Benutzeranleitung / Produktwartung GNS-XL des Produzenten Honeywell
Zur Seite of 353
006-08852-0000 Rev. 4 Nov/04 GNS-X L FLIGHT MANAGEMENT SYSTEM Operator’s Manual Global N.
WARNING Prior to export of this document, review for export license requirement is needed. COPYRIGHT NOTICE Copyright ©1998-2002, 2004 Honeywell International Inc. All rights reserved. Reproduction of this publication or any portion thereof by any means without the express written permission of Honeywell International Inc.
Revision History and Instructions Manual GNS-X L Operator’s Manual Revision 4, November 2004 Part Number 006-08852-0000 This revision adds descriptions of operational procedures required to fly three kinds of SIDs.
GNS-X L Flight Management System R-1 Rev. 3 Oct/02 Revision History and Instructions Manual GNS-X L Operator’s Manual Revision 3, October, 2002 Part Number 006-08852-0000 This revision incorporates AFIS Printer Control, deletes Air Canada and calri- fies SID/STAR operation.
GNS-X L Flight Management System R-1 Rev. 2 Apr/00 Revision History and Instructions Manual GNS-X L Operator’s Manual Revision 2, April, 2000 Part Number 006-08852-0000 This revision incorporates GNS-XL Software Mod 6.
Revision History and Instructions Manual GNS-X L Operator’s Manual Revision 1, July 1998 Part Number 006-08852-0000 This revision consists of the following: Add Company Routes (vi, 2-2, 3.36.1, 3-36.2, I-2) Add Dedicated DME Interface (2-57) Add Approach Note (3-36.
Revision History and Instructions Manual GNS-X L Operator’s Manual Revision 0, October 1996 Part Number 006- 08852-0000 This revision is a complete manual revision and supersedes previous revi- sion level manuals. Superseded manuals should be discarded.
SECTION 1 DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1-1 OVERVIEW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1-1 GENERAL TERMS .
FLIGHT PLAN LIST 1/1 (Page 1 of 1) . . . . . . . . . . . . . . . . . . . . . . . . . .2-2 FLIGHT PLAN “X” 1/1 (Page 1 of 1) . . . . . . . . . . . . . . . . . . . . . . . . . . .2-3 NAVIGATION SECTION (NAV KEY) . . . . . . . . . . . . . . . . . . .
VNAV MODE: (Second line) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2-32 VNAV 2/3 (Page 2 of 3) - FLIGHT PLAN WayPoint . . . . . . . . . . . . . . .2-37 VNAV DATA 1/1 (Page 1 of 1) . . . . . . . . . . . . . . . . . . . . . . . . . .
POSITION FIX PAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2-63 DIRECT TO SECTION ( d KEY) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2-64 DIRECT TO PAGES . . . . . . . . . . . . . . . . . .
CREATING A FLIGHT PLAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3-7 To Delete a Waypoint . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3-8 MODIFYING A FLIGHT PLAN . . . . . . . . . . . . . . .
EDITING AN AIRWAY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3-26 ENTERING A STAR OR PROFILE DESCENT ON ANY STORED FPL OR THE ACTIVE FPL PAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3-27 REVIEWING A STAR FROM A STORED FPL OR THE ACTIVE FPL PAGE .
To Select and Go Direct To HP Waypoint: . . . . . . . . . . . . . . . . . . . . . .3-52 To Cancel Holding Pattern:(from the Holding Pattern page) . . . . . . . .3-52 DIRECT TO - RANDOM WAYPOINT . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Using Active Flight Plan Page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3-75 Using VNAV Flight Plan Waypoints Page . . . . . . . . . . . . . . . . . . . . . . .3-76 VERTICAL NAVIGATION - ENROUTE . . . . . . . . . . . . . . . . . . .
To Enter Manual Groundspeed: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3-98 To Return to Automatic Groundspeed: . . . . . . . . . . . . . . . . . . . . . . . .3-98 To update the TRIP PLAN leg to the current TO waypoint with an Active Flight Plan selected: .
MANUAL HEADING ENTRY only if IRS or VLF is available . . . . . . . . . . .3-119 VLF/OMEGA STATION DESELECTION . . . . . . . . . . . . . . . . . . . . . . . . . .3-120 SENSOR DESELECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SECTION 6 LIST OF ABBREVIATIONS AND DEFINITIONS . . . . . . . . . . . . . . . . . . . . . . . . . . .6-1 SECTION 7 DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-1 Global Data Center (GDC) .
WINDS ALOFT Pages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-13 WINDS ALOFT Data Pages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-13 RECALL AFIS FPL Page . . . . . . . . . . . . . . .
Reviewing AFIS Planned Leg Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-28 Reviewing AFIS Flight Plan Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-29 AFIS Flight Plan Page 1 . . . . . . . . . . . . . . . . .
Turning AUTO WX UPDT OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-46 Returning to AUTO WX UPDT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-47 VHF and Satellite Network Operating Modes . . . . . . . . . . . . . .
Returning to AUTO WX UPDT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-63 Ground Network Operating Modes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7-64 AUTO to MAN or OFF Mode . . . . . . . . . . . . . . . . . . . . .
T able of Contents GNS-X L Flight Management System xvi Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
SECTION 1 DESCRIPTION O VER VIEW The GNS-X L Flight Management System is an integrated system designed to give the pilot centralized control for the navigation sen- sors, computer based flight planning, fuel management, and radio management.
characteristics of each type of sensor. For example, an Inertial Reference System (IRS) has excellent short term characteristics while VLF/Omega has excellent long term stability. The internal GPS sensor has excellent overall characteristics and will usually be the dominant sensor during blending.
course) to any waypoint and establishing an offset parallel course. NAVs, COMMs, ADFs and transponders can be tuned through the system or by using the individual control heads. GENERAL TERMS FIELD: A line of information. CURSOR: Yellow rectangular box placed over a field to enter or change the information in that field.
CONTROLS AND INDICA T ORS ON: Depress and release the ON Key to apply power to the sys- tem. There is a warm-up period of approximately 30 seconds. The display illumination will ini- tially be set at 75% of full bright. Depressing the ON Key for approximately three seconds will initiate the system power off sequence.
Depressing the MSG Key will display the message page. The newest message will be indicated with a flashing asterisk to the left of the message. If the message requires some action be taken by the operator, the MSG annunciator will remain on steadily until the action is completed.
BACK (BACK) KEY: The BACK Key is used to erase errors and page backward when the cursor is not dis- played. It can also be used to change data in a field if the cur- sor is present. SPACE (SP) KEY: The SP Key is used to enter a space when entering a mes- sage on an AFIS Page.
PREVIOUS (PRV) KEY: The PRV Key is used to display the previous page of a section or subsection. This key also allows the operator to remain in a section or subsection by loop- ing from the first to the last and back to the first page of that section or subsection.
Description 1-8 GNS-X L Flight Management System Magenta Lateral TO Waypoint and Vertical TO Waypoint, Yellow FROM Waypoint Caution Messages Data entered, but not yet accepted by the computer.
SECTION 2 P A GE DISPLA Y DEFINITIONS The following section contains definitions pertaining to information and format seen when a particular function key is depressed. P A GE DISPLA YS A T PO WER-UP For a better understanding of the GNS-X L functions, this section should be reviewed prior to operating the system.
IDENT: Displays the airport identifier for the airport closest to the system shut down position. Dashes will be displayed when the cursor is placed over the position (POS) field. POS: Displays the last system position at shut down. Dashes are dis- played when the cursor is over the IDENT field.
There are seven pages pos- sible with a maximum of 56 flight plans stored in non- volatile memory. Each stored flight plan's origin and destination points are listed in alphabetical order. (Figure 2-3) A new FLIGHT PLAN LIST Page is created when the previous page has eight flight plan origin-destination pairs on it.
• HP (Holding Pattern): Indicates a holding pattern is programmed at a particular waypoint. (Figure 2-5) • PT (Procedure Turn): Indicates a procedure turn is programmed at a particular waypoint. • ++++++: A flight plan dis- continuity "fence" separating the missed approach way- point from the rest of the approach (Figure 2-5).
APPROACH: Used to access the APPROACH Page to enter a non-precision approach. (Figure 2-5) XFILL: Used to transfer information between systems in a dual sys- tem installation. In a single system installation, this prompt will not be displayed. SELECT or INVERT: Used to transfer a Stored Flight Plan to the ACTIVE FLIGHT PLAN Page.
SID: The Standard Instrument Departure (SID) can be selected from a list made available by pressing the Line Select Key adjacent to the SID field. TRANSITION: The Transition waypoint can be selected from a list made available by pressing the Line Select Key adjacent to the TRANSITION field.
TRANSITION: The Transition waypoint may be prefilled or selected from a list made available by pressing the Line Select Key adjacent to the TRANSI- TION field. STAR: The Standard Terminal Arrival (STAR) can be selected from a list made available by pressing the Line Select Key adjacent to the STAR field.
RUNWAY: Approach runway prefills if only one runway is available, last waypoint on Flight Plan is a runway, or can be select- ed from a list made available by pressing the Line Select Key adjacent to the RUN- WAY field.
• FCF : Indicates Final Approach Course Alignment Fix. • ++++++: Separates the missed approach procedure waypoint from the rest of the approach. When the approach is flown, the system will continu.
ACTIVE FPL (Flight Plan)Page FR: Current FROM waypoint. May also display DIRECT, PSEUDO VORTAC, DME ARC, or PROCEDURE TURN. (Figure 2-13) TO: Current TO waypoint. (Figure 2-13) Waypoint Identifiers:Up to 100 waypoint identifiers may be placed on the Active Flight Plan Pages.
DEPART: Same as stored Flight Plan Page. ARRIVE: Same as stored Flight Plan Page. APPROACH: Same as stored Flight Plan Page. ETA: (ETE/DIS/ALT) Estimated Time of Arrival at each waypoint on the Active Flight Plan based on current groundspeed.
NOTE: No database altitude constraints will be displayed at the MAP if the MAP is abeam or beyond the runway threshold . No altitude constraints are displayed on an approach if a PT is part of the approach procedure.
NA VIGA TION SECTION (NA V KEY) Upon pressing the NAV Key the NAVIGATION 1/4 Page will be dis- played and the following can be observed. NAVIGATION PAGES NOTE: If AFIS is installed in the system, the NAV section will consist of five pages. NAVIGATION 1/4 (Page 1 of 4) FR : The FROM waypoint identifier is displayed on the left.
DIS: The distance in nautical miles and tenths from the aircraft present position to the TO waypoint. During Waypoint Alert, the distance in whole nautical miles to the NX way- point on the Active Flight Plan is displayed in parenthe- ses.
NOTE: XFILL will not appear when DME ARC, ARC Intercept, Procedure Turn or Holding Pattern are in progress on the system performing the procedure. AUTO: The leg change mode. AUTO or MAN, may be selected if the cursor is over this field using the BACK Key.
• HP (Holding Pattern): Indicates a holding pattern is programmed at the TO waypoint. • PT (Procedure Turn): Indicates a procedure turn is programmed from the database at the TO waypoint. The airplane will fly the procedure turn. The next time over the PT waypoint, the system will sequence to the following way- point on the flight plan.
DIS: The direct distance in nauti- cal miles and tenths from the aircraft present position to the holding fix. (Figure 2-21) ETE: The estimated time enroute to the next time over holding fix based on the path around the Hold “racetrack”. (Figure 2-21) INBOUND CRS (course): The inbound holding course in whole degrees.
WIND: The first field displays head- wind/tailwind in knots with an up arrow ( ↑ ) for tailwind or a down arrow ( ↓ ) for headwind. The second field displays the crosswind component in knots with a right pointing arrow ( → ) for a left cross- wind or a left pointing arrow ( ← ) for a right crosswind.
