Garmin GI 275 User Manual

190-02246-10 GI 275 Part 23 AML STC Installation Manual
Rev. 11 Page E-8
E.5 Bugs
The information obtained in Table E-2 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-2 Advanced Airframe-Specific Configuration Data – Bugs
Alternately, by pressing the Type buttons, the bugs can be changed to VREF, V1, and V2.
Table E-3 Advanced Airframe-Specific Configuration Data – Alternate Bugs
Notes:
[1] These speeds generally apply to only high-performance airplanes and must be calculated
before each flight. The recommended default value is 0 KT.
Bug Description
POH/AFM
Section
Notes
GLIDE Glide speed
3 – Emergency
Procedures
Optional.
Set to 0 KT if not listed in the POH/AFM.
VX Best angle-of-climb speed
4 – Normal
Procedures
Optional.
Set to 0 KT if not listed in the POH/AFM.
If there are two speeds listed (gear up/gear
down), use the speed listed for gear down.
VY Best rate-of-climb speed
4 – Normal
Procedures
Optional.
Set to 0 KT if not listed in the POH/AFM.
If there are two speeds listed (gear up/gear
down), use the speed listed for gear up.
VR Rotation speed
4 – Normal
Procedures
Optional.
Typically set to rotation speed.
Set to 0 KT if not listed in the POH/AFM.
Bug Description POH/AFM Section Notes
VREF Landing reference speed 4 – Normal Procedures [1]
V1 Commit to fly speed 4 – Normal Procedures [1]
V2 Takeoff safety speed 4 – Normal Procedures [1]
VR Rotation speed 4 – Normal Procedures [1]

Garmin GI 275 Specifications

General

Brand	Garmin
Model	GI 275
Category	Avionics Display
Language	English