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Revision History and Instructions
ManualGNS-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.
Insert the contents of this revision packet according to the following
instructions:
Title PageRemove and Replace
Revision History PageInsert Ahead of Existing Revision History Pages
Section 3Remove and Replace Pages 3-17 through 3-22
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Rev. 4
Nov/04
R-1
GNS-XL Flight Management System
Revision History and Instructions
ManualGNS-XL Operator’s Manual
Revision 3, October, 2002
Part Number 006-08852-0000
This revision incorporates AFIS Printer Control, deletes Air Canada and calrifies SID/STAR operation.
Insert the contents of this revision packet according to the following
instructions:
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Title PageRemove and Replace
Revision History PageInsert Ahead of Existing Revision History Page
Table of ContentsRemove and Replace Pages v/vi and xi through
xvi
Section 3 Remove and Replace Pages 3-9 through 3-12
Insert Page 3-12a/3-12b after Page 3-12
Remove and Replace Pages 3-13 through 3-20
and Page 3-75/3-76
Section 7Remove and Replace Pages 7-1/7-2,7-7/7-8,
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R-1
Rev. 3
Oct/02
GNS-XL Flight Management System
Revision History and Instructions
ManualGNS-XL Operator’s Manual
Revision 2, April, 2000
Part Number 006-08852-0000
This revision incorporates GNS-XL Software Mod 6.
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instructions:
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Section 2Remove and Replace Pages 2-1/2-2, 2-73
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Rev. 2
Apr/00
R-1
GNS-XL Flight Management System
Revision History and Instructions
ManualGNS-XL 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 (3-36.3)
Add Waypoint Type Identifier (2-54, 3-48, 3-49, 3-62)
Revise Procedure Turn (3-41, 3-42, 3-43, 3-44)
Remove H Hot Key (3-57, 3-58, 3-61)
Add Fuel Use Reset Function (ix, 2-48, 3-105, 3-106)
Typographic/Administrative Corrections (Front Covers, 2-1, 2-4, 2-9, 2-10,
Revision History and Instructions
ManualGNS-XL 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.
The GNS-XL Flight Management System is an integrated system
designed to give the pilot centralized control for the navigation sensors, computer based flight planning, fuel management, and radio
management. The GNS-XL has a full color flat panel LCD display,
alpha-numeric and function keys, a Global Positioning Sensor (GPS),
and a navigation data base. All these are housed in a panel/pedestal
mounted Control Display Unit (CDU).
All aircraft interface requirements are accomplished through the
GNS-XL. The system supports analog and digital inputs in any combination. Specific aircraft requirements are programmed into a
Configuration Module. This module mounts directly to the rear connector, thus remaining in the aircraft. This allows hardware to be
easily moved between aircraft types without changing system configuration. The following is a summary of the digital and analog interfaces:
DIGITALANALOG
AFISAltitude
Air Data ComputerAltitude Rate
EFISCross Track Deviation
Fuel FlowDiscretes
Inertial Navigation SensorDual VOR/DME
Inertial Reference SensorFuel Flow
VOR/DME, ADF, XPDR, COMMHeading
Radio TuningHSI Course & Bearing
RPU - VLF/OmegaRoll Steering
Cross Side FMSTrue Air Speed
Vertical Deviation
In addition to the GPS sensor, position information is accepted from
up to eight navigation sensors, such as an optional VLF/Omega
RPU, inertial position sensors, or VOR/DME radios. These navigation
sensor inputs can be blended to form a single composite position.
Accuracy of this composite position is enhanced by using the best
Rev. 0
Oct/96
GNS-XL Flight Management System
1-1
Description
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. However, when RAIM is available,
the GPS sensor is the sole contributor to the composite position.
NOTE: RAIM (Receiver Autonomous Integrity Monitoring) is a quality factor used to determine the accuracy of the GPS position. It is an
internal function of the GPS receiver and determines the accuracy of
it’s navigation solution.
The navigation data base is updated on a 28-day cycle by way of a
memory card. This card is inserted in a Personal Computer Memory
Card International Association (PCMCIA) slot located under the lower
portion of the alpha keyboard. This worldwide database contains
over 50,000 waypoints, navaids and airports. It also contains altitudes at appropriate waypoints, SID, STAR, AIRWAY, and
APPROACH procedures. In addition to this database, the memory
can store up to 999 operator generated waypoints. Individual navigation points can be organized into 56 different stored flight plans, each
containing up to 50 waypoints.
Due to the way the GNS-XL database is structured, waypoints must
have unique identifiers. However, some duplicate ICAO identifiers
exist for more than one waypoint. In these cases the waypoint identifiers are renamed in the database. Two naming conventions are
used, one for four character identifiers and one for five character
identifiers.
Four character waypoints keep the first four characters and the last
two characters of the ICAO airport identifier as shown in the following
example.
MA11 at KPRC becomes MA11RC in the database.
Five character waypoints keep the first five characters and add the
last character of the ICAO airport identifier as shown in the following
example.
MA27L at KOAK becomes MA27LK in the database.
Additional capabilities of the GNS-XL include direct navigation from
present position to any waypoint, and data crossfill capability for dual
installations. Trip Plan and Fuel Plan functions are also available.
