 513: ...TATUS 2 2 KEY STA TU S FAIL C ODE KEY VER 0000 SA T TRK 5 GDOP P DOP 11 0 40 3 HOR DOP VE R DOP 2 1 1 0 RAIM HI L W IND 0 34N M 120T 15K T NAV STATUS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R GPS STATUS 2 2...

Page 514: ...itional and temporal accuracy in the horizontal plane A low HDOP is desirable a high HDOP undesirable RAIM HIL 5L Displays the Horizontal Integrity Limit supplied by the GPS RAIM function SIGMA50H con...

Page 515: ...is the result of the departure arrival procedures in the database The possible display formats are shown below A Prior to EXECution EXEC annunciator is illuminated B After EXECution but prior to hold...

Page 516: ...IN PR OG RESS NEW HOLD EXIT HOLD 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R ACT RTE 1 HOLD 1 1 FIX SPD TG T ALT KILLA 220 5000A TURN DI R FI X ETA RIGHT 2332 5Z INBD CR S 050o LEG TIM E DIS 1 0M I N N M EXIT...

Page 517: ...S O N C E I N A C T I V E NEW HOLD 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R RTE 2 HOLD 1 1 FIX SPD TG T ALT KILLA 220 5000A TURN DI R FI X ETA RIGHT Z INBD CR S 050o L E G T I M E D I S 1 0 M I N N M E X...

Page 518: ...icates that exit from the holding pattern must be manually initiated via Direct To or pressing EXIT HOLD ONCE indicates automatic exit at the fix after completion of entry procedure Normally used in l...

Page 519: ...f arrival over holding fix STATUS 5R Indicates the status of the holding pattern INACTIVE The holding pattern is part of the inactive flight plan or active flight plan but not yet reached the active T...

Page 520: ...K if CFG KEY 2 configured to MARK DES SAR or TACTICAL HOVER or if Flight Transdown command of IFDS is sent or TACT HOVER if TACT key configured and HOVER configured on the TACTICAL page Displayed when...

Page 521: ...f the mark point is taken from the database or if the coordinates were entered manually RADALT 2L Displays the radio altitude ft HOVER HEIGHT 2R Displays the hover height ft TRUE WIND 3L Displays the...

Page 522: ...he same conditions as the ACTIVATE prompt See comments on ERASE 6L of RTE 1 X page for the ERASE option CONFIRM 6R If ERASE MODS is configured as CONFIRM Confirm the changes to the active route IDENT...

Page 523: ...nnel during system installation DATE 4R Display the custom database affectivity date Stars are shown when no database is loaded Blanks are shown when the date is not valid DATE 5R Display the user dat...

Page 524: ...s to the inactive route Also all the commands available on this page listed below can be applied to the respective waypoint in the inactive route In the LEGS page it is possible to switch back to the...

Page 525: ...SAR procedure is selected NOTE HOVER 2R Not available Hover is not possible on the inactive route SQUARE 3L Appears when configured The status ACT reverse video cyan is appended to the prompt if an ac...

Page 526: ...e RTE x LEGS 1 X page with only O in the scratchpad If Fly Over waypoint entered in the field REF ID of the DES SAR page display the RTE x LEGS 1 X page with the identifier and O in the scratchpad RAD...

Page 527: ...isplayed in cyan Displaying either of the INACT pages will switch the displayed LEGS pages to the inactive route Also all the commands available on this page listed below can be applied to the respect...

Page 528: ...eld REF ID of the DES SAR page and no CARP procedure exists in the flight plan then display the LEGS page with the identifier and C qualifier in the scratchpad allowing entry in the flight plan If SAR...

Page 529: ...gured and MARK key is not configured display If configured for SEARCH and Tactical Config BULLS EYE is configured and none of the CFG KEY is configured to BULL 1R 2R 3R 4R 5R 6R FMS1 INIT REF INDEX 1...

Page 530: ...cess to the LEGS 1 X page in center step EFIS mode If EFIS step mode is configured BULLS EYE 3L Access to BULLS EYE 1 3 page If BULLS EYE is configured NOTE When the Tactical Config BULLS EYE is confi...

Page 531: ...acknowledged cyan if no alert message or all messages was acknowledged DES SAR or TACTICAL 6R Access to the DES SAR or TACTICAL 1 2 page INIT REF INDEX 2 2 Display the INIT REF INDEX 2 2 page by pres...

Page 532: ...Access to DATA LOAD 1 1 page MAINT 6R Access to MAINT MESSAGES 1 X page Available only if aircraft is on ground and internal FMS failure s present INS STATUS 1 1 if LITTON EGI interface is configured...

Page 533: ...o o K T PITCH R OL L ALT o o F T VERT SP D F T M I N NAV STATUS STOP ALIGN 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R INS STATUS 1 1 POS IT ION MODE ACC UR ACY GROUND A LI GN 40 N M HDG DA TK GS o o o K T PI...

Page 534: ...eading and drift angle Heading display follows current Magnetic or True selection For LTN_92 LTN_101 ADIRU or LASEREF_V Displays IRS True or Mag heading label 314 or 320 and drift angle 321 when LTN92...

Page 535: ...TART TEST prompt is replaced by END TEST to allow the termination of the test in progress MALFUNCT 5R When LTN92 is configured access to the IRS MALF MESSAGE X X page Appears only when an INS fault is...

Page 536: ...ng incorporated in the INS DVS filter because the DVS is unavailable HYB DVS ON Hybrid INS DVS solution is available and being actively updated by INS DVS filter HYB DVS OFF Hybrid INS DVS solution is...

Page 537: ...ge displays the outputs of the INS GPS navigator as well as some INS GPS inputs from the EGI Control over the hybridization mode is also provided All status and data fields will show symbols when the...

Page 538: ...S INDEX 1 1 page POSITION 1R Displays hybrid position HOR ACCURACY 2R Displays hybrid horizontal accuracy 95 quality factor in nm INS GPS ALT 3R Displays INS GPS Baro altitude MSL INS GPS STATUS 2 2 i...

Page 539: ...AV mode RESID GS 5L Displays residual ground speed once a valid reference position is entered in LSK 2L or LSK 2R and INS in NAV mode NAV STATUS 6L Returns to the NAV STATUS INDEX 1 1 page NAV TIME 4R...

Page 540: ...ssed refers to the INS previously displayed on the IRSx STATUS X 3 page Pressing PREV or NEXT key will display other IRSx MAINT MESSAGE X 3 pages Maintenance word contents are displayed in white Aster...

Page 541: ...READY 5L Displays GPS functionality YES means ready NO means not ready NAV STATUS 6L Returns to NAV STATUS INDEX 1 1 page APIRS READY 5R Displays APIRS functionality YES means ready NO means not ready...

Page 542: ...r Maintenance Advisory messages are displayed in white with the latest identified by a leading asterisk The digit to the extreme right of each maintenance advisory message indicates which FMU is repor...

Page 543: ...t MCDU MENU page MESSAGE RECALL 1 X Only system alert messages are displayed on this page All messages are displayed in amber with the latest identified by a leading asterisk The digit to the extreme...

Page 544: ...ction of 1L or 1R line key will place the Radar Target position in the scratchpad A time stamp is displayed above this line showing the last time a Radar Target position has been received If the Radar...

Page 545: ...F WPT ID on the user waypoint page is set to ATOS and the reference position is set to the ATOS target position If the Radar target is selected the REF WPT ID on the user waypoint page is set to RADAR...

Page 546: ...is configured are displayed 1R 2R 3R 4R 5R 6R NAV STATUS INDEX 1 1 GPS GLONASS DME DVS VOR DME TCN INS GPS INS DVS INIT REF DESELECT 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R NAV STATUS INDEX 1 1 GPS GLONA...

