Cockpit Reference Guide

ManualsBrandsGarmin ManualsFlight DecksGarmin Software Version 0648.02

Integrated Flight Deck

Piper

PA32

Summary of content (142 pages)

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Integrated Flight Deck Cockpit Reference Guide Piper PA32
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Copyright © 2004-2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reﬂects the operation of System Software version 0648.02 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.
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WARNINGS, CAUTIONS, & 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.
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WARNINGS, CAUTIONS, & 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: The Garmin G1000, as installed in the Piper PA32 aircraft, has a very high degree of functional integrity.
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WARNINGS, CAUTIONS, & NOTES 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. 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.
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RECORD OF REVISIONS Part Number 190-00416-00 Rev A Rev B 190-00416-01 Rev A 190-00416-01 Rev B Change Summary Initial release. Revised for system software version 0426.01 Added GDU 7.0 software parameters, WAAS, VNAV, electronic charts, TAWS, and full EIS display. Added GDU 8.00 parameters, Airways, new MFD splash screen Changed VNAV to VNV Revision Date of Revision Affected Pages C January, 2007 10-7, 10-13, 10-14 Description Corrected range display in Figure 10-11. Updated Figure 10-19.
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RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-4 MFD Softkeys .......................................................... 1-7 MFD Page Groups ................................................... 1-8 Vertical Navigation ................................................ 1-8 Backlighting ...............
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TABLE OF CONTENTS 7.7 VOR Information ................................................... 7-25 7.8 User Waypoint Information Page ..................... 7-26 7.9 Nearest Airports ................................................... 7-26 Nearest Airport Information on the MFD .................... 7-26 Nearest Airports Information on the PFD .................... 7-27 7.10 Nearest Intersections .......................................... 7-27 7.11 Nearest NDB ......................................................
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TABLE OF CONTENTS Pop-up Alerts .......................................................... 10-14 TAWS Alerts Summary ............................................. 10-15 Alert Annunciations ................................................. 10-16 SECTION 11: ABNORMAL OPERATION ..................... 11-1 11.1 11.2 11.3 11.4 Reversionary Mode .............................................. 11-1 Abnormal COM Operation .................................. 11-1 Unusual Attitudes ....................................
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TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to ﬁnd operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide.
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SECTION 1 SYSTEM OVERVIEW 1.
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SECTION 1 SYSTEM OVERVIEW (1) NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identiﬁer ON and OFF. Volume level is shown in the ﬁeld as a percentage. (2) NAV Frequency Transfer Key – Switches 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 switch the tuning cursor (light blue box) between the NAV1 and NAV2 ﬁelds.
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SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey ON Softkey OFF DME ALERTS VOR1 VOR2 GPS Figure 1-2 Top Level PFD Softkeys DME ALERTS STRMSCP ALERTS Press the BACK or OFF Softkey to return to the top-level softkeys. Figure 1-3 INSET Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD. OFF – Press to remove the Inset Map. DCLTR (3) – Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR Softkey.
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SECTION 1 SYSTEM OVERVIEW DME ALERTS DME ALT UNIT BRG1 (NAV1) BRG2 (NAV2) BRG1 (GPS) BRG2 (GPS) BRG1 (OFF) BRG2 (OFF) ALERTS Press the STD BARO or BACK Softkey to return to the top-level softkeys ALERTS METERS IN HPA ALERTS Figure 1-4 PFD Conﬁguration Softkeys PFD – Press to display the additional softkeys for additional conﬁgurations to the PFD. DFLTS – Press to reset default settings on the PFD. WIND – Displays softkeys to select wind data parameters.
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SECTION 1 SYSTEM OVERVIEW BKSP – Press to remove numbers entered one at a time. BACK – Press to return to the previous level softkeys. IDENT – Press to provide special aircraft position identiﬁcation to Air Trafﬁc Control (ATC) when the transponder is set to ON or ALT. IDENT – Press to provide special aircraft position identiﬁcation to Air Trafﬁc Control (ATC) when the transponder is set to ON or ALT. BACK – Press to return to the previous level softkeys.
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SECTION 1 SYSTEM OVERVIEW 1.3 MFD SOFTKEYS MAP – Pressing this softkey enables the following softkeys: TRAFFIC – Pressing this softkey displays/removes Trafﬁc on the Navigation Map. TOPO – Pressing this softkey displays or removes topographic information on the Navigation Map. TERRAIN – Pressing this softkey displays/removes terrain and obstacle data on the Navigation Map. ENGINE – Pressing this softkey makes available the full size Engine Display and functions.
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SECTION 1 SYSTEM OVERVIEW AIRWAYS – Pressing this softkey displays/removes airways information. The default is dependant on map setup option seledcted. Pressing cycles through all airways displayed (AIRWY ON), low altitude airways only (AIRWY LO), and high altitude airways only (AIRWY HI). STRMSCP (optional) – Pressing this softkey displays/ removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/ removes precipitation data on the Navigation Map.
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SECTION 1 SYSTEM OVERVIEW Since altitudes loaded with an arrival procedure are Altitudes that have been designated for use in vertical published only for turbojet aircraft, the altitudes are guidance may also be made “non-designated” by placing the displayed as white text indicating that the altitudes are cursor over the desired altitude and pressing the CLR Key. displayed for reference only.
