Garmin GPS 400 PILOT GUIDE

GPS 400
Pilot’s Guide and Reference
Part Number Change Summary
190-00140-60
(Rev. C)
Revision Date of Revision Description
A 8/99 Initial Release B 8/00 Revised and Redrawn
RECORD OF REVISIONS
GPS 400 Pilot’s Guide and Reference
i
COPYRIGHT
Copyright © 1999-2006 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of Main System Software version 5.01 or later. Some differences may be observed when comparing the information in this manual to other software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062 USA p: 913.397.8200 f: 913.397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, Oregon 97302 USA p: 503.391.3411 f: 503.364.2138
Garmin (Europe) Ltd., Unit 5, The Quadrangle, Abbey Park, Industrial Estate, Romsey, SO51 9DL, U.K. p: 44/0870.8501241 f: 44/0870.85
01251
Garmin (Asia) Corp., No. 68, Jangshu 2nd Road., Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f : 886/2.2642-9099
Website Address: www.garmin.com Visit the Garmin website for the latest updates and supplemental information concerning the operation of this and other Garmin
products.
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded, or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin® and AutoLocate® are registered trademarks of Garmin Ltd. or its subsidiaries and may not be used without the express permission of Garmin.
GDL™, GPS 400™, GTX™, PhaseTrac12™ and Spell’N’Find™ are trademarks of Garmin Ltd. or its subsidiaries and may not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.
November 2006 190-00140-60 Rev. C Printed in the U.S.A..
ii
GPS 400 Pilot’s Guide and Reference
TABLE OF CONTENTS
SECTION 1: INTRODUCTION ........................................... 1-1
1.1 Accessories and Packing List ................................. 1-1
1.2 Key and Knob Functions ......................................... 1-2
1.3 Takeoff Tour ............................................................... 1-5
SECTION 2: NAV PAGES .................................................. 2-1
2.1 Main Page Groups .................................................... 2-1
2.2 NAV Page Group ....................................................... 2-2
2.3 Default NAV Page .....................................................2-2
2.4 Map Page ...................................................................2-5
2.5 TERRAIN PAGE ......................................................... 2-15
2.6 NAV/COM Page ........................................................ 2-18
2.7 Position Page ..........................................................2-20
2.8 Satellite Status Page ............................................. 2-23
2.9 Vertical Navigation Page ...................................... 2-25
SECTION 3: DIRECT-TO NAVIGATION .........................3-1
3.1 Overview .................................................................... 3-1
SECTION 4: FLIGHT PLANS .............................................4-1
4.1 Flight Plan Catalog Page ........................................ 4-1
4.2 Active Flight Plan Page ........................................... 4-9
SECTION 5: PROCEDURES ............................................... 5-1
5.1 Approaches, Departures, and Arrivals ................. 5-1
5.2 Non-Precision Approach Operations .................... 5-3
5.3 Points to Remember for All Approaches ..........5-26
SECTION 6: WPT PAGES .................................................... 6-1
6.1 WPT Page Group ....................................................... 6-1
6.2 Airport Location Page ............................................. 6-4
6.3 Airport Runway Page .............................................. 6-5
6.4 Airport Frequency Page .......................................... 6-6
6.5 Airport Approach Page ...........................................6-8
6.6 Airport Arrival Page ............................................... 6-10
6.7 Airport Departure Page ........................................ 6-12
6.8 Intersection Page ................................................... 6-13
6.9 NDB Page .................................................................. 6-14
6.10 VOR Page ................................................................6-14
6.11 User Waypoint Page ............................................6-15
SECTION 7: NRST PAGES ................................................. 7-1
7.1 NRST Page Group .....................................................7-1
7.2 Nearest Airport Page ............................................... 7-4
7.3 Nearest Intersection Page ...................................... 7-5
7.4 Nearest NDB Page .................................................... 7-6
7.5 Nearest VOR Page ....................................................7-6
7.6 Nearest User Waypoint Page ................................. 7-7
7.7 Nearest Center (ARTCC) Page ................................ 7-8
7.8 Nearest Flight Service Station (FSS) Page ..........7-8
7.9 Nearest Airspace Page ............................................ 7-9
SECTION 8: AUX PAGES .................................................... 8-1
8.1 AUX Page Group .......................................................8-1
8.2 Flight Planning Page ................................................ 8-2
8.3 Utility Page .............................................................. 8-12
8.4 Setup 1 Page ...........................................................8-20
8.5 Setup 2 Page ...........................................................8-28
SECTION 9: TERRAIN .......................................................... 9-1
9.1 Introduction ............................................................... 9-1
9.2 TERRAIN Operation .................................................. 9-2
9.3 TERRAIN Alerts .......................................................... 9-6
SECTION 10: ADDITIONAL FEATURES ..................... 10-1
10.1 Traffic Information Service (TIS) ...................... 10-1
10.2 Weather Data Link Interface ........................... 10-11
SECTION 11: FAULT DETECTION AND
EXCLUSION ............................................................................ 11-1
11.1 Detection and Exclusion ..................................... 11-1
11.2 Pre-Departure Verification of FDE ....................11-2
SECTION 12: MESSAGES, ABBREVIATIONS, AND
TERMS ............................................................................ 12-1
NAV
12.1 Messages ................................................................ 12-1
12.2 Abbreviations ........................................................12-8
12.3 Navigation Terms ...............................................12-11
Appendix A: Data Card Use ..........................................A-1
Appendix B: Specifications ........................................... B-1
Appendix C: Map Datums ..............................................C-1
Appendix D: Troubleshooting Q & A .......................D-1
GPS 400 Pilot’s Guide and Reference
iii
WARNINGS,
CAUTIONS, AND NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the TERRAIN function. The TERRAIN feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The TERRAIN feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The terrain data should be used only as an aid for situational awareness. Terrain data must not
be used as the sole basis for decisions or maneuvers to avoid terrain or obstacles. Terrain data must not be used for navigation.
WARNING: The altitude calculated by GPS 400 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by pressure altimeters in the aircraft.
WARNING: The Jeppesen database used in the GPS 400 system must be updated regularly in order to ensure that its information remains current. Updates are released every 28 days. A database information packet is included in the GPS 400 package. Pilots using an outdated database do so entirely at their own risk.
WARNING: The basemap (land and water data) must not be used for navigation, but rather only for non­navigational situational awareness. Any basemap indication should be compared with other navigation sources.
WARNING: For safety reasons, GPS 400 operational procedures must be learned on the ground.
WARNING: The United States government operates the Global Positioning System and is solely responsible for
its accuracy and maintenance. GPS is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin GPS 400 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the GPS 400 can be misused or misinterpreted and,
therefore, become unsafe.
iv
GPS 400 Pilot’s Guide and Reference
WARNINGS,
CAUTIONS, AND NOTES
WARNING: Use the GPS 400, Weather Data Link Interface, TIS, and TERRAIN at your own risk. To reduce the risk of unsafe operation, carefully review and understand all aspects of the GPS 400 Pilot’s Guide documentation and the Flight Manual Supplement. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the GPS 400 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
CAUTION: The GPS 400 display screen is coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the screen using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
CAUTION: The Garmin GPS 400 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen images of the GPS 400 panel and displays, are subject to change and may not reflect the most current GPS 400 system. Depictions of equipment may differ slightly from the actual equipment.
NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference and (2) this device must accept any interference received, including interference that may cause undesired operation.
NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our website at www.garmin.com/prop65.
GPS 400 Pilot’s Guide and Reference
v
WARRANTY
LIMITED WARRANTY
This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.
Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit the Garmin website at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.
vi
GPS 400 Pilot’s Guide and Reference
SECTION 1
INTRODUCTION