Page 547: ...DME TCN STATUS 1 1 page Disappears or changes to VOR DME or TACAN depending on the configured equipment INS GPS 4L Access to INS GPS STATUS 1 2 page INS 4R For EGI Access to INS STATUS 1 1 page IRS 4R...

Page 548: ...By selecting the navigation data type an ordered list based on proximity will appear AIRPORT 1L Access to the NEAREST AIRPORT page VHF NAV 2L Access to the NEAREST VHF NAV page NDB 3L Access to the NE...

Page 549: ...d display the LEGS page NEAREST 6L Return to the NEAREST 1 1 page REF ID 5R The center reference identifier can be selected from any of the following database the navigation database the custom databa...

Page 550: ...int is blanked When a user waypoint is created by cross talk no sorting is triggered for the nearest USER WPT list DIRECT TO 5L Transfer the highlighted waypoint to the first waypoint on the LEGS page...

Page 551: ...PLAY 6L Provides access to DISPLAY 1 1 page MOVE UP 2R Moves the display 1 line up RIGHT 3R Moves the display 1 column right MOVE DOWN 4R Moves the display 1 line down PLAN DATA 1 1 if configured Disp...

Page 552: ...field will be update to show the navigation database extracted value if one exists otherwise the FMS default value as configured will be displayed The valid enterable range for this field is 0 to 450...

Page 553: ...configured Display the POS INIT REF 1 2 page by pressing INIT REF and POS INIT or INIT REF IDENT and POS INIT A POS INIT REF 1 2 page after EGI is powered on B POS INIT REF 1 2 page after position en...

Page 554: ...T20 04 CANCEL CONFIRM 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R POS INIT REF 1 2 FMS POS D R N47o 26 28 W122o 18 67 REF WAY PO INT KBFI N47 o 3 1 80W122 o 1 8 00 INS MOD E SE T ALT GROUND A LG IN 025 1234F...

Page 555: ...28 W122o 18 67 INS MOD E NA V TIME NAVIGATI ON 00H 34 7 UTC D ATE 1757 04z OCT20 04 SETUP UPDATE POS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R POS INIT REF 1 3 FMS POS G PS N47o 26 28 W122o 18 67 UTC DATE...

Page 556: ...ANDBY STANDBY CALIBRATE INITIALIZATION ATTITUDE STORE HEADING GROUND ALIGN nn1 GROUND ALIGN nn1 SEA ALIGN nn1 FLIGHT ALIGN nn1 FLIGHT ALIGN NAVIGATION NAVIGATION TEST tt2 FAIL FAIL 1 nn is the alignme...

Page 557: ...Boxes displayed when any IRS in align mode Automatic entry of FMS position upon acquisition of GPS with integrity GPS HIL less or equal to 0 3 nm Manual entry also allowed for as long as any IRS is in...

Page 558: ...INS the value displayed is the accuracy of the inertial navigation mode the accuracy is the accuracy of the previous sensor at the time the INS was selected then the accuracy degrades with the INS dri...

Page 559: ...Displays the current status of each navigation mode The following are the possible values for each navigation mode 1R 2R 3R 4R 5R 6R POS INIT REF 2 2 FMS POS G PS N47o 32 42 E122 o 1 8 51 MODE S TS D...

Page 560: ...atio n mode 2D T 2D T navigation mode HDG Memorized heading mode DSEL Deselecte d ACQ Acquisition mode NAV Navigation mode TEST Selftest mode IFA In Flight Alignment mode INID Almanac Search CAL Calib...

Page 561: ...Ms NOTE 2 Some configured equipment may provide only a subset of these modes Refer to the GPS 1 2 status page For LTN 92 LTN101 or ADIRU IRS ALIGN ALIGN mode NAV Navigation mode ATT ATTITUDE mode DSEL...

Page 562: ...LTN92 B For LTN101 ADIRU or LASEREF_V FMSx POS 1L Displays current FMS system position Navigation mode displayed in white on field title line GPS DME VOR DME INERTIAL or DR 1R 2R 3R 4R 5R 6R POS INIT...

Page 563: ...time greater than 14 minutes the FMS will display the value of 15 if LTN101 is configured When IRS in ALIGN time to alignment in minutes counting down from 7 minutes When IRS in ATTITUDE ATT When the...

Page 564: ...nfigured NEW USER WPT 6L Access to USER WPT 1 2 page TO WAYPOINT 2R Displays the position of the current TO waypoint Selection of 2R line key will place the position of the TO Waypoint in the scratchp...

Page 565: ...layed in reverse video white LAST JOYSTICK 2L 2R Displays the last joystick position received from the Weather Radar interface or the AHCAS AHCAS2 EFIS interface along with the time of reception If th...

Page 566: ...ate no update received on each label Latitude and Longitude are computed by the FMS The PLS operating mode is displayed on this line Possible values are DATA URX BURST or CONT When the PLS operating m...

Page 567: ...PLS displayed parameters are not updated by the FMS and remain unchanged NOTE Enabling Disabling the PLS data is used for display purposes only and the FMS continues to output the PLS waypoint positi...

Page 568: ...ot received the altitude is blank BULLS EYE TGT 5L Access to the BULLS EYE 2 3 page e g bulls eye target page and enters the last received position and altitude of the FLIR into the BULLS EYE TARGET p...

Page 569: ...23 9z DEST CYUl 552 23 35 8z RNP ANP HSI SC ALE 2 00 0 0 5N M 5 0N M NAV MOD E GPS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R PROGRESS 1 3 FROM ALTF T AT A DIRECT 127 20 48 5Z TO DTGN M ET E JFK 275 01 0 5...

Page 570: ...s used ATA 1R Actual time of arrival at the FROM waypoint TO 2L Identifier of active TO waypoint Special attributes are displayed in inverse video white refer to NOTE 2 NOTE If SAR waypoint ident disp...

Page 571: ...quipment The Actual Navigation Performance field displays one of the following depending on the navigation mode GPS ANP INS quality factor or dead reckoning quality factor Refer to Section 15 RNP Capa...

Page 572: ...he search pattern origin is displayed TDN When a Hover Transition down waypoint identifier is displayed MRK When a Hover Mark waypoint identifier is displayed IP When the CARP Identification Point is...

Page 573: ...in nautical miles from the active leg When a ROCKWELL3 EFIS is configured the XTK value displayed will be either the crosstrack relative to the arc when the arc is being flown or to the active leg ot...

Page 574: ...layed Displays a computed value of the mean sea level QNH pressure as a reference value to the pilot The units of this field will be slave to the selected unit on the QNH SET 6L field This field is ri...

Page 575: ...L 4L 5L 6L 1R 2R 3R 4R 5R 6R ACT PROGRESS 1 4 280T DTGN M ET A SAL S 3 5 2 181 7 9Z 280T 01 SAR 88 3 18 30 5Z TRUE WIND TK GS 020T 45K T 281T 228K T MAX SAR G S TK E XTK 107K T R000T L0 00N M RNP ANP...

Page 576: ...waypoint On selection will change to ETE also effects a change on PROGRESS 2 4 ETE 1R Displays estimated time en route to active waypoint NOTE When the aircraft is on ground if PLAN DATA page is not c...

Page 577: ...rformance RNP for the phase of flight and displays Actual Navigation Performance ANP RNP is defined as a statement of the navigation performance necessary for operation within a defined airspace adapt...

Page 578: ...yed 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...

Page 579: ...03 1Z TO DTGN M ET E ARRIE 17 2 00 1 7 9 NEXT TOU 68 7 00 3 0 5 DEST PANC 1279 05 4 7 2 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R ACT PROGRESS 2 4 FROM ALTF T AT A SEA 1300 18 03 1Z TO DTGN M ET A ARRIE 17...

Page 580: ...tude criterion is used If waypoint is after the midway point of the active route Transition Level criterion is used ATA 1R Actual time of arrival at the FROM waypoint TO 2L Identifier of active TO way...

