Garmin G1000 - Piper PA-32 User guide

Type
User guide

This manual is also suitable for

Piper
PA32
Copyright © 2007 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0648.05 or later for the Piper PA32. Some differences in operation may be
observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200 Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411 Fax 503/364.2138
Garmin (Europe) Ltd., Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, Hampshire S051 9DL, U.K.
Tel: 44/0870.851241 Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199 Fax: 886/02.2642.9099
Website Address: www.garmin.com
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 G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts™, and SafeTaxi™ are trademarks of
Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® and SkyWatch® are registered trademarks of L-3 Communications;
and XM® is a registered trademark of XM Satellite Radio, Inc.
April 2007 Printed in the U.S.A.
190-00692-00 Rev. B
Garmin G1000 Pilot’s Guide for Piper PA32
i
LIMITED 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.
Garmin G1000 Pilot’s Guide for Piper PA32
190-00692-00 Rev. Bii
WARNINGS, CAUTIONS, AND NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function.
The G1000 Terrain Proximity 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 Proximity 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 displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be
relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current
aeronautical charts for appropriate minimum clearance altitudes.
WARNING: The Garmin G1000 has a very high degree of functional integrity. However, the pilot must
recognize that providing monitoring and/or self-test capability for all conceivable system failures is not
practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication
shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of
cross-checking with all redundant or correlated information available in the cockpit.
WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and
could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data
Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always
use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.
WARNING: The Jeppesen database used in the G1000 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 G1000 package. Pilots using an outdated database do so entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is
intended only to supplement other approved navigation data sources and should be considered as an aid to
enhance situational awareness.
WARNING: Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually
acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual
acquisition of conflicting traffic.
WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm
penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather
avoidance, not penetration.
WARNING: XM Weather should not be used for hazardous weather penetration. Weather information
provided by the GDL 69 is approved only for weather avoidance, not penetration.
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Garmin G1000 Pilot’s Guide for Piper PA32
iii
WARNINGS, CAUTIONS, AND NOTES
WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent
delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for
short-range weather avoidance.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
CAUTION: The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy
and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be
misused or misinterpreted and, therefore, become unsafe.
CAUTION: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation and the Piper PA32 Pilot’s Operating Handbook (POH). Thoroughly practice
basic operation prior to actual use. During flight operations, carefully compare indications from the G1000
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 illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate
a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airman’s Information
Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an
intense radar echo”.
CAUTION: The Garmin G1000 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.
CAUTION: The GDU 104X PFD and MFD displays use a lens 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 lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
NOTE: All visual depictions contained within this document, including screen images of the G1000 panel
and displays, are subject to change and may not reflect the most current G1000 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.
Garmin G1000 Pilot’s Guide for Piper PA32
190-00692-00 Rev. Biv
WARNINGS, CAUTIONS, AND NOTES
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.
NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms
that can cause isolated discharge points in the strike display mode. However, clusters of two or more
discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after
the screen has been cleared.
190-00692-00 Rev. B
Garmin G1000 Pilot’s Guide for Piper PA32
v
REVISION INFORMATION
Record of Revisions
Part Number
Revision Date Page Range Description
190-00692-00
190-00692-00
190-00692-00
1
A
B
1/15/07
3/15/07
4/4/07
i – I-4
All
All
Initial release
Production release
Editorial changes
Garmin G1000 Pilot’s Guide for Piper PA32
190-00692-00 Rev. Bvi
TABLE OF CONTENTS
SECTION 1 SYSTEM OVERVIEW
1.1 System Description ..............................................1-1
1.2 Line Replaceable Units (LRU) ..............................1-2
1.3 G1000 Controls .....................................................1-7
PFD/MFD Controls .....................................................1-7
Audio Panel Controls .................................................1-9
1.4 Secure Digital (SD) Cards ..................................1-12
1.5 System Power-up ................................................1-13
1.6 System Operation ...............................................1-14
Normal Display Operation ........................................1-14
Reversionary Display Operation ................................1-14
AHRS Operation ......................................................1-15
G1000 System Annunciations ...................................1-17
Softkey Function ......................................................1-17
1.7 Accessing G1000 Functionality ........................1-25
Menus ....................................................................1-25
MFD Page Groups ....................................................1-25
MFD System Pages ..................................................1-29
1.8 Display Backlighting ..........................................1-38
Automatic Adjustment .............................................1-38
Manual Adjustment .................................................1-38
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments ................................................2-4
