Avidyne Corporation
4 Middlesex Green - Suite 221
561 Virginia Road
Concord MA 01742
FAA APPROVED
Date:
2FW
Page 22 of 26
P/N 600-00298-000
Rev 08
Short Text
Long
Text
Comments
TIS Removed
TIS Traffic Removed
TIS traffic communications
have ceased for >12 seconds
TIS Unavailable
TIS Traffic Unavailable
No TIS ground station is
available or communications
have ceased for >60 seconds
Too Low, Terrain
Premature Descent,
below glide path
TAWS PDA algorithm has
determined the aircraft is below
glide path.
Sink Rate
Excessive Descent Rate
TAWS EDR algorithm has
determined a potential CFIT
scenario is developing –
recover the aircraft
Don’t Sink
Negative climb rate or
altitude loss
TAWS NCR algorithm has
determined corrective action
should be t aken immediately.
TAWS Fail
Invalid GPS
Positon/Velocity
The GPS solution is lost or the
GPS velocity quality
parameters drop below required
accuracy limits. A “bing-bong”
chime is played if this condition
occurs. Contact the Avidyne
Service Center if this persists
across power cycles.
TAWS System
Failure
TAWS Failed Self-Test
[reason why]
TAWS failed self-test for the
reason provided and TAWS will
be degraded or not available for
the power cycle. Contact the
Avidyne Service Center if this
persists across power cycles.
The pilot should utilize available instruments/data displays to verify
message(s) and take appropriate action(s) (ref POH/AFM) by
selection of alternate systems or settings. Invalid messages generally
indicate a failed sensor and that other messages associated with that
system will be unavailable. Caution messages indicate the possibility
of a pilot action.
Содержание CHEROKEE WARRIOR II
Страница 253: ...Piper PA 28 161 28 7916159 N3067D ...