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Honeywell KAP 140 Manual

Bendix/king autopilot system.
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KAP 140
®
Bendix/King
Autopilot System
Pilot's Guide

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   Summary of Contents for Honeywell KAP 140

  • Page 1

    KAP 140 ® Bendix/King Autopilot System Pilot’s Guide...

  • Page 2

    All rights reserved. Reproduction of this publication or any portion thereof by any means without the express written permission of Honeywell International Inc. is prohibited. For further information contact Aerospace Technical Publications; Honeywell; One Technology Center; 23500 West 105th Street; Olathe, Kansas 66061.

  • Page 3

    Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 3, November 2005 Part Number 006-18034-0000 This revision changes CW to CCW on page 116.

  • Page 4

    Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 2, May 2002 Part Number 006-18034-0000 This revision makes some of the changes for software version 03/01 more consistent throughout the Pilot’s Guide. The affected pages are 9, 12, 13, 55, 58, 83, 86 and 109.

  • Page 5

    Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 1, April 2002 Part Number 006-18034-0000 This revision incorporates changes for software version 03/01.

  • Page 6

    Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 0, June 1998 Part Number 006-18034-0000 This is the original version of this publication.

  • Page 7: Table Of Contents

    KAP 140 Single Axis Operation ........9...

  • Page 8

    Operations With The KAP 140 ........90...

  • Page 9: Introduction

    The first of a malfunction. In addition to relia- of its type developed by Honeywell, bility, the KAP 140 is designed to be this system brings digital technology easily maintained in the field. and reliability into the light aircraft Qualified Honeywell Service Centers cockpit.

  • Page 10: General Description

    KAP 140 Single Axis KAP 140 Two Axis/Altitude Autopilot System Preselect Autopilot System The KAP 140 Single Axis system is The KAP 140 Two Axis system pro- an entry level digital panel-mount vides both lateral and vertical modes autopilot, offering lateral modes only with altitude preselect.

  • Page 11

    HSI) HSI) HSI) Auto 45-degree Intercept Standard Standard Standard (with DG only) (with DG only) (with DG only) TEST Manual and Auto Trim Monitor Both Both Both Acceleration Monitor KAP 140 System Capabilities Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 12: System Integration

    The individual system diagrams on pages 5, 6, and 7 show the compo- nents and their relationship in typical KAP 140 Single Axis, KAP 140 Two Axis, and KAP 140 Two Axis/Altitude Preselect systems. The actual com- ponents on individual systems may...

  • Page 13

    KI 525A Pictorial Flux Detector Trim Interrupt Navigation Indicator (Optional) AUTO KCS 55A Slaved Compass System (Optional) KA 51B Slaving Accessory Control Manual WheelSteering Electrical Trim (Optional) (Optional) KAP 140 Single Axis System Diagram Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 14

    KI 525A Pictorial Flux Detector Disconnect/ Navigation Indicator Trim Interrupt KCS 55A Slaved AUTO Compass System (Optional) KA 51B Slaving Accessory Control Manual WheelSteering Electrical Trim (optional) KAP 140 Two Axis System Diagram Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 15

    KI 525A Pictorial Flux Detector Disconnect/ Navigation Indicator Trim Interrupt AUTO KCS 55A Slaved Compass System (Optional) KA 51B Slaving Accessory Control Manual WheelSteering Electrical Trim (optional) KAP 140 Two Axis/Altitude Preselect System Diagram Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 16: Power Application And Preflight Tests

    Introduction Power Application and Preflight Tests KAP 140 KAP 140 Preflight Test KAP 140 KAP 140 Preflight Test Complete For two-axis units only: A preflight test is performed upon power application to the com- NOTE: Following the preflight test, puter. This test is a sequence of...

  • Page 17: Kap 140 Single Axis Operation

    Single Axis Operation KAP 140 Single Axis Operation The KAP 140 is a high-performance digital, panel-mounted autopilot sys- tem for light aircraft. KAP 140 Single-axis Flight Control Computer KAP 140 Full Single-axis KAP 140 Display 1. AUTOPILOT ENGAGE/DISEN- and maintain the heading selected...