Airspeed Indicator .....................................................2-4
Attitude Indicator ......................................................2-6
Altimeter ..................................................................2-7
Vertical Speed Indicator (VSI) ......................................2-8
Vertical Deviation, Glideslope, and Glidepath Indicators 2-9
Horizontal Situation Indicator (HSI) ...........................2-10
Course Deviation Indicator .......................................2-14
2.2 Supplemental Flight Data .................................2-21
Generic Timer ..........................................................2-21
System Time ............................................................2-22
Outside Air Temperature ...........................................2-23
Wind Data ..............................................................2-23
Vertical Navigation (VNV) Indications ........................2-24
2.3 PFD Annunciations and Alerting Functions .....
2-25
G1000 Alerting System .............................................2-25
Marker Beacon Annunciations ..................................2-26
Traffic Annunciation .................................................2-26
TAWS Annunciations ................................................2-27
Altitude Alerting ......................................................2-27
Minimum Descent Altitude/Decision Height Alerting ...2-28
2.4 Abnormal Operations ........................................
2-29
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display .............................................................3-2
3.2 Engine Page ..........................................................3-4
Engine Temperature Group .........................................3-6
Electrical Group .........................................................3-7
Fuel Calculations Group .............................................3-7
3.3 EIS Display in Reversionary Mode ......................
3-8
Lean Display .............................................................3-9
System Display ........................................................3-12
SECTION 4 AUDIO PANEL AND CNS
4.1 Overview ...............................................................4-1
PFD/MFD Controls and Frequency Display ....................4-2
Audio Panel Controls .................................................4-4
4.2 COM Operation .....................................................4-6
COM Transceiver Selection and Activation ....................4-6
COM Transceiver Manual Tuning .................................4-7
Quick-Tuning and Activating 121.500 MHz ...................4-8
Auto-Tuning the COM Frequency .................................4-9
Frequency Spacing ...................................................4-13
Automatic Squelch ...................................................4-14
Volume ...................................................................4-14
4.3 NAV Operation ....................................................4-15
NAV Radio Selection and Activation ..........................4-15
NAV Receiver Manual Tuning ....................................4-16
Auto-Tuning the NAV Frequency ................................4-18
Marker Beacon Receiver ...........................................4-23
DME Tuning (Optional) .............................................4-24
4.4 GTX 33 Mode S Transponder .............................4-25
Transponder Controls ...............................................4-25
Transponder Mode Selection .....................................4-26
Entering a Transponder Code ....................................4-28
IDENT Function .......................................................4-30
Flight ID Reporting ..................................................4-31
4.5 Additional Audio Panel Functions ....................4-32
Power-Up ................................................................4-32
Mono/Stereo Headsets .............................................4-32
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TABLE OF CONTENTS
Speaker ..................................................................4-32
Intercom .................................................................4-33
Passenger Address (PA) System .................................4-35
Clearance Recorder and Player ..................................4-35
Split COM ...............................................................4-36
Entertainment Inputs ...............................................4-37
4.6 Audio Panel Preflight Procedure ......................4-38
4.7 Abnormal Operation ..........................................4-39
Stuck Microphone ....................................................4-39
COM Tuning Failure ..................................................4-39
Audio Panel Fail-Safe Operation ................................4-39
Reversionary Mode ..................................................4-39
SECTION 5 GPS NAVIGATION
5.1 Introduction ..........................................................5-1
5.2 Navigation Map (MFD) ........................................5-2
Dead Reckoning ........................................................5-2
Navigation Map Page .................................................5-4
5.3 PFD Inset Map and Windows ............................5-29
Inset Map ...............................................................5-29
PFD Windows ..........................................................5-31
5.4 Direct-to-Navigation (MFD) .............................5-32
Selecting a Direct-to Waypoint ..................................5-33
Clearing Vertical Constraints ....................................5-34
Specifying a Course to a Waypoint ............................5-35
Canceling Direct-to Navigation ................................5-36
Direct-to Navigation Shortcuts .................................5-37
5.5 Direct-to-Navigation (PFD) ..............................5-40
5.6 Airport Information (MFD) ................................5-43
Duplicate Waypoints ................................................5-45
Additional Airport Runway Information ......................5-45
5.7 Intersection Information (MFD) ........................5-47
5.8 NDB Information (MFD) .....................................5-48
5.9 VOR Information (MFD) .....................................5-49
5.10 User Waypoint Information (MFD) ...................5-50
5.11 Nearest Airports (MFD) ......................................5-54