Page 581: ...er is displayed MAP When a Missed approach fix waypoint identified is displayed SAR When a Search pattern waypoint except for the search pattern origin is displayed TDN When a Hover Transition down wa...

Page 582: ...a standard pressure altitude received from the ADC with a QNH baro correction applied or a baro inertial altitude received from the IRS with a QNH baro correction applied STD When a standard pressure...

Page 583: ...xternal QNH is available to the FMS This field is not displayed when the altitude source is GPS INS or manual QNH REF 6R Displayed only when the Pressure Altitude input from the ADC is available Hybri...

Page 584: ...tted to the EFIS and the corresponding waypoint number used on the RADAR display For waypoints without identifier created by the FMS parenthesis e g are displayed to indicate that no identifier is def...

Page 585: ...hanumeric and the maximum size of the identifier is 5 characters and the identifier exists in one of the following databases NDB LIB TMP USR or RTE or is one of the Bulls Eye waypoints and the identif...

Page 586: ...age but does not remove the waypoint from the route Automatically blanked after sequencing the RTA waypoint out of the flight plan RTA TAS 2L Displayed only after entry of the RTA waypoint TAS used fo...

Page 587: ...on line select keys 6L and 6R respectively RESTORE 6L Displayed only if the RTE was erased on the RTE 1 X page Used to restore the active route RTA 1R Estimated time of arrival at the RTA waypoint is...

Page 588: ...round default value is cruise wind from the PLAN DATA 1 1 page if configured otherwise default value is 0 Defaults to system wind in flight and cruise wind on ground Manual entry is displayed in large...

Page 589: ...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 1R 2R 3R 4R 5R 6R MOD RTE 1 1 3 ORIGIN D EST KSE...

Page 590: ...aircraft type configuration 1R 2R 3R 4R 5R 6R MOD RTE 1 1 2 ORIGIN D EST RUNWAY F LT NO DMAP AP PE ND RO UTE OFF CO ROUTES USER ROUTES OFF SET RESTORE R0 0N M 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R RTE...

Page 591: ...CANCEL CONFIRM prompts are displayed 1R 2R 3R 4R 5R 6R MOD RTE 1 1 2 ORIGIN D EST RUNWAY F LT NO DMAP AP PE ND RO UTE OFF CO ROUTES USER ROUTES OFF SET RESTORE R0 0N M 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R...

Page 592: ...llowing page is displayed when a user route or custom route is activated in INVERSE mode and executed and aircraft is airborne 1R 2R 3R 4R 5R 6R RTE 2 1 2 ORIGIN D EST KSEA PANC RUNWAY F LT NO KL007 D...

Page 593: ...estination identifier any navigation database user database digital map temporary waypoint and position if configured for tactical approach Entry or re entry clears arrival procedures of the previous...

Page 594: ...he CMA 9000 FMS is configured for single mode of operation NOTE RTEx corresponds to RTE1 or RTE2 depending on which route is being displayed For the active route When LSK 4L is selected the active rou...

Page 595: ...OFFSET 6R This prompt appears only if the OFFSET display element is configured To initiate offset parallel track navigation enter lateral offset L99 9 R99 9 and press EXEC Maximum desired lateral offs...

Page 596: ...E NEXT or SELECT CO ROUTE 1 X page ROUTE NEXT A Page displayed of an Active route B Active route during modification 1R 2R 3R 4R 5R 6R ACT RTE 1 2 3 VIA TO LACRE3 HUMPP DIRECT RADDT J20 OCS J154 RAMMS...

Page 597: ...closest to being abeam of the aircraft is displayed on the first TO line Subsequent entry of an airway determines the intersection waypoint If the waypoint is unnamed a waypoint is created in latitude...

Page 598: ...RASE a confirmation is requested by displaying CANCEL CONFIRM prompts on line select keys 6L and 6R respectively RESTORE 6L Displayed in amber only when the route s origin is deleted in RTE 1 X page U...

Page 599: ...to the desired waypoint or to enter the waypoint followed by S into the route MOD RTE X SQUARE 1 1 page is displayed 3 Using NEXT or PREV keys select the desired Search pattern page RTE X SQUARE 1 1 R...

Page 600: ...L NEXT SQUARE or LADDER or SECTOR 2 Enter a valid waypoint identifier in ID LSK 1L field or REF ID LSK 2L field 3 Enter desired Search parameters 4 Press CONFIRM softkey to create a Search pattern way...

Page 601: ...EN GTH YUL02 2 0N M REF ID TRACK SP AC ING 1 0N M SAR B RG 155T MAX GS ACTI VE SAR 72 K T LA DDER ERASE 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R RTE 1 LADDER 1 1 ID LEG L EN GTH YUL02 2 0N M REF ID TRACK...

Page 602: ...YUL02 2 0N M REF ID TRACK SP AC ING 1 0N M SA R BRG 155o MAX GS ACTIV E SAR 72 K T LA DDER CURRENT W PT ENTR Y WPT 01 03 ERASE RESUME 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R RTE 2 LADDER 1 1 ID LEG L EN...

Page 603: ...ory NVM This default value is preserved even after a cold start RELATIVE BRG 3L The relative bearing of the search pattern entry waypoint compared to the reference REF ID This field is displayed as lo...

Page 604: ...re the active route NOTE CANCEL appears when NOT in modified and when the ACTIVATE key is present e g Search pattern parameters are entered in the SAR page but no Search pattern waypoint defined in ro...

Page 605: ...w waypoint identifier will be created and displayed in the ID field The REF ID field will be filled with dashes and the RELATIVE BRG DIST fields title and data will disappear Entering a valid waypoint...

Page 606: ...NTIN UI TY KILLA LEGS ETA 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R MOD RTE 1 LEGS 1 2 188o P T 2 25 N M A N C P T R 1600A R053o CR S 4 86 N M ANC FAF 053o CR S 5 09 N M RW06R OMAP THEN ROUTE D ISCONTIN UI...

Page 607: ...1 2 188o P T 2 25 N M ANCPTR 1600A R053o CR S 4 86 N M ANC H 053o CR S 5 09 N M RW06R O THEN ROUTE D ISCONTIN UI TY RW014 O 194 CANCEL SAVE CONFIRM 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R CTR RTE 1 LEGS...

Page 608: ...fix HDG Courses and headings are magnetic or true course T based on configuration Field is blank if the leg direction is undefined e g for a route discontinuity LEG DISTANCE For the active waypoint Di...

Page 609: ...page Entering C over any other existing waypoint in the flight plan is not allowed Entering over any CARP procedure waypoint removes the CARP procedure and CRP01 waypoint from the flight plan From the...

Page 610: ...except for altitude terminated legs the pilot cannot enter an altitude restriction lower than the one from the Navigation Database or the one as determined by the tactical approach geometry computatio...

Page 611: ...the line select key adjacent to the prompt the FMS will automatically sequence the Missed Approach Point MAP to the missed approach procedure NEXT WPT 6R Not shown Prompt is displayed when automatic...

Page 612: ...13 28KG YZP 1950 2z 11 85KG MOCA1 2000 7z 11 79KG BKA 2044 5z 9 50KG KILLA 2127 0z 7 92KG LEGS SIMUL RTE2 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS ETA 1 4 ETA E FA CAFTA 1916 4Z 13 28K G YZP...

Page 613: ...2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS ETA 1 4 ETA CAFTA 1916 4Z YZP 1950 2z MOCA1 2000 7z BKA 2044 5z KILLA 2127 0z LEGS LEGS POS 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS ETA 1 4...

Page 614: ...R 2R 3R 4R 5R Estimated Fuel at Arrival Estimated remaining Fuel quantity at waypoint based on the fuel consumption rate If a route discontinuity exists subsequent EFAs are based on an assumed great c...

Page 615: ...ges are configured A Normal ACTIVE format B LEGS POS during a MOD 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS POS 1 2 CAFTA N51o 17 72 W129 o 0 5 32 YZP N53o 15 13 W131 o 4 8 42 MOCA1 N54o 30 18 W133 o 0 1 90 BK...

