M3 GPS INSTALLATION MANUAL Revision D
PAGE 47
APPENDIX D
SPECIMEN FORM 337
8. Description of Work Accomplished
(If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.)
A. The following equipment and major components were removed:
1. (none)
B. The following equipment and major components were installed:
1. 1 ea. Northstar Avionics M3 Navigator, P/N 1200-02-01, TSO-C129 Class
A1
2. 1 ea. Northern Airborne Technology RS08-001 Remote Switch
(if installed)
3. 1 ea. Comant Industries, Inc. Active GPS Antenna, P/N CI 405-7
(if installed
)
C. All equipment was previously approved under Supplemental Type Certificate
Number SA00464NY.
D. Deviations from STC Number SA00464NY include the following:
(Note: List all equipment and major components removed, if any, and list all equipment and major
components installed which may require reference to manufacturer’s instructions. In addition, if a
“localizer override” function is
NOT
provided as part of a NAV/GPS switching system (if installed),
this must be listed as an STC deviation.)
E. The installation was made with reference to Northstar Avionics M3 GPS
APPROACH Navigator, Installation Manual, P/N GM611, Rev. B, July 1, 1996
(or later, as appropriate)
.
F.
(For VFR Installations:)
The Northstar M3 Navigator is limited to VFR Navigation and was installed and
tested in accordance with AC 20-138, Paragraph 7.c.(2).
(For IFR Installations:)
The Northstar M3 Navigator is approved for VFR and IFR En Route, Terminal
Area, and Non-Precision Approach Navigation, and was installed and tested in
accordance with AC 20-138, Paragraph 8.c.(2).
NOTICE
Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be
compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.
Additional Sheets Are Attached
X
Содержание 1200-02-01
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