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7.7.2 GTX 32/33 Testing
The following tests are recommended if the unit is removed or replaced.
1. The integrated transponder/altitude reporting system must be verified in accordance
with Title 14 of the Code of Federal Regulations (CFR) §§ 91.411 and 91.413.
2. For the GTX 33 transponder, make sure the aircraft registration number is properly
entered in the PFD TRANSPONDER CONFIGURATION page.
3. The GTX 33 test requires the use of a Mode S Ramp Generator. The GTX 32 requires a
Mode A/C Ramp Generator. Refer to Title 14 CFR Part 43 Appendix F for specific testing
criteria.
Page 7-52
Rev. E
Cirrus Perspective™ Line Maintenance Manual
190-00920-00