SECTION 1: INTRODUCTION

1.1 ACCESSORIES AND PACKING LIST

Congratulations on choosing the finest, most advanced panel mount IFR navigation/communication system available. The GPS 400 represents Garmin’s commitment to provide accurate, easy-to-use avionics.
Before installing and getting started with the GPS 400, please check to see that the package includes the following items. If any parts are missing or damaged, please contact a Garmin dealer immediately.
Standard Package:
• GPS 400 Unit
• NavData® Card
• Terrain Data Card
• Installation Rack
• Connectors
The Garmin dealer installs and configures the GPS
400. The GPS 400 is secured in the installation rack with the proper wiring connections performed. After installation, the NavData Card and the TERRAIN Data Card are installed into their correct slots on the front of the unit (see Appendix A). A Garmin dealer can answer any questions about the installation, such as location of antennas or any connections to other equipment in the panel.
NOTE: Help Garmin provide better support by
completing on-line registration. Registration ensures notification of product updates, new products, and provides for lost or stolen unit tracking. Have the serial number of the GPS 400 available and connect to the website (www. garmin.com). Look for the product registration link on the home page.
• GPS Antenna
• Pilot’s Guide
• Quick Reference Guide
• 400/500-series Display Interface Pilot’s Guide Addendum
• Database Subscription Packet
• Warranty Registration Card
• GPS 400 Simulator CD-ROM
GPS 400 Pilot’s Guide and Reference
1-1
SECTION 1
P
INTRODUCTION

