Garmin G3X Installation Manual page 63

impacted). If the static port is located under the wing, it is recommended that the port be moved to
an alternate location as part of the GAP 26 installation. If port relocation is required, obtain
guidance from the aircraft designer regarding acceptable alternate static port locations.
• Route all GAP 26 power and ground wires away from any audio wires.
• To avoid magnetic interference, do not use the airframe to ground the GAP 26 or any other high-
current device. See
2" MAX ALLOWABLE TIP LOCATION
AHEAD OF WING LEADING EDGE
5° MAX
ANGLE BETWEEN CHORD
LINE AND PROBE CENTERLINE
WING LEADING EDGE
5.5.2 Heater Wiring Configuration
The GAP 26 uses two internal heaters that may be powered by 14 or 28 volt systems. Each of the heaters
has two wires, one of these two wires is "banded" (Figure 5-3) to help identify individual heaters. These
heaters can be connected to a power source as shown in Figure 5-4 and
190-01115-01
Rev. AA
Section 13.4 for further magnetometer installation considerations.
25%
OF CHORD LENGTH
GARMIN RECOMMENDED
FARTHEST FORWARD PROBE TIP LOCATION
Figure 5-2 GAP 26, Mounting Location Guidance
"Banded" Wire
Figure 5-3 GAP 26 Banded Wire
G3X/G3X Touch Installation Manual - GAP 26 Installation
CHORD LENGTH
CHORD LINE
4" MIN CENTERLINE
DISTANCE
10" MAX CENTERLINE
PROBE CENTERLINE
GARMIN RECOMMENDED
FARTHEST AFT PROBE TIP LOCATION
Figure 5-5.
DISTANCE
Page 5-3