Markings; Table E-4 Advanced Airframe-Specific Configuration Data - Markings - Garmin GI 275 Installation Manual

E.6

Markings

The information obtained in Table E-4 must be obtained for each installation. The POH/AFM column lists
a suggested location for obtaining this information. If a marking is not defined for the aircraft, then it
should be configured as OFF.
NOTE
These markings must match the Type Data (POH/AFM or aircraft specification) for the
specific aircraft being modified.
NOTE
If the airspeed values are listed in the Type Data (POH/AFM) for both IAS and CAS, use
the IAS values.
Table E-4 Advanced Airframe-Specific Configuration Data – Markings
Marking
Maximum landing gear
Vle
extended speed
Typically marks the single
Blue Bar engine best rate-of-climb speed
for a twin-engine aircraft
Typically marks the minimum
controllable airspeed for twin-
Red Bar
engine aircraft with only one
engine operational (Vmca)
Varies. Sometimes used as a
Red/White Bar
fixed point Vne marking
A small white triangle. Meaning
White Triangle
varies by airframe
190-02246-10
Rev. 11
Description
POH/AFM
Section
Set to OFF for fixed gear
2 – Limitations
aircraft.
Blue radial on ASI of light twins.
3 – Emergency
Set to OFF for single-engine
Procedures
aircraft.
Lower red radial on ASI of light
twins.
3 – Emergency
Procedures
Set to OFF for single-engine
aircraft.
If a fixed Red/White bar (not a
barber pole) is shown in the
2 – Limitations
POH/AFM, set to given value.
Otherwise, set to OFF.
If defined in POH/AFM, set to
2 – Limitations given value. Otherwise, set to
OFF.
GI 275 Part 23 AML STC Installation Manual
Notes
Page E-9