Page 616: ...ive route CANCEL 6L Cancel the changes made to the inactive route SIMUL RTEx 6L Access to the SIMUL RTEx 3 3 page only available on the inactive route LEGS POS page when the SIMULATION pages have been...

Page 617: ...he Search waypoint already defined as a Sector pattern Automatically accessed whenever a route is executed when a search pattern that has not been activated is present in the modified route The displa...

Page 618: ...boxes are displayed Else if an entry was made in REF ID field 5 dashes are displayed NOTE When a new ID is entered the operator should clear the relative bearing and distance data field relative to t...

Page 619: ...VE SAR 4R Type of the active search pattern present in the flight plan When there is no active search pattern none is displayed PPOS 5L The search pattern is started at the present position Toggles be...

Page 620: ...rrent waypoint field freezes to the number of the last TO search waypoint and disables the steering command upon EXEC key press RESUME is used when a SAR pattern needs to be restarted from a search wa...

Page 621: ...priority the current page if already in a SAR page or the last modified SAR page or the last selected SAR page from DES SAR or TACTICAL page NOTE Each pressing of the NEXT PREV key will cause the dis...

Page 622: ...RACK SPACING 1R Value of the leg length between 0 1 and 40 nm The parameter is kept in NVM and its initial default value is 2 0 nm Subsequent change of the parameter value validated by pressing the AC...

Page 623: ...ENT WPT 5L Number of the search waypoint towards which the aircraft flies This value increases as the aircraft overfly the search waypoints The default value for this field is 02 80 if an EFIS of type...

Page 624: ...rrent waypoint field freezes to the number of the last TO search waypoint and disables the steering command upon EXEC key press RESUME is used when a SAR pattern needs to be restarted from a search wa...

Page 625: ...osition resolution is 4 seconds B Waypoint PLB02 is a test message received from a PLB the beacon does not transmit specific ID and the waypoint is not selected for transmission to EFIS if DISPLAY opt...

Page 626: ...ore the position RESOLUTION 1R The position resolution is displayed next to the ID POS static field when the position is available otherwise the resolution is not displayed The position resolution is...

Page 627: ...t 6 digit of the 9 digit MMSI RCS Radio Call Signs of up to seven characters that comply with the ITU Radio Regulations on the formation of call signs see REF E1 SN The beacon unique serial identifica...

Page 628: ...OCKWELL3 BARCO AHCAS2 MEGGIT or Primus Epic otherwise this field is blank SARSAT WPT 5L Access to SARSAT WPT 1 1 page BULLS TGT 5R Access the BULLS EYE 2 3 page and put the SARSAT waypoint coordinates...

Page 629: ...ELT01 EPI03 ELT04 PLB07 and PLB08 are transmitted to the EFIS B When waypoint PLB02 has been selected for deletion 1R 2R 3R 4R 5R 6R SARSAT WPT 1 2 ID AG E BRG DI S ELT01 18 EL T05 090T 20 0N M 190T...

Page 630: ...hen SELECTION is chosen the selected SARSAT waypoints displayed in reverse video green are transmitted to the EFIS When ALL is selected all SARSAT waypoints are transmitted to the EFIS The selection S...

Page 631: ...he latest SARSAT waypoint received from a beacon all duplicate SARSAT waypoints are deleted When toggling from AUTO to MANUAL no deletion is performed This field is only applicable when DF 935 12 is c...

Page 632: ...he CO ROUTE is configured to ORIG_DEST only the particular routes associated with the entered origin and destination will be displayed If CO ROUTES is configured to ALL every CO ROUTE in the database...

Page 633: ...of increasing distance from present position Pressing one of the appropriate LSKs will automatically select the navaid description and return to the previous page from which this page was accessed Th...

Page 634: ...was previously attempted NOTE The ICAO region field will be blanked if the waypoint is found from the Custom or User database or the waypoint is a temporary waypoint SETUP 1 1 This page allows the us...

Page 635: ...2 etc NOTE All navigation functions use Lat Long in WGS84 this function only affect display entry to pilot of positional information When COORD is SWISS GRID DATUM is forced to CH1903 and cannot be mo...

Page 636: ...e will appear when calculated values exceed the permitted range Fields will be left empty when default values are not available A Default Display B Display after manual entry of Gross Wt 1R 2R 3R 4R 5...

Page 637: ...is greater than Computed gross weight The advisory will disappear if the pilot clears it or the page is exited or new simulated values are entered causing the fly away condition to be met If the defau...

Page 638: ...ight required to maintain the specified pressure altitude without any drop in height upon loss of an engine The OEI OGE WT is obtained only when the OAT and PRESS ALT are available and valid OAT 4L Ou...

Page 639: ...advisory FUNCTION NOT COMPUTED message will appear when calculated values exceed the permitted range Fields will be left empty when default values are not available A Default Display B Display after...

Page 640: ...ssure altitude Valid range 2000 ft to 12000ft Defaults to the current pressure altitude in normal video Manual entry is displayed in reverse video and causes a recalculation of Gross Weight and Fly Aw...

Page 641: ...titude are re calculated SIMUL RTEx 3 3 page or 1 1 if SIMUL PG and RTE2 is configured Display SIMUL RTE x 3 3 or 1 1 page by pressing INIT REF NEXT and SIMULATE and PREV The SIMUL RTEx page enables t...

Page 642: ...r or 0 72153 lb hr A default fuel flow value is displayed in medium font When the rate of fuel consumption is available from the fuel sensor the default fuel flow is provided by the fuel sensor otherw...

Page 643: ...igured These pages are only accesible if the TACT key is configured Otherwise the name of the page is DES SAR TACT INIT REF BULLS EYE NEXT TACTICAL INIT REF WPT DATA TACTICAL INIT REF WPT LISTS DMAP W...

Page 644: ...e are used In this example SQUARE LADDER SECTOR HOVER BULLS EYE CENTRAL CLR FLIR and TACT APPR are configured 1R 2R 3R 4R 5R 6R TACTICAL 1 2 REF ID WPT03 BULL TOP RAD DIS T N M BULL WPT SQUARE TACT AP...

Page 645: ...orage 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 thi...

Page 646: ...iv TACTICAL REF ID defined and different from the PI of the existing CARP procedure Brings up the CARP PLAN 1 3 page with the identifier in the scratchpad Case v TACTICAL REF ID defined and has the sa...

Page 647: ...Brings up the LEGS page with the identifier and T in the scratchpad TACTICAL APPR 1 3 page if configured Display TACTICAL APPR 1 3 page 1 For the active route press TACT TACT APPR if TACT key is confi...

Page 648: ...ach Runway Threshold Waypoint on the LEGS page The TACTICAL APPR page displays the parameters defining the tactical approach procedure NOTE This page is only available if the TACTICAL APPROACH option...

Page 649: ...0 o 117FT VPA TRAN S LVL 3 0 o F L060 CANCEL CONFIRM 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R TACTICAL APPR 1 3 REF WPT I D RA D DIS o NM TIAF 3 0 o ALT 090 o 3 00 NM 27 11FT TFAF FAF ALT 090 o 5 00 NM 17...

Page 650: ...WPT ID is deleted If the reference position does locate the TIAF waypoint outside the permitted range an advisory message will be displayed in the scratchpad indicating that the TIAF location is inval...

Page 651: ...ly VPA 5L The FMS will allow crew entry modification of the VPA Vertical Path Angle in degrees required to define the tactical approach geometry The value is left justified and always displayed with o...

Page 652: ...2 3 page if configured Display TACTICAL APPR 2 3 page 1 press TACT TACT APPR NEXT if TACT key is configured and TACT APPR configured on the TACTICAL page 2 INIT REF DES SAR or TACTICAL NEXT TACT APPR...

