SECTION 9
SUPPLEMENT 19 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-108, 6 of 8 REVISED: JUNE 14, 2004
SECTION 4 - NORMAL PROCEDURES
CAUTION
Familiarity with the enroute operation of the GNS
530 does not constitute proficiency in approach
operations. Do not attempt approach operations in
IMC prior to attaining proficiency in the use of the
GNS 530 approach features.
A. DETAILED OPERATING PROCEDURES
Normal operating procedures are described in the GARMIN GNS 530
Pilot’s Guide, p/n 190-00181-00, Rev. A, dated November 1999, or later
appropriate revision.
B. PILOT’S DISPLAY
The GNS 530 System data will appear on the Pilot’s HSI. The source of data
is either GPS or VLOC as annunciated on the display above the CDI key.
C. AUTOPILOT/FLIGHT DIRECTOR OPERATION
Coupling of the GNS 530 System steering information to the autopilot/flight
director can be accomplished by engaging the autopilot/flight director in the
NAV or APR mode.
When the autopilot/flight director system is using course information
supplied by the GNS 530 System and the course pointer is not
automatically driven to the desired track, the course pointer on the HSI must
be manually set to the desired track (DTK) indicated by the GNS 530. For
detailed autopilot/flight director operational instructions, refer to the FAA
Approved Flight Manual Supplement for the autopilot/flight director.
D. CROSSFILL OPERATIONS
Crossfill capabilities exist between the GNS 530 and GNS 430 systems.
Refer to the Garmin GNS 530 Pilot’s Guide for detailed crossfill operating
instructions.
SECTION 9
SUPPLEMENT 19 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-108, 6 of 8 REVISED: JUNE 14, 2004
SECTION 4 - NORMAL PROCEDURES
CAUTION
Familiarity with the enroute operation of the GNS
530 does not constitute proficiency in approach
operations. Do not attempt approach operations in
IMC prior to attaining proficiency in the use of the
GNS 530 approach features.
A. DETAILED OPERATING PROCEDURES
Normal operating procedures are described in the GARMIN GNS 530
Pilot’s Guide, p/n 190-00181-00, Rev. A, dated November 1999, or later
appropriate revision.
B. PILOT’S DISPLAY
The GNS 530 System data will appear on the Pilot’s HSI. The source of data
is either GPS or VLOC as annunciated on the display above the CDI key.
C. AUTOPILOT/FLIGHT DIRECTOR OPERATION
Coupling of the GNS 530 System steering information to the autopilot/flight
director can be accomplished by engaging the autopilot/flight director in the
NAV or APR mode.
When the autopilot/flight director system is using course information
supplied by the GNS 530 System and the course pointer is not
automatically driven to the desired track, the course pointer on the HSI must
be manually set to the desired track (DTK) indicated by the GNS 530. For
detailed autopilot/flight director operational instructions, refer to the FAA
Approved Flight Manual Supplement for the autopilot/flight director.
D. CROSSFILL OPERATIONS
Crossfill capabilities exist between the GNS 530 and GNS 430 systems.
Refer to the Garmin GNS 530 Pilot’s Guide for detailed crossfill operating
instructions.
To Next Page