SXTK: The selected crosstrack distance entered by the pilot to provide steering to an offset course parallel to the desired track (99.9 NM maximum). (Figure 2-22) NAVIGATION 3/4 (Page 3 of 4) Pressing the NAV Key again will display the third NAVIGATION Page and the following can be observed.
HDG: The heading input received from an IRS or the aircraft compass sys- tem. If HDG can be manually inserted, MAN will be displayed. (Figure 2-23) BRG : The bearing in whole degrees from the aircraft present position to the TO waypoint. (Figure 2-23) TK: The track angle in whole degrees.
VLF SUBSECTION PAGES NOTE: The sensor SUBSECTION Pages may be accessed by plac- ing the cursor over the individual position sensor and pressing the ENT Key.
DR#: The number of times the VLF/Omega Sensor has been in DR since first enter- ing the VLF (primary) naviga- tion mode. This information is not displayed if the system has never been in DR. (Figure 2-26) DR TIME: The total number of minutes the VLF/Omega Sensor has been in DR since the operator last man- ually verified position.
VLF SUBSECTION 3/4 (Page 3 of 4) Pressing the NXT Key again will display the third VLF SUBSECTION Page and the following can be observed. Column 1: (Figure 2-27) VLF COMM Stations • WSH: Jim Creek, .
DESELECT: The station has been manually deselected. CUTOUT: The station has been eliminated from use because its position deter- mining information is unacceptable. UNSTABLE: The station has sufficient amplitude for use but has not passed the stability test.
IRS/INS SUBSECTION PAGES IRS (or INS) SUBSECTION 1/2 (Page 1 of 2) POS: The position in this field is the same as POS on NAVI- GATION 4/4. (Figure 2-29) IRS/INS: The actual position comput- ed by the specified sensor when in NAV mode.
VPU SUBSECTION PAGES Accessed through the NAVIGATION 4/4 Page (if AFIS is installed in the system, access is through the NAVIGATION 4/5 Page) by press- ing the Line Select Key corresponding to the VPU sensor, then pressing ENT . VPU SUBSECTION 1/4 (Page 1 of 4) POS: The position in this field is the same as POS on NAVI- GATION 4/4.
NOTE: Entering 99 in this field will eliminate any previously entered value and no CHECK QUALITY message will appear. CURRENT MODE: Indicates the current mode of VPU navigation. The messages that can appear under it: (Figure 2-32) • NO MEASUREMENTS indicates that VPU is not receiving valid data for navigation.
VPU with Multiple Channel DME Inputs (Figure 2-34) NAV 1: The stations received by the NAV 1 VOR/DME receivers. The station identifier is shown adjacent to the field with the ACTIVE frequency. RNG: Same as above. BRG: Same as above. CH 2: The station identifier and frequency for an additional station that the multiple channel DME is receiving.
GPS SUBSECTION PAGES Accessed through the NAVIGATION 4/4 Page (if AFIS is installed in the system, access is through the NAVIGATION 4/5 Page) by press- ing the Line Select Key corresponding to the GPS sensor, then pressing ENT. GPS SUBSECTION 1/3 (Page 1 of 3) See Figure 2-35.
GPS TIME: GPS time in hours, minutes and seconds. The advisory time is dis- played when at least one satellite is being tracked, other-wise the time field displays dashes. NOTE: GPS TIME may vary several seconds from GMT due to leap second input of UTC.
RAIM/FDE?: Indicates RAIM and/or FDE is AVAIL able or UNAVAIL able. SATS TRACKED: Indicates the number satellites presently being tracked. GPS SUBSECTION 3/3 (Page 3 of 3) Pressing the NXT Key again will display the third GPS SUBSECTION Page and the following can be observed.
VERTICAL NA VIGA TION SECTION (VNA V KEY) Upon pressing the VNAV Key the VNAV 1/3 Page will be displayed and the following can be observed. VNAV PAGES NOTE: AFIS flight plans do not support any altitudes, including air- port elevation. As a result no altitude constraints will be provided for SIDS, STARS or Approaches.
• CLIMB: Indicates climb required to cruise altitude or to next altitude restriction. (Figure 2-38) • CRUISE: Indicates holding altitude while enroute to Top of Descent (#TOD) point. (Figure 2-39) • PATH DESCENT: Indicates descent via programmed Flight Path Angle.
• #TOD: Indicates the Top of Descent target altitude where the aircraft should begin its descent in order to arrive at the Descent Reference Waypoint at the required altitude.
DATA: A prompt to access the VNAV DATA Page, by placing the cursor over the DATA field and pressing the ENT Key. (Figure 2-40) Figures 2-41 and 2-42 further illustrate the meanings of the fields on VNAV Page 1. Page Display Definitions 2-35 GNS-X L Flight Management System Rev.
Rev. 0 Page Display Definitions 2-36 GNS-X L Flight Management System Last Departure altitude constraint waypoint Groundspeed Vertical Speed #TOC Cruise Altitude =FL250 #TOC Range 1nm Top of Climb app.
VNAV 2/3 (Page 2 of 3) - FLIGHT PLAN WayPoint Pressing the VNAV Key will display the second VNAV Page and the following can be observed. VNAV MODE: Mode required to fly to the vertical TO waypoint and Baro Altitude in feet. Can display one of the following: • INVALID: Same as on VNAV 1/1.
• #PRESL: Indicates the estimated position where the aircraft will arrive at the altitude shown on the Altitude Pre-Selector. Field does not appear unless the system is configured for an altitude preselector and the aircraft is flying toward this altitude.
The field also goes to dashes during a descent (digital systems only) when the aircraft is 200ft lower than the CRUISE ALT and the Preselect is set to a lower value.
VNAV WAYPOINT 1/1 (Page 1 of 1) Accessed by placing the cursor over a lateral WPT and pressing the VNAV Key or by placing the cursor over a WPT in the VNAV section and pressing ENTER key. WAYPOINT: VNAV waypoint will consist of from one to six alphanumeric charac- ters.
PLAN CROSSING: System determined crossing based on programmed con- straints and flight path angles for descent. (Figure 2-48) This field is displayed for other than the Active Vertical Waypoint and will be dis- played in place of EST CROSSING.
• DEF: Indicates FPA default from VNAV DATA Page. NOTE: DIR, AUTO, and DEF can be accessed using the BACK Key. DIRECT FPA: Direct Flight Path Angle from the current aircraft altitude to the Vertical waypoint in degrees and tenths (valid range 0.0 to 90.
RESERVE: The desired reserve, as entered or verified by the operator, displayed in pounds or kilograms. This may require periodic verification or update. (Figure 2-50) FLOW: The current fuel flow in pounds or kilograms input automatically from fuel flow indicators.
NM/LB: The number of nautical miles for each pound (or kilogram) of fuel consumed. (Figure 2-50)Fuel flow and ground speed must be valid. PLAN 2/8 (Page 2 of 8) TRIP PLAN Pressing the PLAN Key again will display the PLAN 2/8 Page.
DIS/DTK: The distance in nautical miles and tenths between either the FROM and TO waypoints or between the aircraft's present position and the TO waypoint.
PLAN 3/8 (Page 3 of 8) FUEL PLAN Pressing the FPL Key again will display the PLAN 3/8 Page. FUEL PLAN: The "A" indicates that Active Flight Plan information is being displayed. A numeric entry in the field provides fuel planning for stored flight plans.
FPL FUEL: The total amount of fuel anticipated to be consumed to the last way- point on the flight plan that precedes a "fence". This calculated value is based on the current fuel flow, groundspeed values and distance. (Figure 2-53) REM @: Appears only if a DIRECT TO leg is displayed.
PLAN 5/8 (Page 5 of 8) DATE/GMT Pressing the PLAN Key again will display the PLAN 5/8 Page. DATE: Same as the Initialization Page. GMT: Same as the Initialization Page. NOTE: If necessary, both DATE and GMT can be corrected on this page but the takeoff and time values will be affected.
(excluding crew). (Figure 2-56) FUEL ON BOARD: Weight in pounds or kilograms of fuel on board. (Figure 2-56) VERIFY INPUTS: Each of the flashing values must be verified or entered by pressing the ENT Key when the cursor is over each field. This field is displayed only after system turn on.
DEPART DT : Date for which FDE prediction is to be calculated. DEPART GMT : Time for which FDE prediction is to be calculated. ROUTE SPACING : Centerline to centerline route spacing of segment for which FDE is being calculated. 1 to 99 nautical miles may be entered.
• START CALC? ENT : This is displayed when the aircraft is on the ground and all data has been entered. Pressing ENT will start the FDE calcu- lation and display PLAN 7/8 FDE COMPUTATION . See Figure 2-59 • NEED ACTIVE FPL : This will be displayed if there are less than two waypoints on the active flight plan.
PLAN 8/8 (Page 8 of 8) FDE COMPUTATION COMPUTING - STANDBY : This display will flash while FDE prediction is being cal- culated. See Figures 2-61 xx% COMPLETE : The number displayed is the percentage of calculation completed. When the FDE prediction is complete, the system will dis- play either FDE and NAV are available or unavailable.
HEADING SECTION (HDG KEY) Upon pressing the HDG Key the HEADING VECTOR 1/1 Page will be displayed and the following can be observed. HEADING PAGE HEADING VECTOR 1/1 (Page 1 of 1) HDG: Commanded heading in whole degrees. This field may also prefill with current aircraft heading if heading is valid.
TO WAYPOINT: Prefills with current TO Waypoint or is enterable (from one to six alphanumer- ic characters). (Figure 2-65) NOTE: With the cursor over the TO Waypoint field, using the BACK Key will step through to the end of the Active Flight Plan waypoints.
TUNING SECTION (TUNE KEY) Upon pressing the TUNE Key the TUNE 1/4 Page will be displayed and the following can be observed. TUNING PAGES TUNE 1/4 (Page 1 of 4) COMM NOTE: If the system is configured for two or less communications radios, the tune section will display only three pages.
TUNE 3/4 (Page 3 of 4) NAV Pressing the TUNE Key again will display this page and the following information may be observed. NAV 1 or NAV 2: The station identifier to which the respective NAV receiver is tuned. (KEY) will be displayed when the frequency or identifier of the station has been entered using the CDU keyboard.
When the dedicated DM441B or the dedicated DME42 is configured, the TUNE 3/4 page is different (Figure 2-67a). The Bearing information is suppressed and DME is annunciated instead of NAV. When the non-dedicated DM441B is configured, the TUNE 3/4 page is different (Figure 2-67b).
HOLDING P A TTERN SECTION (HOLD KEY) HOLDING PATTERN PAGE This page is accessed by depressing the HOLD Key when the cursor is positioned over a Waypoint Identifier. HOLDING PATTERN 1/1 (Page 1 of 1) AT: The Holding Fix and country name or airport ident.
Rev. 0 Page Display Definitions 2-59 GNS-X L Flight Management System 70 ° Outbound End Turn Point Holding Course Entry Course 70 ° Outbound End Turn Point Holding Course Entry Course Direct Entry P.
Rev. 0 Page Display Definitions 2-60 GNS-X L Flight Management System 70 ° Turn Anticipation Holding Course Leg Length 30 ° From Holding Course Direct to Holding Fix Entry Course 70 ° Holding Cours.
Rev. 0 Page Display Definitions 2-61 GNS-X L Flight Management System Go Direct to Holding Fix Leg Length Holding Course Entry Course 110 ° Note Path of 1st lap of holding pattern after entry procedu.