There is capability for creating a PSEUDO-VORTAC (selected
1-2
GNS-XL Flight Management System
Rev. 0
Oct/96
Description
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. The cursor is normally out of view unless brought into view by depressing
the Line Select Keys on either side of the screen. When
information is entered into a field and the ENT Key is
depressed, the cursor will move to the next enterable
field or disappear from the screen when the last field is
entered. Blinking of a field indicates that the computer
has not accepted the entry because of unreasonable or
invalid information.
PAGE:Information is arranged in sections and subsections
much like chapters in a book. Individual screen displays
are referred to as pages. Each section is selected by
depressing the appropriate Display Selector Key located
at the top of the keyboard. Each subsequent push of the
key will select the next page of that section. A subsection page is selected by depressing the Line Select Key
next to the topic desired, then depressing the ENT Key.
The PRV or NXT Key can be used to move forward or
backward through pages of a subsection. If the first
page of a subsection is displayed, the BACK Key will
exit the subsection.
WAYPOINT:A navigation point consisting of 1 to 6 alpha, numeric
characters that has a specific latitude and longitude.
Rev. 0
Oct/96
GNS-XL Flight Management System
1-3
Description
ENT
BRT
AFIS
HOLDDMSG
GH I J KL
MNOP QR
S
TUVWX
YZ
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
GH I J KL
MNOP QR
S
TUVWX
YZ
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
GH I J KL
MNOP QR
S
TUVWX
YZ
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
CONTROLS AND INDICATORS
ON:
Depress and release the ON
Key to apply power to the system. There is a warm-up period
of approximately 30 seconds.
The display illumination will initially be set at 75% of full bright.
Depressing the ON Key for
approximately three seconds
will initiate the system power off
sequence. During the sequence
the display will show SYSTEM TURNING OFF. This is to prevent
inadvertent system shutdown.
NOTE: The system is also capable of being turned on and off by
cycling aircraft power.
BRIGHTNESS (BRT):
The BRT Key is used to change
the illumination of the display.
This key is also used for parallax adjustment of the Line
Select Keys
NOTE: The illumination of the
front panel and keyboard is normally controlled through the aircraft panel lighting control.
MESSAGE KEY/ANNUNCIATOR (MSG):
The MSG annunciator will flash
to alert the operator that a message needs to be viewed on
one of the SYSTEM MES-
SAGES or SENSOR MESSAGES Pages.
1-4
GNS-XL Flight Management System
Rev. 0
Oct/96
Description
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
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. If no action is required, the MSG annunciator will extinguish when the message page is exited.
ALPHA KEYS:
The alpha keys are used to
enter the 26 letters of the alphabet, and #.
NUMERIC KEYS:
The numeric keys are used to
enter numbers 0 to 9, ± and *.
HOLD KEY:
If the cursor is positioned over a
waypoint identifier, and it is
appropriate to program a
Holding Pattern at that waypoint, depressing the HOLD
Key accesses the Holding
Pattern page.
If the cursor is not displayed,
depressing the HOLD Key
accesses the POSITION FIX
Page and is used for position
updates and verification as well
as entering the primary navigation mode.
Rev. 0
Oct/96
GNS-XL Flight Management System
1-5
Description
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
BACK (BACK) KEY:
The BACK Key is used to erase
errors and page backward
when the cursor is not displayed. It can also be used to
change data in a field if the cursor is present.
SPACE (SP) KEY:
The SP Key is used to enter a
space when entering a message on an AFIS Page. This
key is not functional if AFIS is
not installed in the system.
ENTER (ENT) KEY:
When the ENTKey is
depressed, data is entered into
the computer memory.
DISPLAY SELECTOR KEYS:
NAV(Navigation), VNAV
(Vertical Navigation), AFIS
(Airborne Flight Information
System), FPL (Flight Plan),
PLAN (Planning),HDG
(Heading), TUNE(Radio
Tuning), and d (Direct) are
used to select the pages pertaining to that particular section.
The first page of a section is displayed first when a Display
Selector Key is pressed. With
each subsequent press of the
Key, the next sequential page
will be displayed.
GNS-XL Flight Management System
1-6
Rev. 0
Oct/96
PREVIOUS (PRV) KEY:
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
ENT
BRT
AFIS
HOLDDMSG
G H I J K L
M N O P Q R
S
T U V W X
Y Z
#
SP
1 2 3
4 5 6
7 8 9
± 0
*
A B C D E F
BACK
PLANFPL
NXTPRV
NAV VNAV
HDGTUNE
ON
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 looping from the first to the last and
back to the first page of that
section or subsection.
NEXT (NXT) KEY:
The NXT Key is used to display
the next page of a section or
subsection. This key also
allows the operator to remain in
a section or subsection by looping from the first to the last and
back to the first page of that
section or subsection.
Description
LINE SELECT KEYS:
These keys are used to place
the cursor in the field next to
that key. Each line select key
controls 2 lines of text. White
symbols (< or >) displayed on
either side of the display indicate active Line Select Keys for
each individual page.
Rev. 0
Oct/96
GNS-XL Flight Management System
1-7
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