SECTION 13

TAWS

Table 13-3 shows system status annunciations that may also be issued:

Alert Type

TAWS Page

Pop-Up Alert

 

Aural Message

Annunciation

 

 

 

 

 

TAWS System Test Fail

 

None

 

“TAWS System Failure”

 

 

 

 

 

TAWS Alerting is disabled

 

None

 

None

 

 

 

 

 

No GPS position or excessively degraded

 

None

 

“TAWS Not Available”

GPS signal

 

 

 

“TAWS Available” is generated when sufficient

 

 

 

 

GPS signal is re-established.

System Test in progress

 

None

 

None

 

 

 

 

 

System Test pass

None

None

 

“TAWS System Test OK”

 

Table 13-3 Additional System Annunciations

 

Forward Looking Terrain Avoidance

The Forward Looking Terrain Avoidance (FLTA) alert is used by TAWS and is composed of:

Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) -These alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum clearance values in Table 13-4. When an RTC or ROC alert is issued, a potential impact point is displayed on the TAWS Page.

Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) - These 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 13-4.

Phase of Flight

Minimum Clearance

Minimum Clearance

 

Altitude Level Flight (ft)

Altitude Descending (ft)

Enroute

700

500

Terminal

350

300

Approach

150

100

Departure

100

100

Table 13-4 Minimum Terrain and Obstacle Clearance Values for FLTA Alerts

During the final approach phase of flight, 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.

13-6

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

Page 210
Image 210
3D Connexion GNS 530(A) manual Forward Looking Terrain Avoidance, Pop-Up Alert Aural Message, Phase of Flight

GNS 530(A) specifications

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