Page Display Definitions 2-62 GNS-X L Flight Management System • HOLDING: indicates the system has entered the Holding Pattern. (Figure 2-73) • EXIT HOLD: indicates the system will exit the holding pattern the next time over the holding fix. INBOUND CRS (course): The inbound holding course in whole degrees.
EXIT MODE: The MANUAL default indicates the system will stay in the holding pattern indefinitely. Using the BACK Key with the cursor over this field AUTO can be selected if the ENT key is pressed. The system will then execute a holding pattern entry and exit the next time cross- ing the fix waypoint.
Rev. 0 Page Display Definitions 2-64 GNS-X L Flight Management System DIF: The difference between the composite position and the FIX (or other sensor) position in degrees, minutes and hundredths of minutes.
DIR CLOSEST ARP 2/2 (Page 2 of 2) DIRECT TO CLOSEST AIR- PORT: The Closest Airport page is the last page in the DIRECT TO section. Up to nine airports are displayed, in order of their proximity to the aircraft, with the closest airport listed first.
VHF Navaids WAYPOINT: Alphanumeric designator for the Navaid. (Figure 2-77) NOTE: If the waypoint has a duplicate identifier in the database, for another loca- tion, the closest waypoint to the aircraft position will be shown and the country code will be displayed beneath the waypoint identifier.
Non-Directional Beacons (NDBs) NDBs stored in the internal database are listed in Jeppesen publications with a 2 or 3 letter identifier. To dis- tinguish these NDBs from VHF NAVAIDS, you must add an "NB" suffix to the database identifier. Example: To access the Prince Rupert (PR) NDB, you must enter PRNB.
Page Display Definitions 2-68 GNS-X L Flight Management System Rev. 0 Oct/96 • If the airport shows a 3 let- ter IDENTIFIER, add the cor- rect ICAO prefix letter. Example: NEW (New Orleans Lake Front) add a "K" prefix and enter KNEW (Figure 2-81).
Page Display Definitions 2-69 GNS-X L Flight Management System Rev. 0 Oct/96 Intersections/Enroute Waypoints Most intersection waypoint identifiers consist of 5 letters. However, 3, 4, and 5 letter and number combinations exist. To access these way- points, simply enter the iden- tifier from the Jeppesen chart.
Page Display Definitions 2-70 GNS-X L Flight Management System Rev. 0 Oct/96 WAYPOINT : (Figure 2-86). Same as pre- vious. POS: If the waypoint has been pre- viously defined, the coordi- nates of the waypoint will be displayed as stored in mem- ory. These coordinates may be changed at any time.
Page Display Definitions 2-71 GNS-X L Flight Management System Rev. 0 Oct/96 When the waypoint has been previously defined the coordinates will be displayed and the radial and distance values will be computed based on the location of the parent waypoint.
Page Display Definitions 2-72 GNS-X L Flight Management System Rev. 0 Oct/96 #0 will be defined as the point at which the aircraft completes the turn and intercepts the direct course to the fix. #0 will momentarily be dis- played on an EFIS map. #0 can only be defined by the system.
Page Display Definitions 2-73 GNS-X L Flight Management System Rev. 0 Oct/96 OBSOLETE WAYPOINT Obsolete Waypoints are typically created when a multiply defined database waypoint used on a stored flight plan is no longer found in the database. This may happen when a new data-base is loaded.
Page Display Definitions 2-74 GNS-X L Flight Management System Rev. 2 Apr/00 SYSTEM MESSAGES ACTION REQUIRED: The following are the action required messages that may appear on the SYSTEM MESSAGES Page. All will cause the message annun- ciator to flash.
Page Display Definitions 2-75 GNS-X L Flight Management System Rev. 0 Oct/96 ADVISORY: The following are the advisory messages that may appear on the SYSTEM MESSAGES Page. All will cause the message annuncia- tor to flash unless otherwise noted with an asterisk *.
ADVISORY: (continued) System Message Explanation DR HDG/TAS The system is in the Dead Reckoning (DR) DR TK/TAS Mode and is using one of these four combi- DR TK/GS nations of inputs to compute position. DR HDG/GS EXT WPT REJECT CDU has rejected an external waypoint input from a radar or EFIS.
ADVISORY: (continued) System Message Explanation NO NAV The system is not navigating. Message annunciator will not illuminate. POS WARN>1.7 NM Based on the signal strength or geometry, the VPU sensor quality may be such that the composite position may have more than 1.
ADVISORY: (continued) *WPT ALERT The aircraft is within 30 seconds ETE of the next leg lateral change. Message annuncia- tor will not illuminate. WPT MEM FULL All 999 waypoint locations have been used in flight plans or as FROM or TO waypoints. VNAV WPT ALERT Aircraft is within 1 minute ETE of #TOD or path intercept point.
SENSOR MESSAGES: (continued) Sensor Message Explanation DR Either the VLF (RPU), GPS or VPU sensor is in the Dead Reckoning (DR) mode of nav- igation. The message annunciator will not illuminate for VPU. ENTR SET HDG The IRS is in the attitude mode and a head- ing value must be entered.
Rev. 0 Oct/96 Page Display Definitions 2-80 GNS-X L Flight Management System THIS PAGE INTENTIONALLY LEFT BLANK.
SECTION 3 SYSTEM OPERA TION PRE-DEP ARTURE POWER ON/OFF AND PARALLAX ADJUSTMENT 1. ON Key - DEPRESS (momentarily). The SELF TEST Page (Figure 3-1) will be dis- played for approximately 30 seconds. During the time the SELF TEST message is displayed, the system is performing internal self tests.
INITIALIZATION PAGE It is important that the initial- ization position and the first waypoint of the Active Flight Plan are the same so that the TO/FROM Leg Distance displays the correct informa- tion. The DIRECT TO func- tion to the first waypoint on the flight plan may also be used to insure distance accuracy.
INITIALIZATION POSITION The Initialization Position for non-IRS equipped systems should be the departure runway threshold. For IRS equipped systems, the ramp or alignment LAT/LONG position should be inserted as Initialization Position.
of the departure runway threshold in the waypoint field, the departure air- port identifier will replace the ARP field, and POS coordinates will reflect selected runway thresh- old. (Figure 3-4) 4. ENT Key - DEPRESS. 5. POS Coordinates - VER- IFY coordinates high- lighted by the cursor on the Initialization Page.
Option 2: Using the POS field For IRS equipped systems, the ramp or alignment LAT/LONG posi- tion should be inserted as the Initialization Position using POS Coordinates. 1. Line Select Key - DEPRESS (cursor over POS field). 2. POS Coordinates - VERIFY.
System Operation 3-6 GNS-X L Flight Management System Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
BUILDING FLIGHT PLANS (FPL) CREATING A FLIGHT PLAN 1. FPL Key - DEPRESS to display (Stored) FLIGHT PLAN LIST Page (if required). 2. Line Select Key - DEPRESS to position cursor on blank line and display the NEXT FPL number.
System Operation 3-8 GNS-X L Flight Management System Rev. 0 Oct/96 7. ENT Key - DEPRESS to add waypoint to the FPL. 8. Repeat Steps 4 through 7 for the remaining waypoints. The des- tination airport identifier should be the last waypoint on the flight plan.
System Operation 3-9 GNS-X L Flight Management System Rev. 0 Oct/96 alphabetized FLIGHT PLAN LIST Page. Use the PRV or NXT Keys to cycle through the available pages. NOTE: A change made to the Active Flight Plan does not affect the Stored Flight Plan.
System Operation 3-10 GNS-X L Flight Management System Rev. 3 Oct/02 1 . Line Select Key - DE- PRESS to position the cur- sor over the waypoint iden- tifier that will follow the new entry. (Figure 3-11) 2. Type Waypoint Identifier - INSERT. (Figure 3-12) 3.
System Operation 3-11 GNS-X L Flight Management System Rev. 3 Oct/02 b. Longitude - Use only the last two digits of the first, three-digit longitude value.
System Operation 3-12 GNS-X L Flight Management System Rev. 3 Oct/02 To select an alternate waypoint location: 2. PRV or NXT Key - DEPRESS until desired country name is dis- played. (Figure 3-15) 3. ENT Key- DEPRESS to add the waypoint to the flight plan.
System Operation 3-12a GNS-X L Flight Management System Rev. 3 Oct/02 ERASING A STORED FLIGHT PLAN 1. FPL Key - DEPRESS to display desired FLIGHT PLAN LIST Page. 2. Line Select Key- DE-PRESS to position the cursor over the num- ber of the FPL to be erased.
System Operation 3-12b GNS-X L Flight Management System Rev. 3 Oct/02 THIS PAGE INTENTIONALLY LEFT BLANK.
FLIGHT PLAN (FPL) SELECTION This procedure is used to transfer a stored FPL to active FPL status. It is recommended that the initialization position and the first waypoint of the Active Flight Plan are the same so that the TO/FROM Leg Distance displays the correct information.
System Operation 3-14 GNS-X L Flight Management System Rev. 3 Oct/02 reversed to Active Flight Plan status, press the BACK Key to display INVERT?. (Figure 3-17) 6. ENT Key - DEPRESS. 7. ACTIVE FPL - CON- FIRM. Observe that the Stored Flight Plan trans- ferred to the ACTIVE FPL Page as SELECTED or INVERTED.
System Operation 3-15 GNS-X L Flight Management System Rev. 3 Oct/02 formed prior to departure. Refer to the Special Procedures section for instructions on performing the FDE prediction procedure.
System Operation 3-16 GNS-X L Flight Management System Rev. 3 Oct/02 3. MSG Key - DEPRESS to verify status of all sensors. Observe NAV RDY/NO NAV messages for appropriate sensor and refer to the Flight Manual Supplement for limitations. 4. HOLD Key - DEPRESS to verify departure coordinates.
System Operation 3-17 GNS-X L Flight Management System Rev. 4 Nov/04 point after the airport identifier or departure runway. After loading the SID on to the Active FPL, access NAV Pg 1. Enter the first waypoint after the runway or airport identifier in the FR field.
System Operation 3-17a GNS-X L Flight Management System Rev. 4 Nov/04 4. Select the FMS as the NAV source. 5. The FMS will fly the remainder of the SID to HQM .
System Operation 3-17b GNS-X L Flight Management System Rev. 4 Nov/04 Overfly then DIRECT TO Procedures For procedures that require over-flying a waypoint (Figure 3-21b), then a Direct To the next waypoint, follow these operational require- ments for the example following: 1.
System Operation 3-18 GNS-X L Flight Management System Rev. 4 Nov/04 The following procedures allow the pilot to automatically add way- points stored in the database, as part of a SID, STAR, APPROACH, or Enroute Airway, to either a Stored or Active Flight Plan.
System Operation 3-19 GNS-X L Flight Management System Rev. 4 Nov/04 3. ENT Key - DEPRESS to display DEPARTURE Page. 4. DEPARTURE Airport Identifier - VERIFY or INSERT valid ident. NOTE: I f the first waypoint on the Flight Plan is an airport, the Departure ident prefills and the cursor is positioned over the first SID identifier on the list.
System Operation 3-20 GNS-X L Flight Management System Rev. 4 Nov/04 the first runway on the RUN- WAY identifier list and RUN- WAY field is highlighted in yellow. See Figure 3-25. If runway is not required, pro- ceed to Step 11. 9 . Line Select Key - DEPRESS to position cursor over the desired runway.
System Operation 3-21 GNS-X L Flight Management System Rev. 4 Nov/04 NOTE: SELECT will not appear as an option since a SID already exists in the Flight Plan. EDITING A SID FROM ANY STORED FPL OR THE ACTIVE FPL PAGE 1 . Line Select Key - DEPRESS to position cursor over the DEPART field on the FLIGHT PLAN Page.