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SECTION 1 SYSTEM OVERVIEW 1.6 BACKLIGHTING Manually adjust the backlight for the PFD Large White and MFD: Text 1) Press the MENU Key on the PFD to display the PFD Setup Menu window. Large Light Blue Text SmallLight Blue Text Figure 1-8 VNV Altitudes 2) Press the small FMS Knob to activate the cursor. ‘PFD DSPL > AUTO’ is now highlighted. 3) Turn the small FMS Knob to display the selection window.
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SECTION 1 SYSTEM OVERVIEW Jeppesen Aviation Database NOTE: After the aviation database is installed, the card may be removed after loading the update to each LRU. Updating the Jeppesen aviation database: 1) With the G1000 System OFF, insert the SD card containing the aviation database update into the top card slot of the PFD to be updated (Label of SD card facing left). 2) Turn the G1000 System ON.
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SECTION 1 SYSTEM OVERVIEW 5) Use the FMS Knob to enter a proﬁle name 6) Press the ENT Key. 7) In the next ﬁeld, use the small FMS Knob to select the desired settings upon which to base the new proﬁle. 8) Press the ENT Key. 9) With ‘CREATE’ highlighted, press the ENT Key to create the proﬁle. Selecting a Proﬁle Figure 1-13 Power-Up Splash Screen Window 3) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey.
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SECTION 1 SYSTEM OVERVIEW Deleting a Proﬁle 1) Select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Proﬁle Box. 4) Press the ENT Key. 5) In the ‘Delete Proﬁle’ window, turn the FMS Knob to select the proﬁle to be deleted. 6) Press the ENT Key. 7) With ‘DELETE’ highlighted, press the ENT Key.
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SECTION 1 SYSTEM OVERVIEW Blank Page 1-14 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
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SECTION 2 FLIGHT INSTRUMENTS 15 1 14 13 2 12 3 11 4 10 5 9 7 6 8 1 Trafﬁc Annunciation 9 Alerts Window 2 Vspeed References 10 Barometric Minimums Box 3 Selected Heading Box 11 Selected Course Box 4 Wind Data Window 12 Altitude Reference Bug 5 Inset Map 13 6 BRG1 Information Window 7 DME Information Window 8 BRG2 Information Window Barometric Minimums Bug 14 Vertical Deviation/Glidepath (WAAS enabled systems only)/Glidesope Indicator 15 Marker Beacon Annunciation Figure
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SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration/deceleration is maintained. Speed Ranges Actual Airspeed Airspeed Trend Vector Vspeed References Vspeed References Vspeeds are set using the TMR/REF Softkey. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale.
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SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Barometric Setting Box Altitude Reference Box Altitude Reference Bug Turn the BARO Knob to select the desired setting. Altitude Alerting Within 1000 ft Altitude Trend Vector Current Altitude Within 200 ft Figure 2-8 Altitude Alerting Visual Annunciations Visual annunciations appear in the Altitude Reference Box. Whenever the setting is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System.
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SECTION 2 FLIGHT INSTRUMENTS VNV Target Altitude Vertical Deviation Indicator Figure 2-9 Altimeter (Metric) 2.4 Required Vertical Speed Figure 2-10 Vertical Deviation Indications VERTICAL DEVIATION/GLIDEPATH/ GLIDESLOPE INDICATOR NOTE: VNV altitudes displayed on the Active Flightplan Page must be designated for use in vertical guidance. The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior to executing an approach (see Figure 2-10).
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SECTION 2 FLIGHT INSTRUMENTS The Glideslope Indicator appears when an ILS approach has been activated and an ILS is tuned in the active NAV receiver ﬁeld (see Figure 2-12). 2.6 VERTICAL SPEED INDICATOR Marker Beacon Annunciation Vertical Speed Pointer Glideslope Indicator Figure 2-14 Vertical Speed Indicator The actual vertical speed is displayed inside the pointer. Figure 2-12 Glideslope Indicator 2.5 MARKER BEACON ANNUNCIATIONS Outer Marker Middle Marker Inner Marker 2.
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SECTION 2 FLIGHT INSTRUMENTS The bug appears on the tape in light blue once in range. • When the aircraft passes through 100 feet of the MDA, the bug and text turn white. • Once the aircraft descends past the MDA, the bug and text turn yellow and the aural alert, “Minimums Minimums”, is generated. Alerting is inhibited while the aircraft is on the ground. If the aircraft climbs after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled.
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SECTION 2 FLIGHT INSTRUMENTS 2.9 HORIZONTAL SITUATION INDICATOR (HSI) 15 14 1 13 2 3 12 4 11 5 10 Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate.
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SECTION 2 FLIGHT INSTRUMENTS 1.0 nm decreasing to 350 feet depending on variables (see Figure Approach (LNAV+V) 2-23) Approach (LPV) Missed Approach �� Figure 2-23 Typical LNAV and LNAV+V Approach CDI Scaling �� Approach (LNAV) Approach (LNAV/ VNAV) �� 1.0 nm decreasing to a speciﬁed course width, then 0.3 nm, depending on variables (see Figure 2-24) 0.
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SECTION 2 FLIGHT INSTRUMENTS Bearing Pointers and Information Windows DME (optional) Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys. The BRG1 Pointer is a single line pointer. The BRG2 Pointer is a double line pointer. To display the DME Information Window, press the PFD Softkey followed by the DME Softkey.
