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4. Trim Position Display 16. Switch Panel 28. Trim Switch 40. Circuit Breakers
5. Annunciator Lights 17. Ignition/Start Sw. 29. Intercom 41. Nav/Comm
6. Airspeed Indicator 18. Master Sw. Panel 30. Outside Air Temp. Ind. 42. GPS
7. Artificial Horizon Ind, 19. Flap Control 31. Hour Meter 43. Transponder
8. Altimeter 20. Cabin Heat Control 32. Ammeter 44 Fuel Prime Switch
9. Tachometer 21. Defrost/Floor Lever 33. Voltmeter 45. ELT Remote Switch (Artex ELT-200)
10. Stall Warning Horn 22. Parking Brake Lever 34. Oil Temp. Ind.
11. Turn Coordinator 23. Fuel Shutoff Handle 35. Oil Pressure Ind. 46. Traffic Advisory System Switch (TAS600)
12. Directional Gyro 24. Alternate Air Lever 36. Fuel Pressure Ind.
Figure 7.2. Instrument Panel Diagram
7.4.1. Flight Instruments
The flight instruments are installed on the pilot's side of the instrument panel.
7.4.2. Cabin Heat
The cabin heat and defrost system, directs ram air through the exhaust heat shroud into the cabin heat valve. The warm air is then directed to the window defrosting vents and to the cabin floor as selected by the Floor/Defrost lever.
The cabin heat selector, located in the center console, is used to regulate the flow of heated air. Lever down = cabin heat FULL ON The Floor/Defrost lever directs the heated air to the defrost and floor vents. Lever down = all cabin heat to Floor
7.4.3. Cabin Air
The cabin aeration is controlled by two adjustable air-vent nozzles. The two sliding windows in the canopy can be opened for additional ventilation.
7.5. LANDING GEAR SYSTEM
The landing gear system consists of the two main landing gear wheels mounted to aluminum spring struts and a 60° castering nose wheel. The suspension of the nose wheel is provided by an elastomer spring.
The wheel fairings for the landing gear are removable. When flying without wheel fairings, it should be noted that there is a reduction in some areas of performance (refer to Chapter 5).
7.5.1. Wheel Brakes
CAUTION
WHEN PLACING THE FEET ON THE BRAKE PEDALS, CARE SHOULD BE TAKEN TO USE ONLY THE TOE OF YOUR SHOE SO YOU DO NOT CONTACT THE STRUCTURE ABOVE THE PEDALS, WHICH COULD PREVENT EFFECTIVE APPLICATION OF THE BRAKE(S).
Hydraulically operated disc brakes act on the wheels of the main landing gear. The wheel brakes are operated individually using the toe-brake pedals either on the pilot's or on the co-pilot's side. If either the left or right wheel brake system on the pilot’s side fail, the co-pilot’s brakes fail too. If the co-pilots brake master cylinder or input lines to the pilots master cylinder fails the pilots brakes will still operate. See Figure 7.3, Brake System Schematic Diagram.
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