Piper ARCHER III - Page 305

SECTION 9
PA-28-181, ARCHER III SUPPLEMENT 19
ISSUED: JULY 12, 1995 REPORT: VB-1611
REVISED: JUNE 14, 2004 3 of 8, 9-105
SECTION 9
PA-28-181, ARCHER III SUPPLEMENT 19
ISSUED: JULY 12, 1995 REPORT: VB-1611
REVISED: JUNE 14, 2004 3 of 8, 9-105
SECTION 2 - LIMITATIONS
A. The GARMIN GNS 530 Pilot’s Guide, p/n 190-00181-00, Rev. A, dated
November 1999, or later appropriate revision, must be immediately
available to the flight crew whenever navigation is predicated on the use of
the system.
B. The Garmin 500 Series Pilot’s Guide Addendum, Display Interface for
Traffic and Weather Data, must be immediately available to the flight crew
if the B.F. Goodrich WX-500 Stormscope
®
or the B.F. Goodrich
SKYWATCH
™
Traffic Advisory System (TAS) is installed.
C. The GNS 530 must utilize the following or later FAA approved software
versions:
Sub-System Software Version
Main 2.00
GPS 2.00
Comm 1.22
VOR/LOC 1.25
G/S 2.00
The main software version is displayed on the GNS 530 self test page
immediately after turn-on for 5 seconds. The remaining system software
versions can be verified on the AUX group sub-page 2,
“SOFTWARE/DATABASE VER”.
D. IFR enroute and terminal navigation predicated upon the GNS 530’s GPS
Receiver is prohibited unless the pilot verifies the currency of the data base
or verifies each selected waypoint for accuracy by reference to current
approved data.
E. Instrument approach navigation predicated upon the GNS 530’s GPS
Receiver must be accomplished in accordance with approved instrument
approach procedures that are retrieved from the GPS equipment data base.
The GPS equipment data base must incorporate the current update cycle.
1. Instrument approaches utilizing the GPS receiver must be conducted in
the approach mode and Receiver Autonomous Integrity Monitoring
(RAIM) must be available at the Final Approach Fix.
SECTION 2 - LIMITATIONS
A. The GARMIN GNS 530 Pilot’s Guide, p/n 190-00181-00, Rev. A, dated
November 1999, or later appropriate revision, must be immediately
available to the flight crew whenever navigation is predicated on the use of
the system.
B. The Garmin 500 Series Pilot’s Guide Addendum, Display Interface for
Traffic and Weather Data, must be immediately available to the flight crew
if the B.F. Goodrich WX-500 Stormscope
®
or the B.F. Goodrich
SKYWATCH
™
Traffic Advisory System (TAS) is installed.
C. The GNS 530 must utilize the following or later FAA approved software
versions:
Sub-System Software Version
Main 2.00
GPS 2.00
Comm 1.22
VOR/LOC 1.25
G/S 2.00
The main software version is displayed on the GNS 530 self test page
immediately after turn-on for 5 seconds. The remaining system software
versions can be verified on the AUX group sub-page 2,
“SOFTWARE/DATABASE VER”.
D. IFR enroute and terminal navigation predicated upon the GNS 530’s GPS
Receiver is prohibited unless the pilot verifies the currency of the data base
or verifies each selected waypoint for accuracy by reference to current
approved data.
E. Instrument approach navigation predicated upon the GNS 530’s GPS
Receiver must be accomplished in accordance with approved instrument
approach procedures that are retrieved from the GPS equipment data base.
The GPS equipment data base must incorporate the current update cycle.
1. Instrument approaches utilizing the GPS receiver must be conducted in
the approach mode and Receiver Autonomous Integrity Monitoring
(RAIM) must be available at the Final Approach Fix.