SECTION 9
SUPPLEMENT 7 PA-28-181, ARCHER III
SECTION 9
SUPPLEMENT 7 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-46 REVISED: NOVEMBER 6, 1998
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-46 REVISED: NOVEMBER 6, 1998
SECTION 4 - NORMAL PROCEDURES
WARNING
Familiarity with the enroute operation of the
GNS 430 does not constitute proficiency in
approach operations. Do not attempt approach
operations in IMC prior to attaining proficiency
in the use of the GNS 430 approach feature.
A. DETAILED OPERATING PROCEDURES
Normal operating procedures are described in the GARMIN GNS 430
Pilot’s Guide, p/n 190-00140-00, Rev. A, dated October 1998, or later
appropriate revision.
B. PILOT’S DISPLAY
The GNS 430 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 430 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 430 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
430. For detailed autopilot/flight director operational instructions, refer to
the FAA Approved Flight Manual Supplement for the autopilot/flight
director.
SECTION 4 - NORMAL PROCEDURES
WARNING
Familiarity with the enroute operation of the
GNS 430 does not constitute proficiency in
approach operations. Do not attempt approach
operations in IMC prior to attaining proficiency
in the use of the GNS 430 approach feature.
A. DETAILED OPERATING PROCEDURES
Normal operating procedures are described in the GARMIN GNS 430
Pilot’s Guide, p/n 190-00140-00, Rev. A, dated October 1998, or later
appropriate revision.
B. PILOT’S DISPLAY
The GNS 430 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 430 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 430 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
430. For detailed autopilot/flight director operational instructions, refer to
the FAA Approved Flight Manual Supplement for the autopilot/flight
director.
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