Garmin G5 Installation Manual page 216

Electronic flight instrument, part 23 aml stc
Hide thumbs Also See for G5:
Table of Contents

Advertisement

6.3.12.1.2 VOR Course
1. Apply power to the aircraft and aircraft systems and allow the aircraft systems to initialize.
2. Tune the VHF NAV to the NAV/COM Test Set frequency for VOR operation.
3. Set the Course pointer on the G5 HSI 15 degrees to the left of aircraft heading and ensure that the
G5 HSI CDI is displaying VOR navigation information.
4. Simulate a VOR signal with a "TO" course equal to the aircraft heading.
5. Slowly adjust the course pointer on the G5 HSI CDI toward the aircraft heading until VOR
captures.
6. Center G5 HSI CDI course pointer on the aircraft heading.
7. Engage the autopilot in NAV mode.
8. Adjust the NAV ramp tester course and the G5 HSI CDI course pointer 20 degrees to the left of
current aircraft heading.
9. Verify that the flight controls move toward the left.
10. Adjust NAV ramp tester course to aircraft heading.
11. Adjust the NAV ramp tester course and the G5 HSI CDI course pointer 20 degrees to the right of
current aircraft heading.
12. Verify that the flight controls move toward the right.
13. Adjust the NAV ramp tester course to aircraft heading.
14. Disengage the autopilot.
6.3.12.1.3 LOC
1. Tune the VHF NAV to the NAV/COM Test Set frequency for LOC operation.
2. On the NAV ramp tester simulate centered LOC needle presentation.
3. Set the Course pointer on the G5 HSI to the current aircraft heading.
4. Verify the G5 HSI CDI displays centered deviation for LOC.
5. On the NAV ramp tester simulate 0.093 DDM Left LOC.
6. Verify G5 HSI CDI deviation bar is one dot left.
7. Verify that the flight controls turn to the left.
8. On the NAV ramp tester simulate 0.093 DDM Right LOC.
9. Verify G5 HSI CDI displays one dot right.
10. Verify that the flight controls turn to the right.
11. On the NAV ramp tester simulate centered LOC needle presentation.
12. Disengage the autopilot.
6.3.12.1.4 GPSS Course
This test is only performed for installations that are interfaced to a GPS navigation source and the
interfaced autopilot did not previously have a GPSS function. Conduct this test with the aircraft
positioned where it can receive GPS signal.
1. On the GPS navigator, enter a simple Direct-To flight plan with a waypoint that is on the current
aircraft heading and select the G5 HSI CDI to display GPS. If the navigator has the capability to
enter user waypoints, a user waypoint can be entered to facilitate this test. It is suggested that
the waypoint be within 5 miles of the current aircraft position for best results.
2. On the G5 Attitude display, press the multifunction knob to display the G5 attitude menu,
highlight GPSS and press the multifunction knob to select GPSS.
3. Verify the following;
On the G5 Attitude (if Installed)
Garmin G5 Electronic Flight Instrument Part 23 AML STC Installation Manual
Page 216
190-01112-10
Rev. 21

Advertisement

Table of Contents
loading

Table of Contents