System Operation 3-22 GNS-X L Flight Management System Rev. 0 Oct/96 6. ENT Key - DEPRESS to select desired TRANSI- TION. The system will automatically load the compatible SID associat- ed with the selected TRANSITION. (Figure 3- 31) 7. ENT Key - DEPRESS to select a new SID and insert the new SID into the flight plan.
System Operation 3-23 GNS-X L Flight Management System Rev. 0 Oct/96 ADDING OR DELETING WAYPOINTS WITHIN A SID NOTE: When a SID is modified by adding or deleting waypoints, the sequence of waypoints is no longer identified as a SID. To Add a Waypoint 1.
System Operation 3-24 GNS-X L Flight Management System Rev. 0 Oct/96 ENT ER ING AN AIRWAY FROM ANY STORED FPL OR THE ACTIVE FPL PAGE Enroute Airways include high altitude jet routes and low altitude and colored airways.
System Operation 3-25 GNS-X L Flight Management System Rev. 0 Oct/96 c. Line Select Key - DEPRESS to position cursor over the desired destination waypoint.
System Operation 3-26 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: If the waypoint above the cursor is not a waypoint on the selected airway, the airway identifier will blink and the appropriate air- way or waypoint identifier must be entered.
System Operation 3-27 GNS-X L Flight Management System Rev. 0 Oct/96 3. ENT Key - DEPRESS. (Figure 3-42) 4. Line Select Key - DEPRESS to move the cursor to shorten or lengthen the previously selected segment of the airway. If applicable, use PRV and NXT Keys to access all airway way- point pages.
System Operation 3-28 GNS-X L Flight Management System Rev. 0 Oct/96 If there are no STARs associated with the Arrival Airport, the mes- sage “ NO STARS AVAILABLE” appears and the arrival airport ident field flashes. Depress FPL Key to return to ACTIVE FLIGHT PLAN.
System Operation 3-29 GNS-X L Flight Management System Rev. 0 Oct/96 11. Arrival STAR Waypoints - REVIEW (Figure 3-47), then DEPRESS ENT Key to insert STAR into Active Flight Plan and return to the ACTIVE FLIGHT PLAN Page. NOTE: Look carefully at the flight plan to see if any way- points are out of sequence.
System Operation 3-30 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: A list will appear with other available STARs. 4. Line Select Key - DEPRESS to position cursor over the desired STAR. 5. ENT Key - DEPRESS to select desired STAR. NOTE: Cursor moves to the first waypoint of the TRANSITION list and the TRANSITION field is displayed in yellow.
System Operation 3-31 GNS-X L Flight Management System Rev. 0 Oct/96 ADDING WAYPOINTS WITHIN A STAR NOTE: When a STAR is modified by adding or deleting waypoints, the sequence of waypoints is no longer identified as a STAR. The following may be accomplished from any stored flight plan or the ACTIVE FPL Page.
System Operation 3-32 GNS-X L Flight Management System Rev. 0 Oct/96 ENT ER ING AN APPROACH ON A STORED FPL OR THE ACTIVE FPL PAGE 1. Line Select Key - DEPRESS to position cur- sor over APPROACH? field on the ACTIVE FPL page. (Figure 3-52) 2. ENT Key - DEPRESS to display APPROACH Page.
System Operation 3-33 GNS-X L Flight Management System Rev. 0 Oct/96 7. ENT Key - DEPRESS to select Approach TYPE . (Figure 3-55) NOTE: If there is only one type of approach available the system automatically loads the approach TYPE and the cursor moves over the WPT in the transition list.
System Operation 3-34 GNS-X L Flight Management System Rev. 0 Oct/96 10. Approach Waypoints - REVIEW (Figure 3-57), then DEPRESS ENT Key to insert APPROACH into Active Flight Plan and return to the ACTIVE FLIGHT PLAN Page. REVIEWING AN APPRO A CH FROM A ST ORED FPL OR THE A CTIVE FPL P A GE 1.
System Operation 3-35 GNS-X L Flight Management System Rev. 0 Oct/96 1. Line Select Key (adjacent to RUNWAY field) - DEPRESS to change the field to dashes. 2. Line Select Key (adjacent to TYPE and TRANSITION fields) - DEPRESS to change the field to dashes.
System Operation 3-36 GNS-X L Flight Management System Rev. 0 Oct/96 DELETING AN APPROACH WAYPOINT 1. Display the appropriate FPL Page. 2. Line Select Key - DEPRESS to position cursor over the APPROACH waypoint identifier to be deleted. 3. BACK Key - DEPRESS.
System Operation 3-36.1 GNS-X L Flight Management System Rev. 2 Apr/00 SELECTING A COMPANY ROUTE AND ADDING IT TO THE ACTIVE FLIGHT PLAN 1. Display the COMPANY ROUTES Page (automatically after ini- tialization, or by paging the FPL pages).
System Operation 3-36.2 GNS-X L Flight Management System Rev. 2 Apr/00 NOTE: If the pair is not valid, the COMPANY ROUTES page will remain, and a ROUTE NOT FOUND message will be displayed. (Figure 3-59d) If the route is valid, but the Active FPL is full, an ACTIVE FPL FULL message is displayed.
System Operation 3-36.3 GNS-X L Flight Management System Rev. 1 Jul/98 Note: In order to execute approaches with a specific aircraft installa- tion, the installation must meet the standards set forth by the govern- ing certification agency. Consult the Aircraft Flight Manual Supplement for specific limitations.
System Operation 3-37 GNS-X L Flight Management System Rev. 1 Jul/98 EXECUTING APPRO A CHES WARNING: When entering PTs or HP airspace at high speed the FMS may not constrain the airplane from violating maneuvering airspace. Pilots are responsible for procedural compliance.
System Operation 3-38 GNS-X L Flight Management System Rev. 0 Oct/96 At the MAP the pilot must manually or via the HDG Mode maneuver the aircraft to the Missed Approach Procedure waypoint.
System Operation 3-39 GNS-X L Flight Management System Rev. 0 Oct/96 12. Approach Waypoints - REVIEW. 13. ENT Key - DEPRESS ACTIVE FPL Page is displayed. VERIFY the approach appears as selected. 14. Waypoint Sequencing - Edit, if required, based on assigned route.
System Operation 3-40 GNS-X L Flight Management System Rev. 1 Jul/98 8. ENT Key - DEPRESS twice to engage Heading Select mode. (Figure 3- 64) After receiving the final intercept vector from ATC: 9. HDG Key - DEPRESS to display the HEADING VECTOR Page.
System Operation 3-41 GNS-X L Flight Management System Rev. 1 Jul/98 USING OWN NAVIGATION - NO DME ARC 1. FPL Key - DEPRESS to display the ACTIVE FPL Page.
System Operation 3-42 GNS-X L Flight Management System Rev. 1 Jul/98 NOTE: When flying the approach on a transition that specifies NoPT and a “PT” waypoint is depicted on the flight plan, it will be necessary to do a DIRECT TO the next waypoint beyond the “PT” waypoint to avoid flying the Procedure Turn.
System Operation 3-43 GNS-X L Flight Management System Rev. 1 Jul/98 Figure 3-70 PROCEDURE TURN TO INTCPT ----- NX LEFT INTRCPT 125 DIS (5.2) 6.3 ETE 00:02.5 INBOUND CRS 125 GS 150 WIND ---/--- NAVIGATION 1/4 < > > > Figure 3-71 PROCEDURE TURN TO INTCPT ----- NX LEFT INTCPT 125 DIS (2.
System Operation 3-44 GNS-X L Flight Management System Rev. 1 Jul/98 NOTE: If aircraft is configured for dual systems no XFILL? prompt will be displayed during a PT even if dissimilar data exists in each system.
System Operation 3-45 GNS-X L Flight Management System Rev. 1 Jul/98 6. HDG Key - DEPRESS to display the HEADING VECTOR Page. (Figure 3-75) 7. Heading - INSERT as assigned by ATC. 8. ENT Key - DEPRESS twice to engage HDG SELECT mode. After receiving ARC inter- cept vector from ATC: 9.
System Operation 3-46 GNS-X L Flight Management System Rev. 1 Jul/98 USING OWN NAVIGATION TO FLY DME ARC 1. FPL Key - DEPRESS to display the ACTIVE FPL Page.
System Operation 3-47 GNS-X L Flight Management System Rev. 1 Jul/98 As the aircraft approaches the AR waypoint, a message is displayed on the fourth line of the CDU indicating the next action the aircraft will take (NX DME ARC) . This message is displayed thirty seconds prior to the event and disappears when the action is initiated.
System Operation 3-48 GNS-X L Flight Management System Rev. 1 Jul/98 Use one of the following options to sequence to the missed approach waypoint. OPTION 1, Direct To the Missed Approach Procedure waypoint 1. d Key - DEPRESS. The DIRECT Page will be displayed.
System Operation 3-49 GNS-X L Flight Management System Rev. 1 Jul/98 4. ENT Key - DEPRESS. The cursor moves to the TO field. (Figure 3-85) 5. BACK Key - DEPRESS until the Missed Approach Procedure waypoint is dis- played. 6. ENT Key - DEPRESS. The cursor moves to the DTK field.
System Operation 3-50 GNS-X L Flight Management System Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
System Operation 3-51 GNS-X L Flight Management System Rev. 0 Oct/96 ENROUTE DIRECT TO - ACTIVE FLIGHT PLAN WAYPOINT d function enables the pilot to fly direct to any lateral waypoint on the Active Flight Plan without reinserting the waypoint identifier.
System Operation 3-52 GNS-X L Flight Management System Rev. 0 Oct/96 DIRECT TO - HP WAYPOINT 1. d d Key - DEPRESS. A DIRECT TO Page appears with the cursor over the current TO waypoint. 2. Line Select Key - DEPRESS to position the cursor over the desired HP identifier.
System Operation 3-53 GNS-X L Flight Management System Rev. 0 Oct/96 DIRECT TO - RANDOM WAYPOINT This procedure enables the pilot to add a random waypoint to the ACTIVE FLIGHT PLAN in the desired sequence and proceed direct to it. 1. d d Key - DEPRESS.
System Operation 3-54 GNS-X L Flight Management System Rev. 0 Oct/96 A. Latitude - Insert N or S first, then degrees, minutes, and hun- dredths (6 characters) B.
System Operation 3-55 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: The bearing and distance values to the closest airports are based on the aircraft’s present position at the time this page is accessed. The values are not updated while the page is being dis- played.
System Operation 3-56 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: The d function may also be used to initiate a Pseudo- VORTAC. Following the Direct To entry using the d Key the dis- play automatically advances to NAVIGATION Page 1. Manually position the cursor over DTK field and continue as described above in Steps 5 and 6.
System Operation 3-57 GNS-X L Flight Management System Rev. 1 Jul/98 USING HEADING VECT OR This procedure enables the pilot to program and fly a specific head- ing vector as well as program an automatic intercept of a specified leg. PROGRAMMING A HEADING VECTOR 1.
System Operation 3-58 GNS-X L Flight Management System Rev. 1 Jul/98 CHANGING HEADING VECTOR WHILE IN HEADING SELECT MODE 1. HDG Key - DEPRESS to display HEADING VECTOR Page with cursor over the HDG field. 2. Heading - INSERT desired Heading. 3. ENT Key - DEPRESS.
System Operation 3-59 GNS-X L Flight Management System Rev. 1 Jul/98 6. ENT Key - DEPRESS. OK? ENT message appears. (Figure 3-100) 7. ENT Key - DEPRESS to select TO Waypoint and return to NAVIGATION Page 1. The cursor may be positioned over the Leg Change Mode field.
