Table 5-5 Advanced Airframe Specific Configuration Data - Markings - Garmin GI 275 Maintenance Manual

Attitude indicator
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Arc Color
Caution / smooth air
YELLOW
operational range
Never exceed speed/
max operating speed/
Vne/Vmo/Mmo
max operating mach
number
Table 5-5 Advanced Airframe Specific Configuration Data – Markings
Marking
Vle
BLUE BAR
RED BAR
RED/WHITE BAR
WHITE TRIANGLE
190-02246-11
Rev. 1
POH/AFM
Description
Section
2 - Limitations
2 - Limitations
Description
Maximum landing gear
extended speed
Typically marks the single
engine best rate-of-climb
speed for a twin-engine aircraft
Typically marks the minimum
controllable airspeed for twin-
engine aircraft with only one
engine operational (Vmca)
Varies – sometimes used as a
fixed point Vne marking
A small white triangle –
meaning varies by airframe
If the YELLOW arc is defined by the AFM/
POH or aircraft specification, set to ON with
Min value equal to Maximum structural
speed (Vno). Max value should be
configured to Vne, or the highest value of
Vne if variable.
If the YELLOW arc is not defined, set to
OFF.
If defined as a fixed value, set to Fixed, and
enter POH/AFM defined Vne/Vmo as the
Min value.
If variable with altitude, set to Variable, and
set overspeeds in accordance with
Appendix E in GI 275 Part 23 AML STC
Installation Manual.
POH/AFM
Section
Set to OFF for fixed gear
2 - Limitations
aircraft.
Blue radial on ASI of light
twins.
3 - Emergency
Procedures
Set to OFF for single-engine
aircraft.
Lower red radial on ASI of
3 - Emergency
light twins.Set to OFF for
Procedures
single-engine aircraft.
If a fixed RED/WHITE bar,
(not a barber pole) is shown
2 - Limitations
in the POH/AFM, set to given
value. Else, set to OFF.
If defined in POH/AFM, set to
2 - Limitations
given value. Else, set to OFF.
GI 275 Part 23 AML STC Maintenance Manual
Notes
Note
Page 5-41

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