Garmin gtn 625 GPS Receiver User Manual


 
10-16
Garmin GTN 625/635/650 Pilot’s Guide
190-01004-03 Rev. B
Foreword
Getting
Started
Xpdr Ctrl
Com/Nav
FPL
Direct-To
Proc
Wpt Info
Map
Traffic
Terrain
Weather
Nearest
Music
Utilities
System
Messages
Symbols
Appendix
Index
Flight Phase
Minimum Clearance Altitude (feet)
Level Flight Descending
En Route 700 500
Terminal 350 300
Approach 150 100
Departure 100 100
Table 10-4 FLTA Alert Minimum Terrain and Obstacle Clearance Values
During final approach, 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.
10.3.8.4 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.
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.







(EIGHT!BOVE4ERRAIN&EET
$ISTANCE&ROM$ESTINATION!IRPORTNM
              
0$!!LERTING!REA0$!!LERTING!REA
2UNWAY
4HRESHOLD
Figure 10-13 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 enabled when
appropriate. When TAWS is inhibited, the alert annunciation “TAWS INHB” is
shown.