Page 653: ...10 29FT CLIMB G RA DIENT 2 5 2 0 REF WPT I D RA D DIS o NM ERASE 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R MOD TACTICAL APPR 2 3 PARKKMA P RWY E LEV 090 o 2 00 NM 1 17FT TMAP1 ALT 090 o 5 00NM 4 21FT TMAP2...

Page 654: ...B G RA DIENT 2 5 2 5 REF WPT I D RA D DIS o NM 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R TACTICAL APPR 2 3 PARKKMA P RWY E LEV 090 o 2 00 NM 1 17FT TMAP1 ALT 090 o 5 00NM 4 21FT TMAP2 ALT 10 29FT CLIMB G RA...

Page 655: ...defined by the TMAP1 to TMAP2 altitude constraint distance The two climb gradients are separated by a slash No input is allowed on this field The values displayed are left justified and displayed with...

Page 656: ...page if configured Display TACTICAL APPR 3 3 page by pressing 1 INIT REF DES SAR or TACTICAL NEXT TACT APPR PREV if TACT key is configured and TACT APPR configured on the TACTICAL page 2 Or from DEP A...

Page 657: ...21FT 090 o 4 00NM 2 5 TMAP2 10 29FT ERASE 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R MOD TACTICAL APPR 3 3 TACT AP PR TIAF 27 11FT 090 o 3 00NM 3 0 o TFAF FAF 1757FT 090 o 5 00NM 3 0 o PARKK MAP 1 17FT 090 o...

Page 658: ...00NM 2 5 TMAP1 4 21FT 090 o 4 00NM 2 5 TMAP2 10 29FT 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R TACTICAL APPR 3 3 TACT AP PR TIAF 27 11FT 090 o 3 00NM 3 00 o TFAF FAF 1757FT 090 o 5 00NM 3 00 o PARKK MAP 1...

Page 659: ...DIS IAA 1R This field displays the altitude constraint in ft at the TIAF waypoint the distance between the TIAF waypoint and the TFAF waypoint in nm and the Intermediate Approach Angle between those...

Page 660: ...unt up timer or a certain time duration has elapsed countdown timer A Display when no data is entered or after pressing CLEAR B Display after an alarm time is entered 1R 2R 3R 4R 5R 6R TIMER 1 1 ALARM...

Page 661: ...MER 1 1 ALARM T IM E COUN TD OWN 1234 12z 2329 53 ADD 5 MIN ADD 15 MIN ADD 30 MIN STOP CLEAR 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R TIMER 1 1 ALARM T IM E COUN TD OWN 1234 12z ADD 5 MIN ADD 15 MIN ADD 30...

Page 662: ...5 MIN 2R Adds 5 minutes to the alarm and or countdown time whichever is being displayed If no alarm or countdown time is being displayed the countdown time will be set to 5 minutes Displayed only if a...

Page 663: ...orary position updates the FMS position is not affected but the flight plan waypoints for the CARP tactical function are shifted while and only while the procedure is active Upon exit and re entry to...

Page 664: ...SITION N45o 28 08 W073o 44 48 A CCUR POS D IFF VOR DME 0 07 000 o 0 00 CARP PROG CARP MARK 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R MOD TMP UPDATE POS 2 2 REF BRG D IST 000o 0 00N M UPDATE PO SITION N45o...

Page 665: ...00 to 99 9 nautical miles The second format is XTK OFFSET and is not available when REF is FMS cross track distance from the REF position to the closest point along the path passing through the aircra...

Page 666: ...This LSK is used to mark the current FMS position UPDATE POS 1 1 if PREDEF PAGE and IRS EGI or DVS interface is configured or UPDATE POS 1 2 if CARP is configured Display UPDATE POS 1 1 page by pressi...

Page 667: ...he position may be entered directly or with an identifier The UPDATE POS field will get automatically updated by the CMA 9000 FMS 5 The user selects the navigators for which a position update is sough...

Page 668: ...IFF INS DVS 0 07 000 o 0 00 INS GPS 1 10 090 o 1 00 DVS 2 01 180 o 2 00 UNMARK MARK 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R UPDATE POS 1 1 REF BRG DI ST CYUL o N M ACCUR 0 2 7N M N45o 28 08 W073o 44 48 A...

Page 669: ...REF ACCUR o o A CCUR POS D IFF INS DVS 0 07 o INS GPS 1 10 o DVS 2 01 o PREDEF WPT MARK 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R UPDATE POS 1 1 REF JOYSTICK ACCUR 0 2 7N M o o TRUE JOY POS o o A CCUR POS D...

Page 670: ...TICK ACCUR 0 2 7N M N45o 28 08 W073 o 4 4 48 TRUE JOY POS N45o 21 19 W073o 27 00 A CCUR POS D IFF INS DVS 0 07 000 o 0 00 INS GPS 1 10 090 o 1 00 DVS 2 01 180 o 2 00 PREDEF WPT MARK 1L 2L 3L 4L 5L 6L...

Page 671: ...ered the update position corresponds to the offset reference s position TRUE JOY POS 3R WEATHER RADAR or AHCAS EFIS configured This field is displayed only when the joystick prompt is selected This fi...

Page 672: ...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 When the OUT OF RANGE message is display...

Page 673: ...xisting 10 route names has to be deleted in order to make room for that new route since the maximum number of user routes is 10 LOAD 5L Toggle DIRECT INVERSE direction of the route to be loaded DIRECT...

Page 674: ...ny identifier is entered and all mandatory fields are entered CANCEL CONFIRM prompts will appear Leaving the USER WPT pages without confirmation will automatically perform a CANCEL A Page displayed fo...

Page 675: ...222K T TYPE MOVING REF WPT I D RA D DIS ADED 000o 0 00N M REF WPT P OS N45o 12 23 W043o 32 12 CANCEL SAVE CONFIRM 1L 2L 3L 4L 5 6L 1R 2R 3R 4R 5R 6R USER WPT 1 2 ADFF ID P OS FREE 459 N45o 12 23 W043...

Page 676: ...cond The default value is boxes FREE 1R 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 mov...

Page 677: ...3 3 page the REF WPT ID field displays the identifier FLIR RAD DIS 4R Radial distance from the reference position to the desired user waypoint position The values are blanked when no REF WPT POS is de...

Page 678: ...ties mandatory and optional field When the new waypoint created is of type other than WAYPOINT mandatory fields must be entered as indicated by the display of the page 1R 2R 3R 4R 5R 6R USER WPT 2 2 I...

Page 679: ...ddle East South Asia CAN Canada PAC Pacific EEU Eastern Europe SAM South America EUR Europe SPA South Pacific LAM Latin America USA United States of America CUS Specific to customer Sample ICAO countr...

Page 680: ...LETE ALL 6R Request to delete all user waypoints and triggers the CANCEL and CONFIRM prompts If a moving waypoint is present in the active or modified route then the advisory message MOV WPT IN ROUTE...

Page 681: ...verse white color if there is no indication the user waypoint is FIXED NEW USER WPT 6L Access to the USER WPT page for user waypoint creation modification DELETE Displayed between the CANCEL CONFIRM p...

Page 682: ...V A Only pressure altitude available to the FMS from the Air Data Computer B Baro corrected altitude available to the FMS from the Air Data Computer 1R 2R 3R 4R 5R 6R ACT VNAV NDB24L 1 1 M DA DA 660 2...

Page 683: ...l approach C CARP procedure TRUE MAG WIND and GS 4L Displays current wind direction and speed and ground speed Wind direction is crew selectable to magnetic or true North reference when the A C is out...

Page 684: ...e waypoint is not the FAF or MAP or step down fix Temperature compensated altitude constraints are displayed in reverse video white The altitude is displayed in NORMAL font if the altitude is coming f...

Page 685: ...ORDME or TACAN NOTE The title will change to VOR DME or TACAN as applicable if some of the equipment is not configured A Single VOR and DME configuration Single TACAN B Dual VOR and single DME configu...