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SECTION 2 FLIGHT INSTRUMENTS 2.10 GENERIC TIMER Figure 2-30 Timer Status Prompts Change the Generic Timer: 1) Press the TMR/REF Softkey, then turn the large FMS Knob to select the time ﬁeld (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN ﬁeld is now highlighted. Figure 2-29 GPS LOI, GPS SUSP, LOC1 and VOR2 Enable/disable OBS Mode while navigating with GPS: 1) Press the OBS Softkey to select OBS Mode.
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SECTION 2 FLIGHT INSTRUMENTS Blank Page 2-12 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 DEFAULT ENGINE DISPLAY In all cases white or green indicates normal operation, yellow indicates caution, and red indicates warning. Pressing the ENGINE Softkey makes available the full EIS Page, providing access to the ASSIST and fuel softkeys.
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SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.2 FULL EIS DISPLAY NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calculated from the last entered fuel remaining (GAL REM). In the FUEL CALC box, fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all calculated based on the last adjustment of the fuel remaining (GAL REM). Remaining fuel quantity does not reset when power is cycled. Press the ENGINE Softkey to display the full size engine display.
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SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Figure 3-4 Full Engine Display (Normally Aspirated) Leaning Assist (Normally Aspirated Engine Only) 1) Press the ENGINE Softkey. 2) Press the ASSIST Softkey. 3) Lean the mixture until one of the cylinder’s exhaust temperature peaks. This is indicated by ‘1st’ being displayed below the ﬁrst cylinder to peak. Press the ASSIST Softkey when ﬁnished leaning to remove the leaning function.
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SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Blank Page 3-4 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes share the same locations on the on the Primary Flight Display and the Multi-Function Display.
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SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected NAV Frequency Selected COM Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies. • Press to change tuning box positions.
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SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS 4.4 QUICKLY ACTIVATING 121.500 MHZ • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. Pressing and holding the COM Frequency Transfer Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. 4.
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SECTION 4 – NAV/COM & TRANSPONDER 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD 4.7 TRANSPONDER Mode Selection The STBY, ON, ALT, GND, VFR, CODE, and IDENT Softkeys can be accessed by pressing the XPDR Softkey. Ground Mode (Automatic or Manual) Figure 4-9 Nearest Airports Window (PFD) 1) Press the NRST Softkey to display the Nearest Airports Window. 2) Turn either FMS Knob to highlight the desired frequency. 3) Press the ENT Key to place the frequency in the standby ﬁeld of the active COM.
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SECTION 4 – NAV/COM & TRANSPONDER Altitude Mode (Automatic or Manual) Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey. All transponder replies requesting altitude information are provided with pressure altitude information. ALT Mode (Mode C Altitude Reporting) Enter Code Using Softkeys 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys.
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SECTION 4 – NAV/COM & TRANSPONDER Flight ID Reporting If so conﬁgured, the Flight ID may be entered in the Timer/Reference Window. Flight ID PFD Entry Figure 4-15 Timer/References Window 1) Press the TMR/REF Softkey to display the Timer/ References Window. 2) Turn the large FMS Knob to place the cursor in the Flight ID ﬁeld. 3) Turn the small FMS Knob to enter the desired ﬁrst character. 4) Turn the large FMS knob to place the cursor in the next desired ﬁeld.
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SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters (COM3 MIC is unavailable) Received Audio (COM 3 is unavailable) Split COM Telephone (Unavailable) Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio Aircraft Navigation Radio Audio (AUX unavailable) Manual Squelch Digital Clearance Recorder Play Key ICS Isolation VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1 Audio Panel Controls Garmin G
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SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. In this mode, both the pilot and the copilot can transmit simultaneously over separate radios. The pilot can still monitor NAV1, NAV2, and MKR audio as selected, but the copilot is only able to monitor COM2. 5.
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SECTION 5 – AUDIO PANEL Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity. Figure 5-6 Navigation Radios 5.5 Figure 5-5 Marker Beacon 5.4 NAV RADIO AUDIO SELECTION Pressing NAV1 or NAV2 selects and deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. Pushing the PUSH/VOL/ID Knob at this time allows the navigation facility identifer to be heard.
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SECTION 5 – AUDIO PANEL 5.6 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches between volume and squelch adjustment by lighting VOL or SQ respectively. • Pressing MKR/MUTE while playing a memory block stops play. • Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key will begin playing the next previously recorded block.
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SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL Refer to the pilot’s guide for the installed autopilot system.
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SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page 6-2 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The majority of the following discussions pertain to the Multi Function Display. In discussions pertaining to the PFD, the controls are located on the PFD. 7.1 NAVIGATION MAP PAGE WARNING: The map display should only be used for situational awareness. Any map display indication should be compared with approved navigation sources.
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SECTION 7 – NAVIGATION 9) Press the ENT Key. The cursor is placed in the ‘VNV’ offset distance ﬁeld. 10) Enter the desired target altitude offset from the selected Direct-to. 11) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘COURSE’ ﬁeld. Select a Direct-to Destination to a Nearest Airport 1) Press the Direct-to ( ) Key. 2) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list is displayed as in Figure 7-3.
