Bugs; Table E-2 Advanced Airframe-Specific Configuration Data - Bugs; Table E-3 Advanced Airframe-Specific Configuration Data - Alternate Bugs - Garmin GI 275 Installation Manual

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
Bug Description
GLIDE Glide speed
VX Best angle-of-climb speed
VY Best rate-of-climb speed
VR Rotation speed
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
Bug Description
VREF Landing reference speed
V1 Commit to fly speed
V2 Takeoff safety speed
VR Rotation speed
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.
190-02246-10
Rev. 11
POH/AFM
Section
Optional.
3 – Emergency
Procedures
Set to 0 KT if not listed in the POH/AFM.
Optional.
4 – Normal Set to 0 KT if not listed in the POH/AFM.
Procedures
If there are two speeds listed (gear up/gear
down), use the speed listed for gear down.
Optional.
4 – Normal Set to 0 KT if not listed in the POH/AFM.
Procedures
If there are two speeds listed (gear up/gear
down), use the speed listed for gear up.
Optional.
4 – Normal
Typically set to rotation speed.
Procedures
Set to 0 KT if not listed in the POH/AFM.
POH/AFM Section
4 – Normal Procedures
4 – Normal Procedures
4 – Normal Procedures
4 – Normal Procedures
GI 275 Part 23 AML STC Installation Manual
Notes
Notes
[1]
[1]
[1]
[1]
Page E-8