Page 686: ...ency is changed and the FMS is searching for the new station ident An inverse white H appears next to the frequency when the DME is in HOLD mode The frequency and slant range are values received from...

Page 687: ...esponding to wind data NOTE The altitude data can only be entered at LSK 1L Altitudes are displayed in descending order at 1L 2L 3L 4L If four altitudes already exist one of these must be deleted prio...

Page 688: ...ute WPT DATA 1 1 The WPT DATA 1 1 page allows for the display and partial modification of waypoint information from the navigation temporary custom or user databases Moving if configured and fixed way...

Page 689: ...OM NEW USER WPT DES SAR 1L 2L 3L 4L 5L 6L 1R 2R 3R 4R 5R 6R WPT DATA 1 1 AFVRD WPT POS N03 o 2 1 12 W12 3o 25 56 BRG DI S 134T 1 23 NM DATAB AS E USER REG IO N CAN CY TYPE CL AS S TACAN ELEVAT IO N 23...

Page 690: ...ge and the Bulls Eye Target waypoint will display the BULLS EYE 2 3 page WPT POS 1R Display of waypoint position Pressing this key with an empty scratchpad copies the position to the scratchpad BRG DI...

Page 691: ...play of NAVAID frequency MHz DME ILSDME VOR and VORDME VHF NAV only CHAN 5L 5R upper line Display of TACAN channel CH FREQ 5L 5R Display of TACAN channel and corresponding NAVAID frequency MHz VORTAC...

Page 692: ...er the waypoint information to the REF ID on the DES SAR 1 Y or TACTICAL 1 Y page and display the DES SAR 1 Y or TACTICAL 1 Y page depending on the configuration WPT LISTS 1 1 Display WPT LISTS 1 1 pa...

Page 693: ...B 6 COURSE TO A DME DISTANCE CD LEG B 7 COURSE TO A COURSE INTERCEPT CI LEG B 8 COURSE TO A RADIAL CR LEG B 9 COURSE FROM A FIX TO AN ALTITUDE FA LEG B 10 COURSE FROM A FIX TO A DISTANCE B 11 COURSE F...

Page 694: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page B ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 695: ...ng 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 DIRECT TO A FIX WAYPOIN...

Page 696: ...nding waypoint and a course into the waypoint 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 2 053o CR S 4 8 6 N M ANC OFAF 053o CR S 5 0 9 N M RW06R OMAP 053o 0 7 4 N M 544 R200o HD G 12 4 N M INTC 173o CR S 13...

Page 697: ...the radius and terminates at a waypoint with a terminating tangential course TRUE NORTH ANC CENTER FIX RIGHT TURN ARC D173J J 10 NM RADIUS R173 D10 0 262 STARTING COURSE 0 0 D233J R233 D10 NLD6 NLD6 3...

Page 698: ...lowing course to fix navigation leg TRUE NORTH ANC STARTING POINT ANC R SECOND TURN POINT RIGHT TURN PT ANC L FIRST TURN POINT LEFT TURN PT NLD6 NLD6 4C CDR 053 188 D2 25 233 D3 0 1R 2R 3R 4R 5R 6R AC...

Page 699: ...ilot manually ended hold Crossing the waypoint after completing the entry procedure hold for course reversal the hold page TITLE field display HOLD ONCE Crossing the waypoint and reaching the target a...

Page 700: ...d by a course from previous leg termination position and a target altitude 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 1 053o CR S 3 0 9 N M RW06R OMAP 053o CR S 0 7 4 N M 544 R200o HD G 12 4 N M INTC 173o CR...

Page 701: ...rent aircraft position and terminates when reaching a distance from a DME Navaid 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 2 2 071o CR S 1 5 0 N M FFM 15 O 764A R200o CR S 8 8 0 N M DFW2 2500A 200o CR S 4 5 5...

Page 702: ...ircraft position and terminates when a desired course which is referenced to a waypoint is intercepted and captured 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 2 2 330o CR S 4 7 0 N M MA36 O 330o CR S 1 9 7 N M...

Page 703: ...course from current aircraft position and terminates when crossing a radial from a referenced waypoint 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 1 080o CR S 8 2 3 N M YUL020A 200o CR S 15 1N M YUL 2500A 194...

Page 704: ...DE FA LEG This navigation leg is defined by a waypoint a course and an altitude termination 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 4 142o FR R W14 5 0 0 N M 2900 A L322o CR S 16 3 N M YOW RTE 2 LEGS LEGS...

Page 705: ...a distance to travel from the waypoint TRUE NORTH CMCM3 CMC10 NLD6 NLD6 11B CDR 233 COURSE D10 0 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 1 233o FR C MCM3 3 71 N M CMC10 O 220 5000A L233o CR S 5 62 N M CMCM...

Page 706: ...int and a course and terminates when reaching a distance from a DME Navaid TRUE NORTH RW06R DPK10 DPK NLD6 NLD6 12B CDR D10 038 COURSE 0 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 2 2 038o FR R WO6R 18 5 N M DP...

Page 707: ...EG This navigation leg is defined by a waypoint and a course and terminates on pilot request 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 1 251o FR A GLIN N M VECT A 060o 7 80 N M FANOL 2500 235o CR S 9 13 N M...

Page 708: ...ed by a heading from current aircraft position and terminates when reaching a target altitude 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 2 3 058o CR S 3 9 1 N M RW06R OMAP 057o HD G 1 0 4 N M 1100 090o HD G 8 9...

Page 709: ...heading from current aircraft position and terminates when reaching a distance from a DME Navaid 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 2 3 071o HD G 2 0 0 N M FFM 15 764A 200o CR S 6 8 0 N M DFW2 2500A 200...

Page 710: ...tes when a desired course which is referenced to a waypoint is intercepted and captured TRUE NORTH 090 HEADING 0 INTC NLD6 NLD6 16B CDR 070 COURSE 0 OO 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 2 3 057o FR R W...

Page 711: ...gation leg is defined by a heading from current aircraft position and terminates on pilot request 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 1 1 320o HD G N M VECT F 336o 14 1N M FINEY 2000 142o CR S 3 9 9N M K...

Page 712: ...eading from current aircraft position and terminates when crossing a radial from a referenced waypoint 1R 2R 3R 4R 5R 6R ACT RTE 1 LEGS 2 3 280o CR S 3 5 0 N M RW08 OMAP 053o HDG 2 30N M 2000 053o HD...

Page 713: ...reverse to a radial and a distance to the reference waypoint The reference waypoint can be a waypoint in the route or another waypoint The new leg in inserted in the route 1R 2R 3R 4R 5R 6R RADIAL TO...

Page 714: ...NUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page B 20 November 19 2009 SEARCH PATTERN Refer to Section 11 for detailed information This page is printed under user s responsibility and must not be retained...

Page 715: ...EHSI EFIS DISPLAYS NAVIGATION MODE AND ADVISORY MESSAGES C 9 APPENDIX C 2 NAVIGATION DISPLAYS EFIS GAMA STANDARDS C 10 INTRODUCTION C 10 EFIS DISPLAYS C 12 TYPICAL ROUTE C 12 DIRECT TO INTERCEPT NAVIG...

Page 716: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page C ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 717: ...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: ...rrent 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...

Page 719: ...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 Typical PLAN...

Page 720: ...640 nautical miles via the range switch on the EHSI control panel EHSI DISPLAYS SYMBOLOGY AND COLORS The color conventions used on the EHSI EFIS display are as follows Green G position data White W a...

Page 721: ...5z MAP MAP CTR PLAN Indicates FMS calculated ETA for the active waypoint based on present groundspeed top right corner DISTANCE DISPLAY W 123 4 NM MAP MAP CTR PLAN Distance is displayed to next FMS wa...

