Piper SARATOGA II HP PA-32R-301 Pilot Operating Handbook page 297

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SECTION9
SUPPLEMENT 11
PA-32R-301, SARATOGA II liP
SECTION 4 ·NORMAL PROCEDURES (continued)
SELF TEST (continued)
If
"TRAFFIC ADVISORY SYSTEM TEST FAILED" is heard or the
SKY 497 FAILED screen appears, the SKYWATCH system should be
turned OFF.
NOTE
The SELF TEST is inhibited when the aircraft is
airborne.
STANDBY CHARACTERISTICS
The SKYWATCH system will display SKY497 STANDBY when the
aircraft is on the ground and not tracking or processing traffic
information. Standby gives the system the ability to track targets while on
the ground. Pressing the OPR button activates the system and changes the
display from the Standby screen to the Above (ABV) mode and 6 nm
range. The ranges available are 6 nm and 2 nm and are selected by
1
pressing the Display Range Button.
To go back into Standby, press the STB button. The system will go to the
SKY497 STANDBY screen and will not track targets again until the
system is either manually switched out of Standby, while on the ground or
automatically switched out of Standby 8 seconds after the aircraft
becomes airborne.
The SELF TEST works while in the SKY497 SKYWATCH screen by
pressing the TEST Button.
The SKYWATCH system, while in flight or operating on the ground, will
display 3 altitude display modes. These are: Above (ABV), Normal
(NRM),
and Below (BLW). These modes are activated by pressing the
Altitude display mode button. Refer to the pilot's guide for the
SKYWATCH Traffic System Model SKY497, p/n 009-10801-001, Rev. A
or latest FAA approved revision.
I
REPORT: VB-1669
9-68,
4 of6
ISSUED:
JUNE
30, 1997
REVISED:
JUNE
12, 2000

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