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G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 7-1
190-01180-02 Revision 3
7 G1000 EQUIPMENT CONFIGURATION & TESTING
Refer to Section 3.6 for information on loading software and configuration of G1000 equipment
covered by this STC.
7.1 TRANSPONDER TESTING
The integrated transponder/altitude reporting system must be verified in accordance with Title
14 of the Code of Federal Regulations (14 CFR) §§ 91.411 and 91.413. These tests require the
use of a Mode S ramp generator. Specific instructions for operating the ramp tester are
contained in the applicable operator's manual. Refer to 14 CFR Part 43 Appendices E and F for
testing criteria.
The transponder is tested while operating in the normal mode unless otherwise specified.
Perform the following procedures using an appropriately rated transponder test set.
7.1.1 EXTENDED SQUITTER TEST
For those aircraft with extended squitter enabled, perform the following test procedures. The
transponder is tested while operating in the normal mode unless otherwise specified. Perform
the following procedures using an appropriately rated transponder test set.
a. On PFD, press the XPDR softkey and verify that ADS-B TX softkey is
available. Select ADS-B TX (selection will be greyed out).
b. Using a transponder ramp tester, evaluate ADS-B. Using an appropriately
rated ADTS, input an airspeed of 50 knots. Verify the following information
is displayed on the test set:
Squitter Type
Altitude
Altitude Source
Squitter Period
Latitude and Longitude
Aircraft Type
Squitter Period
7.2 GTS TRAFFIC SYSTEM
CAUTION
After any maintenance or modification is made to the GTS 820 T
A
S
cables such as replacing a connector or entire cable, some important
considerations must be made.
Be sure to adhere to all of the specifications and limitations such as
minimum and maximum cable attenuation, attenuation balance between
cables, phase matching etc. in the Installation Manual referenced in
Table 1.2.
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