5.12 Nearest Intersections (MFD) .............................5-56
5.13 Nearest NDB (MFD) ............................................5-57
5.14 Nearest VOR (MFD) ............................................5-58
5.15 Nearest User Waypoint (MFD) ..........................5-59
5.16 Nearest Airspaces ...............................................5-61
5.17 Nearest Airports (PFD) .......................................5-64
5.18 Flight Planning (MFD) .......................................5-66
Airways/Jetways ......................................................5-78
Display of Airways on the Flight Plan Page .................5-86
Vertical Navigation (VNV) .........................................5-91
Navigating an Example Flight Plan ............................5-98
Parallel Track (PTK) ................................................5-121
5.19 F
light Planning (PFD) ......................................5-124
Operations ............................................................5-124
5.20 Procedures
(MFD) .............................................5-130
Leg Types Supported by the G1000 ..........................5-130
5.21 Procedures
(PFD) ..............................................5-142
Operations ............................................................5-142
SECTION 6 HAZARD AVOIDANCE
6.1 XM Satellite Weather ...........................................6-1
Activating Services .....................................................6-1
Using XM Satellite Weather Products ...........................6-3
Weather Softkeys .......................................................6-5
Legend .....................................................................6-6
Setting Up the Weather Data Link Page .....................6-24
Setting Up XM Weather on the Navigation Map .........6-28
6.2 Stormscope WX-500 Series II Sensor ...............6-30
Setting Up Stormscope on the Navigation Map ..........6-30
Selecting the Stormscope Page .................................6-34
Stormscope Operation with Loss of Heading Input ......6-36
6.3 Terrain Pro
ximity ................................................6-37
Requirements ..........................................................6-37
GPS Position and GPS-MSL Altitude ...........................6-37
Displaying Terrain Proximity Data ..............................6-38
Terrain Proximity Page ..............................................6-40
Navigation Map Page ...............................................6-42
6.4 TAWS
..................................................................6-44
Requirements ..........................................................6-44
Computing GPS Altitude for TAWS .............................6-44
Using TAWS ............................................................6-45
TAWS Symbols ........................................................6-49
TAWS Alerts ............................................................6-50
6.5 Traffic ...................................................................
6-58
Traffic Information Service (TIS) .................................6-58
L-3 SKYWATCH Traffic Advisory System .....................6-66
6.6 Hazard Displays with Loss of GPS Pos
ition .....6-70
Garmin G1000 Pilot’s Guide for Piper PA32
190-00692-00 Rev. Bviii
TABLE OF CONTENTS
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
SECTION 8 ADDITIONAL FEATURES
8.1 SafeTaxi .................................................................8-1
SafeTaxi Cycle Number and Revision ...........................8-4
8.2 ChartView ..............................................................8-7
ChartView Softkeys ....................................................8-7
Terminal Procedures Charts ........................................8-8
Chart Options ..........................................................8-18
Day/Night View .......................................................8-23
ChartView Cycle Number and Expiration Date ............8-25
8.3 FliteCharts ...........................................................8-29
FliteCharts Softkeys .................................................8-29
Terminal Procedures Charts ......................................8-30
Chart Options ..........................................................8-38
Day/Night View .......................................................8-41
FliteCharts Cycle Number and Expiration Date ............8-43
8.4 XM Radio Entertainment (Optional) ................8-47
XM Satellite Radio Service ........................................8-47
XM Service Activation ..............................................8-48
Using XM Radio ......................................................8-49
8.5 Abnormal Operation ..........................................8-53
APPENDICES
Annunciations and Alerts ..............................................A-1
Alert Level Definitions ................................................A-2
Aircraft Alerts ............................................................A-3
TAWS Alerts ..............................................................A-4
TAWS System Status Annunciations .............................A-5
Other G1000 Aural Alerts ...........................................A-5
G1000 System Message Advisories ..............................A-5
SD Card Use ....................................................................
B-1
Jeppesen Databases ...................................................B-1
Garmin Databases .....................................................B-2
Glossary ...........................................................................C-1
Frequently Asked Questions .........................................D-1
General TIS Information ................................................ E-1
Introduction .............................................................. E-1
TIS vs. TAS/TCAS ........................................................ E-1
TIS Limitations ..........................................................E-1
Display Symbols ............................................................. F-1
INDEX
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Garmin G1000 Pilot’s Guide for Piper PA32
1-1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section is designed to provide an overview of the G1000 Integrated Flight Deck as installed in the Piper
PA32 aircraft. This includes the PA32 R-301 (Saratoga II HP) and the PA32 R-301 T (Saratoga II TC), as well as
the PA32-301 FT (Piper 6X) and the PA32-301 XTC (Piper 6XT).
