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CHAPTER 1. AIRCRAFT MODULES
1.7. KING AIR B200
Cowl Flap Switches
The left Cowl Flap switch controls Inverter operation.
The right Cowl Flap switch controls the Auto-feather
feature.
The MDI knob controls the Radar Altimeter. The ALT knob adjusts the altimeter setting. The NAV 2 knob
is non-functional on the King Air module. The CRS knob with corresponding toggle switch in CRS mode
moves the course deviation needle on the HSI. CRS knob in OBS mode moves the three-position selector
on the lower left corner of the HSI. The DIST, TTC or SPD readout is indicated in the top left portion of
the HSI and will provide information from the navigation source selected by the toggle below the HSI. The
HDG knob moves the HSI heading bug.
Collins Flight Control System
Figure 1.48: King Air B200 - Collins Flight Control System
To use the Collins Flight Control System please note the button and functions assignments on the AP 4000
avionics panel:
•
FD button engages the 1/2 BK, one-half bank angle function
•
ALT button engages the altitude hold function
•
HDG button engages the heading hold function
•
NAV button engages the navigation track function
•
APR button engages the APPR, localizer track function
•
BC button engages the AP CPLD, autopilot coupled function
•
AP ENG button engages the manual control knob
•
ENG button engages the VS function
•
ARM button engages the ALT SEL function
To operate in ight director mode, simply press ALT and HDG, NAV or APR. The command bars will
be visible only if HDG, NAV or APR is selected. No ight director function is available with ALT selected
only.
Deviations in heading and/or altitude from the current setting will cause the command bars to tilt and/or
move vertically to indicate prescribed corrective ight action. If the Control Wheel Steering (CWS) button
is pressed during ight director mode the ALT function if selected will trip o and will need to be reset when
desired. If a climb or descent is necessary, use CWS to initiate the necessary pitch attitude and dial the
desired level-o altitude into the "Set Altitude" box. Once the altitude change has commenced select ALT
SEL and the command bars will indicate when altitude level-o is required. Additionally, once the desired
pitch attitude has been set and VS has been selected the command bars will indicate the amount of pitch
57
Summary of Contents for XTS
Page 4: ...CONTENTS CONTENTS 2 Conclusion 84 2 1 Troubleshooting 84 2 2 Notes 85 2 ...
Page 18: ...CHAPTER 1 AIRCRAFT MODULES 1 2 PIPER ARROW Figure 1 13 Gear up Climb Performance 16 ...
Page 28: ...CHAPTER 1 AIRCRAFT MODULES 1 3 BEECH BARON 58 Figure 1 22 Beech Baron 58 Climb 26 ...
Page 30: ...CHAPTER 1 AIRCRAFT MODULES 1 3 BEECH BARON 58 Figure 1 24 Beech Baron 58 Cruise Power 28 ...
Page 34: ...CHAPTER 1 AIRCRAFT MODULES 1 4 BONANZA A36 Figure 1 30 Bonanza A36 Instrument Panel 32 ...
Page 39: ...CHAPTER 1 AIRCRAFT MODULES 1 4 BONANZA A36 Figure 1 32 Bonanza A36 Climb 37 ...
Page 41: ...CHAPTER 1 AIRCRAFT MODULES 1 4 BONANZA A36 Figure 1 34 Bonanza A36 Cruise Power Settings 39 ...
Page 54: ...CHAPTER 1 AIRCRAFT MODULES 1 6 CESSNA 182S 52 ...
Page 55: ...CHAPTER 1 AIRCRAFT MODULES 1 6 CESSNA 182S 53 ...
Page 56: ...CHAPTER 1 AIRCRAFT MODULES 1 6 CESSNA 182S 54 ...
Page 73: ...CHAPTER 1 AIRCRAFT MODULES 1 8 MOONEY M20J Figure 1 56 Mooney M20J Instrument Panel 71 ...
Page 76: ...CHAPTER 1 AIRCRAFT MODULES 1 9 PIPER SENECA III 74 ...
Page 83: ...CHAPTER 1 AIRCRAFT MODULES 1 9 PIPER SENECA III Figure 1 63 Piper Seneca Speed Power 81 ...
Page 84: ...CHAPTER 1 AIRCRAFT MODULES 1 9 PIPER SENECA III Figure 1 64 Piper Seneca Table 82 ...
Page 87: ...CHAPTER 2 CONCLUSION 2 2 NOTES 2 2 Notes Please feel free to add any notes here 85 ...
Page 88: ......