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Kap 140 Autopilot Manual

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Product Overview: KAP140. Autopilot for MSFS & P3D. Is the KAP-140 compatible with Lockheed-Martin Prepar3D 3.0? Yes, the unit also. The KAP 140 Autopilot System is a rate based digital autopilot system offering smooth performance and enhanced features found only in more expensive autopilots. Manual KAP 140 Pilot’s Guide Revision 2, May 2002 Part Number 006- This revision makes some of the changes for software version 03/01 more consistent throughout the Pilot’s Guide. The affected pages are 9. KAP 140 AUTOPILOT SYSTEM Table of Contents i Rev. KAP 140 Pilot’ s Guide Bendix/King ® Autopilot System 006. KAP 140 AUTOPILOT SYSTEM. Manual Electric Trim.

Autopilot KAP 140. The Honeywell KAP 140 is a two Axis autopilot with. For comprehensive reference please refer to the original manual (Honewywell KP 140.

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

Kap 140 Autopilot ManualKap 140 Autopilot Problems

For further information contact Aerospace Technical Publications; Honeywell; One Technology Center; 23500 West 105th Street; Olathe, Kansas 66061. • Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 3, November 2005 Part Number 006- This revision changes CW to CCW on page 116. • Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 2, May 2002 Part Number 006- 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. • Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 1, April 2002 Part Number 006- This revision incorporates changes for software version 03/01. • Revision History and Instructions Manual KAP 140 Pilot’s Guide Revision 0, June 1998 Part Number 006- This is the original version of this publication. • KAP 140 Single Axis Operation.9.

Honeywell Kap 140 Autopilot Manual

• Operations With The KAP 140.90. Sage 50 2015 User Manual there. • 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.

Kap 140 Autopilot Manual

And reliability into the light aircraft Qualified Honeywell Service Centers cockpit. • 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. • 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. • 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. • 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. Xbox 360 Owners Manual on this page. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. • 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. • 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. • 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. • 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. • (for 2 sec- onds).

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. 1 KAP 140 AUTOPILOT SYSTEM Apr/02.

• Single Axis Operation This page intentionally left blank Rev. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. • For software version 03/01 and later, the AP button must be pressed and held for 0.25 seconds to engage the autopilot.

NO PITCH NOTE: The KAP 140 engages into INFORMATION ROL mode as a default. 2 KAP 140 AUTOPILOT SYSTEM May/02. • AP button must be pressed and held for 0.25 seconds to engage the autopilot. 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.

• 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. • 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. 1 KAP 140 AUTOPILOT SYSTEM Apr/02. • 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.

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