CESSNA
SECTION 7
MODEL 172S NAV III
AIRPLANE AND SYSTEM DESCRIPTION
GFC 700 AFCS
U.S.
FLIGHT INSTRUMENTS
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ATTITUDE INDICATOR
The G1000 attitude indicator is shown on the upper center of the PFD.
The attitude indication data is provided by the Attitude and Heading
Reference System (AHRS). The G1000 attitude indicator provides a
horizon line that is the full width of the GDU display.
The roll index scale is conventional with 10° graduations to 30° and
then 15° graduations to 60° of roll. The roll pointer is slaved to the
airplane symbol. The pitch index scale is graduated in 5° increments
with every 10° of pitch labeled. If pitch limits are exceeded in either the
nose-up or nose-down direction, red warning chevrons will appear on
the indicator to point the way back to level flight. A small white
trapezoid located below the roll pointer moves laterally left and right to
provide the slip-skid information previously supplied by the skid
indicator ball. The trapezoid should be centered below the roll pointer
for coordinated turns. The standby (vacuum) attitude indicator is found
on the lower center instrument panel.
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172SPHBUS-00
7-17
Summary of Contents for Cessna C172S PIM
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