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SECTION 7 – NAVIGATION 8) Press the ENT Key. 9) Turn the large FMS Knob to place the cursor in the ‘COURSE’ ﬁeld. 10) Enter the desired course. 11) Press the ENT Key. The cursor now highlights ‘ACTIVATE?’. Figure 7-5 Recently Entered Waypoints List (MFD) 3) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints as shown in Figure 75. 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
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SECTION 7 – NAVIGATION Enter a Direct-to Destination 1) Press the Direct-to Key ( ). Select a Direct-to Destination to a Flight Plan Waypoint 2) Turn the large FMS Knob to place the cursor in the desired selection ﬁeld. 1) While navigating an active ﬂight plan, press the Direct-to ( ) Key. 3) Turn the small FMS Knob to begin selecting the desired identiﬁer, location, etc. 2) Turn the small FMS Knob to the left to display a list of ﬂight plan waypoints as shown in Figure 7-8. 4) Press the ENT Key.
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SECTION 7 – NAVIGATION 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press ENT again to activate a Direct-to. Select a Direct-to Destination to a Recently Entered Identiﬁer 1) Press the Direct-to ( ) Key. 2) Turn the small FMS Knob to the left. Initially, a ﬂight plan waypoint list is displayed as in Figure 7-8. The list is only populated when navigating a ﬂight plan.
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SECTION 7 – NAVIGATION 2) Figure 7-11 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI ﬂight phase displayed on the HSI indicating 1.0 nm CDI scaling. 3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading 290° as seen in Figure 7-12. Note the current CDI ﬂight phase is now ENR (Enroute).
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SECTION 7 – NAVIGATION 4) V4 will now be entered into the ﬂight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight the point that proceeds V4 will be entered as shown in Figure 7-13. c) Turn the small FMS Knob to display the Waypoint Information Window. Enter the desired entry point for V4, in this case Topeka VOR (TOP) will be used as shown in Figure 7-14. Figure 7-14 Entering V4 Entry Point Figure 7-13 Begin Adding V4 to the Flight Plan d) Press the ENT Key.
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SECTION 7 – NAVIGATION e) With SLN still highlighted as in Figure 7-15, turn the small FMS Knob to the right. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available. f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7-16. Figure 7-17 List of Available Exits for V4 i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as seen in Figure 7-17.
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SECTION 7 – NAVIGATION l) V4 is now loaded into the ﬂight plan as shown in Figure 7-19. d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 7-21, the magenta arrow in the ﬂight plan window and magenta line on the map indicating V4 is now the active ﬂight plan leg. Note also, the crosstrack (XTK) distance on the HSI indicating 16.9 nm to the intercept point. Figure 7-19 V4 is Loaded in the Flight Plan 5) V4 will now be made the active leg of the ﬂight plan.
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SECTION 7 – NAVIGATION 6) The aircraft continues on heading 290º. When 2.0 nm from the intercept, the XTK will disappear from the HSI and the CDI will be positioned on the last dot indicating a 2.0 nm distance from the centerline of the next course. 8) At SLN, Victor Airway 244 (V244) will be intercepted. Turn prompts will be displayed in the PFD Navigation Status Box as seen in Figure 7-23. 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 7-22.
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SECTION 7 – NAVIGATION 10) At Lamar VOR (LAA) V263 will be intercepted. See Figure 7-25. Figure 7-26 Direct To OPSHN Figure 7-25 HYS to LAA Leg Active d) Turn the large FMS Knob to place the cursor in the VNV altitude ﬁeld as shown in Figure 7-27. 11) ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure. ATC advises to expect an altitude of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor.
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SECTION 7 – NAVIGATION f) Press the ENT Key. The cursor is now displayed in the VNV offset ﬁeld as shown in Figure 7-28. NOTE: If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database that will be used as is, the altitude must be manually accepted by placing the cursor over the desired altitude, then pressing the ENT Key. The altitude will now be displayed as light blue meaning it will now be used by the system to determine vertical speed and deviation guidance.
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SECTION 7 – NAVIGATION b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 7-30. d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 7-31. e) Press the ENT Key. A list of available transitions for the selected approach is displayed as shown on Figure 7-32. Figure 7-30 Proceudures Window c) Press the ENT Key. A list of available approaches for the destination airport will be displayed as in Figure 7-31.
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SECTION 7 – NAVIGATION g) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the ﬂight plan as seen in Figure 7-33. Figure 7-33 Loaded Approach 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 7-33. These altitudes are loaded from the database and are initially displayed as white text, indicating these values will not be used in computing vertical deviation guidance.
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SECTION 7 – NAVIGATION d) Turn the large FMS Knob to select the altitude constraint associated with FALUR as seen in Figure 7-35. Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values will always be displayed as white text, as in Figure 7-36.
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SECTION 7 – NAVIGATION a) Press the VNV PROF Softkey to place the cursor in the target vertical speed ﬁeld (VS TGT) as shown in Figure 7-37. b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob to select the desired selection ﬁeld, then turn the small FMS Knob to enter the desired value. 15) As seen in Figure 7-38, the aircraft is approaching TOD. Note the target vertical speed required to reached the selected altitude.
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SECTION 7 – NAVIGATION 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7-40. Keep Vertical Deviation Pointer Centered 18) The aircraft is approaching OPSHN. The upcoming turn and next heading will be annunciated at the top left of the PFD as seen in Figure 7-42. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
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SECTION 7 – NAVIGATION 19) After passing OPSHN, the next leg of the arrival will turn magenta as shown in Figure 7-43. The magenta arrow in the ﬂight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 7-43 Tracking the OPSHN to FSHER Leg 20) The ﬂight continues through the arrival procedure to PYNON (see Figure 7-44).
