Garmin Software Version 0648.02 Guía de usuario Pagina 65
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Garmin G1000 Cockpit Reference Guide for the Piper PA32
SECTION 7 – NAVIGATION
7-11
10)
At Lamar VOR (LAA) V263 will be intercepted.
See Figure 7-25.
Figure 7-25 HYS to LAA Leg Active
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.
b)
Turn the large FMS Knob to select OPSHN in the
flight plan list.
c)
Press the
Direct-to
( )
Key. The Direct-to
Window is now displayed as shown in Figure
7-26.
Figure 7-26 Direct To OPSHN
d)
Turn the large FMS Knob to place the cursor in
the VNV altitude field as shown in Figure 7-27.
Figure 7-27 Enter VNV Altitude
e)
An altitude of 10,000 feet is entered as requested
by ATC.
- Integrated Flight Deck 1
- WARNINGS 4
- CAUTIONS, & NOTES 4
- RECORD OF REVISIONS 7
- TABLE OF CONTENTS 10
- SECTION 1: SYSTEM OVERVIEW 13
- 1.1 PFD/MFD CONTROLS 14
- SECTION 1 15
- SYSTEM OVERVIEW 15
- 1.3 MFD SOFTKEYS 19
- 1.4 MFD PAGE GROUPS 20
- 1.5 VERTICAL NAVIGATION 20
- 1.6 BACKLIGHTING 22
- 1.7 DATABASE UPDATES 22
- Jeppesen Aviation Database 23
- Garmin Databases 23
- 1.8 PILOT PROFILES 24
- Deleting a Profile 25
- SECTION 2: FLIGHT INSTRUMENTS 27
- SECTION 2 28
- FLIGHT INSTRUMENTS 28
- 2.1 AIRSPEED INDICATOR 29
- 2.2 ATTITUDE INDICATOR 29
- 2.3 ALTIMETER 30
- GLIDESLOPE INDICATOR 31
- 2.6 VERTICAL SPEED INDICATOR 32
- 2.8 WIND DATA 33
- Course Pointer 34
- 35
- DME (optional) 36
- Navigation Source 36
- 2.10 GENERIC TIMER 37
- SECTION 3: ENGINE INDICATION 39
- SYSTEM (EIS) 39
- 3.2 FULL EIS DISPLAY 40
- SECTION 3 – ENGINE 41
- INDICATION SYSTEM (EIS) 41
- SECTION 4: NAV/COM AND 43
- TRANSPONDER 43
- SECTION 4 – NAV/COM & 44
- 4.1 RADIO STATUS INDICATIONS 45
- 4.2 VOLUME 45
- 4.3 AUTOMATIC SQUELCH 45
- 4.5 OPTIONAL NAV RADIOS 45
- 4.6 FREQUENCY AUTO-TUNING 46
- 4.7 TRANSPONDER 46
- Reply Status 47
- Code Selection 47
- Flight ID Reporting 48
- SECTION 5: AUDIO PANEL 49
- 5.1 COM RADIO SELECTION 50
- 5.2 SPLIT COM FUNCTION 50
- 5.3 MARKER BEACON RECEIVER 50
- SECTION 5 – AUDIO PANEL 51
- 5.6 INTERCOM SQUELCH CONTROL 52
- AND PLAYER 52
- SECTION 6: AUTOMATIC FLIGHT 53
- SECTION 6 – AUTOMATIC 54
- FLIGHT CONTROL 54
- SECTION 7: NAVIGATION 55
- SECTION 7 – NAVIGATION 56
- WPT Location 57
- FT’. Again, if 75
- 7.4 AIRPORT INFORMATION 76
- 7.5 INTERSECTION INFORMATION 78
- 7.6 NDB INFORMATION 79
- 7.7 VOR INFORMATION 79
- 7.9 NEAREST AIRPORTS 80
- 7.10 NEAREST INTERSECTIONS 81
- 7.11 NEAREST NDB 82
- 7.12 NEAREST VOR 82
- 7.13 NEAREST USER WAYPOINT 83
- 7.14 NEAREST FREQUENCIES 83
- 7.15 NEAREST AIRSPACES 84
- SECTION 8: FLIGHT PLANNING 85
- Map Page 86
- SECTION 8 – FLIGHT PLANNING 87
- 8.7 CREATE A NEW FLIGHT PLAN 88
- 8.17 COPY A FLIGHT PLAN 92
- 8.18 DELETE A FLIGHT PLAN 92
- 8.20 TRIP PLANNING 92
- SECTION 9: PROCEDURES 95
- 9.2 APPROACHES 96
- SECTION 9 – PROCEDURES 97
- SECTION 10: HAZARD AVOIDANCE 99
- Stormscope Page 100
- 10.3 XM WEATHER (OPTIONAL) 101
- SECTION 10 – HAZARD 102
- AVOIDANCE 102
- Weather Products and Symbols 103
- Weather Product Age 104
- TIS Voice Alert 105
- 10.5 SKYWATCH 106
- TRAFFIC ADVISORY 106
- SYSTEM (TAS)(OPTIONAL) 106
- Proximity Page 107
- SYSTEM (TAWS) DISPLAY 108
- (OPTIONAL) 108
- Enable/Disable Aviation Data 110
- TAWS Inhibit 110
- Manual System Test 110
- Premature Descent Alert (PDA) 111
- Alert (NCR) 111
- “Five-Hundred” Aural Alert 112
- Navigation Map 112
- Pop-up Alerts 112
- TAWS Alerts Summary 113
- Alert Annunciations 114
- SECTION 11: ABNORMAL 115
- OPERATION 115
- SECTION 11 – ABNORMAL 116
- SECTION 12 – ANNUNCIATIONS 119
- & ALERTS 119
- 12.1 ALERT LEVEL DEFINITIONS 120
- 12.2 AIRCRAFT ALERTS 121
- 12.3 TAWS ALERTS 122
- Message Advisory Alerts 126
- Database Message Advisories 127
- GMA 1347 Message Advisories 129
- GIA 63W Message Advisories 129
- GEA 71 Message Advisories 132
- GTX 33 Message Advisories 132
- GRS 77 Message Advisories 132
- GMU 44 Message Advisories 133
- GDL 69A Message Advisories 133
- GDC 74A Message Advisories 133
- Blank Page 140
- 190-00416-01 Rev. C 142
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