Limitations; Installation Limitations; Operational Limitations - Garmin G5 Installation Manual

2

LIMITATIONS

2.1 Installation Limitations

It is the installer's responsibility to ensure the installation will meet the requirements in this manual prior
to modification the aircraft.
As installed by this STC, the G5:
•
is NOT approved in FAA certified aircraft that:
•
are approved for Flight Into Known Icing (FIKI) conditions
•
have a gross take-off weight more than 6000 lbs
•
can seat more than 6 passengers
•
cannot replace a primary attitude indicator that includes a flight director or is part of an autopilot
system (an existing attitude indicator in the primary location that is part of an autopilot but without
flight director may be moved to the rate of turn indicator location and a G5 installed in the primary
location)
•
cannot replace the rate-of-turn indicator that is part of an autopilot system
•
cannot be installed in a shock mounted instrument panel Reference Section 4.1
•
must be installed in an instrument panel constructed of aluminum with a minimum thickness of .040
inches.
•
is only approved to interface with aircraft systems specified in this manual
•
cables and wiring interfaced to the G5 must not be installed in fuel bays

2.2 Operational Limitations

Refer to the Airplane Flight Manual Supplement (AFMS) for operational limitations.
Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual
Page 16 of 53
190-01112-10
Rev. 2