400/500 Series Garmin Optional Displays

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50 Section 2 TAWS Operation Figure 2-4: Inhibiting Terrain Inhibit Mode TAWS provides an ‘inhibit mode’ (Figure 2-4). This mode is designed to deactivate PDA/FLTA aural and visual alerts when they are deemed unnecessary by the aircrew. Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. Pilots should use discretion when inhibiting the TAWS system and always remember to enable the system when appropriate. Only the PDA and FLTA alerts are disabled in the inhibit mode. See section 3 for more information on TAWS alerts. To inhibit TAWS: 1. Select the TAWS Page and press MENU. ‘Inhibit Terrain?’ is selected by default. 2. Press ENT. The TAWS system is inhibited. The annunciation is displayed in the terrain annunciator field whenever terrain is inhibited (Figure 2-4). To enable TAWS: 1. Select the TAWS Page and press MENU. ‘Enable Terrain?’ is selected by default. 2. Press ENT. The TAWS system is functional again.
TAWS Manual Test <strong>Garmin</strong> TAWS provides a manual test capability which verifies the proper operation of the aural and visual annunciations of the system prior to a flight. To manually test the TAWS system: 1. Select the TAWS Page and press MENU. 2. Select the ‘Test Terrain?’ option (Figure 2-5). 3. Press ENT to confirm the selection. An aural message is played giving the test results: • “TAWS System Test, OK” if the system passes the test. • “TAWS System Failure” if the system fail the test. NOTE: TAWS System Testing is disabled when ground speed exceeds 30 knots so as not to impede TAWS alerting. Section 2 TAWS Operation Figure 2-5: ‘Test Terrain’ selection 51
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400/500 Series Garmin Optional Disp
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WARNING: Terrain data is obtained f
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Section 2: NEXRAD Overview ........
Page 7 and 8: TERRAIN Phase of Flight ...........
Page 9 and 10: PART ONE: TRAFFIC INFORMATION SERVI
Page 11 and 12: TIS information is collected one ra
Page 13 and 14: Section 2: Control and Display TIS
Page 15 and 16: Map Page TIS traffic is displayed o
Page 17 and 18: Section 3: TIS Operational Procedur
Page 19 and 20: Section 1: Introduction PART TWO: W
Page 21 and 22: NEXRAD Intensity Colors are used to
Page 23 and 24: NOTE: It is recommended that the pi
Page 25 and 26: Displaying NEXRAD Data on the Map P
Page 27 and 28: Data Link Request Log Page (GDL 49
Page 29 and 30: 4. Enter the type of METAR Data you
Page 31 and 32: Displaying Textual METARS Once rece
Page 33 and 34: Section 6: Troubleshooting Although
Page 35 and 36: GDL 69/69A Datalink Status • Sat
Page 37 and 38: Section 1: Introduction Overview PA
Page 39 and 40: When an instrument approach is load
Page 41 and 42: Seven display ranges are available,
Page 43 and 44: General Database Information The Ga
Page 45 and 46: TERRAIN Phase of Flight The TERRAIN
Page 47 and 48: Section 3: TERRAIN Alerts TERRAIN a
Page 49 and 50: Premature Descent Alerting (PDA) Th
Page 51 and 52: TERRAIN Alert Summary Table 3-2 sum
Page 53 and 54: Section 1: Introduction Overview PA
Page 55 and 56: PDA alerting is provided for both n
Page 57: To display a 120˚ view: 1. Select
Page 61 and 62: General Database Information Garmin
Page 63 and 64: TAWS Phase of Flight The TAWS Phase
Page 65 and 66: Section 3: TAWS Alerts Alerts are i
Page 67 and 68: Premature Descent Alerting (PDA) Ga
Page 69 and 70: Negative Climb Rate After Takeoff A
Page 71 and 72: TAWS Alert Summary The aural alert
Page 73 and 74: Standard Aviation Forecast Abbrevia
Page 75 and 76: Winds Wind Vector — The wind vect
Page 78: © 2004 - 2006 Garmin Ltd. or its s
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