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SECTION 7 – NAVIGATION 21) Upon passing PYNON the approach procedure will automatically become active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the ﬁnal waypoint of the arrival and the ﬂight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 7-45). 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16.
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SECTION 7 – NAVIGATION 23) After crossing FALUR the next waypoint is the FAF. The ﬂight phase changes to LPV on the HSI indicating the current phase of ﬂight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when ﬂying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 7-48) when the ﬁnal approach course becomes active.
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SECTION 7 – NAVIGATION In this missed approach procedure, the fix immediately following the MAP (in this case ‘6368FT’) is not part of the published procedure. It is simply a ﬁx that deﬁnes a leg which guides the aircraft along the runway centerline until the required altitude to make the ﬁrst turn on the missed approach is exceeded.
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SECTION 7 – NAVIGATION 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern will be established at the MAHP (MOGAL) as shown in Figure 7-51. 7.4 AIRPORT INFORMATION Figure 7-53 Airport Information Page Figure 7-51 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 7-52. Select the Airport Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group.
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SECTION 7 – NAVIGATION Select an Airport from the Active Flight Plan 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to the left to display a list of ﬂight plan airports as shown in Figure 7-54. 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. Select a Recently Entered Airport Identiﬁer 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor.
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SECTION 7 – NAVIGATION Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identiﬁer ﬁeld. 3) Turn the small FMS Knob in the direction of the green arrow to display the next runway for the selected airport. Continue turning the small FMS Knob to select the desired runway. 7.
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SECTION 7 – NAVIGATION 7.6 NDB INFORMATION Figure 7-58 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon View Information on a Speciﬁc NDB 1) With the NDB Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired selection ﬁeld (identiﬁer, name or closest city).
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SECTION 7 – NAVIGATION 7.8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user deﬁned waypoints. 7.9 NEAREST AIRPORTS 2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired airport. 3) Press the FMS Knob to remove the flashing cursor. Access Runway Information for the Selected Airport 1) With the Nearest Airports Page displayed, press the RNWY Softkey to place the cursor in the ‘RUNWAYS’ ﬁeld.
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SECTION 7 – NAVIGATION Nearest Airports Information on the PFD Bearing TO 7.10 NEAREST INTERSECTIONS Distance Airport Symbol Identiﬁer Runway Length Primary COM Frequency Figure 7-61 Nearest Airports Window Press the NRST Softkey to display the PFD Nearest Airports Window. View Information on a Speciﬁc Airport in the List 1) With the Nearest Airports Window displayed, turn either FMS Knob to place the cursor on the desired airport identiﬁer.
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SECTION 7 – NAVIGATION 7.11 NEAREST NDB 7.12 NEAREST VOR Figure 7-64 Nearest VOR Page Figure 7-63 Nearest NDB Page Select the Nearest NDB Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon. Access Information on a Speciﬁc NDB 1) With the Nearest NDB Page displayed, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired NDB.
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SECTION 7 – NAVIGATION 3) Press the FMS Knob to remove the flashing cursor. 7.13 NEAREST USER WAYPOINT Figure 7-65 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the fifth rectangular page icon. Select a Nearest User Waypoint 3) Press the FMS Knob to remove the flashing cursor. 7.
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SECTION 7 – NAVIGATION 7.15 NEAREST AIRSPACES View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to scroll through the list, highlighting the desired airspace. 3) Press the ALERTS Softkey to place the cursor in the ‘AIRSPACE ALERTS’ ﬁeld. 4) Turn either FMS Knob to select the desired airspace. 5) Press the FMS Knob to remove the flashing cursor.
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SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING The following discussions pertain to the Multi Function Display, unless otherwise indicated. 8.1 USER DEFINED WAYPOINTS 4) Repeat steps 2 and 3 until the desired name is entered. 5) Press the ENT Key. 6) Press the ENT Key a again to accept the new waypoint identiﬁer. 7) The cursor is now in the ‘REFERENCE WAYPOINTS’ ﬁeld. If desired, the waypoint can be deﬁned by a reference waypoint.
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SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position. Figure 8-3 Active Flight Plan Page on the MFD 4) Turn the FMS Knobs to select a waypoint name.
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SECTION 8 – FLIGHT PLANNING activation, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. 3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the ﬂight plan.
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SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the NEW Softkey to display a blank ﬂight plan page for the ﬁrst empty storage location. 8) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new ﬂight plan is now in the list.
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SECTION 8 – FLIGHT PLANNING 8.8 ENTER AN AIRWAY IN A FLIGHT PLAN 5) When the desired entry point is entered, press the ENT Key. 1) Press the FPL Key to display the active ﬂight plan or display a stored ﬂight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the waypoint before which the airway will be entered. Figure 8-15 Airway Entry Point Loaded 6) Turn the small FMS Knob to display the Waypoint Information Window.
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SECTION 8 – FLIGHT PLANNING Figure 8-19 Airway Added to Flight Plan 8.9 Figure 8-17 Select Desired Airway LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures. 8) Turn either FMS Knob to highlight the desired airway. 8.10 LOAD AN ARRIVAL 9) Press the ENT Key. A list of available exits is now displayed. See the Procedures section for a discussion on loading and activating arrival procedures.