1.2 KEY AND KNOB FUNCTIONS

The GPS 400 is designed to make operation as simple as possible. The key and knob descriptions (Figure 1-1) provide a general overview of the primary function(s) for each key and knob. The takeoff tour (Section 1.3) is intended to provide a brief overview of the primary functions of the GPS 400.
1
2
3
Experiment with the unit and refer to the reference
sections for more information.
Data is entered using the large and small knobs. Experiment with them to become efficient at entering data. This greatly reduces the amount of time spent operating the GPS 400 in flight.
4
5
7
6
8
1-2
1
NavData Card Slot
2
Power
3
TERRAIN Data Card Slot
4
CLR (clear)
5
Direct-to
9
10
Figure 1-1 Keys and Knobs
6
7
8
9
10
GPS 400 Pilot’s Guide and Reference
11
12
RNG (map range)
MENU
ENT (enter)
NRST (nearest)
OBS
13
15
14
11
MSG (message)
12
FPL (flight plan)
13
PROC (procedures)
14
Large right knob
15
Small right knob
SECTION 1
INTRODUCTION
Left-hand Knob
The Power Knob controls unit power, turn clockwise
to turn the unit on.
See Appendix A for NavData and TERRAIN Data Card
insertion and removal.
Right-hand Keys and Knobs
The CLR Key is used to erase information, remove map detail, or to cancel an entry. Press and hold the CLR Key to immediately display the Default NAV Page.
Pressing the Direct-to Key allows the pilot to enter a destination waypoint and establishes a direct course to the selected destination (Section 3).
The RNG Key allows the pilot to select the desired map range. Use the up arrow to zoom out to a larger area, or the down arrow to zoom in to a smaller area.
The MENU Key displays a context-sensitive list of options. This options list allows the pilot to access additional features or make settings changes which relate to the currently displayed page.
The ENT Key is used to approve an operation or complete data entry. It is also used to confirm information during power on.
The large right knob (CRSR) is used to select page groups: NAV, WPT, AUX, or NRST. With the on-screen cursor enabled, the large right knob allows the pilot to move the cursor about the page. The large right knob is also used to move the target pointer right (turn clockwise) or left (counterclockwise) when the map panning function is active.
The small right knob (CRSR) is used to select pages within one of the groups listed above. Press this knob momentarily to display the on-screen cursor. The cursor allows the pilot to enter data and/or make a selection from a list of options. When entering data, the small knob is used to select the desired letter or number and the large knob is used to move to the next character space. The small right knob is also used to move the target pointer up (turn clockwise) or down (counterclockwise) when the map panning function is active.
`
NOTE: Data is entered using the large and
small right knobs (Figure 1-2). Experiment with them to become efficient at entering data. This will greatly reduce the amount of time spent operating the GPS 400 in flight.
Figure 1-2 Blank Direct-to Page
GPS 400 Pilot’s Guide and Reference
1-3
SECTION 1
INTRODUCTION
NOTE: When the GPS 400 displays a list of
information that is too long for the display screen, a scroll bar appears along the right-hand side of the display (Figure 1-3). The scroll bar graphically indicates the number of additional items available within the selected category. To scroll through the list, press the small right knob to activate the cursor, then turn the large right knob.
Scroll
Bar
Figure 1-3 Scroll Bar
Bottom Row Keys
The NRST Key displays the Nearest Airports Page. Then, turning the small right knob steps through the NRST pages.
Pressing the OBS Key selects OBS mode, which retains the current ‘active to’ waypoint as the navigation reference even after passing the waypoint (i.e., prevents sequencing to the next waypoint). Pressing the OBS Key again returns the unit to normal operation, with automatic sequencing of waypoints. When OBS mode is selected, the pilot may set the desired course to/from a waypoint using the ‘Select OBS Course’ pop-up window, or an external OBS selector on the HSI or CDI.
The MSG Key is used to view system messages and to alert the pilot to important warnings and requirements. See Section 12.1 for more information on messages.
The FPL Key allows the pilot to create, edit, activate, and invert flight plans, as well as access approaches, departures, and arrivals. A closest point to flight plan feature is also made available by pressing the FPL Key. See Section 4 for more information on flight plans.
The PROC Key allows the pilot to select and remove approaches, departures, and arrivals from the flight plan. When using a flight plan, available procedures for the departure and/or arrival airport are offered automatically. Otherwise, the pilot may select the desired airport, then the desired procedure.
1-4
GPS 400 Pilot’s Guide and Reference
SECTION 1
INTRODUCTION

