Garmin G5 Installation Manual

Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual 190-01112-10
Rev. 21
Page 198
• G5 (HSI) with Two-inch GPS Navigator Section - 5.17
• Dual G5 with Two-Inch GPS Navigator Section - 5.18
• G5 (ADI) with Two-Inch GPS Navigator Section - 5.19
• G5 Portable Avionics Unit Interface Section - 5.20
• GAD 13 Interface Section - 5.21
• GAD 29B Interface to Garmin Autopilots Section - 5.22
• G5 Interface to Non-Garmin Autopilots Section - 5.23
6.3.7 G5 POST-INSTALLATION CALIBRATION PROCEDURES
After mechanical and electrical installation of the G5 has been completed, prior to operation, a set of
post-installation calibration procedures must be carried out. Table 6-1 describes the required and
optional calibration procedures.
Table 6-1: Post-Installation Calibration Procedure Summary
Calibration Procedure
Procedure Name
Procedure
Description
Installations
Requiring Procedure
A
Pitch/Roll Offset
Compensation
Level aircraft
Procedure A is required
for all installations
B
Engine Run-Up
Vibration Test
Validate vibration
characteristics of
installation
Procedure B is required
for all installations
C
Air Data Static
Pressure Calibration
Altitude Calibration
Procedure C is only
required if Section
6.3.8.2 results for the
G5 fall outside the
tolerances of the Part
43 Appendix E tests.
D
GMU 11 Magnetometer
Calibration
Magnetometer
Calibration
Procedure D is only
required if a GMU 11
was installed
This area intentionally blank
6.3.7.1 CALIBRATION PROCEDURE A: PITCH/ROLL OFFSET COMPENSATION
NOTE
The G5(s) must be installed within the tolerances shown in Figure 4-4 and Figure 4-5.
NOTE
If two G5’s are installed, this procedure must be done on both and can be done concurrently.
See Section 6.3.7.1.1 for example of this calibration procedure.
Using the following procedure, complete these equations.

Garmin G5 Specifications

General

Brand	Garmin
Model	G5
Category	Avionics Display
Language	English