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Page 7-10 G1000 System Maintenance Manual - Hawker Beechcraft G36

Rev. 5 190-01259-00

Original GTS 820 Reinstalled

No software or configuration loading is required if the removed GTS 820 is re-installed. This

does not include units that were returned for repair as their software and configuration files are

deleted during the repair testing process. Continue to the GTS 820 Test (Section 7.2.1).

New, Repaired or Exchange GTS 820 Installed

If a new, repaired or exchange GTS 820 is installed, the correct software and configuration files

must be loaded to the unit. See Section 3.7 and then continue to the GTS 820 Test (Section

7.2.1).

7.2.1 GTS 820 Test

NOTE

The GTS 8XX Traffic System must be calibrated using the GTS 8XX

Install Tool, Garmin Part Number 006-A0242-00 prior to accomplishment

of the functional check. Reference the GTS 8XX/GPA 65 Installation

Manual, 190-00587-00 for instructions on the use of the GTS 8XX Install

Tool for calibration and accomplishment of the functional check.

The following test will be performed using an appropriate laptop computer with GTS 8XX Install

Tool GPN 006-A0242-00 installed, a USB-A to USB-B cable, and suitable ramp tester such as a

TIC TR220 or equivalent.

To select a scenario that will properly converge and intercept the GTS 8XX, the GTS 8XX must

be in ground test mode. Activate ground test mode by enabling the Ground Test field on the

Normal tab of the GTS 8XX Install Tool. To enable ground test mode, the aircraft must be on the

ground and the GTS 8XX must be in normal system mode and in standby.

NOTE

Using the GTS 8XX Install Tool, Garmin Part Number 006-A0242-00,

place the Ground Sense, and Squat Switch Sense to OPEN, under the

CONFIGURATION tab prior to accomplishment of the functional check.

Reference the GTS 8XX/GPA 65 Installation Manual, 190-00587-00 for

instructions on the use of the GTS 8XX Install Tool.

a. Position the test set directional antenna with a clear line of sight to the GTS 820 antenna at

90 degrees. With the GTS 820 powered up and in Standby mode indicated on the MFD,

cycle the GTS 820 to ‘Operate’.

b. On the test set, select the following:

• Set the intruder type as ATCRBS.

• Intruder Start Distance: 10 nm.

• Intruder Start Altitude: 50,000 ft.

• Vertical Speed: 0 fpm.

• Velocity: 360 kts.

c. Initiate the intruder scenario and observe the following:

• Traffic should be acquired at approximately 10 NM at 90 degree bearing and co-

altitude. Observe intruder closes on own aircraft at a rate of 0.1 NM/sec.

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Garmin Software Version 0858.09 Bedienerhandbuch Seite 64