1.3 TAKEOFF TOUR

reading within this Pilot’s Guide includes:
Overview
The Garmin GPS 400 provides the pilot accurate navigational data, along with non-precision and precision approach certification in the IFR environment. The takeoff tour is designed to familiarize the pilot with:
• Powering up the unit
• Entering data
• Performing a simple direct-to
• Selecting IFR procedures
• Using some limited flight plans
In addition, this section briefly covers the Default NAV Page, the Map Page, and the NAV/COM Page, which are available as part of the NAV Page Group. These pages are used for most of the in-flight navigation.
The takeoff tour assumes that the unit and antennas have been properly installed and that the GPS 400’s default settings have not been changed. If any of the factory default settings (position format, units of measure, selectable fields, etc.) have been changed, the pictures shown here may not exactly match what is shown on the GPS 400. Prior to using the GPS 400 for the first time, Garmin recommends that the aircraft be moved to a location that is well away from buildings and other aircraft so the unit can collect satellite data without interruption.
This takeoff tour is intended to provide a brief introduction of the GPS 400’s major features. Sections 2 through 12 of this manual describe these features, and others, in additional detail. Refer to these sections, as needed, to learn or review the details regarding a particular feature.
Service staff is available during normal business hours (U.S. Central time zone) at the phone and fax numbers listed on page ii. Garmin can also be reached by mail (page ii) or at our website address, www.garmin.com.
Powering up the GPS 400
corner of the unit. Rotating it clockwise turns unit power on. After turning the unit on, a welcome page (Figure 1-4) is displayed while the unit performs a self test, followed sequentially by the the Land Data Page, then (if configured for TERRAIN) the Terrain Data Page, the Obstacle Data Page, and the Airport Terrain Data Page.
After becoming familiar with the basics, some suggested
• Flight plan features - Section 4
• IFR procedures - Section 5
• Waypoint information pages (database information) - Section 6
• Unit settings (configuring the unit to the pilot’s preferences) - Section 8
If more information is needed, Garmin’s Customer
The GPS 400’s Power Knob is located at the top left
Figure 1-4 Welcome Page
GPS 400 Pilot’s Guide and Reference
1-5
SECTION 1
INTRODUCTION
The Database Confirmation Page (Figure 1-5) appears next, which shows the current database information on the NavData Card (with the valid operating dates, cycle number, and database type indicated). The database is updated every 28 days and must be current for approved instrument approach operations. Information on database subscriptions is available inside the GPS 400 package.
Figure 1-5 Database Confirmation Page
Acknowledging the database information:
Press the
ENT Key.
Instrument Panel Self-test Page
Once the database has been acknowledged, the Instrument Panel Self-test Page appears (Figure 1-6).
To ensure that the GPS 400 and any connected instruments are working properly, check for the following indications on the CDI/HSI , RMI, external annunciators, and other connected instruments:
• Course deviation - half left/no flag
• TO/FROM flag - TO
• Bearing to destination - 135°
• Distance to destination - 10.0 nm
• All external annunciators (if installed) - on
• Glideslope - half up/no flag
• Time to destination - 4 minutes
• Desired
track - 149.5°
• Ground speed - 150 knots
The Instrument Panel Self-test Page (Figure 1-6) indicates the currently selected OBS course, fuel capacity (CAP), fuel on board (FOB), and fuel flow (FF). The fuel capacity, fuel on board, and fuel flow may be manually entered if the installation does not include connection to sensors which automatically provide these figures.
Entering fuel capacity, fuel on board, or fuel flow figures (if not provided by sensors):
1-6
Figure 1-6 Instrument Panel Self-Test Page
GPS 400 Pilot’s Guide and Reference
1) Turn the large
right knob to select the ‘CAP’,
‘FOB’, or ‘FF’ field.
2) Turn the small and large
right knobs to enter
the desired figure (Figures 1-6 and 1-7), then press the ENT Key.
INTRODUCTION
Viewing the Checklists Page:
SECTION 1
Figure 1-7 Fuel Flow Selected
The Instrument Panel Self-test Page includes selections to set fuel on board (FOB) to full capacity and access the Checklists Page. This allows the pilot to quickly set fuel to full limits and display any checklists that have been entered, such as start up or takeoff checklists.
Setting fuel on board to full (if not provided by sensor):
1) Turn the large
right knob to highlight ‘Set Full
Fuel?’(Figure 1-8).
1) Turn the large
right knob to highlight ‘Go To
Chklist?’ (Figure 1-9) and press the ENT Key.
Figure 1-9 ‘Go To Chklist?’ Highlighted
2) Turn the large right knob to select the desired
checklist, then execute each step (Section
8.3, Utility Page: Checklists) in the selected checklist.
3) After completing the desired checklist(s), press
the small right knob to return to the Checklists Page. Press the small right knob again to return to normal operation on the Satellite Status Page or the Map Page.
Figure 1-8 ‘Set Full Fuel?’ Highlighted
2) Press the ENT Key and verify that fuel on board
(‘FOB’) now matches the fuel capacity (CAP) figure. Fuel on board is reduced, over time, based on the fuel flow (FF) figure.
GPS 400 Pilot’s Guide and Reference
4) Once instrument operation has been verified with the Instrument Panel Self-test Page displayed, press the
NOTE: The GPS 400 can hold up to nine checklists
with up to 30 entries in each checklist.
ENT Key.
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SECTION 1
INTRODUCTION
Satellite Status Page
The Satellite Status Page (Figure 1-10) appears as the
GPS 400 attempts to collect satellite information.
An ‘Acquiring’ status is displayed on the Satellite Status Page, and the signal strengths of any satellites received appear as ‘bar graph’ readings. This is a good indication that the unit is receiving signals and a position fix is being determined. Following the first-time use of the GPS 400, the time required for a position fix varies, usually from one to two minutes.
Figure 1-10 Satellite Status Page
If the unit can only obtain enough satellites for 2D navigation (no altitude), the unit uses the altitude provided by the altitude encoder (if one is connected).
The ‘INTEG’ annunciator (bottom left corner of the screen) indicates that satellite coverage is insufficient to pass built-in integrity monitoring tests. In the example above, not enough satellites are being received to determine a position. The Satellite Status Page shows the ID numbers for the satellites and the relative signal strength of each satellite received (as a bar graph reading).
‘Searching Sky’ indicates that satelllite almanac data is not availiable or has expired (if the unit hasn’t been used for six months or more). This means the unit is acquiring satellite data to establish almanac and satellite orbit information, which can take five to ten minutes. The data is recollected from the first available satellite. The Satellite Status Page displays a ‘Search Sky’ status, and the message annunciator (MSG), above the MSG Key also flashes to alert the pilot of a system message, ‘Searching the Sky’.
Viewing a system message:
Press the
MSG Key (Figure 1-11).
The Message Page appears and displays the status or warning information applicable to the receiver’s current operating condition.
Figure 1-11 Message Page
Returning to the previous page after viewing a message:
Press the
NOTE: The GPS 400 utilizes certain software
algorithms to ensure reliable GPS receiver operation. Receiver Autonomous Intergrity Monitoring (RAIM) and Fault Detection and Exclusion (FDE) are two examples. These features allow navigation during Oceanic/Remote legs of a flight using the GNC420. For further details, please refer to Sections 8.3 and 11.
MSG Key again.
1-8
GPS 400 Pilot’s Guide and Reference
SECTION 1
INTRODUCTION
Page Groups
Page Groups
NAV Group WPT Group AUX Group NRST Group
see Section 2 see Section 6 see Section 8 see Section 7
Table 1-1 Page Groups
The bottom right corner of the screen (Figure 1-12) indicates which page group (Table 1-1) is currently being displayed (NAV, WPT, AUX, or NRST), the number of pages available within that group (indicated by square icons), and the placement of the current page within that group (indicated by a highlighted square icon).