  • Page 18

    (for 2 sec- onds). 8. AUTOPILOT ENGAGED (AP) ANNUNCIATION - Illuminates whenever the autopilot is engaged. Flashes during pilot initiated or auto- matic disengagement. Only applica- ble for software versions 03/01 or later. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 19

    Single Axis Operation This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 20: System Operating Modes

    For software version 03/01 and later, the AP button must be pressed and held for 0.25 seconds to engage the autopilot. 2 MIN. NO PITCH NOTE: The KAP 140 engages into INFORMATION ROL mode as a default. Rev. 2 KAP 140 AUTOPILOT SYSTEM May/02...

  • Page 21: Heading Select (hdg) Mode

    AP button must be pressed and held for 0.25 seconds to engage the autopilot. 3. Depress the HDG button on the KAP 140 to engage the heading select mode. The autopilot will turn the aircraft in the shortest direction to intercept and fly the heading.

  • Page 22: Navigation (nav) Mode Using A Dg From Hdg Mode (45° Intercept)

    In the navigation (NAV) mode, the autopilot intercepts and tracks TURN COORDINATOR VOR/RNAV and GPS courses. To arm NAV mode (with the KAP 140 currently in the HDG 2 MIN. mode): NO PITCH INFORMATION 1. Select the desired frequency for VOR or RNAV.

  • Page 23

    If the D-Bar is less than 2 to 3 dots: the HDG mode will disengage upon select- ing NAV mode; the NAV annunci- ator will illuminate and the capture/ track sequence will automatically begin. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 24: Navigation (nav) Mode Using A Dg From Rol Mode (all Angle Intercept)

    In the navigation (NAV) mode, TURN COORDINATOR the autopilot intercepts and tracks VOR/RNAV and GPS courses. To arm NAV mode (with the KAP 140 currently in the ROL 2 MIN. mode): NO PITCH INFORMATION 1. Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode.

  • Page 25

    Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 26

    In the navigation (NAV) mode, the autopilot intercepts and tracks TURN COORDINATOR VOR/RNAV and GPS courses. To arm NAV mode (with the KAP 140 currently in the HDG mode): 2 MIN. NO PITCH INFORMATION 1. Select the desired frequency for VOR or RNAV.

  • Page 27

    Note: Intercept angles greater than 45° can result in course overshoot when close to the station. Therefore, intercept angles greater than 45° are not recommended. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 28: Approach (apr) Mode Using A Dg From Hdg Mode (45° Intercept)

    LOC, VOR/RNAV and GPS courses. To arm APR mode (with the 2 MIN. KAP 140 currently in the HDG NO PITCH mode): INFORMATION 1. Select the desired frequency for LOC, VOR or RNAV. For GPS, verify the desired approach.

  • Page 29

    If the D-Bar is less than 2 to 3 dots: the HDG mode will disengage upon select- ing APR mode; the APR annunci- ator will illuminate and the capture/ track sequence will automatically begin. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 30: Approach (apr) Mode Using A Dg From Rol Mode (all Angle Intercept)

    LOC, VOR/RNAV and GPS courses. To arm APR mode (with the 2 MIN. KAP 140 currently in the ROL NO PITCH mode): INFORMATION 1. Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode.

  • Page 31

    Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 32: Approach (apr) Mode Using An Hsi

    The Approach (APR) mode allows the autopilot to intercept and TURN COORDINATOR track LOC, VOR/RNAV and GPS courses. To arm APR mode (with the KAP 140 currently in the HDG 2 MIN. mode): NO PITCH INFORMATION 1. Select the desired frequency for LOC, VOR or RNAV.

  • Page 33

    APR annunciator will illumi- nate and the capture/track sequence will automatically begin. Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 34: Back Course (rev) Mode Using A Dg From Hdg Mode (45° Intercept)

    The Back Course (REV) mode TURN COORDINATOR allows the autopilot to intercept and track a localizer back course. To arm REV mode (with the KAP 140 currently in the HDG 2 MIN. mode): NO PITCH INFORMATION 1. Select the desired frequency for LOC.

