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HAZARD AVOIDANCE

TAWS ALERTS

Alerts are issued when flight conditions meet parameters that are set within TAWS software algorithms. TAWS alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-6 shows TAWS alert types with corresponding annunciations and aural messages.

When an alert is issued, annunciations appear on the PFD and MFD. The TAWS Alert Annunciation is shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TAWS Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the pop-up alert:

Press the CLR Key (returns to the currently viewed page), or

Press the ENT Key (accesses the TAWS Page)

Alert Annunciation

Pop-up

Alert

Figure 6-57 TAWS Alert Annunciations

Terrain Display Enabled

Terrain Legend

Alert Annunciation

Figure 6-58 Navigation Map Page

(After TAWS Pop-up Alert Acknowledgment)

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Garmin G1000 Pilot’s Guide for Cessna Nav III

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HAZARD AVOIDANCE

Alert Type

PFD/MFDAlert

MFD Pop-Up Alert

Aural Message

Annunciation

 

 

 

Excessive Descent Rate Warning

 

 

“Pull Up”

(EDR)

 

 

 

 

 

Reduced Required Terrain

 

*

“Terrain Ahead, Pull Up;Terrain Ahead, Pull Up”*

 

or

or

Clearance Warning (RTC)

 

 

 

“Terrain,Terrain; Pull Up, Pull Up”

 

 

 

 

 

 

 

Imminent Terrain Impact

 

*

Terrain Ahead, Pull Up;Terrain Ahead, Pull Up’*

 

or

or

Warning (ITI)

 

 

 

“Terrain,Terrain; Pull Up, Pull Up”

 

 

 

 

 

 

 

Reduced Required Obstacle

 

*

“ObstacleAhead, Pull Up; ObstacleAhead, Pull Up”*

 

or

or

Clearance Warning (ROC)

 

 

 

“Obstacle, Obstacle; Pull Up, Pull Up”

 

 

 

 

 

 

 

Imminent Obstacle Impact

 

*

“ObstacleAhead, Pull Up; ObstacleAhead, Pull Up”

 

or

or

Warning (IOI)

 

 

 

“Obstacle, Obstacle; Pull Up, Pull Up”

 

 

 

 

 

 

 

Reduced Required Terrain

 

*

“Terrain Ahead;Terrain Ahead”*

 

or

or

Clearance Caution (RTC)

 

 

 

“Caution,Terrain; Caution,Terrain”

 

 

 

 

 

 

 

Imminent Terrain Impact Caution

 

*

“Terrain Ahead;Terrain Ahead”*

 

or

or

(ITI)

 

 

 

“Caution,Terrain; Caution,Terrain”

 

 

 

 

 

 

 

Reduced Required Obstacle

 

*

“Obstacle Ahead; Obstacle Ahead”*

 

or

or

Clearance Caution (ROC)

 

 

 

“Caution, Obstacle; Caution, Obstacle”

 

 

 

 

 

 

 

Imminent Obstacle Impact

 

*

“Obstacle Ahead; Obstacle Ahead”*

 

or

or

Caution (IOI)

 

 

 

“Caution, Obstacle; Caution, Obstacle”

 

 

 

 

 

 

 

Premature Descent Alert

 

 

“Too Low,Terrain”

Caution (PDA)

 

 

 

 

 

Altitude Callout “500”

None

None

“Five-Hundred”

Excessive Descent Rate Caution

 

 

“Sink Rate”

(EDR)

 

 

 

 

 

Negative Climb Rate Caution

 

*

“Don’t Sink”*

 

or

or

(NCR)

 

 

 

“Too Low,Terrain”

 

 

 

 

 

 

 

*Alerts with multiple messages are configurable at installation and are installation-dependent. Alerts for the default configuration are indicated with asterisks.

Table 6-6 TAWS Alerts Summary

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Garmin G1000 Pilot’s Guide for Cessna Nav III

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HAZARD AVOIDANCE

EXCESSIVE DESCENT RATE ALERT

The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 6-59 shows the parameters for the alert as defined by TSO-C151b.

 

6000

 

 

 

 

 

 

5500

 

 

 

 

 

 

5000

 

 

 

 

 

(Feet)

4500

 

 

 

 

 

4000

 

 

ATE"

 

 

 

 

 

 

 

 

Terrain

 

 

 

R

 

 

3500

 

 

"SINK

 

 

 

 

 

 

 

3000

 

 

 

 

 

Above

 

 

 

 

 

2500

 

 

 

 

 

 

 

 

 

 

 

Height

2000

 

 

 

 

 

1500

 

 

 

 

 

 

 

 

 

 

 

 

1000

 

"PULL UP"

 

 

 

500

 

 

 

 

 

 

0

4000

6000

8000

10000

12000

 

2000

Descent Rate (FPM)

Figure 6-59 Excessive Descent Rate Alert Criteria

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Garmin G1000 Pilot’s Guide for Cessna Nav III

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HAZARD AVOIDANCE

FORWARD LOOKING TERRAIN AVOIDANCE

Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum clearance values in Table 6-7. When an RTC alert is issued, a potential impact point is displayed on the TAWS Page.

Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS Page. The alert is annunciated when the projected vertical flight path is calculated to come within minimum clearance altitudes in Table 6-7.

Flight Phase

Minimum Clearance Altitude (ft)

Level Flight

Descending

 

Enroute

700

500

Terminal

350

300

Approach

150

100

Departure

100

100

Table 6-7 FLTA Alert Minimum Terrain and Obstacle Clearance Values

During final approach, Forward Looking Terrain Avoidance (FLTA) alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0.5 nm of the approach runway or below 125 feet AGL while within 1.0 nm of the runway threshold.

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Garmin G1000 Pilot’s Guide for Cessna Nav III

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HAZARD AVOIDANCE

PREMATURE DESCENT ALERTING

A Premature Descent Alert (PDA) is issued when the system detects that the aircraft is significantly below the normal approach path to a runway (Figure 6-60).

PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0.5 nm from the runway threshold OR is at an altitude of 125 feet AGL while within 1.0 nm of the threshold. During the final descent, algorithms set a threshold for alerting based on speed, distance, and other parameters.

Height Above Terrain (Feet)

700

600

500

400

300

200

 

 

 

 

 

 

 

PDA Alerting Area

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

100

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Runway

1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

Threshold

 

 

 

Distance From Destination Airport (nm)

 

 

 

 

 

 

 

 

 

 

 

 

Figure 6-60 PDA Alerting Threshold

PDA and FLTA aural and visual alerts can be manually inhibited. Discretion should be used when inhibiting TAWS and the system should be enable when appropriate. When TAWS is inhibited, the alert annunciation ‘TAWS INHB’ is shown on the PFD and MFD (Figure 6-61).

Figure 6-61 TAWS Alerting Disabled

(TAWS Inhibited) Annunciation

Inhibiting/enabling TAWS alerting:

1)Select the TAWS Page.

2)Press the MENU Key.

3)Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key.

If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach, a ‘LOW ALT’ annunciation may appear on the PFD next to the Altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments Section for details.

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Garmin G1000 Pilot’s Guide for Cessna Nav III

6-45

HAZARD AVOIDANCE

FIVE-HUNDRED AURAL ALERT

The purpose of the aural alert message “Five-hundred”is to provide an advisory alert that the aircraft is 500 feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “Five-hundred” is generated. There are no display annunciations or pop-up alerts that accompany the aural message.

NEGATIVE CLIMB RATE AFTER TAKEOFF ALERT (NCR)

The Negative Climb Rate (NCR) After Takeoff alert (also referred to as “Altitude Loss After Takeoff”) provides alerts when the system determines the aircraft is losing altitude (closing upon terrain) after takeoff. The aural message “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain alert on the display. NCR alerting is only active when departing from an airport and when the following conditions are met:

Height above the terrain is less than 700 feet

Distance from the departure airport is 2 nm or less

Heading change from the departure heading is less than 110 degrees Figure 6-62 shows the NCR alerting parameters as defined by TSO-C151b.

(Feet)

1000

 

 

 

 

 

 

 

800

 

 

 

 

 

 

 

Terrain

 

 

 

 

 

 

 

600

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Above

400

 

 

 

“DON’T SINK”

 

 

 

 

 

 

 

 

200

 

 

 

 

 

 

 

Height

 

 

 

 

 

 

 

0

20

40

60

80

100

120

140

 

Altitude Loss (Feet)

(Feet)

1000

 

 

 

 

 

 

 

 

900

 

 

 

 

 

 

 

 

800

 

 

 

 

 

 

 

 

Terrain

 

 

 

 

 

 

 

 

700

 

 

 

 

 

 

 

 

600

 

 

 

 

 

 

 

 

500

 

 

 

 

 

 

 

 

Above

 

 

 

 

 

 

 

 

400

 

 

 

“DON’T SINK”

 

 

 

300

 

 

 

 

 

 

200

 

 

 

 

 

 

 

 

Height

 

 

 

 

 

 

 

 

100

 

 

 

 

 

 

 

 

0

500

1000

1500

2000

2500

3000

3500

4000

 

Sink Rate (Feet Per Minute)

Figure 6-62 Negative Climb Rate (NCR) Alert Criteria

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Garmin G1000 Pilot’s Guide for Cessna Nav III

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