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SECTION 8 – FLIGHT PLANNING 8.13 STORE A FLIGHT PLAN 1) After creating a ﬂight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 3) With ‘OK’ highlighted, press the ENT Key to store the ﬂight plan. Figure 8-20 Store Flight Plan Conﬁrmation 8.14 EDIT A STORED FLIGHT PLAN 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
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SECTION 8 – FLIGHT PLANNING 8.17 COPY A FLIGHT PLAN 1) From the Flight Plan Catalog press the FMS Knob to activate the cursor 2) Turn the large FMS Knob to highlight the ﬂight plan to be copied. 3) Press the COPY Softkey. 4) A ‘Copy to ﬂight plan #?’ conﬁrmation window is displayed. With ‘OK’ highlighted, press the ENT Key to copy the ﬂight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.
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SECTION 8 – FLIGHT PLANNING 4) For Direct-to planning, press the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). If necessary, press the MENU Key and select ‘Set WPT to Present Position’ to display ‘P.POS’. Press the ENT Key and the ﬂashing cursor moves to the ending waypoint ﬁeld. Turn the FMS Knobs to enter the identiﬁer of the ending waypoint and press the ENT Key to accept the waypoint.
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SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to hightlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. 4) If a ﬂight plan is active, the departure airport will be displayed as the default. A list of available departures is also displayed. If no ﬂight plan is active, use the FMS Knobs to enter the identiﬁer of the desired airport. Press the ENT Key.
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SECTION 9 – PROCEDURES 7) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key. Figure 9-4 Select Arrival Transition 8) A third window is displayed listing the available runways. Turn either FMS Knob to select the desired runway and press the ENT Key. 9.2 APPROACHES Not all approaches in the database are approved for GPS use.
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SECTION 9 – PROCEDURES Load and/or Activate an Approach Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. 4) If a ﬂight plan is active, the destination airport will be displayed as the default. A list of available approaches is also displayed. If no ﬂight plan is active, use the FMS Knobs to enter the identiﬁer of the desired airport. Press the ENT Key. 7) The cursor will move to the TRANSITIONS ﬁeld.
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SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select the ‘Weather’ group (Figure 10-2) to customize the display of weather features. Select ‘Trafﬁc’ to customize the display of trafﬁc. 10.
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SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. Figure 10-5 Lightning Display Range Annunciation Select ‘cell’ or ‘strike’ as the Stormscope lightning mode: 1) With the Weather Group selected, press the ENT Key. The cursor ﬂashes on ‘STRMSCP LTNG’. 2) Turn the large FMS Knob to select ‘STRMSCP MODE’.
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SECTION 10 – HAZARD AVOIDANCE 10.3 XM WEATHER (OPTIONAL) WARNING: Use of XM weather for hazardous weather penetration is not recommended. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. Displaying METAR and TAF information on the Airport Information Page Display METAR and TAF text on the Airport Information Page: 1) Turn the large FMS Knob to select the WPT Page Group. 1) From the Navigation Map Page, press the MAP Softkey.
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SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link Page. 3) Press the available softkeys to select the desired XM weather product. 4) Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list. Press the small FMS Knob or the ENT Key to return to the map.
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SECTION 10 – HAZARD AVOIDANCE CELL MOV – pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – pressing the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – press the METAR Softkey to graphically display METARs. METARS are shown as colored ﬂags at airports providing METAR reports. The display is updated every 12 minutes.
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SECTION 10 – HAZARD AVOIDANCE • • • • Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available.
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SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Trafﬁc Advisory, aircraft is 1200’ TNA Mute above & climbing, moving in the Trafﬁc out of direction of the line Trafﬁc Mode Status range NOTE: If the G1000 is conﬁgured to use the optional SkyWatch Trafﬁc Advisory System, TIS will not be available for use. NOTE: Trafﬁc Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.
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SECTION 10 – HAZARD AVOIDANCE 10.5 SKYWATCH® TRAFFIC ADVISORY SYSTEM (TAS)(OPTIONAL) Trafﬁc Advisory, aircraft is 400’ below Trafﬁc Mode Altitude Mode & climbing Trafﬁc, Out of Range Refer to the SkyWatch pilot’s guide for a detailed discussion of the SkyWatch system. Displaying Trafﬁc on the Trafﬁc Map Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Trafﬁc Map Page. 3) Press the OPERATE Softkey to begin displaying trafﬁc.
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SECTION 10 – HAZARD AVOIDANCE 4) Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Trafﬁc Advisory Non-Bearing Trafﬁc Off Scale Trafﬁc Advisories Banner Non-Threat Trafﬁc Figure 10-13 TAS Trafﬁc on Navigation Map 10.6 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
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SECTION 10 – HAZARD AVOIDANCE Unlighted Obstacle (Height is less than 1000’ AGL) Lighted Obstacle (Height is less than 1000’ AGL) Unlighted Obstacle (Height is greater than 1000’ AGL) Lighted Obstacle (Height is greater than 1000’ AGL) Figure 10-15 Obstacle Symbols Displaying Terrain and Obstacles on the Navigation Map 1) With the Navigation Map displayed, press the MAP Softkey. 2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be displayed on the map. 10.
