Piper Arrow PA-28R-201 Pilot Operating Handbook page 433

SECTION 9
SUPPLEMENT 21
SECTION 2- LIMITATIONS
Pilot's Guide
The Garmin 400W
(or later revisions), must be immediately availablefor the flight crew whenever
whenever
navigation is predicated on the use of the GNS430W
• 400W
Series Pilot'sGuide & Reference P/N 190-00356-00 Rev. B, or later
revision.
This AFM
supplement does not grant approval for IFR operations to aircraft
limitedto VFR operations. Additional aircraft systems may be required for IFR
operational approval.
System Software
The system must utilize the Main and GPS
laterFAA approved versions for this installation). The software versions are
displayed on the self-test page immediately after turn-on, for approximately 5
seconds, or they can be accessed on the AUX-UTILITY
software versions may
Subsequent
400W
Series Pilot'sGuide for furtherinformation.
Software Item
Main Software Version
GPS Software Version
Navigation Data Base
The GNS43OW unit database cards listed in the following table (or laterFAA
approved versions for this installation) must be installed.
• IFR enroute and terminal
the currency of the database or verifies each selected waypoint for accuracy
by reference to current approved data.
accuracy
REPORT: VB-1612
Page 4 of 12
9-176
HB-PQY, Page: 9-176-(0)
Series Pilot's Guide, part number
support different functions. Check
Software
Approved
Approved
(or later FAA-approved
Software Version
3.0
3.0
Table 1
navigation is prohibited unless the pilot verifies
Revision: 22, MAY 12, 2010
PA-28R-201,
and revisionlisted below
unit.
software versions listedbelow (or
page.
Versions
Software Version
versions)
As Displayed on Unit
3.0
3.0
ISSUED:
JULY
REVISED: MAY
ARROW
the
12, 1995
12, 2010
9-176