User manual

Page 35

Aircraft Operation Manual

Piper Cheyenne I, IA, II, IIXL

For ight simulation use only

Primary Instruments - Pilot panel

KCI 310 Attitude Direction Indicator (ADI)

1: Attitude Indicator

2: Flight Director

3: Glidepath Indicator

4: Localizer signal indicator

5: Decision Height Indicator

6: RNAV Indicator: Illuminated when „GPS“ is selected as the NAV

source. Requires a ight plan to be active in the Trimble GPS.

7: ADI test, and light test button (with the KFC300 autopilot only)

8: Slip/Skid Indicator

KPI 553A Horizontal Situation Indicator (HSI)

1: Course Deviation Indicator CDI

2: Glidepath Indicator

3: Heading pointer

4: NAV1/ADF1 pointer

5: OBS Selector Knob

6: Heading Selector Knob

7: NAV2/ADF Selector Switch

8: NAV/ADF Flag

9: DME Readout. DME source (DME1 / hold / DME2) depends on

the position of the DME selector knob on the avionics panel

10: Groundspeed and Time-to-Distance readout for DME1 / hold

/ DME2 (see (9) ). Below 1000ft AGL, the readout changes to

radio altitude

11: To/From Indicator

9 10

Altimeter

1: Altitude readout, numeric

2: Pressure in millibars (QNH)

3: Altimeter pressure in Inches

4: Barometric pressure setting knob

Hint: The „B“ key in Microsoft Flight Simulator sets the altime-

ter to local pressure, or standard pressure, depending on the

aircraft´s altitude. The transistion altitude is dened as 18.000ft

worldwide.