System Operation 3-60 GNS-X L Flight Management System Rev. 1 Jul/98 3. ENT Key - DEPRESS. The cursor advances to Heading Mode field. 4. BACK Key - DEPRESS to select INTERCEPT? (Figure 3-101) 5. ENT Key - DEPRESS. Cursor moves to the TO Waypoint field.
System Operation 3-61 GNS-X L Flight Management System Rev. 1 Jul/98 9. ENT Key - DEPRESS. An Intercept Message may appear (NO COURSE INTERCEPT, NO ARC INTERCEPT, or INTER - CEPT BEYOND FIX (Figure 3-103). If no mes- sage appears the intercept will occur on the TO side of the selected TO waypoint.
System Operation 3-62 GNS-X L Flight Management System Rev. 1 Jul/98 4. BACK Key - DEPRESS to display the INTERCEPT? prompt. (Figure 3-105) 5. ENT Key - DEPRESS. The cursor moves to the TO field. 6. BACK Key - DEPRESS until the FAF waypoint is displayed.
System Operation 3-63 GNS-X L Flight Management System Rev. 0 Oct/96 PROGRAMMING A HOLDING P A TTERN WARNING: When entering PTs or HP airspace the FMS may not constrain the airplane from violating maneuvering airspace. Pilots are responsible for procedural compliance.
System Operation 3-64 GNS-X L Flight Management System Rev. 0 Oct/96 When a Holding Procedure is initiated, the inbound course is dis - played on NAVIGATION Page 1. If the CDI needle does not auto- matically slew to the inbound course, manually set the CDI needle to the inbound course so that the course needle sensing is correct.
System Operation 3-65 GNS-X L Flight Management System Rev. 0 Oct/96 Selecting Exit Mode: 10. Line Select Key - DE- PRESS to position the cursor over MANUAL or AUTO. Press the BACK key to change exit mode option. Selecting MANU- AL will initiate a continu- ous hold.
System Operation 3-66 GNS-X L Flight Management System Rev. 0 Oct/96 EDITING 5. Line Select Key - DEPRESS to position cursor over desired field. a. INSERT value for I NBOUND CRS, LEG TIME, or LEG DIST or b. BACK Key - DEPRESS to change TURN DIR or EXIT MODE.
System Operation 3-67 GNS-X L Flight Management System Rev. 0 Oct/96 EXITING HOLDING PATTERN NEXT TIME OVER HOLDING FIX 1. NAV Key - DEPRESS to display NAVIGATION Page 1, 2 or 3. 2. Line Select Key - DEPRESS to position the cursor over MANU- AL. (Figure 3-112) 3.
System Operation 3-68 GNS-X L Flight Management System Rev. 0 Oct/96 EXITING HOLDING PATTERN BY GOING DIRECT TO HOLDING FIX 1. d Key - DEPRESS to display Direct To Page with cursor over current HP Waypoint. (Figure 3- 115) 2. ENT Key - DEPRESS to display HOLDING PAT- TERN Page with cursor over CANCEL?.
System Operation 3-69 GNS-X L Flight Management System Rev. 0 Oct/96 4. ENT Key - DEPRESS. The next waypoint in the Active Flight Plan sequence will appear in the TO field. (Figure 3- 118) 5. TO Waypoint - VERIFY. To change the TO Waypoint, insert the desired identifier.
System Operation 3-70 GNS-X L Flight Management System Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
System Operation 3-71 GNS-X L Flight Management System Rev. 0 Oct/96 VERTICAL NA VIGA TION (VNA V) OPERA TION - PRE- DEP AR TURE SETTING CRUISE ALTITUDE, TRANSITION LEVEL, AND DEFAULT FLIGHT PATH ANGLE This procedure allows the pilot to define a Cruise Altitude and change the default values for Transition Level and Flight Path Angle.
System Operation 3-72 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: CRUISE ALT may also be inserted on VNAV Page 1, line 3 (adjacent to the TO waypoint field) when #TOC or #TOD are the TO waypoint.
System Operation 3-73 GNS-X L Flight Management System Rev. 0 Oct/96 After initial leg selection on NAV page 1: 1. NAV, FPL, or d Key - DEPRESS to display applicable page. 2. Line Select Key - DEPRESS to position cursor over desired way- point. NOTE: On NAVIGATION Pages, only the TO Waypoint can be selected.
System Operation 3-74 GNS-X L Flight Management System Rev. 0 Oct/96 b. Enter a (+), then the range value to indicate the off set is beyond the waypoint. c. To erase the offset value, INSERT 0 and press ENT Key. The field changes to dashes, indicating no offset is programmed.
System Operation 3-75 GNS-X L Flight Management System Rev. 3 Oct/02 9. ENT Key - DEPRESS to load or verify the FPA value. NOTE: W hen a descent FPA is programmed at a waypoint, a G appears next to the altitude constraint indicating a Glide Path and ver- tical deviation guidance and information will be available.
System Operation 3-76 GNS-X L Flight Management System Rev. 0 Oct/96 6 . Repeat Steps 2 through 5 to review VNAV waypoint data at remaining waypoints. Using VNAV Flight Plan Waypoints Page 1. VNAV Key - DEPRESS to display the VNAV FLIGHT PLAN WAYPOINTS Pages.
System Operation 3-77 GNS-X L Flight Management System Rev. 0 Oct/96 Using Database (DB) FPA The GNS-X L database contains Flight Path Angles associated with waypoints on SIDs, STARs, and Approaches, that prefill when these procedures are programmed into the Active Flight Plan.
3-78 GNS-X L Flight Management System Rev. 0 Oct/96 Using Automatic (AUTO) FPA The (AUTO) mode is pro- vided to link together descent waypoints that have Cross-At type con- straints and provide a com- puted Flight Path Angle between them.
3-79 GNS-X L Flight Management System Rev. 0 Oct/96 EDITING ALTITUDE CONSTRAINTS The following pages allow the pilot to edit altitude constraints for way- points on the VNAV WAYPOINT Page, VNAV pages, referred to as VNAV FPL Pages. One of the three following options may be used: OPTION 1: Using the VNAV Page.
System Operation 3-80 GNS-X L Flight Management System Rev. 0 Oct/96 3. Altitude Constraint - INSERT new altitude constraint followed by A (at or above) or B (at or below), if applicable.
System Operation 3-81 GNS-X L Flight Management System Rev. 0 Oct/96 DIRECT TO - VNAV WAYPOINT AS LATERAL WAYPOINT This procedure enables the pilot to proceed Direct To a waypoint, both vertically and laterally by means of a Vertical Path Descent. If the current To waypoint is the desired VNAV Direct To waypoint, go to Step 4.
System Operation 3-82 GNS-X L Flight Management System Rev. 0 Oct/96 5. VNAV Key - DEPRESS to display the VNAV WAYPOINT Page for TO Waypoint. 6. ALT - INSERT or VERIFY. If an altitude constraint has already been programmed, the cursor will be displayed over the FPA (DIR) field value.
System Operation 3-83 GNS-X L Flight Management System Rev. 0 Oct/96 11. ENT Key - DEPRESS to accept waypoint entries. VNAV Page 1 is displayed, a Vertical Path Descent has been established, and Vertical Deviation information and guidance is enabled if a descent has been programmed.
System Operation 3-84 GNS-X L Flight Management System Rev. 0 Oct/96 5. ENT Key - DEPRESS. Cursor moves to OFFSET field. 6. OFFSET - If applicable, INSERT value in nautical miles (-99 to +99 range). a. If the offset is prior to the waypoint, enter the range value and a (-) prefills as a default or b.
System Operation 3-85 GNS-X L Flight Management System Rev. 0 Oct/96 When #TOC is the TO Waypoint: The pilot may obtain range and ETE to any altitude above the aircraft during a climb. 1. VNAV Key - DEPRESS to display VNAV Page 1. 2. Line Select Key - DEPRESS to position the cursor over the #TOC altitude field.
System Operation 3-86 GNS-X L Flight Management System Rev. 0 Oct/96 One minute prior to arriving at #TOD, the system issues the VNAV WPT ALERT message and the discrete waypoint light will flash for 10 seconds, then go steady.
System Operation 3-87 GNS-X L Flight Management System Rev. 0 Oct/96 Figure 3-141 #TOD 8000 FUELR Descent Reference Wpt 126 KLAX Cruise Altitude FL210 Vertical Constraint FL180B 16500 PLAN CROSSING Programmed FPA 3.0 CIVET 14000A Vertical Constraint As shown, FUELR is the Descent Reference Waypoint that establishes #TOD.
System Operation 3-88 GNS-X L Flight Management System Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
System Operation 3-89 GNS-X L Flight Management System Rev. 0 Oct/96 REMO TE TUNING TUNING COMMS This procedure enables the pilot to keyboard tune the aircraft radios via the CDU. Some control heads may require placement in the Remote Mode in order to accept tuning data from the CDU keyboard.
System Operation 3-90 GNS-X L Flight Management System Rev. 0 Oct/96 The PRESET frequency displayed on the control head is not neces - sarily the PRESET frequency displayed on the CDU. Each may be entered independently. Depending on the system configuration the cursor can appear over the PRESET field for either COMM 1 or COMM 2.
System Operation 3-91 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: NAV tuning is designed to enhance the VPU (VORTAC Position Unit). The VPU will only use VOR/DME or DME only navaids (includes TACAN and ILS) therefore, only VOR/DME or DME only navaids will be displayed.
System Operation 3-92 GNS-X L Flight Management System Rev. 0 Oct/96 When the station is locat- ed in the VPU database the identifier will be dis- played and the (KEY) annunciation will shift to the identifier line. (Figure 3-148) 6. RANGE and BRG - CHECK.
System Operation 3-93 GNS-X L Flight Management System Rev. 0 Oct/96 will change to reflect the Identifier chosen by the system. (Figure 3-151) NOTE: No prompt is dis- played adjacent to the IDENT field when system is in AUTO TUNE mode.
System Operation 3-94 GNS-X L Flight Management System Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
System Operation 3-95 GNS-X L Flight Management System Rev. 0 Oct/96 PLANNING PROCEDURES FUEL PLANNING 1. PLAN Key - DEPRESS to display FUEL STATUS Page. NOTE: REMAINING and RESERVE quantities are stored in non- volatile memory after system shutdown. Upon system turn-on, VERIFY INPUTS is displayed and REMAINING, RESERVE, and FLOW values will flash.
System Operation 3-96 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: HOURS of fuel and RANGE are calculated to the RESERVE fuel, not “0” fuel, unless the RESERVE fuel is “0”. To change the unit of measurement (LB or KG) : a. Line Select Key - DEPRESS to position the cursor over the REMAINING field.
System Operation 3-97 GNS-X L Flight Management System Rev. 0 Oct/96 2. Line Select Key - DEPRESS to position the cursor over the TRIP PLAN field. 3. Desired Flight Plan - INSERT Flight Plan Number (Figure 3-157) or “A” for Active Flight Plan. (Figure 3-158).
System Operation 3-98 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: With TRIP PLAN A selected, the TRIP PLAN leg will automatically advance to display DIRECT TO the cur- rent NAVIGATION Page TO Waypoint each time the TRIP PLAN Page is accessed.
System Operation 3-99 GNS-X L Flight Management System Rev. 0 Oct/96 10. Data - CHECK. When DIRECT is displayed all data except DTK is updated continuously. If data is not continuously updated, it will be recalculated each time: a. The TRIP PLAN Page is selected.
System Operation 3- 100 GNS-X L Flight Management System Rev. 0 Oct/96 To update the TRIP PLAN leg to the current TO waypoint with an Active Flight Plan selected: a. Line Select Key - DEPRESS to position cursor over TRIP PLAN field. b. ENT the letter [A] in the cursor.