In addition to the NAV Page Group, additional page groups are available for waypoint information (WPT), auxiliary (AUX) functions such as flight planning or unit settings, and listings for nearest (NRST) airports or other facilities.
NOTE: The NRST Page Group may be accessed
by using the large right knob as described in the preceding procedure or by pressing the NRST Key.
NAV Pages
There are seven pages available under the NAV Page
Group*:
• Default NAV Page
• Map Page
• TERRAIN Page (if configured)
• NAV/COM Page
• Position Page
• Satellite Status Page
• Vertical Navigation Page
The Default NAV Page, the Map Page, and the NAV/
COM Page are used for most of the in-flight navigation.
Position of
Current Page
within Current
Current Page Group
Figure 1-12 Current Page and Page Group
Number of Pages in
Current Page Group
Page Group
Selecting the desired page group and page:
1) Turn the large right knob until a page from the
desired page group is displayed (Figure 1-12).
2) Turn the small right knob until the desired page
is displayed (Figure 1-12).
GPS 400 Pilot’s Guide and Reference
NOTE: *The NAV Page Group may have eight
or nine NAV pages available when the GPS 400 installation includes connection to traffic and/or weather information sources. See Section 10 of this manual for more information.
Selecting the NAV Page Group and display the Default NAV Page:
Press and hold the
CLR Key.
Selecting the desired NAV Page:
Turn the small right knob until the desired
page is displayed.
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SECTION 1
INTRODUCTION
Map Page
After the GPS 400 acquires satellites and computes a position, the Map Page (Figure 1-13) appears automatically.
Map Display
Map Range
Present Position
Figure 1-13 Map Page
The Map Page displays the present position (using an airplane symbol) relative to nearby airports, VORs, NDBs, intersections, user waypoints, and airspace boundaries. The route is displayed as a solid line.
Data fields for destination waypoint (WPT), distance to waypoint (DIS), desired track (DTK), and ground speed (GS) appear on the right-hand side of the display. These fields are user selectable (Section 2.4, Selecting Desired On-screen Data) to allow the pilot to configure the unit. Available settings include: altitude, bearing, enroute safe altitude, estimated time of arrival, minimum safe altitude, and ground track.
A Map Setup Page is provided to designate the maximum range at which each map feature apppears. These settings provide an automatic decluttering of the map (based upon preferences) while adjusting the range. See Section 12.3 for definitions of these navigation terms.
While viewing the Map Page, the pilot can quickly declutter and remove many of the background map details by pressing the CLR Key (repeatedly) until the desired detail is depicted.
Desired Track
Data Fields
To change the map range, press the up arrow (to zoom out) or the down arrow (to zoom in) of the RNG (map range) Key. The current map range is depicted in the lower left corner of the Map Display.
Direct-to Navigation
The GPS 400 can use direct point-to-point navigation to provide guidance from takeoff to touchdown, even in the IFR environment. Once a destination is selected, the unit provides speed, course, and distance data based upon a direct course from the present position to the destination. A destination can be selected from any page with the Direct-to Key.
Selecting a direct-to destination:
1) Press the Direct-to Key. The Select Direct-to
Waypoint Page appears with the destination field highlighted.
2) Turn the small letter of the destination waypoint identifier. The destination waypoint may be an airport, VOR, NDB, intersection, or user waypoint, as long as it is in the database or stored in memory as a user waypoint.
3) Turn the large the cursor to the next character position.
4) Repeat steps 2 and 3 to spell out the rest of the waypoint identifier (Figure 1-14).
Figure 1-14 Direct-to Waypoint Page
right knob to enter the first
right knob to the right to move
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GPS 400 Pilot’s Guide and Reference
SECTION 1
INTRODUCTION
5) Press the ENT Key to confirm the identifier. The
‘Activate?’ function field is highlighted (Figure 1-15).
Figure 1-15 ‘Activate?’ Highlighted
6) Press the ENT Key to activate a direct-to course
to the selected destination.
Once a direct-to destination is selected, press and hold
the CLR Key to display the Default NAV Page.
Default NAV Page
During most flights, the Default NAV Page, the Map Page, and the NAV/COM Page are the primary pages used for navigation.
Selecting the Default NAV Page:
Press and hold the
Active Leg of
Flight Plan
TO/FROM Flag Course Deviation
CLR Key (Figure 1-16).
Indicator (CDI)
The Default NAV Page displays a graphic course deviation indicator (CDI), the active leg of the flight plan (as defined by the current ‘from’ and ‘to’ waypoints), and six user-selectable data fields. The default settings for these fields are distance to waypoint (DIS), desired track (DTK), bearing to waypoint (BRG), ground speed (GS), ground track (TRK), and estimated time enroute (ETE). See Section 12.3 for definitions of these navigation terms.
Changing the data fields:
1) From the Default NAV page, press the MENU
Key and select ‘Change Fields?’ (Figure 1-17).
Figure 1-17 Default NAV Page Menu
2) Turn the large right knob to select the data
field to be changed.
3) Turn the small
right knob to display a list of
data options (Figure 1-18).
Figure 1-16 Default NAV Page
User-selectable
Data Fields
Figure 1-18 ‘Select Field Type’ Window
4) Press the ENT Key to select the desired data
item and return to the Default NAV Page.
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NAV COM Page
From the Default NAV Page, simply turn the small right knob until the NAV/COM Page (Figure 1-19) is displayed.
Departure, Enroute, or
Arrival Airport
Frequency Type
Figure 1-19 NAV/COM Page
The NAV/COM Page displays the available frequencies (communication and navigation frequencies are shown for reference only) for the departure airport, any enroute airports which are included in the flight plan, and the final destination airport. When using the direct-to function, frequencies are listed for the airport nearest to the starting position and the destination airport.
Frequency List
Displaying the frequency list for the desired flight plan or direct-to airport:
1) Press the small right knob to activate the
cursor on the airport identifier field (in the GPS Window).
2) Turn the small
right knob to display the list
of airports (departure, arrival, and enroute) for the flight plan or direct-to. Continue to turn the small right knob until the desired airport is selected.
3) Press the
ENT Key to display the frequency list
for the selected airport.
Displaying frequencies for a different airport along the flight plan.
1) Press the small right knob to highlight the
airport identifier field.
2) Turn the small
right knob to display the list of
airports within the flight plan (Figure 1-20).
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Figure 1-20 Airport Window
3) Continue turning the small right knob to select the desired airport and press the ENT Key.
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IFR Procedures
Once the direct-to or flight plan is confirmed, the whole range of instrument procedures is available to the pilot. Departures (SIDs), arrivals (STARs), and non-precision and precision approaches are stored within the NavData Card and are available using the
Displaying the Procedures Page:
Press the
PROC Key (Figure 1-21).
Figure 1-21 Procedures Page
This introductory section shows examples of the steps required to select and activate a departure, arrival, or an approach.
Selecting a departure, arrival, or an approach:
1) Turn the large
right knob to select the desired
option (‘Select Departure?’, ‘Select Arrival?’ or‘ Select Approach?’) from the Procedures Page.
PROC (procedures) Key.
fix (IAF) or provide a ‘vectors’ option to select just the final course segment of the approach. Turn the small right knob to select the desired option and press the
ENT Key. The ‘vectors’
option extends the final inbound course beyond the final approach fix, allowing the pilot to intercept the final course segment beyond its normal limits.
