Bendix/King Skymap IIIC, Pilot'S Manual

Page 1: ...Pilots GuL 3 KFC 250 BendixlKingFlightControlSystem APPR CPLD GCCPLD BAfH CRS...

Page 2: ...pilot Engagement AP 14 HeadingSelect PreselectMode HDGSEL 15 YawDampMode 15 NavigationMode NAVIARMand NAVICPLD 16 Approach Mode NAVIARMandAPPRICPLD GSICPLD 17 BackCourseMode BC 18 Go AroundMode 18 Alt...

Page 3: ...trol The system provides all stan operating modes plusaltitudepreselectcapability This system is designed specifically to bring the ntages of advanced technology to single pilot IMPORTANTThisPilot sGu...

Page 4: ...trol System and their relationships The system isfunctionally dividedintofour parts Sense control compute and display All sensor information pitchand roll reference slaved compass RNAVIVORILOCIGS DME...

Page 5: ...edto generatethe aileron elevator displayedon the V bar in the FCI into the re trim and rudder drive commands for the quiredelevatorandaileron positioncommands Autopilot Full integration of Flight Dir...

Page 6: ...1 20 54 2 90 1 31 10 45 A 28 VDC 4 5 VA26VAC 26 96 12 18 4 Inch KCI 310 Flight Command KPI 552 PictorialNavigation KAP 315 Mode Annunciator KVG 350 Vertical Gyro KCS 305 Slaved D G Indicator Indicator...

Page 7: ...de has been selected Flight Director FD Command V bar will call for wings level The pitch attitude of the aircraft will remain the same as at the time of mode selection Select desiredheadingon PNI the...

Page 8: ...tude Provides capability to adjust or slew the Altitude up or down without disengaging and then reengaging ALT Hold If Alti tude Hold is not engaged the Vertical Trim knob will adjust the pitch attitu...

Page 9: ...3A PNI with built in DME display and RMI pointer is availableas an option see picture on page 11 3 THE KCI 310 FLIGHT COMMAND INDICATOR displaysthe following information Pitch and roll attitude Pitch...

Page 10: ...e KC 290 Mode Controller In this config uration the yaw axis is wired so that it automatically engages when the Autopilot is engaged Disengagement of the yaw damper is accomplishedby using the control...

Page 11: ...rs on the annunciator panel Any operatingmodenotcompatiblewith a newly selectedmodewill be automatically cancelled in favor of the pilot s latest selec tion This lets the pilot advance along his fligh...

Page 12: ...isplayingproper heading A NAV flag indicatesthat a valid NAVSignalis not being received 12 When an ILS channel is selectedon the NAV receiver and a valid Glideslope signal is received the Glideslope p...

Page 13: ...e KI 256 FCIdoes not have a computer or attitudeflag or attitudetest sincethegyrois air driven The pilot first engagesthe Flight Director to activate the Command V bar Then he engages the Autopilot Th...

Page 14: ...ment The AUTOPILOT is engaged by moving the solenoid held AP toggle switch on the ModeControllerto the ON position Notethat the AP andthe YAW DAMP YD switches are wired so that the YAW DAMP mode is au...

Page 15: ...ings level With the HDG SEL mode in operation subsequent changes made in the heading bug position on the PNI will immediately causethe V bar on the FCIto call for aturn to the new heading The HDG SEL...

Page 16: ...e a bank command will be displayed on the FCI the HDG if on will becancelledand NAVICPLD will be lighted on the Annun ciator Panel The pilot can manually bank the aircraft to satisfythe commanddisplay...

Page 17: ...t to level flight when the aircraft is on course Automatic crosswind compensation will provide precise tracking VOR LOCdeviationisshownon the PNI and actual crab angle will be shown by offset of the c...

Page 18: ...Depression of the Go Around switch during an approach cancels all Flight Di rector modes and disengages the Autopilot if it is engaged A wings level and pitch up command is displayed by the FCI and G...

Page 19: ...will auto matically hold the aircraft at that altitude The Vertical Trim switch may be used to adjust the selected altitude up or down at a constant rateof approximately 600 fpm without disengagingth...

Page 20: ...ROUND angle Takeoff is on runway 35 as shown on the PNI 2 The aircraft is well off the ground and climbing The heading bug on the PNI is turned to a desired heading and HDG mode has been pushedon The...

Page 21: ...es Desir ed altitude may now be selected and armed on the KAS 297 altitude selector Altitude aler ting will be provided as you approach your selected altitude 4 Desired altitude has been reached ALT H...

Page 22: ...BC mode is selected to go outboundon the front course The capture point is now being computed based on closure rate 22 r 2 When the computed capture point is reached the APPR CPLD mode is automati cal...

Page 23: ...lly that the air craft is flying away from the Localizer cen terline at a 45 angle on a selected heading of 283 4 Now you have reset the heading select bugtol03 and madealapturntothis head ing This 10...

Page 24: ...the LOC course 2 The Autopilot or pilot is following the CommandV bar on the FCIwhich commands the necessaryheadingto maintain on center line of the Localizer At the Outer Marker the Glideslopepointe...

Page 25: ...be reengagedto completethe missed approach Some airplanes are cer tified with autopilotremainingengagedwhen GA selected I 4 The heading bug has been previously setto the missedapproach heading 90 Ac t...

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