  • Page 35

    If the D-Bar is less than 2 to 3 dots: the HDG mode will disengage upon select- ing REV mode; the REV annunci- ator will illuminate and the capture/ track sequence will automatically begin. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 36: Back Course (rev) Mode Using A Dg From Rol Mode (all Angle Intercept)

    The Back Course (REV) mode TURN COORDINATOR allows the autopilot to intercept and track a localizer back course. To arm REV mode (with the KAP 140 currently in the ROL 2 MIN. mode): NO PITCH INFORMATION 1. Maneuver the aircraft to the desired intercept angle prior to selecting ROL mode.

  • Page 37

    Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 38: Back Course (rev) Mode Using An Hsi

    The Back Course (REV) mode allows the autopilot to intercept and TURN COORDINATOR track a localizer back course. To arm REV mode (with the KAP 140 currently in the HDG mode): 2 MIN. NO PITCH 1. Select the desired frequency for INFORMATION LOC.

  • Page 39

    REV annunciator will illumi- nate and the capture/track sequence will automatically begin. Note: Intercept angles greater than 45° can result in course overshoot when close station. Therefore, intercept angles greater than 45° are not recommended. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 40: Operations With The Kap 140

    Single Axis Operation Single Axis Operation OPERATIONS WITH THE KAP 140 Takeoff And Climb To Assigned Altitude 080° D.C. ELEC. D.C. ELEC. D.C. ELEC. D.C. ELEC. TURN COORDINATOR TURN COORDINATOR TURN COORDINATOR TURN COORDINATOR 2 MIN. 2 MIN. 2 MIN.

  • Page 41: Gps Capture Using Dg

    While the annunciation is flashing, move the heading bug to the desired course of 040°. The aircraft will remain wings level until the capture point. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 42: Gps Capture Using Hsi

    040°. The button is annunciation changes to and a ing the GPS course. NAV ARM depressed and is annunciated. right turn is initiated by the autopilot. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 43: Outbound On Front Course For Procedure Turn To Loc Approach Using Dg

    KAP 140. to the right. The aircraft is flying away from the move the heading bug to the front course 058°. localizer centerline at a 45° angle on a selected...

  • Page 44: Outbound On Front Course For Procedure Turn To Loc Approach Using Hsi

    ) mode is selected to autopilot. by depressing the button on the KAP 140. craft is flying away from the localizer centerline go outbound on the front course. The capture at a 45° angle on a selected heading of 283°.

  • Page 45: Front Course Loc Approach Using Dg

    090°. By depressing the button on the The flashing annunciations are displayed and KAP 140, the autopilot engages into the head- a disconnect tone will sound. ing mode, commencing a right turn to a head- ing of 090°. Note: Press and hold the button for 0.25...

  • Page 46: Front Course Loc Approach Using Hsi

    This cancels all operating modes. and the CDI course index will center. 090°. By depressing the button on the KAP 140, the autopilot engages into the head- ing mode, commencing a right turn to a head- ing of 090°. Note: Press and hold the button for 0.25...

  • Page 47: Outbound On Gps Approach Using Dg

    * Check the heading displayed on the DG against Since the 45° intercept is 103°, the aircraft will the magnetic compass and reset if necessary. not turn until the course is captured. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 48: Outbound On Gps Approach Using Hsi

    GPS course at a 058°. Select approach mode by depressing the 45° angle on a selected heading of 283°. button. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 49: Inbound On Gps Approach Using Dg

    090°. By depressing the HDG button on the The flashing annunciations are displayed and annunciator.* KAP 140, the autopilot engages into the head- a disconnect tone will sound. ing mode, commencing a right turn to a head- ing of 090°.

  • Page 50: Inbound On Gps Approach Using Hsi

    The flashing annunciations are displayed and annunciator.* KAP 140, the autopilot engages into the head- a disconnect tone will sound. ing mode, commencing a right turn to a head- ing of 090°. Note: Press and hold the button for 0.25...