The G1000 system is an integrated flight control system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot through large-format displays. The system consists of
the following Line Replaceable Units (LRUs):
GDU 1040
Primary Flight Display (PFD)
GDU 1040
Multi Function Display (MFD)
GIA 63W
Integrated Avionics Unit (IAU)
GDC 74A
Air Data Computer (ADC)
GEA 71
Engine/Airframe Unit
GRS 77
Attitude and Heading Reference System
(AHRS)
GMU 44
Magnetometer
GMA 1347
Audio System with Integrated Marker
Beacon Receiver
GTX 33
Mode S Transponder
GDL 69/69A
Data Link
A top-level G1000 system block diagram is shown in Figure 1-1. The following equipment is also connected
to the G1000 system and interfaces with the GIA 63W:
L-3 STORMSCOPE
®
WX-500 Series II Weather Mapping Sensor
L-3 SKYWATCH
®
Traffic Advisory System
S-TEC System Fifty Five X
®
Autopilot
Honeywell
®
KN 63 DME Transceiver
Honeywell
®
KR 87 ADF Receiver
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Garmin G1000 Pilot’s Guide for Piper PA32
1-2
SYSTEM OVERVIEW
1.2 LINE REPLACEABLE UNITS (LRU)
GDU 1040
The GDU 1040 features a 10.4-inch LCD display with 1024 x 768 resolution. The left display
is configured as a PFD and the right display is configured as an MFD. The GDU 1040 links and displays all
functions of the G1000 system during flight. The displays communicate with each other through a High-Speed
Data Bus (HSDB) Ethernet connection. Each display is also paired via an Ethernet connection with a GIA 63W
Integrated Avionics Unit.
GIA 63W
(2) Functions as the main communication hub, linking all LRUs with the PFD. Each GIA 63W contains
a GPS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors.
The GIA 63W also contains a GPS WAAS receiver. Each GIA is paired with a respective GDU 1040 display
through Ethernet. The GIAs are not paired together and do not communicate with each other directly.
GDC 74A
(1) Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure
altitude, airspeed, vertical speed, and OAT information to the G1000 system, and it communicates with the
GIA 63W, GDU 1040, and GRS 77 using an ARINC 429 digital interface. The GDC 74A also interfaces directly
with the GTP 59. The GDC 74A is designed to operate in Reduced Vertical Separation Minimum (RVSM)
airspace.
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Garmin G1000 Pilot’s Guide for Piper PA32
1-3
SYSTEM OVERVIEW
GEA 71
(1) Receives and processes signals from the engine and airframe sensors. This unit communicates
with both GIA 63Ws using an RS-485 digital interface.
GRS 77
(1) – Provides aircraft attitude and heading information via ARINC 429 to both the GDU 1040 and the
GIA 63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces
with the on-side GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air data, and with
both GIAs to obtain GPS information. AHRS modes of operation are discussed later in this document.
GMU 44
(1) Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft
magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77
using an RS-485 digital interface.
GMA 1347
The GMA 1347 Audio Panel integrates NAV/COM digital audio, intercom system, and marker
beacon controls. The GMA 1347 also controls manual display reversionary mode (red
DISPLAY BACKUP
button) and is installed between the MFD and the PFD. The GMA 1347 communicates with both GIA 63Ws
using an RS-232 digital interface.
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Garmin G1000 Pilot’s Guide for Piper PA32
1-4
SYSTEM OVERVIEW
GTX 33
(1) The GTX 33 is a solid-state, Mode-S transponder that provides Modes A, C, and S operation.
The GTX 33 is controlled through the PFD and communicates with both GIA 63Ws through an RS-232 digital
interface.
GDL 69/69A
(1) A satellite radio receiver that provides real-time weather information to the G1000 MFD
(and indirectly, to the inset map of the PFD) as well as optional digital audio entertainment. The GDL 69/69A
communicates with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required
to enable the GDL 69/69A capability.
GSA 81
(3), and
GSM 85A
The GSA 81 servos are used for the automatic control of roll, pitch, and pitch
trim. These units interface with each GIA 63W.
The GSM 85A servo mount is responsible for transferring the output torque of the GSA 81 servo actuator to the
mechanical flight-control surface linkage.
