EADI / EHSIThe  Electronic Attitude Director Indicator (EADI) and Electronic Horizontal Situation Indicator (EHSI) make up the core of the Electronic Flight Instrument System (EFIS), which are the T-6A's primary navigation aids used when flying.
Temperature Systems ConsoleThe temperature console is responsible for all air conditioning and temperature operations.
Standby IndicatorsL to R: Airspeed, Attitude, Altimeter & Turn and Slip 
Oxygen Systems ConsoleThe oxygen systems console is responsible for the OBOGS (On-Board Oxygen Generation System).
Audio ConsoleToggles On or Off many audio switches for various navigational systems.
Button
Radio Communication SystemDisplays the current radio frequencies for ADF, Communications, Transponder and NAV1.
Flightplan Display Unit (FDU)Displays the flight-planner route mode of the Texan II GPS system.
G-Force IndicatorDisplays the current force in G being applied to the airframe with needles for maximum and minimum attained G-force.
Chronometer Displays the current local time in 24 hour format.
Nosewheel Steering &Speed Brake indicatorsDisplays if the Nosewheel Steering system is active (top indicator) and if the Speedbrake is deployed (bottom indicator).
Digital Airspeed Indicator Shows the current indicated airspeed in knots.
Parking Brake HandleTurn to engage or release the aircraft park brakes.
Engine/Systems/NACWS Display (ESND)Displays current oil, hydraulic and electrical systems data.
Central Warning/Caution/Advisory and Annunciation System (CWS)Displays to the pilot any issues that need to be brought to their attention during aircraft operations.
Magnetic CompassShow directions in a frame of reference in which the directions of the magnetic poles are due north and south.
Emergency Locator TransmitterDesigned to transmit a distress signal on 121.5, 243.0-megahertz frequencies (and for newer ELTs, on 406 MHz).
MK16 Ejection SeatThe seat is designed to accommodate a very wide, size and weight range.
Emergency Landing Gear HandleProvides landing gear extension in the event of electrical, hydraulic, or mechanical failure.
The Beechcraft T-6 Texan II is a single-engined turboprop, two-seat primary trainer designed to train Joint Primary Pilot Training (JPPT) students in basic flying skills common to U.S. Air Force and Navy pilots.  With broad training capabilities, cost effective operation and proven reliability, making it the ideal flight training solution for many other air force units around the world. Stepped-tandem seating in the single cockpit places one crew member in front of the other, with the student and instructor positions being interchangeable. The aircraft is fully aerobatic and features a pressurized cockpit with an anti-G system, ejection seat and an advanced avionics package with sunlight-readable liquid crystal displays.  General CharacteristicsPrimary Function: Entry-level trainer in joint primary pilot trainingPowerplant: 1,100 hp Pratt & Whitney Canada PT6A-68 turbo-prop engineWingspan: 33.5 feet (10.19 meters)Length: 33.4 feet (10.16 meters)Height: 10.7 feet (3.23 meters)Speed: 320 miles per hourStandard Basic Empty Weight: 6,500 pounds (2,955 kilograms)Ceiling: 31,000 feet (9448.8 meters)Range: 900 nautical miles (1,667 kilometers)Crew: Two, student pilot and instructor pilotArmament: NoneDate Deployed: May 2000Unit Cost: $4.272 million
Ejection HandleSeat firing handle pulled causing seat initiation cartridge to fire.
Beechcraft T-6 Texan II
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UnknownUnknown at this time.
NACWS PushbuttonToggles the Engine/Systems/NACWS display.
Angle of Attack Indicator Displays the current angle of attack relative to the airflow over the wing.
Avionics SwitchesThis panel is located on both sides of the Ejection Seat and both are filled with a variety of switches.
Electronic Flight Information System (EFIS)Controls the operation of the EADI and EHSI systems.
Backup Communication RadioA radio for COM2 frequency tuning.
Flap IndicatorDisplays the current position of the wing flaps.
Gear Indicator and HandlePull or push to raise or lower the landing gear.  Also features indication lights, green for down, red for transitioning and no lights indicate gear raised.
Alternate Engine Data Display (AEDD)Displays both cockpits with backup visual indication of engine operations.
Lighting and Trim Aid ConsoleDisplays the aileron, rudder and pitch trim tab positions along with exterior lighting controls.
Flight StickControl the aircraft's direction in flight.
Primary Engine Data Display (PEDD)Displays the aircrafts major engine data.
Digital Vertical Speed IndicatorDisplays the current speed of ascent or descent in feet per minute.
Power Control Lever (PCL) and Flaps ConsoleThe Power Control Lever & Flaps console is used to control engine power and aircraft flaps position. Additionally, by clicking the red 'engine cutoff' switch at idle throttle, you can shut down the engine.
Rudder PedalsControl the planes Yaw.
Seat Control and System Test ConsoleThe switches on this console test numerous lamps and systems and is used during pre-flight.
Digital Altitude IndicatorDisplays baro-corrected altitude and a 10,000 feet counter is covered by a striped flag below 10,000 feet. The Baro-set Data displays millibars (MB) and inches of mercury (IN HG) to provides correct altitude indication.
Propulsion ConsoleThe propulsion console is responsible for all startup and engine operations.