  • Page 51

    Single Axis Operation This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 52: Kap 140 Two Axis Operation

    Two Axis Operation KAP 140 Two Axis Operation The KAP 140 is a digital, panel-mounted autopilot system for light air- craft. KAP 140 Two-axis Flight Control Computer KAP 140 Full Two-Axis KAP 140 Display 1. PITCH AXIS, (P) ANNUNCIATOR and later, the AP button must be - When illuminated, indicates failure pressed and held for 0.25 seconds...

  • Page 53

    ALT button is pressed. If the be indicated by a solid PT. When the ALT button is pressed with an estab- fault is corrected, the annunciation lished VS rate present, there will be will extinguish. altitude overshoot (approximately Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 54: System Operating Modes

    Displays the active and armed pitch The lateral modes (HDG, NAV, APR modes (VS, ALT ARM, ALT, and and REV) operate identically as described in the KAP 140 Single Axis Operating Modes section. 13. ROLL MODE DISPLAY Please refer to that section for text...

  • Page 55: Vertical Speed (vs) Mode

    VS and current vertical cal speed modes. speed is displayed. Note: The KAP 140 engages into VS 2. UP or DN button - Select mode as a default. desired climb or descent rate.

  • Page 56: Altitude Hold (alt) Mode

    20 feet per press, or if held continuously will com- mand a 500 ft/min altitude change, acquiring a new reference altitude upon button release. Note: Incremented altitude changes should be limited to 500 ft. of change. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 57: Operations With The Kap 140

    Two Axis Operation Two Axis Operation OPERATIONS WITH THE KAP 140 Takeoff And Climb To Assigned Altitude 080° D.C. ELEC. D.C. ELEC. D.C. ELEC. D.C. ELEC. TURN COORDINATOR TURN COORDINATOR TURN COORDINATOR TURN COORDINATOR 2 MIN. 2 MIN. 2 MIN.

  • Page 58: Gps Capture Using Dg

    While the annunciation is flashing, move the heading bug to the desired course of 040°. The aircraft will remain wings level until the capture point. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 59: Gps Capture Using Hsi

    040°. The button is annunciation changes to and a ing the GPS course. NAV ARM depressed and is annunciated. right turn is initiated by the autopilot. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 60: Outbound On Front Course For Procedure Turn To Ils Approach Using Dg

    ) button. The annunciation will flash the autopilot. by depressing the button on the KAP 140. to the right. The aircraft is flying away from the for five seconds then extinguish. While the localizer centerline at a 45° angle on a selected...

  • Page 61: Outbound On Front Course For Procedure Turn To Ils Approach Using Hsi

    The back course ( ) mode is autopilot. by depressing the button on the KAP 140. craft is flying away from the localizer centerline selected to go outbound on the front course. at a 45° angle on a selected heading of 283°.

  • Page 62: Front Course Ils Approach Using Dg

    CDI course index will center. annunciator extinguishes and is displayed. KAP 140, the autopilot engages into the head- nect tone will sound. The autopilot will make pitch and bank changes ing and vertical speed modes, commencing a as necessary to maintain localizer and glides- right turn to a heading of 090°...

  • Page 63: Front Course Ils Approach Using Hsi

    CDI course index will center. annunciator extinguishes and is displayed. KAP 140, the autopilot engages into the head- nect tone will sound. The autopilot will make pitch and bank changes ing and vertical speed modes, commencing a as necessary to maintain localizer and glides- right turn to a heading of 090°...

  • Page 64: Outbound On Gps Approach Using Dg

    Move the heading bug within five seconds to 058°. Since the 45° intercept is 103°, the aircraft will not turn until the course is captured. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 65: Outbound On Gps Approach Using Hsi

    GPS course at a 058°. Select approach mode by depressing the 45° angle on a selected heading of 283°. button. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 66: Inbound On Gps Approach Using Dg

    KAP 140, the autopilot engages into the head- wheel. A flashing annunciation is displayed and a distinctive tone will sound. ing mode, commencing a right turn to a head- ing of 090°.

  • Page 67: Inbound On Gps Approach Using Hsi

    KAP 140, the autopilot engages into the head- wheel. A flashing annunciation is displayed and a distinctive tone will sound. ing and vertical speed modes, commencing a right turn to a heading of 090°...

