Garmin 200 Istruzione Sull'Installazione
GMX 200 STC Installation
005-C0315-00 Rev A
STC Master Data List
Page 5 of 6
2.3 Equipment
List
All equipment must have the Part Numbers and Software Versions contained in the following table, or
later FAA Approved revisions or versions.
later FAA Approved revisions or versions.
Table 3 Required Equipment List
Model Description
Part
Number
Number
Mfg.
Software Ver.
(or later FAA
approved version)
OR
GMX 200, Black
GMX 200, Gray
GMX 200 I/O Traffic, Black
GMX 200 I/O Traffic, Gray
GMX 200 I/O Radar/TAWS, Black
GMX 200 I/O Radar/TAWS, Gray
GMX 200 I/O Traffic/Radar, Black
GMX 200 I/O Traffic/Radar, Gray
GMX 200, Gray
GMX 200 I/O Traffic, Black
GMX 200 I/O Traffic, Gray
GMX 200 I/O Radar/TAWS, Black
GMX 200 I/O Radar/TAWS, Gray
GMX 200 I/O Traffic/Radar, Black
GMX 200 I/O Traffic/Radar, Gray
011-01271-00
011-01271-10
011-01465-00
011-01465-10
011-01466-00
011-01466-10
011-01467-00
011-01467-10
011-01271-10
011-01465-00
011-01465-10
011-01466-00
011-01466-10
011-01467-00
011-01467-10
Garmin 2.02
Mounting Tube
115-00746-00
Garmin
n/a
Database data card
010-10820-00
Garmin
n/a
Connector Kit
Connector Kit, I/O (see note 1)
Connector Kit, I/O (see note 1)
011-01283-00
011-01283-01
011-01283-01
Garmin n/a
Configuration Module
011-00979-02
Garmin
n/a
Note 1: I/O Connector Kit required for I/O models only.
3. GENERAL INSTALLATION REQUIREMENTS
4. GENERAL
The installation must be done in accordance with all applicable FARs. The installation shall conform to
the data listed in Section 2.1, Data Required for Installation with exception of special instructions as
defined in Section 5 Special Installation Instructions, which shall have precedence over the data listed in
Section 2.1.
the data listed in Section 2.1, Data Required for Installation with exception of special instructions as
defined in Section 5 Special Installation Instructions, which shall have precedence over the data listed in
Section 2.1.
4.1 Mechanical
Mechanical installation, wiring, cable bundling and routing, and connections to existing aircraft systems
must conform to those specific instructions or requirements found in the STC data. Those aspects of the
STC where specific installation instructions or requirements are not provided in the STC data, the
installer shall conform to the recommended practices and procedures found in AC 43.13-2A, Chapter 2,
Radio Installations, and AC 43.13-1B, Chapter 11, Electrical Systems, Section 3, 4 and 7.
must conform to those specific instructions or requirements found in the STC data. Those aspects of the
STC where specific installation instructions or requirements are not provided in the STC data, the
installer shall conform to the recommended practices and procedures found in AC 43.13-2A, Chapter 2,
Radio Installations, and AC 43.13-1B, Chapter 11, Electrical Systems, Section 3, 4 and 7.
4.2 Hardware
Hardware not supplied with the equipment, or otherwise specified in the appropriate installation manuals
or other STC data (ie screws, nuts, tie wrap, etc) shall be from standard aircraft hardware as described
by AC 43.13-1B, Chapter 5, Aircraft Hardware.
or other STC data (ie screws, nuts, tie wrap, etc) shall be from standard aircraft hardware as described
by AC 43.13-1B, Chapter 5, Aircraft Hardware.