Garmin Approach G5 - GPS-Enabled Golf Handheld, Руководство пользователя

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Garmin G5 User's Manual 190-02072-00 Rev. B
39
Installation Manual
Installation Manual
Pilot's Guide
Index
3)
Ensure that aircraft and the unit comply with all on-screen instructions then
select Start.
4)
A progress screen will then be displayed. There is a 30 second countdown
timer for the procedure that resets when the aircraft moves.
5)
When the calibration is complete, a successful status message will be
displayed along with the new pitch and roll offsets.
NOTE: The pilot may adjust the displayed pitch attitude in normal mode. The
maximum amount of pitch display adjustment available in normal mode is ±5.0°.
This feature should not be used to compensate for a non-conforming installation
that does not meet the requirements of the pitch/roll offset compensation
calibration procedure.
NOTE: I
n
a G3X system, or a non-G3X system with multiple G5 units, if the pitch/
roll offset procedure is performed for one unit, it should be performed on all other
G3X AHRS units or G5 units before moving the aircraft.
1.7.4.2.3 C
aLibration
P
roCedure
b: e
nGine
r
un
-u
P
v
ibration
t
eSt
NOTE: Calibration Procedure B is required for all installations to validate the
vibration characteristics of the installation.
Passing the Engine Run-Up Vibration test does not remove the requirement to rigidly
mount the G5. The Engine Run-Up Vibration Test is intended to help discover mounting
issues but successful completion of the test does not validate the mounting of the G5,
and does not account for all possible vibration profiles that may be encountered during
normal aircraft operation
1)
Select the Attitude configuration page.
2)
Select Vibration Test.
3) Ensure the aircraft complies with all on-screen instructions, then select
Start.
4) Gradually increase engine power from idle to full power and back over the
course of 1-2 minutes. A progress screen will be displayed showing the
status of the test.