uAvionix AV-30-C - Flight Direction Indicator; Barometric Corrected Altitude Indicator

UAV-1003947-001, AV-30-C, Installation Manual 25
Rev E
11.3 Non-Supplied Components
Table 5 - Non-Supplied Components
Component
Description
Pitot / Static Tubing
Length as required
Pitot Static T’s
Quantity as required
Circuit Breakers (2A)
One required for each instrument
OAT Probe
Davtron P/N C307PS
Power and Interconnect
Wire
See AC 43.13-1B Chapter 11 § 7 for
acceptable wire types
11.4 Installation Records
The date of installation should be recorded in the aircraft’s log-book.
Entry should include instrument(s) being replaced (AI or DG, or both), or, if
the installation is being performed as a non-required instrument.
Entry should also include a description of any optional connections made.