System Operation 3- 101 GNS-X L Flight Management System Rev. 0 Oct/96 3. Desired Flight Plan - INSERT Flight Plan Number (Figure 3-165) or “A” for Active Flight Plan. 4. ENT Key - DEPRESS. NOTE: If a flight plan num- ber is left in the Fuel Plan field and not returned to “A” , no updated Active Flight Plan information will appear.
System Operation 3- 102 GNS-X L Flight Management System Rev. 0 Oct/96 To Enter Manual Groundspeed: a. Line Select Key - DEPRESS to position cursor over GS value field. b. Groundspeed - INSERT. c. ENT Key - DEPRESS. (MAN) will appear adjacent to the GS field.
System Operation 3- 103 GNS-X L Flight Management System Rev. 0 Oct/96 b. The FUEL PLAN Page is selected. c. Leg or GS change is made on the FUEL PLAN Page. LEG FUEL and FPL FUEL are recalculated whenever the FLOW changes. d. FUEL FLOW is changed on FUEL STATUS Page.
System Operation 3- 104 GNS-X L Flight Management System Rev. 0 Oct/96 Selecting another display page (other than MSG and TRIP PLAN ) and returning to FUEL PLAN Page also updates the leg with DIRECT TO the current NAVIGATION Page TO waypoint.
System Operation 3- 105 GNS-X L Flight Management System Rev. 1 Jul/98 VERIFYING OR CHANGING AIRCRAFT WEIGHT PARAMETERS This procedure allows the pilot to confirm or adjust basic operating weight, payload, or fuel to current on board data.
System Operation 3- 106 GNS-X L Flight Management System Rev. 1 Jul/98 RESETTING FUEL USED 1. PLAN Key - DEPRESS to display aircraft weight page. 2. Line Select Key - DEPRESS to place the cursor over FUEL USED .
System Operation 3- 107 GNS-X L Flight Management System Rev. 0 Oct/96 SPECIAL PROCEDURES The following are various procedures that can be performed during navigation, when applicable. PILOT ENTED LEG CHANGE 1. NAV Key - DEPRESS to select NAVIGATION Page 1.
System Operation 3- 108 GNS-X L Flight Management System Rev. 0 Oct/96 If Waypoint Page Appears: a. Waypoint Page Co- ordinates - VERIFY Database Waypoint or INSERT Waypoint Data. (Figure 3-174) To Insert Waypoint Coordinates (cursor over POS Field): (1) Latitude - IN- SERT (N or S first, then de- grees, minutes, and hundredths).
System Operation 3- 109 GNS-X L Flight Management System Rev. 0 Oct/96 PREVENTING AUTOMATIC LEG CHANGES The Auto Leg change function allows the system to automatically sequence from waypoint to waypoint on the Active Flight Plan. When the system is initialized it is in the Automatic Leg Change Mode unless changed by the pilot.
System Operation 3- 110 GNS-X L Flight Management System Rev. 2 Apr/00 DEAD RECKONING (DR) TO PRIMARY NAVIGATION MODE - VLF (RPU) ONLY EQUIPPED NOTE: System automatically reverts to the Primary Navigation Mode 30 seconds after the NAV RDY-VERIFY POSITION message appears.
System Operation 3- 111 GNS-X L Flight Management System Rev. 0 Oct/96 Over Known Point This procedure is used to cross check or update the system by over- flying a known reference point such as a radio navaid or visual check point. 1. HOLD Key - DEPRESS over known point.
System Operation 3- 112 GNS-X L Flight Management System Rev. 0 Oct/96 b. Latitude - INSERT (N or S first, then degrees, minutes, and hundredths). c. ENT Key - DEPRESS. d. Longitude - INSERT (E or W first, then degrees, minutes, and hundredths). e. ENT Key - DEPRESS.
System Operation 3- 113 GNS-X L Flight Management System Rev. 0 Oct/96 4. Recorded Radial - INSERT. 5. ENT Key - DEPRESS. 6. Recorded Distance - INSERT (NM and tenths). 7. ENT Key - DEPRESS. 8. Waypoint Coordinates - VERIFY for reasonabili- ty. (Figure 3-181) 9.
System Operation 3- 114 GNS-X L Flight Management System Rev. 0 Oct/96 PARALLEL COURSE This procedure is used to establish an offset course (steering refer- ence) parallel to the current leg. This field is inactive when in APPROACH ARMED mode (within 30 nm of the destination airport).
System Operation 3- 115 GNS-X L Flight Management System Rev. 0 Oct/96 MANUAL MAGNETIC VARIATION ENTRY A manual magnetic variation entry is required north of 70° N latitude and south of 60°S latitude. 1. NAV Key - DEPRESS to display NAVIGATION 3/4 Page with VAR.
System Operation 3- 116 GNS-X L Flight Management System Rev. 0 Oct/96 4. ENT Key - DEPRESS to select option. (Figure 3-185) NOTE: To display numbers when the DIS option is selected, a Flight Plan must be selected and a leg defined. To display numbers when the ETE or ETA option is selected, a valid ground speed is required.
System Operation 3- 117 GNS-X L Flight Management System Rev. 0 Oct/96 To Return to ETA: 5. Line Select Key - DEPRESS to position the cursor over the alti- tude constraint field. 6. BACK Key - DEPRESS. ETA? appears in cursor. 7. ENT Key - DEPRESS to display ETA.
System Operation 3- 118 GNS-X L Flight Management System Rev. 0 Oct/96 Position Update: A position update must be performed to give the system an accurate starting position. An update may be accomplished over a known point or by using an offset. If necessary, refer to the procedure for Position Check and Update.
System Operation 3- 119 GNS-X L Flight Management System Rev. 0 Oct/96 To Enter Manual TAS: 1. NAV Key - DEPRESS to display page with TAS. 2. Line Select Key - DEPRESS to place the cursor over TAS field. 3. TAS - INSERT in knots. 4. ENT Key - DEPRESS.
System Operation 3- 120 GNS-X L Flight Management System Rev. 0 Oct/96 VLF/OMEGA STATION DESELECTION The following procedure allows a VLF Communication or Omega sta- tion to be removed from an RPU’s navigation solution.
System Operation 3- 121 GNS-X L Flight Management System Rev. 0 Oct/96 b. BACK Key - DEPRESS. RESTORE? will appear to inform the pilot of the pending change.
System Operation 3- 122 GNS-X L Flight Management System Rev. 0 Oct/96 contributes to GPS accuracy by providing GPS with velocity aiding. It will always be displayed in green. EXTERNAL WAYPOINT ACCEPTANCE Up to 99 external waypoints may be accepted from an interfaced radar or EFIS system.
System Operation 3- 123 GNS-X L Flight Management System Rev. 0 Oct/96 4. ENT Key - DEPRESS. NOTE: The EX# waypoint identifier will flash if an unassigned num- ber is entered. EX# waypoint coordinates can ONLY be assigned by an external source (radar or EFIS).
System Operation 3- 124 GNS-X L Flight Management System Rev. 0 Oct/96 NAVIGATION AT EXTREME LATITUDES (North of 70° N or South of 60° S) CAUTION: THE PROCEDURES LISTED IN THIS SECTION CON- TAIN INSTRUCTIONS FOR OPERATION OF THE GNS-Xl AT SPECIFIED LATITUDES BEYOND THE AUTO-COMPUTED MAG- NETIC VARIATION MODEL.
System Operation 3- 125 GNS-X L Flight Management System Rev. 0 Oct/96 Aircraft Not Equipped With A TRUE/MAG Switch NOTE: This procedure must be accompanied by the input of TRUE heading into the system. 1. NAV Key - DEPRESS until NAVIGATION Page 3 appears.
System Operation 3- 126 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: In some cases, (MAN) will appear in the HDG field and the SYSTEM MESSAGES Page will display USING MAN HDG mes- sage.
System Operation 3- 127 GNS-X L Flight Management System Rev. 0 Oct/96 8. BACK Key - DEPRESS to return to HOLD Page. NOTE: An Offset Waypoint (#OFF*) can be input with a radial based on the LAST TK va.
System Operation 3- 128 GNS-X L Flight Management System Rev. 0 Oct/96 The CDU has non-volatile storage for up to 999 waypoints which are retained in memory ONLY if the waypoints are entered on a Stored Flight Plan. The ICAO identifiers stored in the database can not be used for personalized waypoints.
System Operation 3- 129 GNS-X L Flight Management System Rev. 0 Oct/96 CREATING AN OFFSET WAYPOINT This procedure enables the system to create a waypoint at a given radial and distance from a known point. The known point (parent waypoint) may be any stored personalized or database waypoint.
System Operation 3- 130 GNS-X L Flight Management System Rev. 0 Oct/96 7. POS Coordinates- VER- IFY for reasonability. (Figure 3-205) 8. ENT Key-DEPRESS.
System Operation 3- 131 GNS-X L Flight Management System Rev. 0 Oct/96 6. Enter the desired route spacing in nautical miles. 60NM is nor- mal. 7. ENT Key - DEPRESS. 8. Enter the expected ground speed in knots. A value of 100 to 999 Kts may be entered.
System Operation 3- 132 GNS-X L Flight Management System Rev. 0 Oct/96 NOTE: Entering a number already listed and pressing ENT will remove the number from the list. Pressing the Line Select Key next to CLEAR ALL and pressing ENT will remove all satellites from the exclusion list.
System Operation 3- 133 GNS-X L Flight Management System Rev. 0 Oct/96 21. ENT Key - DEPRESS. PLAN 8/8 FDE COMPUTA- TION Page is now displayed. COMPUTING - STANDBY will flash while FDE predic- tion is being calculated and the percentage completed will be shown.
System Operation 3- 134 GNS-X L Flight Management System Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
SECTION 4 VLF/OMEGA TRANSMITTER SITES VLF COMMUNICATIONS STATIONS LETTER DESIGNATION WASHINGTON (WSH) Jim Creek, Washington USA AUSTRALIA (AUS) Northwest Cape, Australia ANTHORNE (ANT) Anthorne, Engla.
VHF/OMEGA T ransmitter sites 4-2 GNS-X L Flight Management System Rev. 0 Oct/96 OMEGA NAVIGATIONAL NETWORK (CONTINUED) ARGENTINA (ARG) Gulfo Nuevo, Argentina AUSTRALIA (AUS) Darriman, Australia JAPAN .
Database Update 5-1 GNS-X L Flight Management System Rev. 0 Oct/96 SECTION 5 DA T ABASE UPDA TE DA T A BASE UPDA TE PROCEDURES 1. Apply aircraft power. 2. Open the hinged door located at the top of the CDU. 3. Insert current Data Base Update card firmly into the slot.
Database Update 5-2 GNS-X L Flight Management System Rev. 0 Oct/96 WHEN UPDATE IS COMPLETE If the update is successful, Figure 5-3 is displayed. 8. Turn system OFF or DEPRESS ENT Key to restart navigation. IF UPDATE FAILS If the database update fails, Figure 5-4 is displayed.
SECTION 6 LIST OF ABBREVIA TIONS AND DEFINITIONS DEFINITION A AT or ABOVE (Ref. to VNAV Altitude Constraint) ADC Air Data Computer ADF Automatic Direction Finder AFIS Airborne Flight Information System AFM Aircraft Flight Manual AHRS Attitude Heading Reference System ALT Altitude APRCH Approach AR DME Arc ARINC Aeronautical Radio, Inc.
DEFINITION CDI Course Deviation Indicator CDU Control Display Unit CH Channel CLIMB GRAD Current Aircraft Climb Performance in feet per Nautical Mile CRUISE ALT Cruise Altitude Æ Direct To (Laterally.