Page 722: ...ted Available when HSI range is 80 160 320 or 640 nm For tactical approaches no airport identifier pr runway number is displayed AIRPORT and RUNWAY W 22L MAP MAP CTR PLAN Appears when selected Availab...

Page 723: ...OINTER G N PLAN Indicates map background is oriented and referenced to true north SELECTED REFERENCE POINT and BEARING DISTANCE INFORMATION G ABC MAP MAP CTR PLAN Displays the reference point selected...

Page 724: ...ts are displayed when selected range is greater than 20 nm 2 segments are displayed on the 20 nm scale and one segment on 10 nm scale ALTITUDE RANGE ARC G MAP MAP CTR When intersected with the track l...

Page 725: ...Search active indication GPS approach armed status GPS integrity lost Unable RNP Offset route active with magnitude and direction of offset Active navigation mode e g GPS VOR DME TACAN DME INERTIAL D...

Page 726: ...sented below EFISs which do not support background data do not have this page available for display on the FMS 1 Active Route these symbols represent waypoints on the active route within current EFIS...

Page 727: ...FLIGHT MANAGEMENT SYSTEM Page C 11 November 19 2009 Navigation Display MAP Mode Navigation Display Arc Mode Navigation Display Rose Mode This page is printed under user s responsibility and must not...

Page 728: ...es CMA 9000 FMS as the source 6 Course Deviation the CMA 9000 FMS lateral deviation when the source of course track data is NAV 7 Waypoint Alert announces an upcoming flight leg change by the CMA 9000...

Page 729: ...ing fix identifier refer to Note 1 Examples of EFIS displays for the standard holding pattern and for the different types of entry procedures are provided in the following paragraphs For more informat...

Page 730: ...nd turn direction This example represents a direct entry into a right turn hold with an inbound course of 173 as it would appear after completion of the outbound turn PARALLEL ENTRY A parallel entry i...

Page 731: ...along the arc The DME arc in this example is represented by five segments located between the arc s initial fix D350J and final fix D233J For more information on DME arc navigation refer to Section 7...

Page 732: ...Rockwell Collins 3 EFIS has the capability to display procedure turns using arcs OFFSET NAVIGATION This example shows a typical EFIS display for an aircraft flying a route with a right offset of 20 n...

Page 733: ...t waypoint before the discontinuity This would ensure continuous availability of flight data throughout the route If the FMS does sequence the last waypoint prior to a discontinuity and the flight pla...

Page 734: ...tedly until the CTR cursor appears beside the desired waypoint 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...

Page 735: ...FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 5 of 12 D 9 FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 6 of 12 D 11 FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 7 of 12 D 13 FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 8 of 12 D...

Page 736: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page D ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 737: ...TEM NOTE This is a top down flow diagram Dash lines represent configured items FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 1 of 12 Page D 1 D 2 blank November 19 2009 This page is printed under user s respo...

Page 738: ...T MANAGEMENT SYSTEM NOTE Dash lines represent configured items FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 2 of 12 Page D 3 D 4 blank November 19 2009 This page is printed under user s responsibility and mu...

Page 739: ...MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 3 of 12 Page D 5 D 6 blank November 19 2009 This page is printed under user s responsibility and must not be retained for...

Page 740: ...MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 4 of 12 Page D 7 D 8 blank November 19 2009 This page is printed under user s responsibility and must not be retained for...

Page 741: ...MANAGEMENT SYSTEM NOTE Dash lines represent configured items FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 5 of 12 Page D 9 D 10 blank November 19 2009 This page is printed under user s responsibility and mu...

Page 742: ...MANAGEMENT SYSTEM NOTE Dash lines represent configured items FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 6 of 12 Page D 11 D 12 blank November 19 2009 This page is printed under user s responsibility and m...

Page 743: ...MANAGEMENT SYSTEM NOTE Dash lines represent configured items FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 7 of 12 Page D 13 D 14 blank November 19 2009 This page is printed under user s responsibility and m...

Page 744: ...ANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 8 of 12 Page D 15 D 16 blank November 19 2009 This page is printed under user s responsibility and must not be retained fo...

Page 745: ...ANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 9 of 12 Page D 17 D 18 blank November 19 2009 This page is printed under user s responsibility and must not be retained fo...

Page 746: ...ANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 10 of 12 Page D 19 D 20 blank November 19 2009 This page is printed under user s responsibility and must not be retained f...

Page 747: ...ANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 11 of 12 Page D 21 D 22 blank November 19 2009 This page is printed under user s responsibility and must not be retained f...

Page 748: ...ANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM FMS DISPLAY PAGES FLOW DIAGRAMS Sheet 12 of 12 Page D 23 D 24 blank November 19 2009 This page is printed under user s responsibility and must not be retained f...

Page 749: ...TENTS 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 E 51...

Page 750: ...PERATOR S MANUAL CMA 9000 FLIGHT MANAGEMENT SYSTEM Page E ii November 19 2009 This Page Intentionally Left Blank This page is printed under user s responsibility and must not be retained for reference...

Page 751: ...e CMA 9000 FMS front panel MSG annunciator and the remote MSG annunciator to illuminate until all messages are cleared acknowledged by the pilot Alert messages are cleared thus acknowledged from the s...

Page 752: ...the ADC s operate s normally Advise maintenance ADC interface AMU CONTROL LOST The FMS cannot set a radio volume level or has detected a failure of the AMU or the AMU communication bus Control the AMU...

Page 753: ...gation Use another sensor for navigation Civil GPS and EGI interface installed at the same time cGPS POS UNCERTAIN The FMS is using civil GPS position data for which the integrity does not meet requir...

Page 754: ...oint triggered for non published procedures only As deemed necessary modify flight plan if such a course change is not desired Message configured to alert DATABASE OUT OF DATE Navigation Database sele...

Page 755: ...IRECT TO FIX When flying a VI or CI leg followed by a CF leg these legs being part of a published procedure the FMS detects that the predicted intercept point is so close to the CF leg termination tha...

Page 756: ...urce DME receiver is no longer operational use other navigation aids Advise maintenance DME interface DVS NAV LOST The FMS detects a total loss of DVS input data on the onside and offside FMSs DVS sen...

Page 757: ...sition and VOR DME position greater than maximum accuracy of the two sensors Verify if DME and VOR receivers operate normally Advise maintenance Nav cross check configured FMS FAILED The FMS has detec...

Page 758: ...n greater than maximum accuracy of the two sensors Verify if EGI and civil GPS receivers operate normally Advise maintenance Civil GPS and EGI interface installed at the same time Nav cross check conf...

Page 759: ...of this approach and report issue to maintenance operations VNAV configuration HIGH HOLDING SPEED The combination of current TAS and computed wind may cause the ICAO holding pattern protected airspac...

Page 760: ...ance Multi FMS installations INDEPENDENT OP cont d 4 Verify Op Program on IDENT 1 1 page and advise mainten ance if different 5 Verify active navigation database on IDENT 1 1 page select appropriate...

Page 761: ...orts that some of its navigation parameters may have become unreliable or FMS determined that INS inertial position drift exceeds 3 3T nm where T is the INS Time in Nav in hours Message enabled for AD...

Page 762: ...ll available as long as one inertial sensor is still operating normally Move appropriate INS Mode Selector Unit switch position to ATT position IRS interface configured KALMAN NAV LOST Kalman filter n...

Page 763: ...n accuracy is reduced The FMS is not using the military GPS as active sensor but it detects a loss of integrity and a procedure SID Star Transition Approaches or Tactical Approaches is loaded in the a...

Page 764: ...rolled by the FMS Advise maintenance Phone interface PLS INPUT LOST The FMS has detected a total loss of PLS input data on the onside and offside FMSs Ensure that PLS is powered Verify if PLS operates...

Page 765: ...Enter ALTIMETER SETTING current pressure in inches of mercury in Hg or in millibars mb on PROGRESS 4 4 or 3 3 page The FMS will correct its pressure altitude input accordingly For item 3 Set altimeter...