  • Page 68

    Two Axis Operation This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 69: Kap 140 Two Axis With Altitude Preselect Operation

    Two Axis/Altitude Preselect Operations KAP 140 Two Axis with Altitude Preselect Operation The KAP 140 is a digital, panel-mounted autopilot system for light air- craft. BARO KAP 140 Two-axis w/Altitude PreSelect Flight Control Computer BARO KAP 140 Full KAP 140 Two-Axis with Altitude Preselect Display 1.

  • Page 70

    3 seconds. If pushed and held for This button will engage the autopilot 2 seconds, will change the baro set- in units with software prior to soft- ting display from IN HG to HPA or ware version 03/01. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 71

    Flashes during pilot initiated or auto- guishes 200 ft. prior to the selected matic disengagement. Only applica- altitude and illuminates momentarily ble for software versions 03/01 or when the selected altitude is later. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 72: System Operating Modes

    Two Axis/Altitude Preselect Operations System Operating Modes The lateral modes (HDG, NAV, APR and REV) operate identically as depicted in the KAP 140 Single Axis Operating Modes section. Please refer to that sec- tion for text descriptions of lateral mode operation. BARO...

  • Page 73: Altitude Hold (alt) Mode

    20 feet per press, or if held continuously will com- mand a 500 ft/min altitude change, acquiring a new reference altitude upon button release. Note: Incremented altitude changes should be limited to 500 ft. of change. Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 74: Altitude Alerting And Preselect

    The Altitude Preselect function allows capturing of a desired altitude and transferring into altitude hold. Manual input of desired altitude is accomplished through the rotary knobs on the faceplate of the KAP 140. The Altitude Alerting function will visually and aurally announce approaching, acquiring and deviation from a selected altitude.

  • Page 75: Altitude Preselect

    MDA. Glideslope coupling will preclude an 3. “AUTOPILOT” - Autopilot has altitude capture on an ILS. disengaged, either through pilot action or automatically. BARO KFC 140 Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 76: Operations With The Kap 140

    Two Axis/Altitude Preselect Operations Two Axis/Altitude Preselect Operations OPERATIONS WITH THE KAP 140 Takeoff And Climb To Assigned Altitude 080° D.C. ELEC. D.C. ELEC. D.C. ELEC. D.C. ELEC. TURN COORDINATOR TURN COORDINATOR TURN COORDINATOR TURN COORDINATOR 2 MIN. 2 MIN.

  • Page 77: Gps Capture Using Dg

    While the annunciation is flashing, move the heading bug to the desired course of 040°. The aircraft will remain wings level until the capture point. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 78: Gps Capture Using Hsi

    040°. The button is annunciation changes to and a ing the GPS course. NAV ARM depressed and is annunciated. right turn is initiated by the autopilot. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 79: Outbound On Front Course For Procedure Turn To Ils Approach Using Dg

    ) button. The annunciation will flash the autopilot. by depressing the button on the KAP 140. to the right. The aircraft is flying away from the for five seconds then extinguish. While the localizer centerline at a 45° angle on a selected...

  • Page 80: Outbound On Front Course For Procedure Turn To Ils Approach Using Hsi

    The back course ( ) mode is autopilot. by depressing the button on the KAP 140. line at a 45° angle on a selected heading of selected to go outbound on the front course. 283°. Automatic capture of the localizer will occur.

  • Page 81: Front Course Ils Approach Using Dg

    CDI course index will center. annunciator extinguishes and is displayed. KAP 140, the autopilot engages into the head- nect tone will sound. The autopilot will make pitch and bank changes ing and vertical speed modes, commencing a as necessary to maintain localizer and glides- right turn to a heading of 090°...

  • Page 82: Front Course Ils Approach Using Hsi

    CDI course index will center. annunciation extinguishes and is displayed. KAP 140, the autopilot engages into the head- nect tone will sound. The autopilot will make pitch and bank changes ing and vertical speed modes, commencing a as necessary to maintain localizer and glides- right turn to a heading of 090°...