List of Abbreviations & Definitions 6-3 GNS-X L Flight Management System Rev. 0 Oct/96 DEFINITION FCF Final Course (Alignment) Fix. FL Flight Level FAF Final Approach Fix FDE Fault Detection and Exclusion. Detection mean- ing the capability of the system to detect a satel- lite failure that will affect navigation.
DEFINITION HPE Horizontal Position Error (A Quality Factor for the GPS.) HSI Horizontal Situation Indicator IAF Initial Approach Fix ICAO International Civil Aviation Organization IDENT Identifier ILS.
DEFINITION MAP Missed Approach Point MHz Megahertz MSG Message NAV Navigation NAVAID Navigation Aid (Typically a Radio Station Providing VOR and/or DME Position Data) NDB NAV Database or Non-Direction.
List of Abbreviations & Definitions 6-6 GNS-X L Flight Management System Rev. 0 Oct/96 DEFINITION REM Remaining REQ FPM Required Feet Per Minute RCVD Received RMI Radio Magnetic Indicator RNAV Are.
DEFINITION TRANS LEVEL Transition Level (The Altitude at which Altitudes Become Flight Levels) TRCK Track (Satellite Status) TRMNL Terminal VAR Magnetic Variation VERT DEV Vertical Deviation VHF Very .
List of Abbreviations & Definitions 6-8 GNS-X L Flight Management System Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 SECTION 7 AFIS AIRBORNE FLIGHT INFORMA TION SYSTEM AND SA TELLITE DA T A COMMUNICA TIONS SYSTEM This section applies only to aircraft equipped with an AFIS system.
GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
DESCRIPTION AFIS is an Airborne Flight Information System that provides integrat- ed flight planning and performance management interfaces to the GNS-X L Nav Management System.
7-2 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 GLOBAL DATA CENTER (GDC) The Global Data Center (GDC) is a ground based computer facility built and operated by Honeywell for the purpose of providing flight planning, aviation weather, and message forwarding services to AFIS operators on a subscription basis.
7-3 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 The Satellite Data Communications System consists of the following components: Satellite Communications Unit (SCU), High Power Amplifier/ Low Noise Amplifier (HPA/LNA), and Satellite Antenna.
7-4 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 NOTE: Once the system is initialized, the page appears between the Active Flight Plan Page and the first GNS-X L FLIGHT PLAN LIST Page. AFIS FLT PLAN LIST: A list of AFIS generated Flight Plan ori- gin/destination identifiers with date of issue.
7-5 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 NOTE: Planned fields become dashes when no planned data is available for the current leg. (Figure 7-4). ACT: Actual This column is GNS-X L data. NOTE: Actual fields become dashes when cursor is posi- tioned over the leg identifiers.
NOTE: Field changes to ETE when cursor is positioned over the leg identifiers. (Figure 7-6) ETE: Estimated Time Enroute Planned: The AFIS planned time enroute for leg displayed. TAS: True Airspeed Planned: AFIS planned true air- speed for leg displayed.
METS(SIGnificant METeorology) transferred via the disk and/or received via the data link. TERMINAL WX: Review of all Terminal Weather transferred via the disk and/or received via the data link. Additional requests can be entered. WINDS ALOFT: Review of all Winds Aloft identifiers transferred via the disk and/or received via the data link.
7-8 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 UPDATE refers to the Lat/Lon position of aircraft at time of last update request. (Figure 7-9). TO: The TO waypoint identifier. TO/FUEL: Projected fuel required from FROM waypoint to TO waypoint as transferred from disk or updated enroute via the data link.
AFIS FLT PLAN PAGE 2 WEIGHTS, FLIGHT LEVEL AND ROUTE RAMP WT: Planned ramp weight in lbs prior to starting engines as transferred from disk or received via the data link. (Figure 7-10) GROSS WT: Sum of basic operating weight, payload, and fuel remaining as calculated by GNS-X L .
7-10 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 AFIS FLT PLAN PAGE 3 OPERATOR INPUTS FROM: Origin airport identifier as transferred from disk or received via the data link, or UPDATE waypoint defining position of air- craft at time of last update request.
7-11 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 AFIS FLT PLAN PAGE 4 PERFORMANCE BIAS This page allows a review of the operator entered performance bias data transferred from disk or received via the data link. (Figure 7-14) SIGMETS PAGES AFIS SIGMETS pages are accessed by selecting Option 2 on the AFIS MENU Page.
7-12 GNS-X L Flight Management System AFIS Operation Rev. 1 Jul/98 TRANSMIT REQUEST?: When cursor is on this field and ENT is pressed, a SIGMET update request is sent to the Global Data Center via data link. DATA LINK DISABLED will appear if the data link is disabled and the request will not be transmitted.
TERMINAL WX DATA PAGES These pages are accessed by selecting a terminal weather identifier on the TERMINAL WEATHER Menu Page. They allow review of Terminal Weather by identifier as trans- ferred from disk or received by the Global Data Center via the data link.
DATE/TIME: Actual day and time of the issue of the wind informa- tion. This field may be blank if transferred from disk. The number is read 12th day 2356 ZULU.
7-15 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 TRANSMIT REQUEST?: When cursor is on this field and ENT is pressed, the recall request is sent to the Global Data Center via data link.
7-16 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 Phone number #206 869 6450 • GDC will deliver message verbally to given number . AFIS-equipped aircraft #N4322B • GDC will deliver message to aircraft specified. "A" followed b y phone number #A206 869 6458 • GDC will deliver message to PC at given number .
7-17 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 PPM MENU PAGE (PREPROGRAMMED MESSAGES) This page is accessed from the SEND MESSAGE Page by selecting PPM in the upper right hand corner. PPM can only be selected when an entry has been made in the TO or # fields on the SEND MESSAGE Page.
7-18 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 DISPLAY AFIS MSG PAGE The message page is displayed by selecting Option 7 on the AFIS MENU Page. All text messages sent to the tail number of the aircraft being flown appear in this section.
VHF NETWORK: Ground networks that AFIS interfaces with to establish a data link with the Global Data Center. ON: The appropriate VHF network will automatically be selected whenever the aircraft present position is within the specified bound- aries. (Figure 7-28) OFF: Network is not enabled.
7-20 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 VHF LINK CONTROL PAGE This page is accessed when the VHF Network is turned ON . ARINC, SITA/AVICOM: Ground networks that AFIS interfaces with to establish a data link with the Global Data Center.
7-21 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 REGION: The four satellite regions, West Atlantic, East Atlantic, Pacific Ocean and Indian Ocean, that AFIS inter- faces with to establish a data link with the Global Data Center. (Figure 7-31) LINK: OPERATIONAL: Message indi- cating the SAT COMM link is enabled.
7-22 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 AUTO WX UPDT (WEATHER UPDATE): ON: The Global Data Center will automatically send weath- er/wind updates for the dis- played idents when new infor- mation is issued. OFF: The auto weather update function is not enabled.
ACTIVE FLIGHT PLAN PAGE (FOR AFIS FLIGHT PLAN UPDATING) AFIS UPDATE: Allows pilot to: • Amend an existing AFIS Flight Plan • Update SIGMETS • Request a new AFIS Flight Plan AFIS UPDATE VERIFICATION PAGE ACTUAL FL: Actual flight level of aircraft rounded to nearest 100 ft.
7-24 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 SYSTEM MESSAGES PAGE AFIS related messages appear on the SYSTEM MESSAGES Page (see Section 2 of the Operators Manual). When new messages are added, the MSG Key will flash and a flashing asterisk will appear next to the new message.
AFIS CONFIG FAIL Configuration module has failed. DMU non- volatile memory configuration information will be used. AFIS CONFIG LOST DMU non-volatile memory has lost its con- figuration information and the configuration module has failed. NOTE: Message may not cause MSG Annunciator to flash.
7-26 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 THIS PAGE INTENTIONALLY LEFT BLANK.
SYSTEM OPERA TION PRE-DEP ARTURE AFIS FLIGHT PLAN SELECTION The AFIS FLIGHT PLAN LIST Page appears after the Initialization Page. The page also appears between the Active Flight Plan Page and the first GNS-XL FLIGHT PLAN LIST Page.
7-28 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 4. FPL Date - VERIFY. 5. ENT Key - DEPRESS. NOTE: If an Active Flight Plan exists, the message REPLACE ACTIVE FPL? appears. DEPRESS ENTER to replace the Active Flight Plan with the AFIS Flight Plan.
7-29 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 legs of the AFIS Flight Plan. 6. Line Select Key - DEPRESS to remove cursor from page and return to Current Leg Progress. NOTE: If the current leg displayed does not agree with a planned AFIS leg, the PLAN fields display dashes.
7-30 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 5. AFIS or NXT Key - DEPRESS to display AFIS Flight Plan Page 2. NOTE: Pressing the PRV or BACK Key will re-display the AFIS MENU Page with the cur- sor positioned over Option 1. AFIS FLIGHT PLAN PAGE 2 6.
7-31 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 AFIS FLIGHT PLAN PAGE 3 8. Pilot Inputs - REVIEW. (Figure 7-49) NOTE: If there has been an update to the flight plan: FROM identifier.
7-32 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 SIGMETS REVIEW/UPDATE 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2. Line Select Key - DEPRESS to position cursor over Option 2, SIGMETS . 3. ENT Key - DEPRESS to display first SIGMETS Page.
7-33 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 NOTE: Wait for DATA CENTER AK message if sending multiple requests. A ( ) around the FR and TO waypoints indicates that the updated information has not yet been received. 10. AFIS or NXT Key - DEPRESS.
8. ENT Key - DEPRESS. Identifiers listed on this page will be trans- mitted to the ground via the data link. NOTE: Wait for DATA CEN- TER AK message if sending multiple requests.
7-35 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 3. ENT Key - DEPRESS to display WINDS ALOFT Menu Page. (Figure 7-60) 4 . Line Select Key - DEPRESS to position cur- sor over the desired Wind identifier.
7-36 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 13. ENT Key - DEPRESS. The WINDS ALOFT Menu Page appears with the new identifier in place of the original identifier, and the cursor positioned at the location of the original identifier selected.
7-37 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 6. ENT Key - DEPRESS. Cursor is positioned over TRANSMIT REQUEST? (Figure 7-65) 7. ENT Key - DEPRESS to ini- tiate recalling of AFIS Flight Plan from Global Data Center.
9. ENT Key - DEPRESS. Cursor is positioned over TRANSMIT REQUEST? (Figure 7-67) 10. ENT Key - DEPRESS to ini- tiate recalling of AFIS Flight Plan from Global Data Center. AFIS MENU Page will appear with cursor posi- tioned over Option 6. NOTE: SIGMETS ,Winds and Term Wx are automatically updated once the FPL is recalled.
7-39 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 8. ENT Key - DEPRESS. 9. FR - INSERT sender's iden- tification (name or tail num- ber). 10. ENT Key - DEPRESS. 11. # - INSERT receiver's address. See Table 1 for possible addresses.
7-40 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 f. The Line Select Key moves cursor to SEND MESSAGE? field if a TO or # entry field has been inserted.
7-41 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 SENDING/BUILDING A PREPROGRAMMED MESSAGE The PREPROGRAMMED MESSAGES MENU Page is accessed from the SEND AFIS MSG Page. (Figure 7-73) An entry in the TO or # field must be made before access to PPM is avail- able.
EDITING/ENTERING A PREPROGRAMMED MESSAGE 6. TEXT - EDIT or ENTER using the following guidelines. a. Entering a character causes the character at the cursor posi- tion and all the characters to the right to be shifted one position. b. The BACK Key may be used to delete characters one at a time from right to left.