Figure 1-22 Approach Window
5) For departures and arrivals, a window appears to select the desired transition. Turn the small right knob to select the desired option and press the ENT Key.
In the flight plan or direct-to, the departure or arrival airport is replaced with the sequence of waypoints contained within the selected procedure.
2) Press the
ENT Key to display a list of available
procedures for the departure (when using SIDs) or arrival (when using approaches or STARs) airport.
3) Turn the small right knob to select the desired procedure and press the ENT Key.
4) For approaches, a window appears (Figure 1-22) to select the desired initial approach
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INTRODUCTION
Nearest (NRST) Pages
The NRST Page Group provides detailed information on the nine nearest airports, VORs, NDBs, intersections, and user-created waypoints within 200 nm of the current position. In addition, pages are also provided to display the five nearest center (ARTCC/FIR) and Flight Service Station (FSS) points of communication, plus alert the pilot to any nearby special-use or controlled airspaces.
There are eight pages available in the NRST group:
• Nearest Airport Page
• Nearest NDB Page
• Nearest User Waypoint Page
• Nearest FSS Page
• Nearest Intersection Page
• Nearest VOR Page
• Nearest ARTCC Page
• Nearest Airspace Page
The communication frequencies and information may both be examined directly from the Nearest Airport Page.
runway
Displaying the NRST pages:
1) Press the NRST Key to select the Nearest
Airport Page (Figure 1-23).
2) Turn the small right knob to select the desired
NRST Page.
Displaying a list of nearby airports:
1) Press the NRST Key to select the Nearest
Airport Page (Figure 1-23).
Figure 1-23 Nearest Airport Page
2) To scroll through the list, press the small right knob, then turn the large right knob (Figure 1-24).
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Figure 1-24 Scrolling the Nearest Airport List
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Viewing additional information for a nearby airport:
1) Press the small right knob to activate the
cursor.
2) Turn the large
right knob to select the desired
airport from the list.
3) Press the
ENT Key to display waypoint (WPT)
information pages for the selected airport (Figure 1-25).
Figure 1-25 Airport Location Page
4) To display runway and frequency information,
press the small right knob to remove the cursor and turn the small right knob to display the desired information page.
The Nearest Airport Page may be used in conjunction with the Direct-to Key to quickly set a course to a nearby facility in an in-flight emergency. Selecting a nearby airport as a direct-to destination overrides the flight plan or cancels a previously selected direct-to destination. The pilot will still have the option of returning to the flight plan by cancelling the direct-to; see Section 3.1, Cancelling Direct-to Navigation.
Selecting a nearby airport as a direct-to destination from the Nearest Airport Page:
1) Press the small right knob to activate the
cursor.
2) Turn the large
right knob to select the desired
airport from the list.
3) Press the Direct-to Key.
4) Press the
ENT Key twice to navigate to the
nearby airport.
Selecting a nearby airport as a direct-to destination from the Airport Information Page:
1) Press the Direct-to Key.
2) Press the
ENT Key (Figure 1-26).
Figure 1-26 ‘Activate?’ Highlighted
3) Press the ENT Key again to navigate to the
nearby airport.
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INTRODUCTION
Nearest (NRST) Airspace Page
The last page in the NRST Page Group, the Nearest Airspace Page (Figure 1-27), provides information for up to nine controlled or special-use airspaces near or in the flight path. Airspace information appears on this page based on the same criteria used for airspace alert messages:
• If the projected course will take the aircraft inside an airspace within the next ten minutes, the message ‘Airspace ahead -- less than 10 minutes’ appears.
• If the aircraft is within 2 nm of an airspace and the current course will take the aircraft inside, the message ‘Airspace near and ahead’ appears.
• If the aircraft is within 2 nm of an airspace and the current course will not take the aircraft inside, the message ‘Near airspace less than 2nm’ appears.
• If the aircraft has entered an airspace, the message ‘Inside airspace’ appears.
Figure 1-27 Nearest Airspace Page
By default, airspace alert messages are turned off. When turned on, the message (MSG) annunciator located directly above the MSG Key flashes to alert the pilot to the airspace message. See Section 8.4, Setup 1 Page: Airspace Alarms for information on enabling airspace alert messages.
Viewing an airspace alert message:
1) Press the MSG Key. The Messages Page appears
with the alert message (Figure 1-28).
Figure 1-28 Message Page
2) Press the MSG Key again to return to the
previous display.
Note that the airspace alerts are based upon three­dimensional data (latitude, longitude, and altitude) to avoid nuisance alerts. The alert boundaries for controlled airspace are also sectorized to provide complete information on any nearby airspace. Additional information about a nearby airspace (such as controlling agency, frequency, and floor/ceiling limits) is available from the Nearest Airspace Page (Section 7.9).
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Viewing additional airspace information:
1) Press the small right knob to activate the
cursor.
2) Turn the large airspace from the list.
3) Press the ENT Key to view the airspace information.
GPS 400 Pilot’s Guide and Reference
right knob to select the desired
SECTION 1
INTRODUCTION
Flight Plans (FPL)
The GPS 400 lets the pilot create up to 20 flight plans, with up to 31 waypoints in each flight plan. Flight plans are created, edited, and activated using the FPL Key. The FPL Page Group includes two pages: the Active Flight Plan Page and the Flight Plan Catalog Page (Figures 1-29 and 1-30). The Active Flight Plan Page provides information and editing features for the flight plan currently in use (referred to as ‘flight plan 00’). The Flight Plan Catalog Page serves as the main page for creating new flight plans, as well as editing or activating previously created flight plans.
Figure 1-29 Active Flight Plan Page
Since using flight plans is arguably one of the more complex features of the GPS 400, it will only be discussed briefly here, with focus on creating a new flight plan and activating it to use for navigation. After reading through this brief introduction, answers to additional questions about flight plans can be found in Section 4, Flight Plans.
Creating a new flight plan:
1) Press the
2) Turn the small
FPL Key.
right knob to select the Flight
Plan Catalog Page.
3) Press the
MENU Key to display the Flight Plan
Catalog Page Menu (Figure 1-31).
Figure 1-31 Flight Plan Catalog Page Menu
Figure 1-30 Flight Plan Catalog Page
GPS 400 Pilot’s Guide and Reference
4) Turn the large right knob to select ‘Create New Flight Plan?’ and press the ENT Key.
5) The cursor appears on the first waypoint identifier field (located directly below ‘WAYPOINT’). Use the large and small
right knobs to enter the
identifier of the first waypoint in the flight plan. (The small knob is used to select the desired letter or number and the large knob is used to move to the next character space.)
6) Press the ENT Key once the identifier has been selected. The cursor moves to the next blank waypoint identifier field.
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7) Repeat steps 5 and 6 until all waypoints for the flight plan have been entered (Figure 1-32).
Figure 1-32 Enter Flight Plan Waypoints
Once the flight plan is created, it may be activated from the Flight Plan Catalog Page Menu. Activating the flight plan places it into ‘flight plan 00’ (a copy of it still resides in the original catalog location) and replaces any flight plan which currently exists in ‘flight plan 00’.
Activating the new flight plan:
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1) Press the
MENU Key to display the Flight Plan
Catalog Page Menu.
2) Turn the small
right knob to select ‘Activate
Flight Plan?’ (Figure 1-33) and press the ENT Key
Figure 1-33 Flight Plan Catalog Page Menu
GPS 400 Pilot’s Guide and Reference