  • Page 83: Outbound On Gps Approach Using Dg

    Since the 45° intercept is 103°, the aircraft will not turn until the course is captured. * Check the heading displayed on the DG against the magnetic compass and reset if necessary. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 84: Outbound On Gps Approach Using Hsi

    GPS course at a 058°. Select approach mode by depressing the 45° angle on a selected heading of 283°. button. Rev. 1 Rev. 1 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Apr/02 Apr/02...

  • Page 85: Inbound On Gps Approach Using Dg

    KAP 140, the autopilot engages into the head- wheel. A flashing annunciation is displayed and a distinctive tone will sound. ing and vertical speed modes, commencing a right turn to a heading of 090°...

  • Page 86: Inbound On Gps Approach Using Hsi

    KAP 140, the autopilot engages into the head- wheel. The flashing annunciations are dis- played and a distinctive tone will sound. ing and vertical speed modes, commencing a right turn to a heading of 090°...

  • Page 87

    Two Axis/Altitude Preselect Operations This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02...

  • Page 88: Kcs 55a Compass System

    Directional Gyro as well as the KI ception and tracking, while eliminat- 525A Pictorial Navigation Indicator is ing the need for scan coordination an optional part of the KAP 140 between two separate indicators. Autopilot System. AUTO KA 51B ı...

  • Page 89: Ki 525a Indicator

    This play so that the aircraft heading is miniature aircraft always points always at the top, under the lubber toward the top of the display and the line. lubber line. Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 90

    This pointer is set by rotating the to fly. This desired heading is cou- course select knob. pled to the KAP 140 Autopilot to pro- vide the “Heading Select” function. Course Select Knob - Used to rotate the course pointer to the...

  • Page 91: Slaving Meter ( Ka 51b)

    The KA 51B can be mounted either vertically or horizon- tally. Rev. 3 KAP 140 AUTOPILOT SYSTEM Nov/05...

  • Page 92: Kmt 112 Magnetic Slaving Transmitter

    KCS 55A System, and gyro up degrees per minute to keep the to operating speed, the red “HDG” system aligned with the earth’s flag should disappear from view. magnetic field. Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 93

    If 7. Rotate the course select knob to they do not come into view, a position the course pointer to the usable glideslope signal is not desired VOR course. being received. Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 94: Abnormal Circumstances

    Note: For system limitations in your is malfunctioning. Glideslope is usu- particular aircraft type, refer to your ally not available during a back Flight Manual Supplement. course approach. (The VOR and LOC course display will continue to Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 95: Flight Procedures With The Kcs 55a

    Rev. 0 Rev. 0 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Jun/98 Jun/98...

  • Page 96

    Note: For system limitations St. Louis VORTAC on the NAV refer to your Flight Manual receiver and set the course Supplement. pointer on the STL 062° course. Rev. 0 Rev. 0 KAP 140 AUTOPILOT SYSTEM KAP 140 AUTOPILOT SYSTEM Jun/98 Jun/98...

  • Page 97

    By keeping the top of the deviation bar on the lubber line, you can complete your turn and roll out precisely on course. Note: For system limitations refer to your Flight Manual Supplement. Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 98

    5° to the display indicates your aircraft is still the right to maintain the localizer course. below the glidepath at this point. Note: For system limitations refer to your Flight Manual Supplement. Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 99

    You may reset the tion. heading bug to 058° for easy reference. Note: For system limitations refer to your Flight Manual Supplement. Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 100: Abnormal Procedures

    Manipulate the controls as required to safely main- tain operation of the airplane within all of its operating limitations. CAUTION: Refer to the Airplane Flight Manual or the Airplane Flight Manual Supplement for your particular aircraft for pertinent emergency procedures. Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 101

    Abnormal Procedures This page intentionally left blank Rev. 0 KAP 140 AUTOPILOT SYSTEM Jun/98...

  • Page 102

    Honeywell Aerospace Business and General Aviation Honeywell International Inc. 23500 West 105th Street Olathe, KS 66061 Tel: 913-712-0400 Fax: 913-712-1302 www.honeywell.com 006-18034-0000 Rev. 3 November 2005 ©1998, 2002, 2005 Honeywell International Inc.

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Bendix/king kap 140

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