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Garmin G1000 Pilot’s Guide for Piper PA32
1-5
SYSTEM OVERVIEW
Figure 1-1 Basic G1000 System
No. 1 GIA 63W
Integrated Avionics Unit
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
No. 2 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
GTX 33
Transponder
High-Speed Data Bus (Ethernet)
Reversionary
Control
GEA 71
Engine/Airframe
Unit
GDC 74A
Air Data
Computer
OAT
Airspeed
Altitude
Ve
rtical Speed
GRS 77
AHRS
Attitude
Rate of Turn
Slip/Skid
GMU 44
Magnetometer
Heading
GPS Output
GPS Output
Reversionary
Control
GMA 1347
Audio Panel
PFD
GDU 1040
S-TEC System
Fifty-Five
X
Autopilot
MFD
GDU 1040
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Garmin G1000 Pilot’s Guide for Piper PA32
1-6
SYSTEM OVERVIEW
High-Speed Data Bus (Ethernet)
No. 2 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
L3
Stormscope
Lightning Strike and
Thunderstorm Detection
(optional)
Honeywell
KR 87
ADF Receiver
(optional)
Honeywell
KN 63
DME Transceiver
(optional)
GDL 69/69A
Data Link
Real-time Weather
Digital Audio Entertainment
S-TEC System
Fifty Five X
Autopilot
L-3
Skywatc
h
Traffic Avoidance
System
(Optional)
No. 1 GIA 63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
Figure 1-2 Additional G1000 Interfaces
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Garmin G1000 Pilot’s Guide for Piper PA32
1-7
SYSTEM OVERVIEW
1.3 G1000 CONTROLS
NOTE: The Audio Panel (GMA 1347) is described in the CNS & Audio Panel section. The autopilot controls
are described in the S-TEC System Fifty Five X Autopilot manufacturer’s documentation.
The G1000 system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD
and MFD are discussed in the following pages of this section.
PFD/MFD CONTROLS
Figure 1-3 PFD/MFD Controls
1 2 4 6
12
8
7
5
13
9
17
11
3
16
15
3
Dual NAV Knob
1
NAV VOL / ID Control
2
NAV Frequency Transfer Key
12
CLR Key (DFLT MAP)
11
FPL Key
10
Direct-to Key
4
Heading Knob
6
CRS/BARO Knob
COM VOL/SQ Knob
9
13
Dual FMS Knob
14
MENU Key
8
COM Frequency Transfer Key
7
Dual COM Knob
5
Joystick
15
PROC Key
16
ENTKey
17
Dual ALT Knob
10
14
190-00692-00 Rev. B
Garmin G1000 Pilot’s Guide for Piper PA32
1-8
SYSTEM OVERVIEW
PFD and MFD controls function the same way, except where indicated.
1
NAV VOL/ID Knob
Controls the NAV audio level. Press to toggle the Morse code identifier ON and OFF.
Volume level is shown in the field as a percentage.
2
NAV Frequency Transfer Key
– Transfers the standby and active NAV frequencies.
3
Dual
NAV Knob
Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV
receiver. Press to toggle the tuning cursor (light blue box) between the NAV1 and NAV2 fields.
4
Heading Knob
– Turn to manually select a heading on the HSI. When pressed, it synchronizes the heading
bug with the compass lubber line. Selected heading provides the heading reference to the Flight Director
while operating in Heading Select mode.
5
Joystick
Changes the map range (distance top to bottom of map display) when rotated. Activates the map
pointer when pressed.
6
CRS/BARO Knob
The large
knob sets the altimeter barometric pressure and the small
knob adjusts the
course. The course is only adjustable when the HSI is in VOR1, VOR2, or OBS/SUSP mode. Pressing this
knob centers the CDI on the currently selected VOR. Selected course provides course reference to the Flight
Director when operating in Navigation and Approach modes.
7
Dual COM Knob
Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM
transceiver. Pressing this knob toggles the tuning cursor (light blue box) between the COM1 and COM2
fields.
8
COM Frequency Transfer Key
Transfers the standby and active COM frequencies. Pressing and holding
this key for two seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency
field.
9
COM
VOL/SQ Knob
Controls COM audio level. Audio volume level is shown in the field as a percentage.
Pressing this knob turns the COM automatic squelch ON and OFF.
10
Direct-to Key
– Allows the user to enter a destination waypoint and establish a direct course to the selected
destination (specified by the identifier, chosen from the active route, or taken from the map pointer
position).
11
FPL Key
Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing
stored flight plans.
12
CLR
Key (DFLT MAP)
Erases information, cancels an entry, or removes page menus. To display the
Navigation Map Page immediately, press and hold
CLR
(MFD only).