SECTION 2: NAV PAGES

2.1 MAIN PAGE GROUPS

SECTION 2
NAV PAGES
The GPS 400’s main pages are divided into four separate page groups: NAV, WPT, AUX, and NRST (Table 2-1). Each page group is comprised of multiple pages. The page groups are selected using the large right knob. The individual pages are selected using the small right knob.
Page Groups
NAV Group WPT Group AUX Group NRST Group
7 NAV Pages
see Section 6 see Section 8 see Section 7
Table 2-1 Page Groups
The bottom right corner of the screen (Figure 2-1) indicates which page group is currently being displayed (e.g., NAV, WPT, AUX, or NRST), the number of pages available within that group (indicated by the square icons) and the placement of the current page within that group (indicated by a highlighted square icon).
The bottom right corner of the screen is also used to display the GPS 400’s turn advisories (‘Turn to 230°’) and waypoint alerts (‘Next DTK 230°’) during flight plan and approach operations. See Section 5 for more information.
Position of
Current Page
within Current
Page Group
Current Page Group
Figure 2-1 Current Page and Page Group
Number of Pages in
Current Page Group
Selecting the desired page group (from any page):
Press and hold the CLR Key to select the
Default NAV Page. Turn the large
right knob
to select the desired page group (Table 2-1 and Figure 2-1).
Selecting the desired page within the group:
Turn the small right knob to select the desired
page (Figures 2-1 and 2-2).
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Default NAV
Map
TERRAIN
NAV/COM
Position
Satellite Status
VNAV
(if configured)
NAV PAGES