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SECTION 10 – HAZARD AVOIDANCE Figure 10-17 TAWS Page (ARC View) Figure 10-16 TAWS Page (360˚ View) Color Terrain/Obstacle Location Alert Level Terrain/Obstacle at or within 100’ below current aircraft altitude. WARNING Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. CAUTION Black Terrain/Obstacle is more than 1000’ below aircraft altitude.
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SECTION 10 – HAZARD AVOIDANCE Enable/Disable Aviation Data 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”. 3) Press the ENT Key. Manual System Test A system test is automatically performed at power-up. After sucessful completion of the test, “TAWS System Test, OK” will be heard. The system test may also be initiated manually, but only when the aircraft is on the ground.
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SECTION 10 – HAZARD AVOIDANCE Phase of Flight Level Flight Descending Enroute 700 ft. 500 ft. Terminal 350 ft. 300 ft. Approach 150 ft. 100 ft. Departure 100 ft. 100 ft. During the ﬁnal approach phase of ﬂight, RTC/ROC/ ITI/IOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0.5 nm of the approach runway or is below 125 feet AGL while within 1 nm of the runway.
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�� SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map �� 1) With the Navigation Map displayed, press the MAP Softkey. �� 2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be displayed on the map.
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SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
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SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufﬁcient GPS signal is re-established.
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SECTION 11 – ABNORMAL OPERATION SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters Reversionary Mode. In Reversionary Mode, critical ﬂight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the Reversionary Mode display. Normal PFD Display 11.
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SECTION 11 – ABNORMAL OPERATION 11.3 UNUSUAL ATTITUDES The PFD will ‘declutter’ when the aircraft enters an unusual attitude. Only the primary functions will be displayed in these situations.
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SECTION 11 – ABNORMAL OPERATION DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’ superimposed in yellow over the ‘own aircraft’ symbol as shown in Figure 11-4. In addition, ‘DR’ will be prominently displayed, also in yellow, on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in Figure 11-4. Also, the CDI deviation bar is removed from the display. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message will appear on the PFD.
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SECTION 11 – ABNORMAL OPERATION Blank Page 11-4 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The PA32 Pilot’s Operating Handbook supersedes information found in this document. System Annunciation Red ‘X’ Annunciation Window Alerts Window Figure 12-1 G1000 Alerting System ALERTS Softkey Annunciation The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation Window displays abbreviated annunciation text.
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SECTION 12 – ANNUNCIATIONS & ALERTS • System Annunciations: Typically, a large red ‘X’ appears in a window when a related LRU fails or detects invalid data. • Audio Alerting System: The G1000 system issues audio alert tones when speciﬁc system conditions are met. See the Alert Levels Deﬁnitions section for more information. 12.1 ALERT LEVEL DEFINITIONS of the message advisory alert and displays the alert text message in the Alerts Window.
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SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS The following alerts are conﬁgured speciﬁcally for the Piper PA32 aircraft. See the Pilot’s Operating Handbook for information regarding pilot responses. WARNING Alerts Annunciation Window Text OIL PRES LO OIL PRES HI ALTNTR INOP NO STBY ALT STARTER ENGD ESS BUS LOW EMER BAT LOW Alerts Window Message Oil pressure is below 25 psi. Oil pressure is above 115 psi. No output from main alternator. No output from standby alternator. Starter is engaged.
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SECTION 12 – ANNUNCIATIONS & ALERTS 12.3 TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
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SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufﬁcient GPS signal is re-established. System Test in progress None None None “TAWS System Test OK” Alert Type System Test pass None 12.
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SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-5 illustrates all possible ﬂags and the responsible LRUs.
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SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Indicates a conﬁguration module failure. This annunciation will only be seen when the autopilot is engaged. The annunciation indicates an AHRS monitor has detected an abnormal ﬂight parameter, possibly caused by strong turbulence. In this case, the situation should correct itself within a few seconds. If there is an actual failure, a red “X” will soon appear over the Attitude Indicator.
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SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display is not receiving valid heading input from AHRS. Display is not receiving valid transponder information. Other Various Red X Indications A red ‘X’ through any other display ﬁeld, such as engine instrumentation ﬁelds, indicates that the ﬁeld is not receiving valid data. Message Advisory Alerts Alerts Window Message PFD FAN FAIL – The cooling fan for the PFD is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative.
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SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories (Cont.) Message PFD1 COOLING – PFD1 has poor cooling. Reducing power usage. MFD1 COOLING – MFD1 has poor cooling. Reducing power usage. PFD1 “KEY” KEYSTK – Key is stuck. MFD1 “KEY” KEYSTK – Key is stuck. Comments The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the G1000 system should be serviced. A key is stuck on the PFD and/or MFD bezel.
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SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. MFD1 DB ERR – MFD1 SafeTaxi database error exists. PFD1 DB ERR – PFD1 SafeTaxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists. MFD1 DB ERR – MFD1 FliteCharts database error exists. DB MISMATCH – Aviation database version mismatch. Xtalk is off.
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SECTION 12 – ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Message GMA1 FAIL – GMA1 is inoperative. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. GMA1 CONFIG – GMA1 conﬁguration The audio panel conﬁguration settings do not match backup conﬁguration error. Conﬁg service req’d. memory. The G1000 system should be serviced. MANIFEST – GMA1 software The audio panel has incorrect software installed.