7-43 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 AFIS MESSAGES REVIEW 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 7, DISPL AFIS MSG . (Figure 7-77) 3. ENT Key - DEPRESS.
7-44 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 TURNING AUTO REPORT / AUTO WX UPDATE OFF 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2. Line Select Key - DEPRESS to position cursor over Option 8, OPERATING MODES . (Figure 7-79) 3.
7-45 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 RETURNING TO AUTO REPORT/AUTO WX UPDATE 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2. Line Select Key - DEPRESS to position cursor over Option 8, OPERATING MODES . (Figure 7-82) 3.
7-46 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 AUTO WEATHER UPDATE When the system is initialized, the Automatic Weather Update function will retain the status at aircraft shutdown. The following procedures allow the function to be turned OFF and back ON .
7-47 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 RETURNING TO AUTO WX UPDT 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 8, OPER- ATING MODES . (Figure 7- 88) 3. ENT Key - DEPRESS.
7-48 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 VHF AND SATELLITE NETWORK OPERATING MODES The status of each network is held in non-volatile memory. When the system is initialized, all networks will prefill with the status at system shut-down.
7-49 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 TURNING VHF NETWORK ON 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 8, OPER- ATING MODES . 3. ENT Key - DEPRESS. 4. Line Select Key - DEPRESS to position cursor over OFF option of VHF NETWORK field.
7-50 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 TURNING AUTO TO MAN OR OFF NOTE: SITA/AVICOM are two different ground networks covering different regions. The appropriate network is automatically selected for operation based on current Lat/Lon location of aircraft, if mode is set to AUTO.
7-51 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 TURNING SATELLITE NETWORK OFF 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 8, OPER- ATING MODES . (Figure 7- 99) 3. ENT Key - DEPRESS.
7-52 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 TURNING SATELLITE NETWORK ON The satellite network must be turned ON to send non-flight related messages. Since the VHF network has precedence over the satellite network in areas of shared coverage, the VHF NETWORK must be turned OFF in order for SATCOM to be the Active Link.
7-53 GNS-X L Flight Management System AFIS Operation Rev. 0 Oct/96 TURNING AUTO TO MAN 7 . Line Select Key - DEPRESS until MAN appears in the cursor. 8. ENT Key - DEPRESS. Cursor moves to REGION field. 9. BACK Key - DEPRESS until desired region appears in cursor, either W.
PRINTER CTRL The AFIS DMU has two RS-232 printer interfaces. Users may print messages or weather to either or both printer ports. Automatic print- ing is also available. Controls for these options, as well as Auto Form Feed control, are accessed on the PRINTER CONTROL page.
3. ENTER Key - DEPRESS. 4. Line Select Key - DEPRESS to position cursor over SEL option of PRINTER CTRL field. 5. ENTER Key - DEPRESS to access the PRINTER CONTROL page. 6. Line Select Key - DEPRESS to position cursor over WEATHER DEST . 7. BACK Key - DEPRESS to cycle destination field between PRT1 , PRT2 , and BOTH .
AUTO PRINT MSG The Auto Print Message field is used to select or deselect the auto- matic printing of messages. If AUTO PRINT MSG is set to YES , then messages will automatically be printed upon receipt. If AUTO PRINT MSG is set to NO , then messages will not be printed upon receipt.
PRINT WX . 7. BACK Key - DEPRESS to toggle Auto Print Weather field between YES and NO . 8. ENTER Key - DEPRESS to set Auto Print Weather field to its present value ( YES or NO .
To Manually Print All Messages: 1. From the AFIS MENU , select the SEND AFIS MSG page. 2. On the send message page, leave the TO and FR fields blank. At the address (#) field, type ONE of the following commands: MSG 1 Send messages to printer one. MSG 2 Send messages to printer two.
TWX 1 Send Terminal Weather to printer one. TWX 2 Send Terminal Weather to printer two. TWX 3 Send Terminal Weather to both printers. 3. Press ENTER until the SEND MESSAGE? prompt is displayed. Press ENTER again to initiate printing to the specified printer.
7-60 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 SELECTING OPERATING MODES (FOR AFIS USERS NOT EQUIPPED WITH SATELLITE DATA COMMUNICATIONS SYSTEM) AUTO REPORTING When the system is initialized, the Automatic Reporting and or Auto Wx update function will retain the status at aircraft shut- down.
7-61 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 RETURNING TO AUTO REPORT 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 8, OPER- ATING MODES . (Figure 7- 110) 3. ENT Key - DEPRESS.
7-62 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 AUTO WEATHER UPDATE When the system is initialized, the Automatic Weather Update function will retain the status at aircraft shutdown. The following procedures allow the function to be turned OFF and back ON .
7-63 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 RETURNING TO AUTO WX UPDT 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 8, OPER- ATING MODES . (Figure 7- 116) 3. ENT Key - DEPRESS.
GROUND NETWORK OPERATING MODES The status of each network is held in non-volatile memory. When the system is initialized, all networks will prefill with the status at system shut-down. The following procedures allow the ground networks to be man- ually operated, turned OFF , or returned to AUTO .
7-65 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 RETURNING TO AUTO 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 8, OPER- ATING MODES . (Figure 7- 122) 3. ENT Key - DEPRESS.
7-66 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 UPDATING AFIS FLIGHT PLAN AND WEATHER UPDATING AFIS FLIGHT PLAN 1. FPL Key - DEPRESS to dis- play Active Flight Plan Page. 2. Active Flight Plan - VERIFY the Active Flight Plan route or AMEND as necessary.
7-67 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 13. CRUISE MODE - VERIFY or INSERT an amended cruise mode. 14. ENT Key - DEPRESS. T h e cursor positions over TRANSMIT REQUEST ? field. (Figure 7-127) 15. ENT Key - DEPRESS to initi- ate a Flight Plan Update.
7-68 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 UPDATING SIGMETS 1. AFIS Key - DEPRESS to display AFIS MENU Page. 2 . Line Select Key - DEPRESS to position cur- sor over Option 2, SIG- METS . (Figure 7-130) 3. ENT Key - DEPRESS to display first SIGMETS Page.
7-69 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 UPDATING WEATHER 1. AFIS Key - DEPRESS to dis- play AFIS MENU Page. 2. Line Select Key - DEPRESS to position cursor over Option 3, TERMINAL WX . (Figure 7-133) 3. ENT Key - DEPRESS to dis- play TERMINAL WX Menu Page.
7-70 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 TO INSERT A NEW IDENTIFIER 11. Line Select Key - DEPRESS to position the cursor over the iden- tifier field. 12. IDENTIFIER - INSERT. The data text fields will go blank. 13. ENT Key - DEPRESS.
7-71 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 9. ENT Key - DEPRESS. Identifiers listed on this page will be trans- mitted to the ground via the data link. NOTE: Wait for DATA CENTER AK if sending multiple requests. TO UPDATE THE WINDS ALOFT DATA PAGES 10.
7-72 GNS-X L Flight Management System AFIS Operation Rev. 3 Oct/02 THIS PAGE INTENTIONALLY LEFT BLANK.
A ACARS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-2 Actual Vertical Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-34 ADF .
At or Above/Below . . . . . . . . . . . . . . . . . 2-12, 2-33, 2-37, 2-40, 3-72~3-73, 3-80, 6-1 ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-39~3-40, 3-44, 6-1, 7-23 Atlantic . . . . . . . . . . . . . . . .
Cross-at. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-78, 3-86 Cross-AT-or-BELOW . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-78 Cross-AT-or-ABOVE .
DIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-62, 3-64, 3-66, 6-4 DME Arc . . . . . . 2-4, 2-8, 2-10, 2-13, 2-15~2-17, 2-19, 3-33, 3-39, 3-41, 3-44~3-47, 3-60, 6-1 DN . . . . . . . . . . . . . . .
FDE Computation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-51, 3-133 FDE Prediction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-49, 3-15, 3-130~3-131, 3-133 Fence . . . . . . . 2-4, 2-9~2-11, 2-18, 2-45, 2-47, 3-12, 3-36~3-37, 3-54, 3-108, 3-122 FF .
HLTH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-31, 6-3 Holding. . . . 1-5, 2-4, 2-8, 2-10, 2-13, 2-15~2-17, 2-19, 2-33, 2-58, 2-62~2-64, 2-76, 3-33, 3-52, 3-63, 6-3, 7-8 Holding Fix .
INTERCEPT BEYOND FIX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-54, 3-61 Intercept Messages . . . . . . . . . . . .
MAN HDG REQD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-74, 3-119 MAN TAS REQD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-74, 3-118 Manual Fuel Flow . . .
NO SIDS AVAILABLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5, 3-19 No SIDs Available . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5, 3-19 NO SIGMETS . . . .
Pre-departure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1, 3-71, 7-1, 7-27 Pre-selected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-39, 3-84, 3-86 PRED IN PROGRESS .
Runway Thresholds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-68 Runways (RWY) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-8, 2-65, 3-33, 3-35~3-36 S SATCOM . . . . . . . . .
STRG (INVALID) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-77, 3-58 Subscription . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-2 SYNC .
UPDA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-61 UPDA-XXXX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-4 Update .
Obsolete Waypoint . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-65, 2-73 Oceanic Waypoint . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-50, 3-130 Offset Waypoint . . . . . . . . .
N Honeywell International Inc. One Technology Center 23500 West 105th Street Olathe, Kansas 66061 FAX 913-791-1302 Telephone: (913) 712-0400 006-08852-0000 Rev.
Ein wichtiger Punkt beim Kauf des Geräts Honeywell GNS-XL (oder sogar vor seinem Kauf) ist das durchlesen seiner Bedienungsanleitung. Dies sollten wir wegen ein paar einfacher Gründe machen:
Wenn Sie Honeywell GNS-XL noch nicht gekauft haben, ist jetzt ein guter Moment, um sich mit den grundliegenden Daten des Produkts bekannt zu machen. Schauen Sie zuerst die ersten Seiten der Anleitung durch, die Sie oben finden. Dort finden Sie die wichtigsten technischen Daten für Honeywell GNS-XL - auf diese Weise prüfen Sie, ob das Gerät Ihren Wünschen entspricht. Wenn Sie tiefer in die Benutzeranleitung von Honeywell GNS-XL reinschauen, lernen Sie alle zugänglichen Produktfunktionen kennen, sowie erhalten Informationen über die Nutzung. Die Informationen, die Sie über Honeywell GNS-XL erhalten, werden Ihnen bestimmt bei der Kaufentscheidung helfen.
Wenn Sie aber schon Honeywell GNS-XL besitzen, und noch keine Gelegenheit dazu hatten, die Bedienungsanleitung zu lesen, sollten Sie es aufgrund der oben beschriebenen Gründe machen. Sie erfahren dann, ob Sie die zugänglichen Funktionen richtig genutzt haben, aber auch, ob Sie keine Fehler begangen haben, die den Nutzungszeitraum von Honeywell GNS-XL verkürzen könnten.
Jedoch ist die eine der wichtigsten Rollen, die eine Bedienungsanleitung für den Nutzer spielt, die Hilfe bei der Lösung von Problemen mit Honeywell GNS-XL. Sie finden dort fast immer Troubleshooting, also die am häufigsten auftauchenden Störungen und Mängel bei Honeywell GNS-XL gemeinsam mit Hinweisen bezüglich der Arten ihrer Lösung. Sogar wenn es Ihnen nicht gelingen sollte das Problem alleine zu bewältigen, die Anleitung zeigt Ihnen die weitere Vorgehensweise – den Kontakt zur Kundenberatung oder dem naheliegenden Service.