Page 766: ...cted around navigation database airports If the message is configured and the FMS is in terminal and approach operations TACAN NAV LOST No TACAN sensor data is available for the onside and offside FMS...

Page 767: ...emains within protected airspace at all times Verify that the RNP value is appropriate for the phase of flight Modify as necessary All configurations VHF CONTROL LOST VHF1 CONTROL LOST VHF2 CONTROL LO...

Page 768: ...rate normally Advise maintenance NAV interface DME interface TACAN interface VUHF CONTROL LOST VUHF1 CONTROL LOST VUHF2 CONTROL LOST FMS cannot control the VUHF radio Control VUHF radio from another s...

Page 769: ...is inactive Advise maintenance None H W A429 IP FAILED ARINC 429 receiver failure detected Where is 1 to 24 SYSTEM DEGRADED displayed on MESSAGE RECALL page Do not use the FMS to communicate with the...

Page 770: ...th the SERIAL I O Controller SYSTEM FAILED displayed on MESSAGE RECALL page CDU keyboard discretes and annunciators may no longer operate Advise Maintenance FMS FAILED H W UART RX FAILED The SYSTEM de...

Page 771: ...ally deselect this mode Advise Maintenance to verify the SAGEM EGI EGI interface AAIM SAT FAILED Non isolated satellite failure As above EGI interface ADC1 FAILED ADC2 FAILED The FMS has detected a fa...

Page 772: ...r altitude bus Do not use transponder Mode C capability Advise maintenance ATC transponder interface ATC transponder name configured as ATC ATC1 FAILED ATC2 FAILED The FMS has detected a failure of th...

Page 773: ...that of the off side FMS Advise maintenance crew to ensure that the same preferred datum list is selected on all configured FMSs Multi FMS installations DCU1 FAILED DCU2 FAILED DCU3 FAILED If IS S EFI...

Page 774: ...ATC or DME Hold channel control 4 Failure of the cross talk bus detected 1 Ensure that identified FMS is powered Verify if identified FMS operates normally Advise maintenance 2 Any automatically sync...

Page 775: ...GI interface GPS FAILED GPS1 FAILED GPS2 FAILED The FMS has detected a failure of the GPS unit or a failure of the GPS unit communication bus Entry of date and time may be required Functions requiring...

Page 776: ...hen convenient IRS interface configured IRSx EXCESS MOTION LTN 92 INS or ADIRS reports excessive motion during alignment phase ALIGN mode automatically re sequences to 10 minutes 32 seconds if in rapi...

Page 777: ...erent SSMs from each other for 5 seconds Ensure that the RADAR is powered Verify if the Radar operate s normally Advise maintenance Installations in which the FIAR 1500B Radar is configured RALT FAILE...

Page 778: ...o from another source NAV receiver is no longer operational use other navigation aids Advise maintenance NAV radio interface NAV radio name configured as VIR VUHF FAILED VUHF1 FAILED VUHF2 FAILED The...

Page 779: ...remains prior to reaching the CRP waypoint Prepare for CARP per the CARP procedure checklist Configurations supporting CARP HARP AIR TEMP NOT VALID Air temperature is invalid or out of bounds valid r...

Page 780: ...DU ENTRY CONFLICT The FMS detects conflict of entry in dual triple FMS operations Insure no conflicting action between flight crew members Multi FMS installations cGPS NAV DESELECTED The civil GPS sen...

Page 781: ...vely via external switch CHECK UPDATE The FMS detects that the position difference between the sensor to be updated and the reference position is greater than the accuracy of the sensor to be updated...

Page 782: ...ation with Digital Map Display System Interface Verify the DMAP power and self test status Advise maintenance DMAP interface DME NAV DESELECTED DME Sensor manually de selected by the pilot Ensure DME...

Page 783: ...N LIGHT CARP Green Light waypoint has been reached Message is enabled when the CARP function is configured Start CARP drop Configurations supporting CARP HARP GROSS WEIGHT NOT VALID Gross weight inval...

Page 784: ...ssage is not raised Press WPT LISTS then SARSAT LSKs to display the information about the new SARSAT beacon received DF 935 or DF430 interface NEW TARGET POSITION The FMS has received a new valid targ...

Page 785: ...has been reached Configurations supporting CARP HARP SMS NOT TRANSMITTED The FMS detects that SMS was not transmitted by the Iridium phone Retry to send the SMS Iridium Phone interface SMS TRANSMITTE...

Page 786: ...ses the EXEC button and activates the flight plan and b a transition altitude level is stored in the tactical approach database for the selected tactical approach procedure and c a manual entry curren...

Page 787: ...n DESELECT page configured Ensure VOR DME navigation mode is deselected NAV interface DME interface WAYPOINT BYPASSED FMS detects that the airplane crosses the wayline perpendicular line to the next l...

Page 788: ...gured 2ND MOV WPT NOT ALLOWED Operator is attempting to enter a second moving waypoint in the active or in the modified flight plan Cancel entry or cancel the first moving point then enter the new one...

Page 789: ...nt if Tactical Config BULLS EYE is configured BULLS EYE DATA MISSING Operator is attempting to confirm a Bulls Eye or Bulls Eye Target modification without having defined all mandatory information Ens...

Page 790: ...WAYPOINT Operator is attempting to enter a waypoint with an identifier already existing in the database except the user database Choose another ident All configuration DUPLICATE USER WAYPOINT Operato...

Page 791: ...ORIGIN Operator is attempting to execute a flight plan without an origin airport or to enter the destination airport prior to the ORIGIN airport Enter the ORIGIN airport All configurations except for...

Page 792: ...terface GUARD BAND Operator is attempting to enter a frequency that is in a guard band based on the preset maritime offset mode Enter a frequency not in a guard band based on the preset maritime offse...

Page 793: ...ing a DIRECT TO procedure All configurations Multi FMS installations INACTIVE ROUTE IN MOD The operator attempts to access the HOVER or DES SAR or TACTICAL 1 2 page while the inactive route is being m...

Page 794: ...quency One of the following element is configured COM VUHF VOR ILS ADF INVALID IDENT An invalid Ident was entered in the library Enter a valid Ident 5 characters max One of the following element is co...

Page 795: ...P waypoints to be greater than 30NM Message is enabled when the CARP function is configured Correct IP or PI position on the CARP PLAN pages Configurations supporting CARP HARP LIBRARIES IN USE Operat...

Page 796: ...t is not part of the route before deletion Moving waypoint MOV WPT NOT ALLOWED The operator is attempting to enter a moving waypoint in the second route Cancel entry Moving waypoint MOVING WAYPOINT Th...

Page 797: ...ld not find entered identifier in the navigation database or in the company route database or in the user database or as a Bulls Eye waypoint or a Bulls Eye Target waypoint Check identifier or re ente...

Page 798: ...Operator is attempting to change a radio frequency while FMS radio tuning is inhibited Verify reason for radio tuning inhibit One of the following element is configured COM ADF VOR ILS DME RALT FAILE...

Page 799: ...oint e g TO waypoint Ensure that no tactical approach procedure waypoint is the TO Then proceed with modification to the tactical approach procedure If tactical approach is configured TE TO IP OUT OF...

Page 800: ...ist is full 450 fixed and 10 moving waypoints Cancel entry or delete unnecessary waypoints to make room for the new one s All configurations VERIFY POSITIVE TEMP Operator entering a positive temperatu...

Page 801: ...th GPS approach TX1 Green Illuminates when the VUHF1 radio is emitting RF power None TX2 Green Illuminates when the VUHF2 radio is emitting RF power None GSM Green Illuminates when a voice call is bei...

Page 802: ...not in the approach zone The NAV flag will be accompanied by a number of possible alert or advisory messages depending on the cause ACTION Depending on the cause eliminate or change the operational co...

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