Installation Limitations; Installation Approval Limitations - uAvionix AV-30-S Installation Manual

6

Installation Limitations

The following section provides the FAA approved installation limitations.
6.1

Installation Approval Limitations

This article meets the minimum performance and quality control
standards required by an Approved Model List - Supplemental Type
Certificate (AML-STC) and when installed on aircraft approved on the
AML can be approved for return to service after installation.
If installation for an aircraft that is not listed on the AML, separate
approval must be obtained. The following installation limitations apply:
 Installation is restricted to CFR Part 23, Class I and II, single engine aircraft
only (gross take-off weight of no more than 6000 lbs, 6 seats or less,
including pilot/copilot).
 Installation is restricted to aircraft with a 25,000-foot maximum (or less)
ceiling limitation.
 Installation is restricted to aircraft with equal to or less than 300 knot Vne
airspeed.
 Installation may not be performed as part of an integrated autopilot system
including heading bug interface, attitude source or flight director display.
 Installation may not be performed as a replacement of a Horizontal
Situational Awareness Indicator (HSI).
 In installations where the primary attitude indicator is being replaced, the
existing airspeed and altimeter must remain in their factory locations.
 An electrical load analysis must be performed in association with the
installation.
 Connection to the Audio interface is not allowed for IFR approved non-
metallic aircraft due to indirect lightning protection limitations.

A Wet compass must be installed in the aircraft.
UAV-1003947-001, AV-30-C, Installation Manual 14 Revision C