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PA-32R-301, SARATOGA II HP
SECTION 4- NORMAL PROCEDURES (continued)
E. AUTOMATIC LOCALIZER COURSE CAPTURE
SECTION9
SUPPLEMENT 10
By default, the GNS 530 automatic localizer course capture feature is
enabled. This feature provides a method for system navigation data present
on the external indicators to be switched automatically from GPS guidance
to localizer/glide slope guidance at the point of course intercept on a
localizer at which GPS derived course deviation equals localizer derived
course deviation.
If
an offset from the final approach course is being
flown, it is possible that the automatic switch from GPS course guidance
to localizer/glide slope course guidance will not occur.
It
is the pilot's
responsibility to ensure correct system navigation data is present on the
external indicator before continuing a localizer based approach beyond the
final approach fix.
F.
DISPLAY OF LIGHTNING STRIKE DATA
Lightning strike data detected by the BF Goodrich WX-500 Storrnscope
will appear on the moving map and weather pages of theGNS 530. For
detailed operating instructions regarding the interface of the GNS 530 with
the WX-500, refer to the WX-500 Pilot's Guide and the GNS 530 Pilot's
Guide Addendum for the WX -500 Stormscope interface.
CAUTION
During activation and deactivation of the air conditioning
system, false lightning strikes/cells may appear on the
Stormscope display due to electrical interference caused
during operation of the air conditioner condenser door motor.
This phenomenon will also occur during air conditioning
operation with movement of the throttle between full and
partial power due to the automatic retraction and
extension of the air conditioner condenser door with throttle
movement. False lightning strikes/cells can be cleared via the
remote Stormscope clear button on the panel or using the
controls on the GNS 430/GNS 530
if
so equipped.
G. DISPLAY OF TRAFFIC ADVISORY DATA
Traffic data detected by the BF Goodrich SKYWATCHru Traffic Advisory
System (TAS) will appear on the moving map and traffic display pages of
the GNS 530. For detailed operating instructions regarding the interface of
the GNS 530 with the SKYWATCH, refer to the FAA approved Flight
Manual Supplement for the SKYWATCH, the Pilot's Guide for the
SKYWATCH and the GNS 530 Pilot's Guide Addendum for the
SKYWATCH Traffic Advisory System interface.
ISSUED:
JUNE
30, 1997
REVISED: DECEMBER 10, 2003
REPORT: VB-1669
7 of8,
9-63
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