13
Dual FMS Knob
Used to select the page to be viewed (only on the MFD). The large
knob selects a page
group (MAP, WPT, AUX, NRST), while the small
knob selects a specific page within the page group. Pressing
the small
knob turns the selection cursor ON and OFF. When the cursor is ON, data may be entered in the
different windows using the small and large
knobs. The large
knob is used to move the cursor on the page,
while the small
knob is used to select individual characters for the highlighted cursor location. When the
G1000 displays a list that is too long for the display screen, a scroll bar appears along the right side of the
display, indicating the availability of additional items within the selected category. Press the small
FMS
Knob
to activate the cursor and turn the large
FMS
Knob to scroll through the list.
190-00692-00 Rev. B
Garmin G1000 Pilot’s Guide for Piper PA32
1-9
SYSTEM OVERVIEW
14
MENU Key
Displays a context-sensitive list of options. This list allows the user to access additional features
or to make setting changes that relate to certain pages.
15
PROC Key
Selects approaches, departures, and arrivals from the flight plan. If a flight plan is used, available
procedures for the departure and/or arrival airport are automatically suggested. If a flight plan is not used,
the desired airport and the desired procedure may be selected. This key selects IFR departure procedures
(DPs), arrival procedures (STARs), and approaches (IAPs) from the database and loads them into the active
flight plan.
16
ENT Key
Accepts a menu selection or data entry. This key is used to approve an operation or complete
data entry. It is also used to confirm selections and information entries.
17
Dual
ALT Knob
Sets the selected altitude in the box located above the Altimeter. The
large
knob selects
the thousands, while the small
knob selects the hundreds. Altitude Select is used by the Automatic Flight
Control System in certain modes, in addition to the standard G1000 Altitude Alerter function.
AUDIO PANEL CONTROLS
Figure 1-4 Audio Panel Controls (GMA 1347)
17
18
15
13
11
9
20
7
5
3
1
14
2
16
4
6
8
10
12
22
24
23
21
19
190-00692-00 Rev. B
Garmin G1000 Pilot’s Guide for Piper PA32
1-10
SYSTEM OVERVIEW
NOTE: When a key is selected, a triangular annunciator above the key is illuminated.
1
COM1 MIC
Selects the #1 transmitter for transmitting. COM1 receiver is simultaneously selected when
this key is pressed, allowing received audio from the #1 Com receiver to be heard. COM2 receiver audio
can be added by pressing the COM2 Key.
2
COM1
– When selected, audio from the #1 Com receiver can be heard.
3
COM2 MIC
Selects the #2 transmitter for transmitting. COM2 receiver is simultaneously selected when
this key is pressed, allowing received audio from the #2 Com receiver to be heard. COM2 can be deselected
by pressing the COM2 Key, or COM1 can be added by pressing the COM1 Key.
4
COM2
– When selected, audio from the #2 Com receiver can be heard.
5
COM3 MIC
– Not used.
6
COM3
– Not used.
7
COM 1/2
– Split COM is disabled.
8
TEL
– Not used.
9
PA
Selects the passenger address system. The selected Com transmitter is deselected when the PA Key
is pressed.
10
SPKR
– Pressing this key selects and deselects the corresponding cockpit speaker. Com and Nav receiver
audio will be heard on the speaker.
11
MKR/MUTE
Mutes the currently received Marker Beacon Receiver audio. Unmutes when new marker
beacon audio is received. Also stops play of the Clearance Recorder.
12
HI SENS
– Press to increase Marker Beacon Receiver sensitivity. Press again to return to normal.
13
DME
– Pressing turns DME audio on or off.
14
NAV1
– When selected, audio from the #1 Nav receiver can be heard.
15
ADF
– Pressing turns on or off the audio from the ADF receiver.
16
NAV2
– When selected, audio from the #2 Nav receiver can be heard.
17
AUX
– Not used.
18
MAN SQ
Press to enable manual squelch for the intercom. When active, press the PILOT Knob to
illuminate ‘SQ’. Turn the PILOT/PASS Knobs to adjust squelch.
19
PLAY
– Press once to play the last recorded audio.
Press again to begin playing the previously recorded memory
block. Each subsequent press of the PLAY Key will begin playing the next recorded block
. Press the MKR/MUTE
Key to stop play.
20
PILOT
– Pressing selects the pilot intercom isolation. Press again to deselect pilot isolation.
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Garmin G1000 - Piper PA-32 User guide

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