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SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message HW MISMATCH – GIA hardware mismatch. GIA1 communication halted. HW MISMATCH – GIA hardware mismatch. GIA2 communication halted. MANIFEST – GIA1 software mismatch. Communication halted. MANIFEST – GIA2 software mismatch. Communication halted. COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair.
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SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message GPS NAV LOST – Loss of GPS navigation. GPS fail. ABORT APR – Loss of GPS navigation. Abort approach. APR DWNGRADE – Approach downgraded. Use LNAV minima. TRUE APR – True north approach. All angles are TRUE. GPS1 SERVICE – GPS1 needs service. Return unit for repair. GPS2 SERVICE – GPS2 needs service. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service.
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SECTION 12 – ANNUNCIATIONS & ALERTS GEA 71 Message Advisories Message GEA1 CONFIG – GEA1 conﬁguration error. Conﬁg service req’d. MANIFEST – GEA1 software mismatch. Communication halted. Comments The GEA1 conﬁguration settings do not match those of backup conﬁguration memory. The G1000 system should be serviced. The #1 GEA 71 has incorrect software installed. The G1000 system should be serviced. GTX 33 Message Advisories Message XPDR1 CONFIG – XPDR1 conﬁg error. Conﬁg service req’d.
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SECTION 12 – ANNUNCIATIONS & ALERTS GRS 77 Message Advisories (Cont.) Message GEO LIMITS – AHRS1 too far North/ South, no magnetic compass. MANIFEST – GRS1 software mismatch. Communication halted. Comments The aircraft is outside geographical limits for approved AHRS operation. Heading is ﬂagged as invalid. The #1 AHRS has incorrect software installed. The G1000 system should be serviced. GMU 44 Message Advisories Message HDG FAULT – AHRS1 magnetometer fault has occurred.
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SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored ﬂight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The ﬂight plan cannot ﬁnd the speciﬁed waypoint and ﬂags this message. This can also occur with user waypoints in a ﬂight plan that is deleted.
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SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message ARSPC NEAR – Airspace near – less than 2 nm. LEG UNSMOOTH – Flight plan leg will not be smooth. APPR INACTV – Approach is not active. SLCT FREQ – Select appropriate frequency for approach. SLCT NAV – Select NAV on CDI for approach. PTK FAIL – Bad geometry, parallel offset not activated. PTK FAIL – Invalid leg type, parallel offset not activated. PTK FAIL – Past IAF, parallel offset not activated.
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SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message STRMSCP FAIL – Stormscope has failed. FAILED PATH – A data path has failed.. MAG VAR WARN – Large magnetic variance. Verify all course angles. SCHEDULER [#] – . 12-18 Comments Stormscope has failed. The G1000 system should be serviced. A data path connected to the GDU or the GIA 63/W has failed.
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INDEX A B E Abnormal COM operation 11-1 Activate a ﬂight plan 8-3 Active ﬂight plan 8-2 ADF 1-5 ADVISORY 12-1 Advisory alerts 12-8 Age 10-6 AHRS 12-6, 12-7, 12-8, 12-14, 12-15 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-26 Airport information 7-22 Airspace alerts 7-30 Airspeed indicator 2-3 Airspeed trend vector 2-3 Airways 8-5 Alerting System 12-1 Alerts 12-1 Alert levels 12-2 Alert Pop-Up 10-14 ALT 1-3, 1-6, 2-4, 7-20, 10-8, 12-3, 12-15 Altitude alerter 2-4 Altitude alerting 2-4 Altitude const
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INDEX IOI 10-12, 10-13, 10-15, 12-4 ITI 10-12 J Joystick (bezel) 1-2 K Key(s) 1-3 CLR 1-2 COM Frequency Transfer 1-2 Direct-to 1-2 ENT 1-2 FPL 1-2 MENU 1-2 NAV Frequency Transfer 1-2 PROC 1-2 Knob(s) ALT 1-2 COM 1-2 COM VOL/SQ 1-2 CRS/BARO 1-2 FMS 1-2 HDG 1-2 NAV 1-2 NAV VOL/ID 1-2 P MAP 7-1 Map panning 10-5 Marker beacon 2-6 MDA 2-6, 2-7 messages 12-1 Message advisories 12-2, 12-8 – 1218 METAR 10-3, 10-5 Metric display 2-4 MFD 1-1, 4-4 Minimum descent altitude 2-6 Mixture 3-3 MKR/MUTE 5-2, 5-4 Mode S 1
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INDEX TAS 10-8, 10-9, 12-14 TAWS 10-10, 10-11, 10-12, 10-14, 10-15, 10-16, 12-4, 12-5 TAWS-B 10-10 TAWS system test 10-12 Terrain 10-9 – 10-12, 10-14, 10-15, 10-16, 11-2, 12-4, 12-10 Terrain proximity 10-9 TIS 10-7 TNA Mute 10-7 TOD 7-16, 7-19 Top of Descent 7-16 Tornado 10-5 Trafﬁc advisory 10-7, 10-8, 10-9, 10-16 Trafﬁc map page 10-7, 10-8, 10-10, 10-14 Transponder 4-4 Transponder standby mode 4-4 Transponder Status bar 4-5 Tropical storms 10-5 Ture airspeed box 2-3 TX 4-3 W WAAS 2-5, 7-5, 12-12 WARN 2-1
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INDEX Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Piper PA32
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Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. 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: 44/0870.851241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com 190-00416-01 Rev. C © 2004-2007 Garmin Ltd.