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AUDIO PANEL AND CNS<br />

SYSTEM<br />

OVERVIEW<br />

FLIGHT<br />

INSTRUMENTS<br />

EIS<br />

AUDIO PANEL<br />

& CNS<br />

FLIGHT<br />

MANAGEMENT<br />

HAZARD<br />

AVOIDANCE<br />

AFCS<br />

ADDITIONAL<br />

FEATURES<br />

APPENDICES<br />

INDEX<br />

4.4 GTX 32/GTX 33 TRANSPONDER<br />

The GTX 32 Transponder provides Mode A and Mode C interrogation and reply capabilities.<br />

The GTX 33 or GTX 33 with Extended Squitter Mode S Transponder provides Mode A, Mode C, and Mode S<br />

interrogation and reply capabilities. Selective addressing or Mode Select (Mode S) capability includes the<br />

following features:<br />

• Level-2 reply data link capability (used to exchange information between aircraft and ATC facilities)<br />

• Surveillance identifier capability<br />

• Flight ID (Flight Identification) reporting – The Mode S Transponder reports aircraft identification as either the<br />

aircraft registration or a unique Flight ID.<br />

• Altitude reporting<br />

• Airborne status determination<br />

• Transponder capability reporting<br />

• Mode S Enhanced Surveillance (EHS) requirements<br />

• Acquisition squitter – Acquisition squitter, or short squitter, is the transponder 24-bit identification address.<br />

The transmission is sent periodically, regardless of the presence of interrogations. The purpose of acquisition<br />

squitter is to enable Mode S ground stations and aircraft equipped with a Traffic Avoidance System (TAS) to<br />

recognize the presence of Mode S-equipped aircraft for selective interrogation.<br />

• Extended squitter (optional with GTX 33 w/Extended Squitter only) – The extended squitter is transmitted<br />

periodically and contains information such as altitude (barometric and GPS), GPS position, and aircraft<br />

identification. The purpose of extended squitter is to provide aircraft position and identification to ADS-B<br />

Ground-Based Transceivers (GBTs) and other aircraft.<br />

The Hazard Avoidance Section provides more details on traffic avoidance systems.<br />

TRANSPONDER CONTROLS<br />

Transponder function is displayed on three levels of softkeys on the PFD: Top-level, Mode Selection, and<br />

Code Selection. When the top-level XPDR Softkey is pressed, the Mode Selection softkeys appear: STBY, ON,<br />

ALT, VFR, CODE, IDENT, BACK.<br />

When the CODE Softkey is pressed, the number softkeys appear: 0, 1, 2, 3, 4, 5, 6, 7, IDENT, BKSP,<br />

BACK. The digits 8 and 9 are not used for code entry. Pressing the numbered softkeys in sequence enters<br />

the transponder code. If an error is made, pressing the BKSP Softkey moves the code selection cursor to the<br />

previous digit. Pressing the BKSP Softkey again moves the cursor to the next previous digit.<br />

Pressing the BACK Softkey during code selection reverts to the Mode Selection Softkeys. Pressing the BACK<br />

Softkey during mode selection reverts to the top-level softkeys.<br />

The code can also be entered with the FMS Knob on the PFD or the XPDR Key and numeric keypad or<br />

FMS/XPDR NAV/COM Knob. Code entry must be completed with either the softkeys, numeric keypad, or the<br />

FMS Knob, but not a combination of both.<br />

Pressing the IDENT Softkey while in Mode or Code Selection initiates the ident function and reverts to the<br />

top-level softkeys.<br />

After 45 seconds of transponder control inactivity, the system reverts back to the top-level softkeys.<br />

136<br />

Pilot’s Guide for the <strong>Cirrus</strong> <strong>SR2x</strong> with <strong>Cirrus</strong> Perspective by Garmin<br />

190-00820-11 Rev. A

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