Garmin GAD 43e Installation Manual - Page 19

Materials Required But Not Supplied - g500

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2. INSTALLATION OVERVIEW 2.1 Introduction This section provides hardware equipment information for installing the GAD 43 and related hardware. Installation of the GAD 43 should follow the aircraft TC or STC requirements. Cabling is fabricated by the installing agency to fit each particular aircraft. The guidance of FAA advisory circulars AC 43.13-1B and AC 43.13-2A, where applicable, may be found useful for making retro-fit installations that comply with FAA regulations. 2.2 Installation Materials 2.2.1 Configurations Available The GAD 43 is available under the following part numbers. Catalog part numbers are shown with and without the installation kit. Table 2-1. Catalog Part Numbers Model GAD 43 Unit P/N 011-01970-00 Catalog P/N Without Installation Kit 010-00724-00 Catalog P/N With Installation Kit (G600) 010-00724-01 Catalog P/N With Installation Kit (G500) 010-00724-02 Table 2-2. Installation Accessories Item GAD 43 Connector Kit Garmin P/N 011-01990-00 2.2.2 Materials Required But Not Supplied The GAD 43 is intended for use with the standard aviation accessories. The following items are required for installation, but not supplied: • Wire (MIL-W-22759/16 or equivalent) • Shielded Wire (MIL-C-27500 or equivalent) • Circuit Breaker (2.5A) • Tie Wraps or Lacing Cord • Ring Terminals (for grounding) 2.3 Optional Reference Material Item G500 Pilot's Guide G500 Cockpit Reference Guide G600 Pilot's Guide G600 Cockpit Reference Guide GDU 620 Installation Manual Garmin P/N 190-01102-02 190-01102-03 190-00601-02 190-00601-03 190-00601-04 2.4 Installation Considerations The existing remote-mounted or panel-mounted gyro can be removed, and the GAD 43 will be installed to emulate the signals from the removed instrument. The following sections describe issues that must be considered for each installation. GAD 43 Installation Manual 190-00899-00 Page 2-1 Rev. B

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GAD 43 Installation Manual
Page 2-1
190-00899-00
Rev. B
2.
INSTALLATION OVERVIEW
2.1 Introduction
This section provides hardware equipment information for installing the GAD 43 and related hardware.
Installation of the GAD 43 should follow the aircraft TC or STC requirements. Cabling is fabricated by
the installing agency to fit each particular aircraft. The guidance of FAA advisory circulars AC 43.13-1B
and AC 43.13-2A, where applicable, may be found useful for making retro-fit installations that comply
with FAA regulations.
2.2 Installation Materials
2.2.1 Configurations Available
The GAD 43 is available under the following part numbers. Catalog part numbers are shown with and
without the installation kit.
Table 2-1. Catalog Part Numbers
Model
Unit P/N
Catalog P/N
Without
Installation Kit
Catalog P/N
With Installation
Kit (G600)
Catalog P/N
With Installation
Kit (G500)
GAD 43
011-01970-00
010-00724-00
010-00724-01
010-00724-02
Table 2-2. Installation Accessories
Item
Garmin P/N
GAD 43 Connector Kit
011-01990-00
2.2.2 Materials Required But Not Supplied
The GAD 43 is intended for use with the standard aviation accessories. The following items are required
for installation, but not supplied:
•
Wire (MIL-W-22759/16 or equivalent)
•
Shielded Wire (MIL-C-27500 or equivalent)
•
Circuit Breaker (2.5A)
•
Tie Wraps or Lacing Cord
•
Ring Terminals (for grounding)
2.3 Optional Reference Material
Item
Garmin P/N
G500 Pilot’s Guide
190-01102-02
G500 Cockpit Reference Guide
190-01102-03
G600 Pilot’s Guide
190-00601-02
G600 Cockpit Reference Guide
190-00601-03
GDU 620 Installation Manual
190-00601-04
2.4 Installation Considerations
The existing remote-mounted or panel-mounted gyro can be removed, and the GAD 43 will be installed
to emulate the signals from the removed instrument.
The following sections describe issues that must be considered for each installation.