2.2 NAV PAGE GROUP

The NAV Page Group includes seven pages (Figure 3-2). While viewing any NAV page, turn the small right knob to select a different NAV page. The pilot may find this selection process convenient to cycle between the Default NAV Page and the Map Page, two of the most frequently used pages. Other pages are provided for terrain information, (if configured for TERRAIN) to list frequencies for the flight plan, to show the current position, to display current satellite reception, and to make vertical navigation settings.
Figure 2-2 NAV Pages
NOTE: The NAV Page Group may have eight or
nine NAV pages available when the GPS 400 installation includes connection to traffic and/or weather information sources. See Section 10 of this manual for more information.

2.3 DEFAULT NAV PAGE

The first NAV page is the Default NAV Page (Figure 2-3). This page may be quickly selected from any page by pressing and holding the CLR Key.
Active Leg of Flight Plan
TO/FROM Flag
User-selectable
Data Fields
Current Page Group
Figure 2-3 Default NAV Page
The Default NAV Page displays a graphic course deviation indicator (CDI) across the top of the page. Unlike the angular limits used on a mechanical CDI coupled to a VOR or ILS receiver, full scale limits for this CDI are defined by a GPS-derived distance (0.3, 1.0, or
5.0 nm), as indicated at both ends of the CDI. By default, the CDI scale automatically adjusts to the desired limits based upon the current phase of flight: enroute, terminal area, or approach. The pilot may also manually select the desired scale setting as outlined in Section 8.4.
The graphic CDI shows the aircraft’s position at the center of the indicator, relative to the desired course (the moving course deviation needle). As with a traditional mechanical CDI, when off course simply steer toward the needle. The TO/FROM arrow in the center of the scale indicates whether the aircraft is heading TO (up arrow) the waypoint or FROM the waypoint (down arrow).
Course Deviation
Indicator (CDI)
Position of
Current Page
within Current
Page Group
Number of Pages in
Current Page Group
2-2
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NAV PAGES
NOTE: The GPS 400 always navigates TO a
waypoint unless the OBS switch is set (preventing automatic waypoint sequencing), or the aircraft has passed the last waypoint in the flight plan.
Directly below the CDI appears the active leg of the flight plan, or the direct-to destination when using the Direct-to Key. This automatically sequences to the next leg of the flight plan as the aircraft reaches each interim waypoint. If no flight plan or direct-to destination has been selected, the destination field remains blank.
The symbols in Table 2-2 are used on the Default NAV Page (directly below the CDI), to depict the ‘active leg’ of a flight plan or direct to:
Symbol Description
Direct-to a Waypoint
Course to a Waypoint, or Desired Course between Two Waypoints
Procedure Turn
Procedure Turn
Vectors-to-Final
Selecting Desired On-Screen Data
At the bottom of the Default NAV Page there are six user-definable fields which display the data needed as the flight progresses (Figure 2-3). By default these fields display: distance to destination (DIS), desired track (DTK), bearing to destination (BRG), ground speed (GS), ground track (TRK) and estimated time enroute (ETE). However, each of these fields can be customized to display a different data item. Available data items include:
• Bearing to destination (BRG)
• Course to steer (CTS)
• Cross track error (XTK)
• Desired
• Distance to destination (
• Enroute safe altitude (ESA)
• Estimated time of arrival (ETA)
• Estimate time enroute (
• Fuel flow (FLOW) (when configured)
• Ground speed (GS)
• Ground
track (DTK)
DIS)
ETE)
track (TRK)
DME Arc to the Left
DME Arc to the Right
Left-hand Holding Pattern
Right-hand Holding Pattern
Table 2-2 NAV Page Symbols
• Minimum safe altitude (
• Track angle error (TKE)
• Vertical speed required (
If no flight plan or direct-to destination has been selected, only speed, track, altitude, and minimum safe altitude data may be displayed. All other data types appear as blank lines on the Default NAV Page until a destination is selected.
GPS 400 Pilot’s Guide and Reference
MSA)
VSR)
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NAV PAGES
Selecting a different data item for any data field:
1) Starting with the Default NAV Page, press the
MENU Key to display the Default NAV Page Menu (Figure 2-4).
Figure 2-4 Default NAV Page Menu
2) The ‘Change Fields?’ option is already
highlighted, so press the ENT Key to select this option.
3) Use the large
right knob to highlight the data
field to be changed (Figure 2-5).
4) Turn the small right knob to display the list
of available data items (Figure 2-6). Continue turning the small right knob to select the desired data item from the list.
Figure 2-6 Select Field Type Window
5) Press the ENT Key to select the desired data
item and return to the Default NAV Page.
6) Press the small right knob momentarily to
remove the cursor from the page.
2-4
Figure 2-5 ‘DIS’ Field Highlighted
GPS 400 Pilot’s Guide and Reference
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